IP Library › Granted Patent US 6,912,480
Granted Patent B2
US 6,912,480 · App. 10/765,973 · Granted Jun 28, 2005

Method and apparatus for determining the mass flow through an engine

Assignee: Rolls-Royce, PLC
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Quick Facts
Patent No.
US 6,912,480
App. No.
10/765,973
Granted
Jun 28, 2005
Kind
B2
Abstract

A method for determining the total mass flow through an engine ( 10 ) comprises measuring ( 32 ) the fuel flow to the engine ( 10 ) and measuring the concentration of carbon dioxide in the gases exhausted ( 22 ) from the engine ( 10 ). The concentration of carbon dioxide is measured by detecting the infrared radiation absorption spectrum of carbon dioxide using a laser ( 38 ) and a detector ( 46 ). The method comprises determining ( 48 ) the air to fuel ratio in the engine ( 10 ) from the fuel flow and the concentration of carbon dioxide. The method comprises determining ( 48 ) the air mass flow through the engine ( 10 ) from the air to fuel ratio and calculating ( 48 ) the total air and fuel mass flow through the engine ( 10 ) by adding the air mass flow through the engine ( 10 ) to the fuel mass flow to the engine ( 10 ).

Claims (38)

1. A method for determining the total mass flow through an engine, comprising:

measuring the fuel mass flow to the engine,

measuring the concentration of carbon dioxide, measuring the ratio of water to oxygen, measuring the ratio of carbon dioxide to oxygen or measuring the ratio of water to carbon dioxide in the gases exhausted from the engine,

determining the air to fuel ratio in the engine from the fuel mass flow and the concentration of carbon dioxide, the ratio of water to oxygen, the ratio of carbon dioxide to oxygen or the ratio of water to carbon dioxide,

determining the air mass flow through the engine from the air to fuel ratio, and

calculating the total air and fuel mass flow through the engine by adding the air mass flow through the engine to the fuel mass flow to the engine.

2. A method as claimed in claim 1 wherein measuring the concentration of carbon dioxide comprises detecting infra-red radiation emitted by carbon dioxide in the gases exhausted from the engine and determining the concentration of carbon dioxide.

3. A method as claimed in claim 1 wherein measuring the concentration of carbon dioxide comprises detecting infra-red radiation absorbed by carbon dioxide in the gases exhausted from the engine and determining the concentration of carbon dioxide.

4. A method as claimed in claim 1 wherein measuring the ratio of water to oxygen comprises detecting infra-red radiation absorbed by water in the gases exhausted from the engine, detecting near infra-red radiation absorbed by oxygen in the gases exhausted from the engine, determining the concentration of water, determining the concentration of oxygen and calculating the ratio of water to oxygen.

5. A method as claimed in claim 1 wherein measuring the ratio of carbon dioxide to oxygen comprises detecting infra-red radiation absorbed by carbon dioxide in the gases exhausted from the engine, detecting near infra-red radiation absorbed by oxygen in the gases exhausted from the engine, determining the concentration of carbon dioxide, determining the concentration of oxygen and calculating the ratio of carbon dioxide to oxygen.

6. A method as claimed in claim 1 wherein measuring the ratio of water to carbon dioxide comprises detecting infra-red radiation absorbed by water in the gases exhausted from the engine, detecting infra-red radiation absorbed by carbon dioxide in the gases exhausted from the engine, determining the concentration of water, determining the concentration of carbon dioxide and calculating the ratio of water to carbon dioxide.

7. A method as claimed in claim 1 comprises irradiating the gases exhausted from the engine with a light.

8. A method as claimed in claim 7 comprising irradiating the gases exhausted from the engine with a laser light.

9. A method as claimed in claim 1 comprising detecting infrared radiation absorbed or emitted by the gases exhausted from the engine at a plurality of lines across the exhaust of the engine.

10. A method as claimed in claim 9 comprising moving a detector.

11. A method as claimed in claim 9 comprising moving a light source.

12. A method as claimed in claim 9 comprising moving at least one mirror.

13. A method as claimed in claim 1 wherein the engine is a gas turbine engine.

14. A method as claimed in claim 13 wherein the engine is a turbofan gas turbine engine.

15. An apparatus for determining the total mass flow through an engine, comprising:

means for measuring the fuel mass flow to the engine,

means for measuring the concentration of carbon dioxide, means for measuring the ratio of water to oxygen, means for measuring the ratio of carbon dioxide to oxygen or means for measuring the ratio of water to carbon dioxide in the gases exhausted from the engine,

means for determining the air to fuel ratio in the engine from the fuel mass flow and the concentration of carbon dioxide, the ratio of water to oxygen, the ratio of carbon dioxide to oxygen or the ratio of water to carbon dioxide,

means for determining the air mass flow through the engine from the air to fuel ratio, and

means for calculating the total air and fuel mass flow through the engine by adding the air mass flow through the engine to the fuel mass flow to the engine.

16. An apparatus as claimed in claim 15 wherein the engine is a gas turbine engine.

17. An apparatus as claimed in claim 16 wherein the gas turbine engine is a turbofan gas turbine engine.

18. An apparatus as claimed in claim 15 wherein the means for measuring the concentration of carbon dioxide comprises at least one detector.

19. An apparatus as claimed in claim 18 wherein the detector comprises a spectrometer and a photo-detector, the spectrometer is optically coupled to the photo-detector.

20. An apparatus as claimed in claim 19 wherein the spectrometer is a Fourier transform spectrometer.

21. An apparatus as claimed in claim 19 wherein the means for measuring the concentration of carbon dioxide comprises a light source.

22. An apparatus as claimed in claim 21 wherein the light source is a laser.

23. An apparatus as claimed in claim 22 wherein the laser is a tunable laser.

24. An apparatus as claimed in claim 22 wherein the laser is a diode laser.

25. An apparatus as claimed in claim 15 wherein there are means to scan the gases exhausted from the engine.

26. An apparatus as claimed in claim 25 wherein the means to scan comprises one or more mirrors.

27. An apparatus as claimed in claim 22 wherein there are a plurality of lasers.

28. An apparatus as claimed in claim 27 wherein the lasers are tuned to different wavelengths, there are means to switch the lasers on sequentially.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 29, 2004
From: BLACK, JOHN DAVID
To: ROLLS-ROYCE PLC
Reel/Frame 014939/0658 →
Priority Claims (1)
GB 0303639 · Feb 18, 2003 · national
Continuity (1)
Related Publication 20040182143A1 · Sep 23, 2004