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Design and Testing of a Unique Compressor Test Facility Jörgen Olsson

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Presentation on theme: "Design and Testing of a Unique Compressor Test Facility Jörgen Olsson"— Presentation transcript:

1 Design and Testing of a Unique Compressor Test Facility Jörgen Olsson
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2 Outline of the presentation
Introduction Specifications Design Hardware Test Compressors Testing Summary STARCS Proprietary

3 What type of compressors are tested?
Low Pressure Compressor RM 12 (GE F404) STARCS Proprietary

4 Why are compressors tested?
Measure the performance of a new design Map the operational envelope Establish the operational limits to avoid stall, surge and flutter Verification of design models STARCS Proprietary

5 Main design criteria for the Compressor Research Facility
Drive power 4.3 MW Rotation speed ranges: rpm and rpm, continuously variable Variable inlet pressure Variable outlet pressure Air flow through the test facility without a test compressor installed Efficient sound proofing of the control room and to the external environment. Control system with safety monitoring and logging STARCS Proprietary

6 Envelope of the Compressor Test Facility
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7 STAL-LAVAL (Siemens Turbomachinery Finspång Sweden) Compressor Test Facility
In service fall 1973 6 MW STARCS Proprietary

8 First sketch STARCS Proprietary

9 Compressor Test Facility Overview
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10 Side view of the Compressor Test Facility
Asynchronous motor 4.3 MW Inlet valve Test object (rig) Outlet valve (2) Counter weight Control valve for ejector primary flow STARCS Proprietary

11 The Compressor Test Facility seen from the motor
Inlet valve Outlet valve Outlet valve To acoustic baffles and exhaust tower Floor level Ejector Control valve for ejector primary flow STARCS Proprietary

12 Inlet flow manipulators
Perforated plate Net Net Net STARCS Proprietary

13 Cross section at the ejector
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14 Modified ejector Insert STARCS Proprietary

15 16 MPa pipe for the ejector drive air
Compressor building for wind tunnel T1500 Connection to pressure vessel Compressor Research Facility Shut off valve Pipe Pipe support Control valve STARCS Proprietary

16 Gearboxes Sketch of the gear box for 25000 rpm
Cut away sketch of the gearbox for 5500 rpm STARCS Proprietary

17 Drive shafts between gear box and test compressor
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18 Torque meters 0-10 kNm 0-8000 rpm 0-1400 Nm 0-30000 rpm
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19 Situation plan STARCS Proprietary

20 External view of the building
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21 Motor and rpm gear box STARCS Proprietary

22 Gear box and exhaust annular collector
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23 Air inlet with inlet valve and stagnation chamber
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24 Hardware needed to adapt a test compressor
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25 Inlet pipe STARCS Proprietary

26 Diffuser STARCS Proprietary

27 Vital booster and instrumentation rack
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28 Overview of the control and measurement system
Zephyr Recording of fast response data Bandwidth: 30 kHz On-line monitoring IDA Recording of data Bandwidth:10 Hz On-line monitoring. Electronic Pressure Scanners (ESP) Recording of ”slow” pressures. (10 Hz) ABB 800 Control system for motor and valves FFA 1260 Signal conditioning Alarm System Compilation of data and presentation online of data, RMS, FFT etc. Alarm can invoke emergency stop FFA 1220 Strain gauges Temperatures Instationary Pressures Facility fixed transducers Stationary Pressures Data to customer Bearing temperature and vibration Emergency stop Motor control sensors MAESTRO Test sequence control STARCS Proprietary

29 Control Room STARCS Proprietary

30 Control System Display
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31 On-Line Compressor Performance Map
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32 Hulda low pressure compressor
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33 Vital LPC STARCS Proprietary

34 AIDA Aggressive Duct With Hulda Compressor
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35 Test compressor for max 5500 rpm
Front view of Siemens Industrial Turbo-machinery test compressor with first stage guide vanes. (inlet hub not present) STARCS Proprietary

36 What is measured? Inlet and outlet pressures and temperatures
Mass flow, rotational speed and drive shaft torque Vibration and loads on the rotor blades using strain gauges or tip-timing Vibration and loads on the stator vanes and the inlet guide vanes using strain gauges Stall detection using temperature sensors and unsteady pressure transducers Static pressures in the flow channel For monitoring: Rotor tip clearance, shaft position, temperature and vibration of the compressor bearings, lubrication oil pressure, temperature and mass flow Flow properties in the channel using traversing probes: pressure, temperature and flow angles

37 STARCS in-house designed and built Compressor Test Research Facility
Summary STARCS in-house designed and built Compressor Test Research Facility Today a well proven concept Drive power and mass flow capabilities in parity with customer demands Unique capabilities with sub atmospheric outlet STARCS Proprietary


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