ger4606_6-4-2010

Upload: hemanthsatish

Post on 02-Jun-2018

219 views

Category:

Documents


0 download

TRANSCRIPT

  • 8/10/2019 GER4606_6-4-2010

    1/12

    GE Energy

    Wireless Connecting RodTemperature Measurementsfor Reciprocating Compressor

    MonitoringGER-4606 (06/10)

    Author:

    Brian Howard, P.E.

    Sr. Technologist

    Reciprocating Compressor Condition MonitoringGE Energy

  • 8/10/2019 GER4606_6-4-2010

    2/12

  • 8/10/2019 GER4606_6-4-2010

    3/12

    IntroductionUndetected bearing failures result in long outages and extensive

    repairs for reciprocating machinery. In slow speed reciprocating

    compressors and engines, main bearing temperature monitoring

    has proven to be valuable in assessing bearing condition1,2.

    Monitoring of the moving bearings at either end of the connecting

    rod has proven to be more difficult. As the crankpin bearing often

    shares design features with the main bearing, temperature

    measurements on this bearing would have the same benefits as

    it does on the main bearings. On the other end of the connecting

    rod, industry experience in operating reciprocating compressors

    has shown how important loads and reversal can be in determining

    the crosshead pin bushing condition3,4,5. The ability to correlate

    these loads with temperature results in improved ability todetermine crosshead pin bushing condition.

    Wireless Connecting Rod Temperature Measurementsfor Reciprocating Compressor Monitoring

    Eutectic devices have provided one method for indicating bearing

    temperature. In recent years a radar-based wireless temperature

    system has come to the market that enables end-users to make

    connecting rod bearing temperature measurements on-line. This

    application note provides background on the radar measurement,

    legacy discrete measurement technology, detail on the installation

    arrangements and describes how to interface it with GEs Bently

    Nevada* 3500 Series Monitoring Systems and System 1* Condition

    Monitoring Software (referred to as 3500/S1 hereafter).

    GE Energy | GER-4606 (06/10) 1

    Crankpin Bearing

    Connecting Rod

    Crosshead Pin Bushing

    Figure 1. Reciprocating Compressor Assembly.

  • 8/10/2019 GER4606_6-4-2010

    4/12

    Eutectic-Style Connecting RodBearing Temperature Installation

    ArrangementsThe relative motion between the connecting rod and compressor

    frame presents a special challenge to those trying to make a

    temperature measurement on the main connecting rod bearing

    and crosshead pin bushing. One technique that has been used for

    decades involves installing a device assembled with a eutectic

    alloy weld that melts at a pre-determined temperature6.

    When the local temperature reaches the melting point of the

    fusible alloy used to weld the actuator rod to the spring retainer

    end, the inner spring forces the actuator rod out through the

    detector body (See Figure 2 and Figure 3 for installation details).

    GE Energy | GER-4606 (06/10) 2

    Fusible Alloy Weld

    Spring Retainer End

    Detector Body

    Pressure Switch

    Actuator RodActuator Rod Sleeve

    Inner Compression Spring

    Outer Compression Spring

    Figure 2. Eutectic-Type Wireless Switch Arrangement. Re-drawn from (6).

    Detector Body

    Actuator Rod

    Actuator Rod

    Figure 3. Crankpin Eutectic Switch Installation.

  • 8/10/2019 GER4606_6-4-2010

    5/12

    The extension of the actuator rod allows contact with a pressure

    switch. The contact with the pressure switch opens the line to

    atmosphere, releasing air pressure in the sensing line. The drop in

    pressure causes a pressure switch connected to this line to change

    state. This switch, in turn, provides an alarm for the operators.

    Integration to Reciprocating Compressor

    Condition Monitoring System

    The 3500/62 Process Variable monitor, combined with an

    external power supply, can be used to detect a change in state

    of the pressure switch as shown in Figure 4. Although this method

    involves more cost than using the discrete input of a PLC or DCS,

    it has the advantage of driving data collection directly on the

    3500 rack when an alarm condition is reached. This high-resolution

    alarm event dataset includes the static and dynamic data from the

    compressor and is very useful when trying to understand what led

    to a change in machine condition. In particular, when the condition

    monitoring system includes crosshead pin bushing temperature

    and cylinder pressure data, the effects of overload and/or lack

    of reversal can be effectively assessed.

    GE Energy | GER-4606 (06/10) 3

    Figure 4. 3500/62 Process Variable Monitor Field Wiring (Internal Terminations Shown, External Terminations Similar).

  • 8/10/2019 GER4606_6-4-2010

    6/12

    Wireless Connecting Rod BearingTemperature Installation

    ArrangementsRadar-based wireless temperature sensors have gained

    acceptance in application to low speed reciprocating compressors.

    These systems enable trending of moving bearing temperature,

    rather than the discrete values provided by the eutectic systems.

    The concept for radar-based sensors grew out of technology

    used for tagging automobiles as they pass through automated

    toll collecting systems7. Initial testing of these toll identification

    systems revealed an appreciable sensitivity to temperature. While

    this made reading the tags difficult, it turned out that the system

    could be used to estimate temperature.

    Unlike traditional wireless radio frequency systems, which require

    power to transmit a signal, radar-based systems induce a signal in

    the moving component. This has the advantage of not requiring

    power for the moving component.

    The measurement process begins when the stationary antenna

    outputs an interrogation pulse. When this pulse reaches the

    antenna wires, the electromagnetic energy excites elastic surface

    waves that radiate out from the transducer on the sensing element

    substrate. The acoustic waves travel from the transducer to each

    of the reflectors mounted on the substrate. When the waves

    reach a reflector, an electromagnetic pulse is generated that is

    then picked up by the stationary antenna.

    The speed of the surface acoustic wave propagation through

    the substrate is much lower than the speed of light. The resultingdelay between the interrogation pulse and pulse response from

    the moving sensors allows the signal processing equipment to

    separate out the valid sensor responses from electromagnetic

    echoes within the compressor frame7. The signal processing

    equipment then evaluates the shape and spacing interval of

    the pulse response from the sensing element to determine the

    temperature of the probe tip.

    Figure 6 shows the typical packaging layout and radar signal path.

    The assembly on the left mounts in either the crank pin bearing

    or crosshead pin/crosshead pin bushing. The stationary antennamounts to the compressor frame. The air gap between the moving

    and stationary elements can be as large as 50 mm (1.97 in) 7.

    Figure 7 shows the mechanical installation of the wireless

    temperature sensor.

    GE Energy | GER-4606 (06/10) 4

    Wireless Temperature Sensor Stationary Antenna

    Pulse Response From Sensor

    Interrogation Pulse From Antenna

    Figure 6. Radar-Based System Arrangement. Redrawn from (7).

    Antenna Wires

    Transducer

    Reflector 1

    Reflector n

    Absorber

    Piezoelectric Substrate

    Figure 5. Radar Sensing Element. Re-drawn from (7).

  • 8/10/2019 GER4606_6-4-2010

    7/12

    Integration to Reciprocating Compressor

    Condition Monitoring System

    The radar-based systems provide a continuous signal, available

    for trending and analysis. Kongsbergs Sentry system has gained

    acceptance in reciprocating compressor application in the

    downstream/petrochemical segments and will be used as an

    example of integration to 3500/S1.

    The Sentry system has the ability to output a 4-20mA signal

    that can be accepted by the 3500/62 process variable monitor.

    Figure 8 shows a field-wiring diagram for the Sentry system

    connected to a 3500/62 monitor. Figure 9 shows a sample of

    one of the channel configuration options. Table 1 outlines initial

    alarm and filter settings for the monitor.

    GE Energy | GER-4606 (06/10) 5

    Figure 7. Wireless Temperature Sensors Installation on Connecting Rod.

    Figure 8. 3500/62 Process Variable Monitor Field Wiring (External Terminations Shown, Internal Terminations Similar).

  • 8/10/2019 GER4606_6-4-2010

    8/12

    Within System 1 software, the points should be mapped to therespective throws as shown in Figure 10. No associations are

    required for these points.

    Software alarms can be set, if desired. In the case that the Cylinder

    Trim RulePak has been installed, the result of the crosshead pin

    condition rule can be combined with the temperature measurement

    to drive an alert specific to crosshead pin wear as shown in

    Figure 11.

    System 1 Display client plot sessions should include a plot

    group with a trend of degrees of reversal, combined rod load

    tension/compression, crankpin bearing temperature and

    crosshead bushing temperature. Figure 12 shows a sample

    of this plot arrangement.

    GE Energy | GER-4606 (06/10) 6

    Crankshaft

    Stg 1 X-Head Temp B

    Stg 1 X-Head Temp A

    Throw 1 Diagnostics - Hydrogen

    Stg 1 Xhead Accel

    Cylinder 1 (Stage 1)

    Throw 1 (Stage 1)

    Figure 10. Radar-Based Temperature Mapping.

    Figure 11. Sample Rule Combining Pin Load and Radar-Based WirelessTemperature.

    Figure 9. 3500/62 Process Variable Configuration Screen.

    Table 1. Initial Monitor Alarm and Filter Settings.

    Filtering Not Applicable

    Alarm / Danger - In the absence of

    OEM recommendations or engineering

    data, these are the recommended*initial alarm and danger set points.

    Alarm: 200F (82C)

    Danger: 220F (93C)

    *These should be adjusted based on actual operating conditions

  • 8/10/2019 GER4606_6-4-2010

    9/12

    ConclusionThe wireless measurement systems provide critical information

    about the health of the connecting rod bearings. Combining this

    measurement with other condition monitoring parameters

    provides helpful insight into machine condition.

    GE Energy | GER-4606 (06/10) 7

    Stage 1 Rod ReversalRecip. Comp. From 17MAY2008 17:40:00 To 29MAY2008 17:40:00 Historical

    17:4017MAY2008

    17:4021MAY2008

    17:4025MAY2008

    17:40

    TIME : 12 Hours /div

    AMPLITUDE:

    0

    50

    100

    150

    26MA Y2 00 8 18 :3 6:3 4 17 9 deg 3 00 rpm Stage 1 Pk. Rod Load (C)Recip. Comp. From 17MAY2008 17:40:00 To 29MAY2008 17:40:00 HistoricalStage 1 Pk. Rod Load (T)Recip. Comp. From 17MAY2008 17:40:00 To 29MAY2008 17:40:00 Historical

    17:4017MAY2008

    17:4021MAY2008

    17:4025MAY2008

    17:40

    TIME : 12 Hours /div

    AMPLITUDE:

    0

    50

    100

    150

    26MAY2008 18:19:54 110966 lbf 300 rpm

    26MAY2008 18:29:29 117973 lbf 300 rpm

    Stage 1 Crank Pin Temp

    Recip. Comp. From 17MAY2008 17:40:00 To 29MAY2008 17:40:00 Historical

    17:4017MAY2008

    17:4021MAY2008

    17:4025MAY2008

    17:40

    TIME : 12 Hours /div

    AMPLITUDE:

    50

    100

    150

    200

    26MAY2008 18:36:32 147 deg F NA Stg 1 X-Head Pin Temp ARecip. Comp. From 17MAY2008 17:40:00 To 29MAY2008 17:40:00 HistoricalStg 1 X-Head Pin Temp BRecip. Comp. From 17MAY2008 17:40:00 To 29MAY2008 17:40:00 Historical

    17:4017MAY2008

    17:4021MAY2008

    17:4025MAY2008

    17:40

    TIME : 12 Hours /div

    AMPLITUDE:

    50

    100

    150

    200

    26MAY2008 22:00:08 148 deg F NA

    26MAY2008 21:26:17 146 deg F NA

    29MAY2008

    10

    38

    66

    93

    10degF/div

    AMPLITUDE:

    5.6

    degF/div

    10deg/div

    29MAY2008 29MAY2008

    29MAY2008

    10

    38

    66

    93

    AMPLITUDE:

    5.6

    degF/div

    10degF/div

    0

    220

    440

    660

    10klbf/div

    AMPLITUDE:

    44kN/div

    Figure 12. Radar-Based Temperature Plot Group Layout.

  • 8/10/2019 GER4606_6-4-2010

    10/12

    Bibliography[1] Leon-Gomez, Steve and Smalley, Anthony. Main Bearing

    Temperature Monitoring. Report No. TR 97-7. Gas Machinery

    Research Council, 1997

    [2] General Electric. Protecting and Managing API-618

    Reciprocating Compressors. Document Number 178896,

    Revision NC.

    [3] Davis, Greg. Using PV Curves to Diagnose A Recip Valve

    Problem. Orbit, pp48-54, First Quarter, 2004.

    [4] Diab, Sary and Howard, Brian. Reciprocating Compressor

    Management Systems Provide Solid Return on Investment.

    Proceedings of the ROTATE 2004 Conference.

    [5] Howard, Brian and John Kitchens. On-line Acceleration and

    Cylinder Pressure (PV) Measurements for Reciprocating

    Compressor Diagnostics. Proceedings of the Gas Machinery

    Conference, 2007.

    [6] Munroe, William O. Temperature Detecting Actuator For

    Bearings. Amot Controls Corporation, assignee. Patent

    3,401,666. 1968.

    [7] Gemdjian, Ed and Cornelius, Larry. Safety And Prevention Of

    Costly Undetected, Developing Failures In Crank And Crosshead

    Bearings Of Gas And Process Compressors. Proceedings of theGas Machinery Conference, 2007.

    GE Energy | GER-4606 (06/10) 8

  • 8/10/2019 GER4606_6-4-2010

    11/12

  • 8/10/2019 GER4606_6-4-2010

    12/12

    GE Energy

    Optimization and Control

    1631 Bently Parkway South

    Minden, NV 89423

    +1 775.782.3611

    www.ge-energy.com/oc

    *Bently Nevada and System 1 are trademarks of the General Electric Company.

    2010, General Electric Company.

    All rights reserved. GER-4606 (06/10)