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    UNIVERSITY OF BATH

    DEPARTMENT OF MECHANICAL ENGINEERING

    DESIGN AND DEVELOPMENT OF A MEDICAL

    DEVICE TO IMPROVE THE ASSEMBLY OF

    HEAD/NECK TAPER JUNCTIONS IN MODULAR

    TOTAL HIP REPLACEMENTS

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    COPYRIGHT

    Attention is drawn to the fact that copyright of this dissertation rests with the

    author. This copy of the dissertation has been supplied on condition that

    anyone who consults it is understood to recognise that its copyright rests with

    its author and that no quotation from this dissertation and no information

    derived from it may be published without the prior written consent of the

    author.

    This dissertation may be available for consultation within the University

    Library and may be photocopied or loaned to other libraries for the purpose of

    consultation.

    CHEATING AND PLAGIARISM

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    ABSTRACT

    There has been a significant failure rate in modular total hip replacements

    (MTHR) over the past few years, particularly with the use of large diameter

    Metal on Metal (MoM) bearings. Various studies have shown that sub-optimal

    strength of the head-neck taper junction plays an important role in these high

    failure rates.

    The purpose of this project is to design and develop a medical device to

    improve the assembly of this taper junction with an overall aim to reduce the

    occurrence of early revision surgeries on MTHRs. The device aims to ensure

    axial alignment of the head and neck tapers before providing an adjustable

    impact force between 4KN and 6KN to achieve the strongest possible junction

    assembly, with the target of reducing the incidence of fretting and corrosion at

    thi j ti d it i t d bl

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    CONTENTS

    1. INTRODUCTION 1

    1.1 What is a Total Hip Replacement? 1

    1.2 What are THRs used to treat? 2

    1.3 What is a Modular Total Hip Replacement? 3

    1.4 Why are they Modular? 4

    1.5 How are MTHRs implanted? 4

    1.6 How are MTHR assembled? 5

    1.8 What is the problem effecting MTHR? 6

    2 AIMS AND OBJECTIVES 8

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    4.3.2Generation of PDS 39

    5. DEVELOPMENT & EVALUATION 40

    5.1 Concept Generation and Evaluation 40

    5.1.1 Initial Product Design Specification (PDS) 41

    5.1.2 Discretisation of Design Challenge 42

    5.1.3 Radial Thinking 43

    5.1.4 Visual Concept Analysis 44

    5.1.5 Critical Assessment and Selection 52

    5.1.6 Further Investigation of Powering Concept 55

    5.1.7 Development of Final Powering Concept 60

    5.1.8 Mechanical Feasibility of Chosen Concept 67

    5.1.9 Development of Proof-Of-Concept Testing Rig 73

    5.2 Detailed Design 79

    5 2 1 Solid Modelling 79

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    7.4 Discussion 95

    8. CONCLUSIONS 96

    10. REFERENCES 98

    11. APPENDICES 101

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    NOMENCLATURE

    N = Newtons

    KN = Kilo Newtons

    F = Force

    m = Mass

    g = acceleration due to gravity (9.81m/s)

    m/s = meters per second

    Kg = Kilograms

    t = Time (in seconds)

    t = Impact duration

    v = Velocity

    v = change in velocity

    k = Spring Stiffness (in N/m)

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    LIST OF FIGURES AND TABLES

    FIGURES

    Figure 1: Illustrated Hip Replacement; Before and After [2] ....................................... 1

    Figure 2: Charnleys Low Friction Arthroplasty [4] ..................................................... 2

    Figure 3: Illustration of Normal Vs. Arthritic Hip [5] .................................................... 3

    Figure 4: Exploded View of MTHR Assembly [7] ....................................................... 3

    Figure 5: Illustration of MTHR Surgical Procedure [11] .............................................. 4

    Figure 6: Orthopaedic Mallet and Impactor [12] ......................................................... 6

    Figure 7: Example of matched and mismatched taper angles [20] .......................... 13

    Figure 8: Stuart Pughs Design Process Model [33]................................................. 25

    Figure 9: Orthopaedic Surgeon Survey Introduction ................................................ 28

    Fi 10 S S Q1 28

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    Figure 23: Device for Handling Hip joint Heads [39] Figure 24: Head

    holder and impactor [40] .................................................................................. 36

    Figure 25: Method of applying Femoral head Resurfacing [41] Figure 26: Nail

    gun Patent 1 [42] ............................................................................................. 36

    Figure 27: Nail gun Patent 2 [43] Figure 28: Wire Shelf

    Driver [44] ........................................................................................................ 36

    Figure 29: Automatic Centre Punch [44] .................................................................. 37

    Figure 30: Inserter jaw for knee prosthesis impaction and extraction [45] ................ 37

    Figure 31: Comparison in grading between EU and USA Device Classification [48] 38

    Figure 32: Initial sketch to capture ideas ................................................................. 42

    Figure 33: Development of Objective B ................................................................... 43

    Figure 34: Development of Objective C ................................................................... 44

    Figure 35: Three Prong Flexible Support and Centring Cone Sketch ...................... 45

    Figure 36: Semi-Cup + Centring Cone Sketch ......................................................... 45

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    Figure 51: The Solenoid Powered Nail Gun [49] ...................................................... 57

    Figure 52: Electric Powered Nail Gun [49] ............................................................... 58

    Figure 53: Can-Crushing Device [50] ...................................................................... 59

    Figure 54: Adapted Juicer Sketch ............................................................................ 60

    Figure 55: Adapted Can Crusher Sketch ................................................................. 61

    Figure 56: Corkscrew Lever System Sketch ............................................................ 62

    Figure 57: Twisting Adjustment and Release Concept Sketch ................................. 63

    Figure 58: Gearbox Style Spring Compression Adjustment Concept Sketch ........... 63

    Figure 59: Spring Compression adjustment System Sketch .................................... 64

    Figure 60: Slotted Trigger Release Mechanism Sketch ........................................... 65

    Figure 61: Firearm Trigger Concept Sketch ............................................................. 65

    Figure 62: Handle Trigger System Sketch ............................................................... 65

    Figure 63: Final Developed Concept Sketch ........................................................... 66

    Figure 64: Tubular Casing Surrounding Spring Sketch ............................................ 67

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    Figure 78: Base plate fixed to table with and without Rubber Base ......................... 86

    Figure 79: Table of Data recorded from Instron ....................................................... 88

    Figure 80: Test 2, Steel, 2KN (with rubber base) ..................................................... 89

    Figure 81: Extrapolated Load Cell Data, >2KN ........................................................ 90

    Figure 82: Extrapolated Load Cell Data, 4KN and 6KN ........................................... 91

    Figure 83: Images of Failed PVC and Rubber Tips at 4KN Load ............................. 92

    TABLES

    Table 1: Data from Pennock et al. (2002) study [29], [10] ........................................ 17

    Table 2: Data from Lavernia et al. (2009) Study [30], [10]........................................ 18

    Table 3: Data from Heiney et al. (2009) Study [31], [10] .......................................... 19

    Table 4: Data from Rehmer et al. (2012) Study [32], [10]......................................... 21

    T bl 5 I iti l PDS 41

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    1. INTRODUCTION

    1.1 What is a Total Hip Replacement?

    There are two types of Hip Replacement surgery, Hip Resurfacing and Total Hip

    Replacement (THR). This project focusses on the THR procedure, which is also

    known as Total Hip Arthroplasty. THRs are among the most common orthopaedic

    procedures performed today [1]. The THR procedure involves removing the femoral

    head (top of the thigh bone) and a layer of bone from in and around the acetabulum

    (hip socket) and replacing them with artificial materials, thus resulting in an artificial

    hip joint. The before and after pictures of a hip joint that has undergone a THR is

    shown in Figure 1 [2] below, with the original diseased hip joint shown on the left

    and the new replacement joint shown on the right.

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    The first modern THRs were designed by John Charnley in the 1960s, which

    stemmed from his paper Surgery of the Hip Joint - present and future

    developments [3] published in 1960. Charnleys THR consisted of a high density

    polyethylene cup that was fixed inside the hip joint socket and a stainless steel

    component that made up the artificial femoral head and stem which slotted into the

    patients femur. This low friction arthroplasty [4] hip design was first implanted in

    November 1962 and can be seen in Figure 2 [4] below.

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    Figure 3: Illustration of Normal Vs. Arthritic Hip [5]

    1.3 What is a Modular Total Hip Replacement?

    Modular THRs (MTHR) were introduced in the 1970s [6]. The previous leg (femoral)

    component used in Charnleys original design was separated into head and stem

    components and the previous plastic cup was separated into shell and liner

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    1.4 Why are they Modular?

    Modularisation was introduced into the design of THRs in the 1970s [8] to allow

    more flexibility in material selection/combination and component sizing to ensure a

    more individually suited THR for each patient. It also allows surgeons to reduce

    inventory [9] and simplifies revision surgeries [8]. Several different material choices

    and combinations are available to surgeons. For the stem and head; Cobalt Chrome

    or Ceramic Heads can be used on Titanium stems. For the bearing combinations;

    Metal on Metal (MoM), Ceramic on Ceramic (CoC) and Ceramic on Metal (CoM),

    and finally Ceramic or Metal heads can also be used on Ultra High Molecular

    Weight Polyethylene (UHMWPE). [10]

    1.5 How are MTHRs implanted?

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    Step A involves making an incision to gain access to the joint area and dislocating

    or disarticulating [11] the femoral head from the acetabulum (or hip socket).

    Step B involves cutting off the femoral head with a surgical saw.

    Step C involves reaming out the acetabulum and the femur to prepare them to

    receive the shell and stem respectively.

    Step D involves the introduction of the prosthetic components and the final image in

    the bottom right hand side of the figure shows the fully installed THR.

    1.6 How are MTHR assembled?

    The order in which the components are introduced in this procedure is important to

    note. The acetabulum shell is first introduced and fixed in place before the stem is

    inserted into the femur. There are two types of stem designs; cemented, where

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    stem taper using a mallet and impactor (usually tipped with a softer material than

    the head so as not to damage the surface of the head). An example of the sort of

    mallet and impactor commonly used is shown in Figure 6 [12] below.

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    product recalls. Large diameter (>36mm) MoM bearings are by far the worst

    offenders when it comes to early revisions and product recalls. The use of large

    diameter MoM bearings amplifies an existing issue regarding the strength of the

    head/neck taper junction more so than other joint material and geometry selections.

    Large diameter bearings produce an increase in the torque in the joint, as a larger

    frictional torque is generated since there is a longer lever arm acting between the

    fulcrum or centre of the joints rotation and the surface where the head makes

    contact with the liner, especially MoM. This increase in force about the junction,

    leads to increased levels of fretting wear and corrosion, which causes the liberation

    of prosthesis material and hence early revision surgeries (as the human body has

    an adverse reaction to the presence of these foreign particles).

    Fretting corrosion and wear can still occur in all material and geometry combinations

    but the accelerated and extreme instances found in some of the large diameter

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    2. AIMS AND OBJECTIVES

    Aim: To design and develop a medical device to improve the assembly of

    head/neck taper junctions in MTHRs with an overall aim to contribute to the

    reduction of early revision surgeries for MTHRs

    Objectives:

    1. Review relevant literature to gain greater understanding/scope of problem

    2. Establish User Needs and Design Requirements

    3. Produce Product Design Specification (PDS)

    4. Generate and evaluate design concepts

    5. Design and develop a prototype for proof-of-concept

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    3. LITERATURE REVIEW

    This section of the report contains the findings from the literature review carried out

    on the failure of MTHRs due to head/neck taper junctions. The review spread out

    beyond the borders of this specific issue to ensure an understanding of the bigger

    picture could be taken into account before focussing on the specific problem itself

    towards the end of the review. The findings are now presented under two headings,

    Understanding the Problem and why it is occurring, followed by How to reducing

    or eliminate the problem.

    3.1 Understanding the problem and why it is occurring

    Before trying to solve the problem it is essential to take the time to fully understand

    the background and history of the problem and the reason behind its occurrence.

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    diameter of the bearing. This increase in torque caused wear and fretting corrosion

    which again led to the liberation of metal particles and thus patient complications, as

    with the first failure method. The reason why the second failure method is the most

    important to this project is because the use of large diameters in MoM bearings is

    not unique to the ASR design and so plays a role in the failure rates of various other

    MTHR designs. Both Henghan et al. (2012) [14] and Langton et al. (2011) [13]

    agree on this point and Langton et al. go on to suggest that bearing diameters of

    36mm or greater are most at risk to this failure method.

    Smith et al. (2102) [15] concluded, following an in depth analysis of National Joint

    Registry Data covering England and Wales, that MoM bearings are more likely than

    other bearing material combinations to fail, and also found that their failure rates

    were increasing proportional to increasing bearing diameter size. Langton et al.

    (2011) [13] also came to the same conclusion in their study into the failure of the

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    greatest frictional moments followed by Metal on UHMWPE and then CoC with the

    lowest frictional moments, thus adding to the growing evidence pointing at the

    failings of MoM bearings. Langton et al. (2011) [13] found that as the trend in

    increasing bearing diameter grew, there was no increase in the diameter of the neck

    taper to counter the associated increase in torque. In a different study by Langton et

    al. (2012) [18] they noted that neck diameters actually decreased as larger and

    larger bearings sizes became available, thus exacerbating the problem. The

    reasoning behind reducing the diameter of the neck taper was to increase the range

    of motion of the prosthesis.

    One of the biggest studies of MTHR neck/taper junctions was carried out by

    Goldberg et al. (2002) [19] and looked into various different aspects and failure

    methods in this junction. One of the recommendations that they put forward

    following their research was to increase the neck taper diameter with an aim to

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    Now that the severity and reasoning behind the failure MTHRs has been established

    the next step is to look at who has influence or control over the reduction or

    elimination of the problem.

    3.2 How to reduce or eliminate the problem

    This part of the chapter looks at who has control over or influence on the key factors

    that contribute towards the strength of the head/neck taper junction. This part

    finishes with an in depth analysis of four particularly relevant studies with an aim to

    establishing the optimum conditions and provisions for assembling a head/neck

    taper junction.

    3.2.1 What influence do Manufacturers have on the assembly?

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    Figure 7: Example of matched and mismatched taper angles [20]

    Figure 7 Part A shows the correct fit with the maximum contact area between the

    head and neck tapers. Figure 7 Part B on the right shows a poor fit where there is a

    significant taper angle mismatch leaving low contact area creating stress

    concentrations and room for micro-motion (also described as toggling) which leads

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    resistant materials plays an important part in the improvement of these designs,

    along with the recognition that only a very small mismatch is required to begin a

    cycle of fretting corrosion and wear.

    In a study which involved measuring the forces required to disassemble three

    different model of MTHRs, which had been retrieved from patients undergoing

    revision surgeries, Lieberman et al. (1994) [23] made an interesting discovery. One

    of the models required a much greater force than the other two to be disassembled

    and was the only model type of the three examined not to show any signs of

    corrosion after a 78 month period. These particular MTHRs had a different assembly

    history from the other two model types in that they had been assembled by the

    manufacturer and were supplied to the surgeon in a preassembled condition. These

    MTHRs had been shrink fitted with a sealant, applied during this assembly.

    Lieberman et al. (1994) [23] believe the greater junction strength and resistance to

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    3.2.2 What influence do Surgeons have on the assembly?

    The fit of the spigot head is noted as the most important source of error in

    Fessler and Frickers (1989) [21] study into the Stresses in Alumina Universal

    Heads of Femoral Prosthesis. Bobyn et al. (1994) [24] would agree with their

    statement since they found a reduction in taper surface contact area and an

    increase in wear and fretting corrosion in two Modular Femoral Prosthesis, after

    assembling them both using one fifth of the manufacturers recommended assembly

    force and exposing them to the sort of cyclic loading that they would experience in-

    vivo. Thus the impact load applied has a significant influence on the fit or the

    assembly of the head on the neck. A study carried out by Goldberg and Gilbert

    (2003) [25] entitled In vitro corrosion testing of hip tapers concluded that the

    proper seating of the head onto the neck increases the forces required to cause

    micro-motion, and hence wear and fretting corrosion. A study by Mroczkowski et al.

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    The impact force is not the only important factor that the surgeon has influence over

    during assembly. The axial alignment when placing the head on the neck taper prior

    to impact and the axial alignment of the impact delivered is also extremely

    important. Both Callaway et al. (1995) [27] and Pansard et al. (2012) [28] traced

    back the failure of a number of MTHRs to incorrect fitting of the head on the neck

    taper by examining retrieved MTHRs removed during revision surgeries. They both

    found that their retrieved Hip Replacements had failed due to extreme corrosion

    caused by incorrect fitting of the head during original assembly. Due to varying

    manufacturing tolerances between different brands, it is also strongly recommended

    not to mix different manufacturers components as this can result in poorly fitted

    parts that can reduce the life of the prosthesis.

    Four key papers are now discussed with a focus on the effects of the impact/s

    applied during the assembly of the head/neck taper junction with an aim to

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    Table 1: Data from Pennock et al. (2002) study [29], [10]

    This study looks at the effects of varying the magnitude of the impact force, the

    order in which the different impact forces are applied and the total number of

    impacts delivered during assembly and their effect on the resulting junction strength

    (determined by pull-off tests). This study also looked at the effects of wet and dry

    taper surfaces on junction strength, but the wetted samples were not included in this

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    [29]. Pennock et al. (2002) [29] also states the importance of axial alignment when

    delivering the impacts, to ensure that all of the force is transmitted during the

    impaction. One of the findings taken from their study (especially when the wet

    tapers were taken into consideration) was that they noted an increase in junction

    strength with increasing impact magnitude [29].

    The next study was carried out by Lavernia et al. (2009) [30] and looked mainly at

    the effects of blood and fat contamination on the taper surfaces and the effect they

    had on the junctions strength. However, as they used control or dry tapers for

    comparison the data recorded for these was of benefit to this investigation and has

    been recorded in Table 2 [10] below.

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    this study can be considered to be a more realistic representation of the average

    magnitude of a surgeons impact as they recorded the impact forces applied by 8

    different surgeons as opposed to the previous study by Pennock et al. (2002) [29]

    that only used 11 impacts by a single surgeon. The result is a 27% (approx.)

    decrease of the force used by Pennock et al (2002). It is worth noting that this study

    does not vary the impact magnitude or the number of impacts applied, but does give

    a good representation of the average pull-off force for the prescribed magnitude with

    a single impaction and provides another average value for surgeon impaction

    magnitude, which will both be of use later when comparing this study to those that

    follow on in this part of the chapter. The overall study showed that a clean and dry

    taper provides the optimum assembly condition to facilitate maximum junction

    strength.

    The next study was carried out by Heiney et al (2009) [31] and had a much larger

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    assembly forces. The average surgeons impact force applied during assembly in

    this study is roughly twice that of either of the two previous studies showing a large

    range of magnitudes arising across the different surgeons used to create the

    averages in each study.

    Heiney et al. (2009) [31] found there to be a difference in junction strength between

    using one impaction and two impactions but found no difference when applying

    more than two impactions. This finding compliments one of the findings from the

    study by Pennock et al. (2002) [29], in that the first impaction provides the majority

    of the junction strength with subsequent impacts providing a small but additional

    increase. Heiney et al. (2009) [31] also found that the junction strength increased

    along with the impact magnitude thus adding weight to this original finding by

    Pennock et al (2002) [29]. It is unfortunate that neither Pennock et al (2002) [29]

    nor Heiney et al. (2009) [31] provided the impact forces in newton values instead of

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    studies. The relevant data acquired from this study is shown in Table 4 [10] as

    follows.

    Table 4: Data from Rehmer et al. (2012) Study [32], [10]

    Using pull-off and twist-off disassembly tests, Rehmer et al. (2012) [32] found that a

    single impact of a minimum of 4KN (kilo-newtons) was required to ensure optimum

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    head connections on a modular shoulder prosthesis. In this study, they use a

    surgeon to try to acquire an average assembly impact force for which they can

    design a drop rig. The drop rig is then used to assemble their specimens with a

    constant impact force but under different conditions (i.e. dry or wet) prior to

    disassembly testing. The surgeon assembled 6 shoulder taper junctions using a

    mallet and impactor (the same as is used in a modular femoral hip assembly), and

    Loch et al. (1994) [8] then measured the force required to pull the joints apart. They

    repeated this process with the surgeon and the same six specimens 16 times to

    acquire their average pull-off value, which they then used to set a drop rig to

    assemble the test specimens to replicate this average pull-off value (under control

    conditions). It is acknowledged the average pull-off values may have been affected

    by the reduction in strength that can be experienced when repeatedly assembling

    and disassembling the same specimens. The pull-off forces, from the surgeon s

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    head is correctly seated on the neck taper before providing a single impact of no

    less than 4KN, which is axially aligned with the taper axis. The impact should also

    not exceed 6KN to ensure that it does not stray into the region where it could cause

    internal damage to the patient or damage to the tapers, as mentioned previously.

    The findings from this review will be used to guide the design of the device

    proposed in this project, and to aid the assembly of MTHRs. The next step in the

    process is to establish the user needs and hence design requirements for such a

    device.

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    4. USER NEEDS & DESIGN REQUIREMENTS

    It is now clear from the Literature Review that there is room for improvement in the

    assembly of head/neck taper junctions in MTHRs. This room for improvement

    grows and becomes a serious problem when considered in the use of large

    diameter bearings, particularly MoM bearings. Even if manufacturers applied perfect

    tolerances, surfaces finishes and optimum neck taper diameters it is still essential to

    correctly assemble this taper junction to benefit from these improvements. It is clear

    from the wide ranging impact forces applied by different surgeons that it is unfair to

    expect them to be able to repeatedly provide the very specific forces and alignments

    required for the optimum assembly of MTHRs using the current tools at their

    disposal (mallet and impactor). Therefore the development of a new device is

    completely justified.

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    producing a Product Design Specification (PDS), which can then be used to guide

    the next stage of the project.

    4.1 Fundamental Design Requirements

    These design requirements have been extracted directly from the findings in the

    literature review and form the foundation and basis for the entire design, i.e. the

    design must achieve all of these requirements to be successful. The fundamental

    design requirements are listed as follows.

    1. Ensure axially aligned seating of head on neck taper axis prior to impaction

    2. Impact must be delivered in axial alignment with neck taper axis

    3. Deliver impact force of between 4KN and 6KN, adjustable to 0.5KN

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    minimum force, compared to larger metal taper junctions that may require slightly

    more force for optimum assembly.

    The fourth requirement involves trying to concentrate the impact to the taper

    junction and not down the stem where it could cause damage to the stem/femur

    interface. It is also intended to ensure the efficient transfer of impact energy into the

    junction and not to have it wasted through dissipation into the surrounding region.

    4.2 Establishing and Defining User Needs

    Since the fundamental design requirements had now been established, the next

    step was to look beyond these fundamentals to establish other design requirements.

    It is extremely important to involve the end user in the design of anything to ensure

    that it meets their specific needs, so a survey was used to try to gather design

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    Figure 9: Orthopaedic Surgeon Survey Introduction

    After the introduction to the survey, the first question posed attempted to gain an

    understanding of the size of the range of different hip implants that were being used

    and whether or not they were cemented or cement-less. This would influence

    whether or not the device would be designed solely for use with a very popular

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    The next task was to establish the range of femoral head sizes. This was important

    to establish so that the device could be designed to facilitate the most common

    head sizes. This also fulfils the purpose of establishing a general impression of the

    current use of large diameter (>36mm) MoM bearings, given their associated

    problems previously mentioned in the literature review. The wording and layout of

    this question is shown in Figure 11 below.

    Figure 11: Surgeon Survey, Q2

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    Figure 12: Surgeon Survey, Q3

    The next question aims to establish the size of the access area or incision in the

    patient that the device must fit and function inside. The average size is 10cm, so this

    question looks to see if many surgeons work under or above this incision size. This

    question is shown in Figure 13 below.

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    Figure 14: Surgeon Survey, Q5

    The next question was not so much based on the establishment of design

    requirements for the device, but more so at gathering data to compare with the four

    studies listed at the end of the literature review. It was acknowledged that the

    responses could not be looked upon too strongly, as the information provided by the

    surgeons is opinion-based and thus is quite subjective. This question is shown in

    Figure 15 below.

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    question was provided in a format where the participant rates the level of

    importance out of 10. This question is shown in Figure 16 below.

    Figure 16: Surgeon Survey, Q7

    The final question allowed the surgeons to propose any features that they felt

    should be included in the design of the device. The intention of this question was to

    give the user an opportunity to directly propose things that were of importance to

    them so that the design would have some sort of user-centred-design approach.

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    However, a brief analysis of the survey has shown that there is a significant amount

    of very relevant data available which would be of great value to the future

    development of the device. A summary of the survey response is contained in

    Appendix 1.

    The original plan had been to gather the findings from the literature review and the

    feedback from the survey and allow this to contribute to the PDS, but as mentioned

    above this was not possible so for this reason none of the feedback from the survey

    influenced the PDS. The PDS will now be discussed in more detail in the next

    section.

    4.3 Product Design Specification

    The purpose of a PDS is to provide the designer with a list of design requirements

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    Figure 18: Stuart Pughs Design Core [33]

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    4.3.2 Commercially available designs and patent research

    As mentioned previously, the only commercially-available designs for the assembly

    of the head/neck taper junctions are the orthopaedic hammer and impactor

    methods. An in-depth patent search was carried out to establish what other like-

    minded or similar and applicable designs already existed. Samples of some of the

    more interesting designs are shown as follows. Some of these have made an

    influence on the design of the device rig as can be seen later on in the Design and

    Development stage.

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    Figure 23: Device for Handling Hip joint Heads [39] Figure 24: Head holder and impactor [40]

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    this case involved delivering an impact or maintaining an alignment. Rough notes

    were taken during the patent search to keep track of any good ideas, which could

    then be applied directly or manipulated to fit into the device proposed in this project.

    Figure 29 and Figure 30, shown below; display two more applicable technologies

    that could be of use for the concept generation stage later in the project.

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    4.3.1 Medical device standards review

    Medical Device Classifications exist to grade the level of risk that a medical device

    poses to a patient or user; the higher the grading, the more stringent the regulations

    imposed on the development and manufacture of the device. There are different

    classification systems for both the EU (EU/ISO [46]) and USA (FAA/ISO [47]), and

    as the risk or grading increases, so too do the design regulations imposed by the

    standardisation bodies to meet their audit requirements. The two grading streams

    are illustrated side by side in an extract from medical Device Design by P.J.

    Ogrodnik [48], as shown in Figure 31 below.

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    for clinical trials, so the standards review is of greater value further down the line in

    future clinical design and development of this device.

    4.3.2 Generation of PDS

    The PDS pooled all of the design requirements acquired through the project so far,

    and so took information from the Literature Review, the Surgeons Survey (although

    left open, pending response from participants), the Standards Review, and the

    patent and existing design research. The PDS is a working document, and can be

    added to and edited as future work progresses on the development of the device

    proposed in this project. The most up-to-date version of the PDS is included in

    Appendix 2 [10].

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    5. DEVELOPMENT & EVALUATION

    This chapter of the report looks at the generation, evaluation and development of a

    concept for the device proposed in this project. It then examines the concept

    generation, development, detailed design and manufacture of a proof-of-concept

    Testing Rig, to verify the functionality of the overall device concept established in

    the first phase.

    5.1 Concept Generation and Evaluation

    Since the PDS created in the previous chapter was quite detailed and in-depth, not

    all of the points covered will be relevant at this stage in the design. It is for this

    reason that the PDS was condensed down into its more critical attributes. This

    created a less constrained environment to work in when generating creative

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    5.1.1 Initial Product Design Specification (PDS)

    A full PDS was developed for a prototype device aimed at use in clinical trials but for

    the purpose of this project, which will only be tested in laboratory conditions, the

    original PDS was condensed down. This was carried out in order to focus on the

    fundamental design requirements and to allow more creative freedom for concept

    development. The PDS used for the project at this stage is shown below.

    1. Performance

    1.1 Must hold head taper axially aligned with neck taper axis

    1.2 Must deliver impact axially aligned with neck taper axis

    1.3 Must deliver adjustable impact from 4KN - 6KN to +/- 0.5KN

    1.4 Must isolate impact to head-neck taper junction

    2. Customer

    2 1 Must be able to use with varying head size

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    An initial sketch was made at this point to record any design ideas that had come to

    mind so far. This initial sketch is shown in Figure 32 as follows.

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    5.1.3 Radial Thinking

    Radial thinking was used to expand on different concepts and help to develop and

    record different concept ideas. Each of the four key objectives, A to D, were listed in

    a bubble in the middle of a blank page and ideas stemmed outwards from this

    starting point. Two examples of this exercise are shown as follows. Figures 33

    shows the development of Objective B, and Figure 34 shows the development of

    Objective C.

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    Figure 34: Development of Objective C

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    (A1). Three Prong Flexible Support and Centring Cone

    Figure 35: Three Prong Flexible Support and Centring Cone Sketch

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    (B). Holding impactor axially aligned with neck taper axis

    *DATUM* Surgeon holding impactor aligned by hand

    (B1). Bent Hex-Rod

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    (B3). Split Cup/Split Mould

    Figure 39: Split Cup/Split Mould Sketch

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    (C2). Slide Hammer - To Charge Spring

    Figure 41: Slide Hammer - To Charge Spring Sketch

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    (C4). Electro-Magnets (Solenoid Actuator)

    Figure 43: Electro-Magnets Sketch

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    (C6). Screw Mechanism - To Charge Spring

    Figure 45: Screw Mechanism - To Charge Spring Sketch

    (C7) Lever To Charge Spring

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    (C8). Pneumatic Piston

    Figure 47: Pneumatic Piston Sketch

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    (D2). Mechanism to Hook around the Lips at Base

    Figure 49: Mechanism to Hook around the Lips at Base Sketch

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    The result of this exercise is the selection of concepts to address each of the four

    key performance requirements. This exercise was carried out using an excel spread

    sheet and is shown on the following page in Table 6. The highest scoring concept

    from each of the four sections was highlighted in yellow.

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    As the outcome from Table 6 has shown, the following sub-system concepts have

    been chosen and are listed as follows.

    (A1) 3 Prong Flexible Support + Centring Cone

    (B1) Bent Hex-Rod

    (C8) Pneumatic Piston

    (D1) Rod Inserted In Stem Hole

    Since the main function of the device is key requirement C (Must deliver adjustable

    impact from 4KN to 6KN, to +/- 0.5KN) and the second and third ranked ideas in

    this category, which were Electro-Magnets (C4) and Lever to charge spring (C7),

    also scored relatively high, all of the top three designs in this category will be looked

    into in more detail before finally settling on a single concept. It is also worth

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    in the design. This investigation was performed by looking into existing products that

    were applying these three powering methods, and checking the suitability of each

    method for the device in this project. These are examined as follows, starting with

    the Pneumatic approach.

    Pneumatic Piston

    One of the best products to look at to examine the functionality of the different

    methods of powering a device that provides an impact is the Nail Gun. A pneumatic

    Nail Gun is shown in Figure 50 [49], below.

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    can become quite complex and expensive when designing and manufacturing. This

    project is trying to provide the simplest possible powering method, so for this reason

    the pneumatic approach does not seem to be the best fit.

    Electro magnets

    Electro magnets, or specifically in this case electro solenoids, can be used to

    electrically initiate magnetic fields, which can propel objects to create an impact.

    This type of system is explained once again using a nail gun example in Figure 51

    [49] below.

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    that may be close to the device when in use. This also, much like the pneumatic

    option, this greatly increases the complexity in the design and means that the device

    will have to abide by more constraining standards during the design process. This

    will add difficulty and complexity to the future work on a clinical device, and thus

    rules out this technology as a possible option.

    Lever to Charge Spring

    The final option for powering the device is a charged spring, which is compressed

    using mechanical advantage, such as a lever system. An electrically powered

    mechanical spring system is shown in Figure 52 below, again using an example of

    an electric powered nail gun.

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    more sustainable and reliable with no dependency on other inputs such as electricity

    and compressed air. The surgeon could use their energy to provide the work

    required to compress/charge the spring could be made easier with a leverage

    system. An example of the employment of this sort of powering mechanism is

    demonstrated in a simple can-crushing device as shown in Figure 53 below.

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    5.1.7 Development of Final Powering Concept

    Now that the method which would power the device had been chosen, the next step

    was to develop the design in more detail to prove that it could actually work.

    There were three main design objectives that had to be met for the device to be able

    to function. The first was to confirm the final leverage method to compress the

    spring. The second was to come up with a way in which the device could deliver an

    adjustable impact (which had not been focussed on previously). Finally, the third

    objective was to design a trigger/release mechanism to actuate or initiate the

    impact.

    Mechanical Leverage System

    This stage involved more sketching and research, but this time just focussed on

    leveraging systems. Items such as hand-operated juicers, in which they compress

    the fruit to extract juice were seen as applicable to the design of the device A

    M h d l i i d d l f f h

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    More can-crusher products were also investigated, and an example of one of the

    sketches trying to use this approach is shown in Figure 55 below.

    Figure 55: Adapted Can Crusher Sketch

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    Figure 56: Corkscrew Lever System Sketch

    This sort of mechanism could be attached onto the end of the device, and the

    surgeon could use both hands to push the levers down to the sides of the device.

    This would compress a spring that can be held in place by a locking mechanism and

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    Figure 57: Twisting Adjustment and Release Concept Sketch

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    Figure 59: Spring Compression adjustment System Sketch

    Trigger/Release Mechanism

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    Figure 60: Slotted Trigger Release Mechanism Sketch

    Selection of the Concept for Objective C

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    Selection of the Concept for Objective C

    The final selection of the concept for the device is shown in Figure 63 below. This

    incorporates the corkscrew method of leverage seen in Figure 56 previously,

    positioned out of sight to the left of the lower sketch within Figure 63 below. It also

    incorporates an adjustable force mechanism behind the spring and a trigger

    mechanism as shown.

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    Figure 64: Tubular Casing Surrounding Spring Sketch

    5.1.8 Mechanical Feasibility of Chosen Concept

    Before progressing further, the leverage mechanism must be validated theoretically

    to ensure that it could realistically function and be used by a surgeon. A rough

    sketch of the device moving through the charging motion is shown in Figure 65

    The leverage force has been simplified and marked out on the Figure 56 which is

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    The leverage force has been simplified and marked out on the Figure 56 which is

    shown again below and renamed Figure 66 for clarity.

    Figure 66: Force Balancing Free Body Diagram

    Using static force balancing analysis, Equation 1 can be derived and is as shown

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    Using static force balancing analysis, Equation 1 can be derived and is as shown

    below.

    =

    (1)

    Substituting in the values;

    2 =(6 10) 0.01

    0.3

    Solving for F2;

    2 = 200

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    Substitute in known values;

    100 = (9.81)

    Rearrange and solve for m;

    = 10.2

    Where;Kg = Kilogram

    This means that a 10.2Kg weight could be hung on one side, and it can be

    Where;

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    F= Impact Force

    t= Impact duration (time over which impact occurs)

    m= Mass

    v= change in velocity

    The force used in this equation is 6KN, since it is the highest end of the scale.

    The mass used for this calculation was based on the average mass of an

    orthopaedic mallet, which was found to be approx. 0.4Kg (kilograms).

    Since the impact duration is unknown, a previously-recorded impulse value was

    taken from a PhD student at the University of Bath who had carried out a study on

    impacts and had acquired this data for 2KN, 4KN and 6KN impact forces. It should

    be noted that the tip material used during these tests is unknown, and this may have

    a large effect on the testing results. The impulse recorded for 6KN was 11.1Ns

    (newtons per second)

    Now that the initial velocity has been found, this can then be used to find the kinetic

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    energy (KE) at the point of impact. This can be found using Equation 4.

    =

    (4)

    Substituting in the known values;

    =1

    2(0.4)(27.75)

    Solving for KE;

    Since both k and x are both unknown at this point, it is decided to use a spring

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    displacement (x) of 60mm (millimetres) or 0.06m (meters). This has been chosen as

    this displacement should leave enough room for sensitive adjustments to be made

    to the spring later in the design process.

    Substituting these values into Equation 5;

    154.0125 =1

    2(0.06)

    Rearranging and solving for k;

    = 85562.5/

    had to be proven experimentally first. This was to be proven using a testing rig

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    designed purely for this purpose.

    The first step in this process was to size a spring. The k value found in the last

    section and the displacement of approx. 60mm was used to source a spring from

    Lee Springs. The specifications for this spring are shown in Appendix 3.

    It was also decided to use three magnitudes of impact force during testing. This was

    done so that a line could be graphed through the three averaged points on an

    impact impulse vs. spring compression displacement chart to show the predictability

    and repeatability of the spring method. It could also be used as an opportunity to

    explore the effects of different tip material on the impactor, and what effect they

    have on the process.

    To simplify the design, an Instron Impact Loading machine (30KN max load), as

    shown in Figure 67 below, would be used to compress the spring to the required

    The key functions of the testing rig were to allow the Instron to compress the spring,

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    to hold the spring in its compressed state and then to allow the spring to be

    released over a load cell in order to measure the impact force administered.

    One of the early sketches in the concept development stage for this rig is shown in

    Figure 68 below.

    Figure 68 includes a lever release mechanism, which is actuated by twisting a collar

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    fixed on the outside of the top cylinder (illustrated in the top left of the Figure). It also

    features a threaded shaft with a threaded stopper disc that can be adjusted to allow

    varied spring compression displacements. The design was refined further to try to

    reduce its complexity, so as to save time during the detailed design phase and

    manufacture. Figure 69, below, shows the refined version of the concept for the

    testing rig.

    The device could be removed from a solid plate base on which a load cell would be

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    secured, and then mounted using a special jig. This would be done so as to allow

    the Instron to push down the body of the device with the impactor tip placed on a

    fixed spigot so that the spring could be compressed inside.

    Various trigger mechanisms were generated, with the final idea being a side-acting

    lever. This lever would then fit into one of three specifically laid out slots that were

    designed to allow the spring to be held in a compressed state under 6KN, 4KN and

    just over 2KN of load in the Instron. Figure 70 below, shows the first concept,

    followed by Figure 71, which shows the next development, and then finally Figure

    72 showing the simplified lever release mechanism.

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    Figure 71: Lever Design Development

    5.2 Detailed Design

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    The Test Rig concept could now be developed further on SolidEdge. Stress

    calculations and considerations could also be made for the manufacture of the

    device, and could be followed by, the provision of draft drawings to the Machine

    Shop and the manufacture of the testing rig.

    5.2.1 Solid Modelling

    The design had three specific compression displacement slots, slotted into an

    internal impactor rod (visible in Figure 73 below protruding from the top of the

    device), which was propelled by the release of the compressed spring. An isometric

    view of the finished model is shown in Figure 73 below, with fasteners removed for

    clarity. The assembled model is shown at the 6KN load setting.

    5.2.3 Draft Drawings

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    Once the final solid models had been completed a full set of draft drawings were

    produced for the design. These drawing are listed in Appendix 4 and can also be

    found towards the end of the report.

    5.2.4 Manufacturing

    The SolidEdge solid modelling program allowed the interaction between the parts to

    become visible, and the manufacturing methods could be taken into consideration.

    The Testing Rig was manufactured in a machine shop based in the University of

    Bath and so the development of the design on SolidEdge was reviewed in stages

    with the Machine Shop Technician that would be manufacturing the Rig. This helped

    to simplify the manufacturing stage, as the design was customised to make use of

    the most easily-available materials that were currently in stock The device was

    6. TESTING

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    This section of the report covers the calibration of the load cell and the testing

    carried out on the Rig. The Results from this testing will be discussed in the next

    Chapter.

    6.1 Calibration of the Load Cell

    The first step was to calibrate the Load Cell, which would be used to measure the

    impact loading during the Rig testing. This was performed to ensure that the load

    cell was fully functional, and also to establish a scale factor so that the output, when

    Rig testing, could be provided in newton instead of in volts, which is what the load

    cell measures.

    An Instron loading machine (max loading of 30KN) was programmed to descend

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    Figure 74: First Calibration Test plot of Voltage Vs. Time

    This Data was then plotted and a trend line added across the average points so that

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    the slope, and hence the scale factor, could be established. This chart is shown in

    Figure 75 below.

    y = -2678.5x + 13.413

    0

    1000

    2000

    3000

    4000

    5000

    6000

    7000

    8000

    9000

    -4.0000 -3.0000 -2.0000 -1.0000 0.0000

    Load Vs. Voltage

    Load Vs. Voltage

    Linear (Load Vs. Voltage)

    6.2.1 Procedure

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    The testing involved measuring and recording several variables. These variables

    are listed as follows.

    1. Final displacement of spring during spring compression on Instron

    2. Final load recorded during spring compression on Instron

    3. Impact data recorded via LabView

    Variable 1 and 2 were read directly from the computer monitor hooked up to the

    Instron. The LabView data was analysed later using Matlab.

    The Testing procedure involved several steps. The first step involved slotting the

    required material tip into the hole at the tip of the impactor rod and then holding it in

    place with the grub screw. The next step was to mount the Spring Section of the

    Testing Rig onto the test fixtures, which had been designed and manufactured as a

    part of this project. They held the rig in a safe and secure position during the

    Figure 77, as follows, shows the Spring Section of the Device fixed securely in the

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    mounting points.

    Figure 77: Spring Section in mounting points, close up view of top, close up view of bottom

    ger

    The top fixture was then lowered to the point where the device was securely in

    g-clamps. Figure 78, as follows, shows the base plate mounted to the table with and

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    without the rubber base and finally with the spring section sitting top of the base

    structure prior to the assembly nuts being screwed attached.

    accessed by copying the following file link into the address bar on an internet

    b

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    browser.

    https://www.dropbox.com/s/6o668aoik0xtirz/video-2013-08-21-12-46-46.mp4

    6.2.2 Data recorded

    The materials were changed over after each test. The material testing order was

    steel, nylon, PVC rubber and then back to steel again, which started off the next

    round of testing. This allowed the rubber time to return to its original shape and

    elasticity, as it temporarily deformed following impaction.

    Figure 79, as follows, displays the displacement and load data which was recorded

    during the Rig testing on an excel spread sheet. This figure also contains notes that

    were taken to record changes in material tip samples following the failure of a

    material tip during a test

    https://www.dropbox.com/s/6o668aoik0xtirz/video-2013-08-21-12-46-46.mp4https://www.dropbox.com/s/6o668aoik0xtirz/video-2013-08-21-12-46-46.mp4https://www.dropbox.com/s/6o668aoik0xtirz/video-2013-08-21-12-46-46.mp4
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    The impact data recorded using LabView was extracted from the text file output

    sing Matlab and then inserted into an e cel spread sheet for anal sis The

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    using Matlab and then inserted into an excel spread sheet for analysis. The

    parameters analysed for each impact test were as follows.

    1. Peak Force recorded during impact in Newtons

    2. Duration of Max Peak in Seconds

    3. Duration of impact

    These were extracted from graphs generated on Matlab and then fed into the excel

    spread sheet. Figure 80, below illustrates the 3 parameters recorded from these

    graphs.

    vibration damping. The rubber can be considered as a representation of the soft

    tissue in a patient as it absorbs some of the impact force from the Testing Rig

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    tissue in a patient as it absorbs some of the impact force from the Testing Rig.

    However, it must be noted that an error occurred and the steel test wrote over the

    Nylon test, hence why they both have the same data in the single round of testing

    without the rubber base. The analysis of this data is covered in the next section of

    the report.

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    Figure 82: Extrapolated Load Cell Data, 4KN and 6KN

    The extrapolated load cell data for the 4KN and 6KN loads are shown in Figure 82

    as follows.

    7. RESULTS AND DISCUSSION

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    This section of the report covers the analysis and discussion of the Instron and Test

    Rig Data acquired in the previous chapter and also an evaluation of the Testing Rig.

    7.1 Evaluation of Instron Data

    During the testing phase, some notes were made on the spread sheet where the

    Instron data was being recorded. For example, as can be noted from the comments

    on Figure 79 shown previously, both PVC and Rubber failed on the first round of

    testing at 4KN of loading on the Instron. New replacement tips for both materials

    failed after Round 2 (their first impacts) at 4KN loading. Figure 83 below shows

    images of the PVC and Rubber Tip materials which were destroyed on Round 1 of

    It was also clear from the average max displacement figures shown previously in

    Figure 79 that the Rubber Tip Sample compressed during loading on the Instron to

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    Figure 79 that the Rubber Tip Sample compressed during loading on the Instron to

    approx. two thirds of its original thickness. This pre-deformation may have reduced

    the ability of the material to lower the impulse force (as it would normally prolong the

    impact duration of the peak force as seen from the load cell data).

    There was some error present in the inconsistency at the point at which the load

    and the displacement were reset to zero on the Instron before the spring was

    compressed. There was a learning curve during the experimentation and it was

    discovered towards the end of the testing that the best time to reset the load and

    displacement readings to zero, before compressing the spring, was to watch to see

    the top of the Impactor rod move in relation to the devices outer structure. This way

    it was sure to be the point at which the spring was about to experience actual

    compression, as opposed to the rig just settling out. However, even taking this error

    extremely large effect on the duration of the max peak which in turn affects the

    resulting calculation of the impulse force. It is important to note that when using

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    resulting calculation of the impulse force. It is important to note that when using

    these original impulse values the tip material used in the study in which the impulses

    were recorded, was not provided to this project. This would explain to some degree

    the significantly high impact forces recorded, especially with steel, which in many

    cases exceeded the measurement band of the Load Cell. As per the specifications

    on the Load Cell it has a max measurement capacity of 5,000 lbs (or 2267.69 Kg, or

    22,246 N). The Load Cell can only measure up to 10 Volts which works out as

    approximately 26,785 N, when referring back to the scale factor. It is clear that the

    bandwidth of the Load Cell could not cope with the large magnitudes of force being

    delivered. This brings into question the remaining results as the forces being

    recorded were far greater than what was to be expected. When the Steel testing

    was performed for the 6KN loading it was deemed that the load cell had been

    cell data) due to the extremely sudden momentum change, as it bounces off the

    load cell.

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    oad ce

    7.3 Evaluation of Testing Rig

    Despite the greater peak forces than expected, the Testing Rig performed extremely

    well given that the load cell failed before the Testing Rig. It functioned safely under

    the loads and was quick and simple to use. The only improvements for future use

    would be shortening the four threaded studs holding the spring section to the base

    plate as this could be a little time consuming screwing the nuts on and off the long

    sections when assembling and disassembling the rig during tests. The edge of the

    release lever that fitted into the slots came under great deal of stress and future

    designs may benefit from heat treating to harden the edge to reduce wear when

    i th l d l d

    8. CONCLUSIONS

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    This section looks at the overall outcome from the different sections of this project

    and their contribution to the overall aim of designing and developing a medical

    device to improve the assembly of head/neck taper junctions in MTHRs.

    To start with, a significant literature review was carried out for this project which

    resulted in the definition of fundamental design requirements for the proposed

    device. These requirements were based on an analysis of the most relevant and

    credible sources available.

    The user needs and design requirements developed in the next stage of the project

    were of significant value, particularly the Surgeons Survey and the PDS. The

    Surgeons Survey, although the feedback came late in the projects life it is still of

    great value to this project and other studies in the region of MTHR taper junction

    l i Th S S th d l t i f ti f

    The development and manufacture of the Testing Rig has produced a finished

    device which can be reused for future testing or can be manufactured again on a

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    g g

    smaller scale to suit a smaller spring size. All of the manufacturing draft drawings

    are contained in the Appendix and only need to have the dimensions scaled down

    and another smaller version could easily be produced.

    The data acquired from the testing phase has shown the dramatic influence that the

    tip material has on the impulse force. It has also uncovered improvements for future

    testing, such as impacting a head/neck assembly fixed to a load cell and using a

    smaller spring size, followed by comparing the assembly and disassembly data with

    specimens assembled using a mallet and impactor.

    Overall, this project has produced a detailed final design concept which can meet

    the design requirements established in this project. It has also produced a testing rig

    capable of aiding the laboratory development of this design concept. The feasibility

    10. REFERENCES

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    3. Charnley, J., Surgery of the hip-joint: present and future developments. Br Med J,1960. 1(5176): p. 821-6.

    4. Delaunay, C. The Charnley Total Hip Replacement - The Gold Standard of primaryhip replacement, 36 years on. 1998 [cited 2013 May]; Available from:http://www.maitrise-orthop.com/corpusmaitri/orthopaedic/mo83_delaunay/delaunay_us.shtml.

    5. UK, S. Hip Replacements. 2013 [cited 2013 August]; Available from:http://www.stryker.co.uk/index/st_pag_patients-home/st_pag_patients-hip/st_pag_patients-hip-replacement.htm.

    6. McCarthy, J.C., J.V. Bono, and P.J. O'Donnell, Custom and modular components inprimary total hip replacement. Clin Orthop Relat Res, 1997(344): p. 162-71.

    7. Smith, E. Mr. Everet Smith, Innovations in Total Hip Replacement. 2008 [cited 2013May].

    16. Medical Device Alert: MDA/2012/036 - All metal-on-metal (MoM) hip replacements,MHRA, Editor. 2012: United Kingdom.

    17 Bishop N E F Waldow and M M Morlock Friction moments of large metal on

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    17. Bishop, N.E., F. Waldow, and M.M. Morlock, Friction moments of large metal-on-

    metal hip joint bearings and other modern designs. Med Eng Phys, 2008. 30(8): p.1057-64.

    18. Langton, D.J., et al., Taper junction failure in large-diameter metal-on-metalbearings. Bone Joint Res, 2012. 1(4): p. 56-63.

    19. Goldberg, J.R., et al., A multicenter retrieval study of the taper interfaces of modularhip prostheses. Clin Orthop Relat Res, 2002(401): p. 149-61.

    20. LLP, P.S. Mismatched Hip Replacement Components. 2012 [cited 2013 August];Available from: http://www.pryers-solicitors.co.uk/blog/clinical-negligence-news/mismatched-hip-replacement-components/.

    21. Fessler, H. and D.C. Fricker, A study of stresses in alumina universal heads offemoral prostheses. ARCHIVE: Proceedings of the Institution of MechanicalEngineers, Part H: Journal of Engineering in Medicine 1989-1996 (vols 203-210),1989. 203(18): p. 15-34.

    22. Shareef, N. and D. Levine, Effect of manufacturing tolerances on the micromotion atthe Morse taper interface in modular hip implants using the finite element technique.Biomaterials, 1996. 17(6): p. 623-30.

    23. Lieberman, J.R., et al., An analysis of the head-neck taper interface in retrieved hipprostheses. Clin Orthop Relat Res, 1994(300): p. 162-7.

    32. Rehmer, A., N.E. Bishop, and M.M. Morlock, Influence of assembly procedure andmaterial combination on the strength of the taper connection at the head-neckjunction of modular hip endoprostheses. Clin Biomech (Bristol, Avon), 2012. 27(1):p 77 83

    http://www.pryers-solicitors.co.uk/blog/clinical-negligence-news/mismatched-hip-replacement-components/http://www.pryers-solicitors.co.uk/blog/clinical-negligence-news/mismatched-hip-replacement-components/http://www.pryers-solicitors.co.uk/blog/clinical-negligence-news/mismatched-hip-replacement-components/http://www.pryers-solicitors.co.uk/blog/clinical-negligence-news/mismatched-hip-replacement-components/http://www.pryers-solicitors.co.uk/blog/clinical-negligence-news/mismatched-hip-replacement-components/
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    p. 77-83.

    33. S, P., Total Design: Integrated methods for successful product engineering. 1991:Addison-Wesley Publishing Company Inc.

    34. Martin, J.L., et al., Capturing user requirements in medical device development: therole of ergonomics. Physiol Meas, 2006. 27(8): p. R49-62.

    35. Controlled Force Mallet. 24/12/1992.

    36. Controlled Force Impacting Device. 31/03/2006.

    37. Handling Device for hip Prosthesis implant. 2/3/1988.

    38. Hip Joint Prosthesis and Fitting Tool. 24/10/1997.

    39. Device for handling ball heads of joint prostheses. 2003.

    40. Femoral Head Holder and Impaction Instrument and Method of use. 2003.

    41. Method of applying a femoral head resurfacing prosthesis. 2007.

    42. Geraet zum Eindruecken von Heftzwecken. 1952.

    43 Hand-held nail gun has helical driving spring made of tubular spring steel 2007

    11. APPENDICES

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    APPENDIX: 1

    SURGEONS SURVEY RESPONCE

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    APPENDIX: 2

    PDS [10]

    1. Performance

    1.1 Must axially aligned seating of head on neck taper axis prior to impaction

    1.2 Impact must be delivered in axial alignment with neck taper axis

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    p g p

    1.3 Deliver impact force of between 4KN and 6KN, adjustable to 0.5KN

    1.4 Must try to isolate majority of impact to head/neck taper junction

    2. Customer

    2.1 Must be able to facilitate a range of different head sizes (Determine using Surgeons Survey)

    2.2 Must be able to fit into the exposed cavity in the patient created by the incision (Surgeons

    Survey will determine the exact figures)

    3. Medical Standards

    3.1 Must comply with ISO13485:2003/AC:2007, has been