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Automatic Mill Cutter Insert Replacement Members: Kisa Brostrom Joseph McKenna Andrew Clements Connor McBride Josiah Wai Nicholas Wood Trevor Douglas Aaron Thonney Conor Moloney Scott Olivares

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Page 1: Full Boeing

Automatic Mill Cutter Insert Replacement

Members:

Kisa BrostromJoseph McKennaAndrew ClementsConnor McBride

Josiah WaiNicholas WoodTrevor DouglasAaron ThonneyConor MoloneyScott Olivares

Page 2: Full Boeing

OBJECTIVE

● End mills use 10,000+ inserts per week

used to cut titanium

● Boeing workers spend too much time and

effort preparing end mills

● System that automates the removal and

replacement of 85 cutter inserts

Page 3: Full Boeing

DESIGN APPROACH

● Split whole team into three

subsections

a. Screwdriver

b. Carousel

c. Programming

● Set high but realistic time/design

goals

● Transition into a complete integration

● Transition to programming

Page 4: Full Boeing

A.M.C.I.R. - Programming and Electronics

Programming:Josiah Wai

Conor Moloney

Integration:Andrew Clements

Nicholas Wood Connor McBride

Scott OlivaresTrevor Douglas

Joseph McKennaAaron ThonneyKisa Brostrom

Page 5: Full Boeing

Objectives● Learn the programming languages

○ TIA portal and FCT

● Program all the subsystems

○ Must work independently

○ Linear Actuator

■ Move tool

■ Rotate tool

○ Carousel

■ Rotate carousel

■ Actuate pneumatic arm

○ Screwdriver

■ Actuate screwdriver

■ Insert/remove screw

Page 6: Full Boeing

Previous Work● Programming

o Linear actuator and carousel basic TIA programming

● Untested basic/plan Only actuator configured

o screwdriver No code

● Electronicso Two PLCs

Wired separatelyo Grounded to boltso No sensorso No HMI

Page 7: Full Boeing

Final Product● Programming

o All systems home and position correctly

o Linear Actuator both motors move tool

● rotational motor underpowered

o Carousel Calibrated to rotate 1 cutting

insert per increment Jerkiness of movement

eliminated with higher power motor.

o Screwdriver linear and rotational

calibrated requires an I/O module to

obtain sufficient activation of all signal commands (screw & unscrew)

Page 8: Full Boeing

Final Product ● Pneumatic Piston and Vacuum Generator piston and vacuum by solenoids through

PLC 2 pneumatic valves

● with 4 actuators Vacuum system improved by higher

pressure inlet supply Piston position improved by ordering

FESTO module for PID dynamic control. (Currently operates with position control.)

● Electronicso Overhauled electronics board

PLCs interconnected and to HMI All components fused for safety Cleaned and organized wiring with

grounding/terminal blocks Grounded with aluminum plate

o Sensors for subsystems 2 contact limit switches 2 inductor switches 1 reed switch All for positioning and homing

Page 9: Full Boeing

Electronics Layout● Components

o 24 VDC power supplieso carousel, linear rail, and worm

gear motor controllerso 2 PLCso HMIo Communication moduleo Distributed 16 signals I/O moduleo ethernet cabling for

HMI/communication module/PLC connections and (test phase only) motor controller PC diagnostics.

o Wiring connection to all sensor and actuators

Page 10: Full Boeing

Combined PLC Wiring Diagram

Page 11: Full Boeing

Future Work● Programming

o Functionality and control-via-PLC/HMI demonstrated for every system.

requirements for full, independent automation:● increase mechanical soundness w/ higher

power motors● time in order to program

proves mechanical soundness o Full PLC-PLC communication

Currently only a finite number of binary data can be transferred. Requirements for full communication:

● time to learn Siemens communication protocol

● either I/O module or communication module● Electronics

o Mount HMI and E-Stop Machine or water jet aluminum plate

o cover the electronics board Protect with a full non-metal housing

Page 12: Full Boeing

Bill of Materials

Page 13: Full Boeing

A.M.C.I.R. - Screwdriver Subsystem

Members:

Trevor DouglasAaron ThonneyNicholas WoodScott Olivares

Page 14: Full Boeing

Objective

● Loosen and fasten Torx screws in a cutter body

● Torque screws to 35 in-lbs without cross

threading errors

● No time constraints related to performance

● Integrate with carousel and cutter body linear

actuator

Page 15: Full Boeing

Previous Work

● Built a stand to support two Festo servo motors

a. One to drive a ball screw to raise/lower an actuator

b. One mounted at end of beam to be used as a screwdriver

● Poor motor selection - Incorrect torques

a. Linear - Too Much

b. Screwdriver - Too Little

● Intended to remove screws and place them into a hopper

● No wiring or programming completed

Page 16: Full Boeing

Final Product● Redesign frame

○ New mounting brackets with ample adjustability

○ New Minitec linear actuator components

○ Couplers and adapters bought and manufactured

○ Adjustable feet added to new framing system

● Swap motors

○ Large servo motor - screwdriver

○ Small servo motor - linear actuator

● Flexible shaft to reduce load on cantilever beam

● Wired both servos to PLC, power, limit switch, and serial

ports

● Mounted limit switch for homing purposes

Page 17: Full Boeing

Bill of Materials

Page 18: Full Boeing

Problems

● Motors

○ Unable to read torque values

○ Lack of error detection

● Flexible shaft did not perform as

expected

● Linear actuator is imprecise

Page 19: Full Boeing

Future Recommendations

● Replace large servo motor with adequate stepper

motor and separate motor controller

○ Usable torque readings

○ Less weight

○ Direct drive

● More stability and repeatability

○ Gantry style frame

○ Purpose built linear actuator

Page 20: Full Boeing

A.M.C.I.R. - Linear Actuator Subsystem

Members:

Kisa BrostromJoseph McKennaAndrew Clements

Connor McBride

Page 21: Full Boeing

ITERATIONS

● Collaboration with all three subsections

● Create stability and support

o Add brackets which allow for no

movement

o Create a stand which aligns with

carousel and screwdriver

o Levels the linear actuator ● Troubleshoot system so system can be

programmed correctly

Page 22: Full Boeing

ITERATIONS

● Limit switches were

incorporated to home the

linear and rotational position of

the mill head mount

o solenoid

o touch

● Worm Gear Reinforced

o Mounts and shaft

remanufactured

o Addition of Bearing for

support

Page 23: Full Boeing

FINAL PRODUCT

● Rotational and Linear Motion

achieved

o Gear Box Added to Linear

● Integrated with HMI controls

● New Motor Mounts and Bearings

manufactured

● Design for Angle Stand and

Subsystem Connections finalized

Page 24: Full Boeing

FUTURE

● Addition of Vertical Actuator

● Worm Gear Refinement

o Stronger Material of Shaft

o Addition of Second Bearing

● Better Bearings

● Stronger Motors

Page 25: Full Boeing

A.M.C.I.R. - Carousel Subsystem

Members:

Kisa Brostrom

Joseph McKenna

Andrew Clements

Connor McBride

Page 26: Full Boeing

OBJECTIVE

● Remove inserts after screw

removal

● Catalog inserts for inspection

● Design easily removable insert

cataloging system

● Removal system must also be able

to replace inserts

Page 27: Full Boeing

OBJECTIVE

● Ease of ring removal

● Redesign air system for better suction

● Be dynamic enough to handle 85 inserts

● Able to adapt to more or less inserts

easily

● Allow for flawless integration with other

systems

Page 28: Full Boeing

PREVIOUS WORK

● System designed and manufactured which

o Spins carousel to store inserts

o Ejects screws through magazine

o Pneumatic actuator pushes inserts to and

from carousel and mill

● Plastic ring designed to hold 80 inserts

● System contained on Bosch frame as tabletop

● Little to no wiring or programming complete

Page 29: Full Boeing

ITERATIONS

● Top mounted components for easy access

● Components on top are hinged for ring replacement

● Redesigned ring with larger diameter to accommodate 85

inserts

● Designed suction head which conforms to insert perfectly

● Designed new pneumatic system for actuator

● Homing system designed

Page 30: Full Boeing

ITERATIONS

● Brackets for motors, carousel and homing

● Pneumatic valve system added

● Suction head casted

● Ring 3D printed

● Insert guide milled

● Bosch frame assembled

● Legs machined so system is level

● Feet added for stability

Page 31: Full Boeing

FINAL PRODUCT

● Top mounted components

● Best location of pneumatic actuator

● Hard resin casted suction head with soft silicone

surface

● Reed switch on actuator

● Dynamic mounts for ease of modification

● Stepper gear and track are compatible

● Hinge stops so system is in position

● All components’ positions can be read and moved

Page 32: Full Boeing

BILL OF MATERIALSPart Quantity Unit Price per Unit Total Price

Carousel Ring 10 sections $5 $50

Suction head mold 3 sets $1 $3

Stepper gear 1 unit $1 $1

Hinges 2 sets 24.53 49.06

Waterjet brackets 10 brackets 4.00 40.00

Gussets 5 gussets 5.05 25.25

Bosch Tubing 6000 mm .01849 113.80

Total 282.11

Page 33: Full Boeing

FUTURE WORK

● Reliability of suction system

● Print/machine ring as one solid

part for complete accuracy

● Redesign of top mounting

hinges for repeatability

● Heavy duty bearing for carousel

track

● Accuracy of ring rotation

Page 34: Full Boeing

Final Product