p14453
DESCRIPTION
P14453. Dresser-Rand Compressor Bearing Dynamic Similarity Tester. Agenda. Team Introduction Background – Steve Lucchesi Problem Statement – Steve Kaiser Deliverables – Josh Plumeau Stakeholders – Luke Trapani Engineering Requirements – Shawn Avery Benchmarking – Shawn Avery - PowerPoint PPT PresentationTRANSCRIPT
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P14453
Dresser-Rand Compressor Bearing Dynamic Similarity
Tester
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AgendaTeam IntroductionBackground – Steve LucchesiProblem Statement – Steve KaiserDeliverables – Josh PlumeauStakeholders – Luke TrapaniEngineering Requirements – Shawn AveryBenchmarking – Shawn AveryMilestones Timeline – Luke TrapaniIssues – Josh Plumeau
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Introduction/RolesTeam Member Major Role
Steve Lucchesi Mechanical Engineering Project Manager
Shawn Avery Mechanical Engineering Team Facilitator
Steve Kaiser Mechanical Engineering Project Engineer
Josh Plumeau Mechanical Engineering Project Engineer
Luke Trapani Mechanical Engineering Project Engineer
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Project BackgroundObjective:
Develop a bearing dynamic similarity test rig to more carefully investigate the dynamics of the Dresser-Rand floating ring main compressor bearings.
Design the rig such that it can incorporate all journal bearings for the purpose of fault detection research at RIT.
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What is a Journal Bearing? Journal, or plain bearings, consist of a
shaft or journal which rotates freely in a supporting sleeve with lubricant film to provide a low friction surface
A floating ring journal bearing is similar, but consists of an additional component (the ring) that floats in the lubricant between the journal and the sleeve, creating two lubricant layers
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Past ProjectsP09452: Installed Dresser-Rand ESH-1 reciprocating
compressorP12453: Installed a range of sensors on the compressor and
expanded the capabilities of the data acquisition (DAQ) systemP13453: Dresser-Rand Compressor Wireless Instrumentation.
Monitored health of main crank bearing on the reciprocation compressor
P13505: Designed roller bearing failure test stand.Markus Holzenkamp’s Thesis
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Problem StatementCurrent State
Bearing monitoring is currently performed on the compressor itself No current test rig exists on site at RIT
Desired State Two system level design proposals; one full scale model and one scaled down version Working concept to remain on site at RIT to allow for further research and development
Project Goals Allows for quick change-over Control and measure the following:
Shaft speed Dynamic/Variable Load Profiles Oil Temperature and Pressure Gap measurement between journal and sleeve
Constraints Budget of $5,000 Understanding of floating journal ring bearings
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Project DeliverablesTwo system design proposals by SLDR
A full scale design replicating the ESH-1 compressorA small scale rig that will give useful data while saving space and
controlling project costs
Detailed design of selected proposal by DDRA functional test rig capable of dynamically loading a
journal bearing in two axesTest rig must be small enough to install at RITThe oiling system must replicate that of the Dresser-Rand ESH-1
compressor
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Project DeliverablesData collection system
Measurement of gap between journal and sleeveMeasurement of vibration experienced by bearingMonitoring of oil temperature, pressure, and flow rate during testsCondition monitoring must interface with existing DAQ
Test data proving functionality of equipmentAdditional desired features
Quick bearing replacementLow cost to operate and maintain
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StakeholdersRIT:
Researchers: RIT:
Industry Engineers: Dresser-Rand:
Industries pertaining to the use and/or manufacturing of journal bearings.
• Dr. Jason Kolodziej Assistant Professor (Primary Customer)• Dr. Stephen Boedo
Associate Professor (Subject Matter Expert)
?• James Sorokes Principal Engineer Financial Support• Scott Delmotte
Mgr. Project Engineering Point of Contact
• MSD1 Team – 14453• Graduate/Masters Students• William Nowak (Xerox)
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Engineering Requirements
Function Engr. Requirement (metric) Unit of Measure Marginal Value Ideal Value
Read/Select Load Profile Yes/No, Time Min. 2 1
Control Shaft Speed Measurement Range, Accuracy rpm 0 to 400, ±30 0 to 2000, ±20
Control Load Measurement Range, Accuracy Lbf TBD 0 to 900, ±10
Control Oil Pressure Measurement Range, Accuracy Psi TBD TBD
Measure Shaft Speed Measurement Range, Accuracy rpm 0 to 400, ±30 0 to 2000, ±20
Measure Load Measurement Range, Accuracy Lbf TBD 0 to 900, ±10
Measure Oil Pressure at Bearing Inlet/Outlet Measurement Range, Accuracy Psi TBD TBD
Measure Oil Temp. Measurement Range, Accuracy ᵒF TBD TBD
Measure Bearing Vibration (Frequency & Amplitude) Measurement Range, Accuracy Hz, in. TBD TBD
Meaure Journal to Sleeve Clearance Measurement Range, Accuracy in. TBD TBD
Measures Oil Flow Rate In/Out Measurement Range, Accuracy in3/s TBD TBD
Measure Torque Transmitted in the Fluid Film Measurement Range, Accuracy lbf-in TBD TBD
Display Shaft Speed Refresh Rate Hz. 0.5 1
Display Load Refresh Rate Hz. 0.5 1
Display Oil Pressure Refresh Rate Hz. 0.5 1
Display Oil Temperature Refresh Rate Hz. 0.5 1
Display Bearing Vibration Refresh Rate Hz. 0.5 1
Display Journal to Sleeve Clearance Refresh Rate Hz. 0.5 1
Provide Component Power Voltage Range V N/A 110 to 240
Record/Save Data Delay Time Sec. 5 2
*link to House of Quality upon request: https://edge.rit.edu/edge/P14453/public/Problem%20Definition
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BenchmarkingQualitative benchmarking of other bearing test
rigs Speed Range Load Capabilities Load application method Bearing type
Sub-system Benchmarking Pump Load application equipment Motor Sensors User Interface
NASA
Ghent U. LBTR
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MSD I Milestones Timeline
Week 1 Week 2 Week 3 Week 4 Week 1 Week 2 Week 3 Week 4 Week 5 Week 1 Week 2 Week 3 Week 4September October November
Problem Definition
System Design
Sub-System Design
Detailed Design & Component Selection
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MSD I Milestones Timeline Problem Definition [09/10/13]:
Define problem Define customer requirements Define engineering requirements Plan project
System Design Kick-Off [09/17/13]: Problem definition completed Begin concept development Decomposition analysis Risk assessment Benchmarking concepts
System Design Review [10/01/13]: System design completed Meet with guides/panels/stakeholders Select feasible system
Sub-System Design [10/08/13]: Subsystem design and interactions Requirement flow-down Next level of decomposition analysis Feasibility analysis
Subsystem Design Review [10/24/13]: Subsystem design completed Meet with guides/panels/stakeholders
Detailed Design & Component Selection [10/31/13]:
Fully completed drawings Component list Any FEA/Simulations Risk assessment Benchmarking plans
Preliminary DDR [11/19/13]: Meet with guides/panels/stakeholders Ensure that all design components are complete
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IssuesComponent understanding of journal bearings
Limited experience with bearing analysisControl systems
The team has limited electrical and controls experienceComplex load control system requiredIncorporating current data acquisition system
Availability of required equipmentDrive and loading system will require higher-end equipment
that may not be readily available
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