Powered total pressure measurement rake with telemetry

Patent metadata

Field	Value
Publication number	US-10684183-B2
Application number	US-201815961730-A
Country	US
Kind code	B2
Filing date	Apr 24, 2018
Priority date	Apr 24, 2018
Publication date	Jun 16, 2020
Grant date	Jun 16, 2020

Abstract

A system for total pressure measurement of a propulsive stream through a turbine engine, the system incorporates a track circumferentially mounted on a fan exhaust nozzle proximate a trailing edge. A carriage is mounted in the track and adapted for translation through a range of azimuthal angles relative to an engine centerline. A pressure measurement rake extends from the carriage and has a probe mount protruding radially inward into a fan flow duct with a plurality of pressure probes mounted to a leading edge of the probe mount.

First claim

What is claimed is:

1. A system for total pressure measurement of a propulsive stream, the system comprising:
a track circumferentially mounted on an exhaust nozzle proximate a trailing edge of the exhaust nozzle;
a carriage mounted in the track and adapted for angular translation relative to an engine centerline; and,
a pressure measurement rake extending from the carriage and having
a probe mount protruding inward into a flow duct, and
a plurality of pressure probes mounted to a leading edge of the probe mount.

2. The system for total pressure measurement of a propulsive stream as defined in claim 1 further comprising:
a telemetry unit connected to the plurality of pressure probes; and,
a data processor receiving pressure data from the telemetry unit.

3. The system for total pressure measurement of a propulsive stream as defined in claim 2 wherein the carriage comprises:
a base plate;
roller sets supported by axles extending from the base plate and engaging the track; and,
a motor adapted to translate the carriage in the track.

4. The system for total pressure measurement of a propulsive stream as defined in claim 3 wherein the roller sets comprise:
two lower roller sets attached with axles to the base plate, said lower roller sets rolling on an inner radial surface of a race in the track; and,
two upper roller sets attached with axles to the base plate and engaging an outer radial surface of the race.

5. The system for total pressure measurement of a propulsive stream as defined in claim 4 wherein the motor is engaged to one of the lower roller sets or one of the upper roller sets.

6. The system for total pressure measurement of a propulsive stream as defined in claim 3 wherein the motor is a stepper motor and further comprising a motor controller adapted to provide position signals to the stepper motor.

7. The system for total pressure measurement of a propulsive stream as defined in claim 5 wherein one of the roller sets comprises a pinion operably engaging a rack in the race.

8. The system for total pressure measurement of a propulsive stream as defined in claim 6 wherein the telemetry unit further comprises a battery interconnected to provide power to the plurality of pressure probes and the motor.

9. The system for total pressure measurement of a propulsive stream as defined in claim 3 further comprising a mounting arm extending aft from the carriage, said probe mount depending from the mounting arm to protrude into the flow duct.

10. The system for total pressure measurement of a propulsive stream as defined in claim 9 wherein the mounting arm has a length to position the probe mount longitudinally aft of the trailing edge of the exhaust nozzle.

11. The system for total pressure measurement of a propulsive stream as defined in claim 1 wherein the probe mount has an airfoil cross section to minimize aerodynamic distortion and drag.

12. The system for total pressure measurement of a propulsive stream as defined in claim 9 wherein the plurality of pressure probes are positioned by the probe mount between the trailing edge of the exhaust nozzle and a core cowl.

13. The system for total pressure measurement of a propulsive stream as defined in claim 12 wherein spacing of the plurality of pressure probes is 1 inch or less.

14. The system for total pressure measurement of a propulsive stream as defined in claim 12 wherein multiple probes of the plurality of pressure probes are spaced at 0.10 inch or less in an outer boundary layer proximate an inner wall of the exhaust nozzle and an inner boundary layer proximate an outer wall of the core cowl.

15. The system for total pressure measurement of a propulsive stream as defined in claim 3 wherein the telemetry unit incorporates a wireless transmitter and receiver for transmission of pressure data from the plurality of pressure probes to the data processor.

16. The system for total pressure measurement of a propulsive as defined in claim 15 wherein the wireless transmitter and receiver is connected to provide a control input through a motor controller providing position signals to the motor from a control system.

17. The system for total pressure measurement of a propulsive stream as defined in claim 16 wherein the control system integrates processing requirements for the motor controller and data processor.

18. The system for total pressure measurement of a propulsive stream as defined in claim 2 further comprising transmission cables interconnecting the telemetry unit and data processor.

19. A method for total pressure measurement of a propulsive stream, the method comprising:
activating a motor through a motor controller as commanded by a control system;
positioning a carriage of a pressure measurement rake at a desired location in a track;
transmitting pressure data from radially spaced locations of a plurality of pressure probes mounted to the carriage through a telemetry unit to a data processor; and
activating the motor to reposition the carriage at a next selected location.

20. The method as defined in claim 19 further comprising transmitting additional pressure data from the plurality of pressure probes and reactivating the motor to reposition the carriage through a range of selected locations.

Assignees

• The Boeing Campany
• Boeing Co

Inventors

• Burgan Christopher R

Classifications

• G01L5/133 Primary

  for measuring thrust of propulsive devices, e.g. of propellers (aeroplanes B64C; marine propulsion B63H; jet-engines F02K) · CPC title

• G01M15/14

  Testing gas-turbine engines or jet-propulsion engines · CPC title

• F01D17/08 Primary

  responsive to condition of working-fluid, e.g. pressure · CPC title

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F05D2260/83

  Testing, e.g. methods, components or tools therefor · CPC title