IP Library Granted Patent US 7,061,607
Granted Patent B2
US 7,061,607 · App. 10/428,693 · Granted Jun 13, 2006

Engine spectrometer probe and method of use

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Quick Facts
Patent No.
US 7,061,607
App. No.
10/428,693
Granted
Jun 13, 2006
Kind
B2
Abstract

The engine spectrometer probe and method of using the same of the present invention provides a simple engine spectrometer probe which is both lightweight and rugged, allowing an exhaust plume monitoring system to be attached to a vehicle, such as the space shuttle. The engine spectrometer probe can be mounted to limit exposure to the heat and debris of the exhaust plume. The spectrometer probe 50 comprises a housing 52 having an aperture 55 and a fiber optic cable 60 having a fiber optic tip 65 . The fiber optic tip 65 has an acceptance angle 87 and is coupled to the aperture 55 so that the acceptance angle 87 intersects the exhaust plume 30 . The spectrometer probe can generate a spectrum signal from light in the acceptance angle 506 and the spectrum signal can be provided to a spectrometer 508.

Claims (74)

1. A spectrometer probe for detecting possible damage occurring to an engine generating an exhaust plume, the spectrometer probe comprising:

a housing, the housing having an aperture; and

an optical transmitting component, the optical transmitting component having a tip, the tip having an acceptance angle;

wherein the tip is disposed adjacent the aperture so that the acceptance angle intersects the exhaust plume and collects a signal for spectral analysis to detect the presence of a material in the exhaust plume relating to a component of the engine, to thus indicate possible damage occurring to the engine.

2. The spectrometer probe of claim 1 , wherein the aperture is conical.

3. The spectrometer probe of claim 2 , wherein the aperture has a vertex angle and the acceptance angle is about equal to the vertex angle of the aperture.

4. The spectrometer probe of claim 1 , wherein the acceptance angle is between 10 and 90 degrees.

5. The spectrometer probe of claim 1 , wherein the acceptance angle is about 25 degrees.

6. The spectrometer probe of claim 1 , wherein the shape of the aperture is selected from the group consisting of conical, cylindrical, parabolic, and spherical.

7. The spectrometer probe of claim 1 , wherein the housing has a wall about the aperture, and light striking the wall is scattered outside the acceptance angle of the tip of the optical transmitting component.

8. The spectrometer probe of claim 1 , wherein the housing has a wall about the aperture, and debris striking the wall is scattered away from the tip of the optical transmitting component.

9. The spectrometer probe of claim 1 , wherein the optical transmitting component comprises a fiber optic cable made of a material selected from the group consisting of fused silica, glass, and plastic.

10. The spectrometer probe of claim 1 , wherein additional components are disposed in the aperture, the additional components being selected from the group consisting of screens, gratings, optical gratings, lenses, prisms, mirrors, partial mirrors, transparent plates, diffusers, and combinations thereof.

11. The spectrometer probe of claim 1 , wherein the housing is compact.

12. The spectrometer probe of claim 1 , wherein the engine has a nozzle and the housing is integral to the nozzle.

13. An exhaust plume monitoring system for detecting possible damage occurring to an engine generating an exhaust plume, the system comprising:

a fiber optic cable, the a fiber optic cable having an acceptance angle;

a housing, the housing supporting a portion of the fiber optic cable and directing the acceptance angle toward the exhaust plume; and

a spectrometer, the spectrometer operably coupled to the fiber optic cable to receive a signal for spectral analysis to detect the presence of a material in the exhaust plume relating to a component of the engine, to thus indicate possible damage occurring to the engine.

14. The exhaust plume monitoring system of claim 13 , further comprising a data processor, the data processor being operably coupled to the spectrometer.

15. The exhaust plume monitoring system of claim 14 , further comprising an engine control device, the engine control device being operably coupled to the data processor.

16. The exhaust plume monitoring system of claim 13 , wherein the housing includes an aperture, the acceptance angle being disposed within the aperture.

17. The exhaust plume monitoring system of claim 13 , further comprising:

a second fiber optic cable, the second fiber optic cable having second acceptance angle; and

a second housing, the second housing directing the second acceptance angle toward the exhaust plume;

wherein the spectrometer is operably coupled to the second fiber optic cable to receive a second signal for spectral analysis to detect the presence of a material in the exhaust plume relating to a component of the engine, to thus indicate possible damage occurring to the engine.

18. A method of monitoring an exhaust plume of an engine to detect possible damage occurring to the engine comprising:

directing an optical transmitting element having an acceptance angle toward the exhaust plume;

generating a spectrum signal from light in the acceptance angle; and

providing the spectrum signal through the optical transmitting element to a spectrometer to detect the presence of a material in the exhaust plume relating to a component of the engine, to thus indicate possible damage occurring to the engine.

19. The method of claim 18 , further comprising generating a spectrometer signal in response to the spectrum signal and providing the spectrometer signal to a data processor.

20. The method of claim 19 , further comprising storing the spectrometer signal.

21. The method of claim 19 , further comprising analyzing the spectrometer signal.

22. The method of claim 21 , wherein analyzing the spectrometer signal comprises comparing the spectrometer signal to baseline data.

23. The method of claim 22 , wherein the baseline data is for a current engine run.

24. The method of claim 22 , wherein the baseline data is from a data library.

25. The method of claim 24 , wherein the data library is selected from the group consisting of off-normal data from injection testing and sacrificial element data.

26. The method of claim 21 , wherein analyzing the spectrometer signal comprises analyzing the spectrometer signal to determine the fuel mixture.

27. The method of claim 19 , further comprising:

generating an engine health signal in response to the spectrometer signal;

providing the engine health signal to an engine control device, the engine control device generating an engine control signal in response to the engine health signal; and

providing the engine control signal to the engine.

28. The method of claim 27 , wherein the engine is responsive to the engine control signal to take action selected from the group consisting of adjusting fuel mixture, reducing engine power, isolating engine components, and shutting down the engine.

29. The method of claim 27 , wherein the engine is responsive to the engine control signal to take action in real time.

30. The method of claim 27 , wherein the engine is responsive to a plurality of engine status signals.

31. The method of claim 27 , further comprising:

including measured hydroxyl radical emission data in the engine health signal;

adjusting the engine control signal in response to the measured hydroxyl radical emission data; and

adjusting fuel mixture in response to the engine control signal.

32. The method of claim 27 , further comprising:

including measured metal emission data in the engine health signal;

adjusting the engine control signal in response to the measured metal emission data; and

taking action in response to the engine control signal, the action selected from the group consisting of reducing engine power and shutting down the engine.

33. The method of claim 27 , further comprising:

including measured emission data in the engine health signal; adjusting the engine control signal in response to the measured emission data; and

operating the engine in response to the engine control signal to maintain the measured emission data within predetermined emission limits.

34. The method of claim 33 , wherein the measured emission data is for chemicals selected from the group consisting of oxides of nitrogen, oxides of carbon, hydrocarbons, and carbon monoxide.

35. The method of claim 19 , further comprising:

using a second optical transmitting element having a second acceptance angle and directing the second acceptance angle toward the exhaust plume;

generating a second spectrum signal from light in the second acceptance angle;

generating a second spectrometer signal in response to the second spectrum signal; and

providing the second spectrometer signal to the data processor to detect the presence of a material in the exhaust plume relating to a component of the engine, to thus indicate possible damage occurring to the engine.

36. The method of claim 35 , further comprising analyzing the spectrometer signal and the second spectrometer signal to generate three dimensional plume data.

37. The method of claim 35 , further comprising analyzing the spectrometer signal and the second spectrometer signal by a method selected from the group consisting of triangulation and tomography.

38. A system for monitoring an exhaust plume of an engine comprising:

means for transmitting an optical signal for spectral analysis to detect the presence of at least one predetermined element in the exhaust plume, the optical signal transmitting means having an acceptance angle; and

means for directing the acceptance angle toward the exhaust plume.

39. The system of claim 38 , wherein light in the acceptance angle generates a spectrum signal and further comprising means for providing the spectrum signal to a means for measuring the spectrum signal.

40. The system of claim 39 , wherein the spectrum signal measuring means generates a spectrometer signal and further comprising means for processing the spectrometer signal.

41. The system of claim 40 , wherein the spectrometer signal processing means generates an engine health signal and further comprising means for controlling the engine responsive to the engine health signal.

42. A spectrometer probe fore detecting possible damage occurring to an engine generating an exhaust plume, the spectrometer probe comprising:

a housing, the housing having an aperture; and

an optical transmission medium have a tip portion, the tip portion imaging a selected area within the housing through the aperture, the exhaust plume flowing through the selected area; and

wherein the optical transmission medium collects a signal for spectral analysis to detect the presence of a material in the exhaust plume relating to a component of the engine, to thus indicate possible damage occurring to the engine.

Assignments (4)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT (AS SUCCESSOR AGENT TO WELLS FARGO BANK, NATIONAL ASSOCIATION (AS SUCCESSOR-IN-INTEREST TO WACHOVIA BANK, N.A.), AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 064424/0050 →
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
NOTICE OF SUCCESSION OF AGENCY (INTELLECTUAL PROPERTY) Recorded Jun 20, 2016
From: WELLS FARGO BANK, NATIONAL ASSOCIATION, AS THE RESIGNING AGENT
To: BANK OF AMERICA, N.A., AS THE SUCCESSOR AGENT
Reel/Frame 039079/0857 →
CHANGE OF NAME Recorded May 14, 2016
From: PRATT & WHITNEY ROCKETDYNE, INC.
To: AEROJET ROCKETDYNE OF DE, INC.
Reel/Frame 038707/0175 →