[미국특허]
Method for monitoring a degree of clogging of the starting injectors of a turbine engine
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F01D-017/08
F01D-019/00
F02C-007/264
F02C-007/22
출원번호
US-0768666
(2014-02-14)
등록번호
US-10145262
(2018-12-04)
우선권정보
FR-13 51359 (2013-02-18)
국제출원번호
PCT/FR2014/050309
(2014-02-14)
국제공개번호
WO2014/125229
(2014-08-21)
발명자
/ 주소
Debbouz, Nadir Christian
De Barbeyrac, Philippe Patrick Marc
Enguehard, Florian Arnaud Jonathan
Faupin, Francois Xavier Marie
Lamazere, Fabien
출원인 / 주소
SAFRAN HELICOPTER ENGINES
대리인 / 주소
Oblon, McClelland, Maier & Neustadt, L.L.P.
인용정보
피인용 횟수 :
0인용 특허 :
3
초록▼
A method for monitoring a degree of clogging of the starting injectors of a turbine engine, which includes: a combustion chamber into which at least one starting injector supplied with fuel leads, the starting injectors being suitable for initiating the combustion in the chamber by igniting the fuel
A method for monitoring a degree of clogging of the starting injectors of a turbine engine, which includes: a combustion chamber into which at least one starting injector supplied with fuel leads, the starting injectors being suitable for initiating the combustion in the chamber by igniting the fuel; and a turbine rotated by the gases resulting from the combustion of the fuel in the chamber, the method including the steps involving: the measurement, during a phase of starting the turbine engine, of the temperature of the exhaust gases at the outlet of the turbine; and the determination, from the changes over time in the temperature thus measured, of a degree of clogging of the starting injectors. A system for monitoring a degree of clogging capable of implementing the method, and a turbine engine including such a system.
대표청구항▼
1. A method for monitoring a degree of clogging of a starting injector of a turbine engine comprising: a combustion chamber, into which a starting injector supplied with fuel opens, said starting injector being suitable for initiating a combustion in said combustion chamber by igniting the fuel, and
1. A method for monitoring a degree of clogging of a starting injector of a turbine engine comprising: a combustion chamber, into which a starting injector supplied with fuel opens, said starting injector being suitable for initiating a combustion in said combustion chamber by igniting the fuel, anda turbine, rotated by gases resulting from the combustion of the fuel in the combustion chamber,the method comprising:measuring, during a phase of starting the turbine engine, a temperature of exhaust gases at an outlet of the turbine; anddetermining, from changes over time in the temperature of exhaust gases thus measured, a degree of clogging of the starting injector,wherein the determining the degree of clogging of the starting injector as a function of the changes over time in the temperature of the exhaust gases at the outlet of the turbine comprises: detecting a phase of a fall of the temperature during a phase of rise of said temperature, an absence of detecting said fall corresponding to an absence of clogging of the starting injector, andmeasuring an amplitude of said fall. 2. The method for monitoring according to claim 1, further comprising: comparing a variation in the amplitude of the fall in the temperature of the exhaust gases at the outlet of the turbine during successive startings with at least one predetermined threshold, anddetermining the degree of clogging of the starting injector based on the comparing. 3. The method for monitoring according to claim 1, further comprising, during the measuring the temperature of the exhaust gases at the outlet of the turbine, measuring a speed of rotation of the turbine, and in which the determining the degree of clogging of the starting injector is carried out from the changes over time in the temperature of the gases and measurements of the speed of rotation of the turbine. 4. The method for monitoring according to claim 3, wherein the determining the degree of clogging of the starting injector comprises: measuring the value of the speed of rotation of the turbine at a moment of an inflection point of the temperature of the exhaust gases at the outlet of the turbine initiating the fall in said temperature,comparing a variation in said value during successive startings with a predetermined threshold, anddetermining, from comparisons of the variations of the amplitude of the fall in temperature and the value of speed of the turbine with their respective thresholds, the degree of clogging of the starting injector. 5. The method for monitoring according to claim 1, further comprising determining, from the degree of clogging of the starting injector, a remaining number of startings of the turbine engine before the degree of clogging of the starting injector reaches a level resulting in an impossibility of starting said turbine engine. 6. The method for monitoring according to claim 5, further comprising activating an alert so that a maintenance or a replacement of the starting injector is carried out before the degree of clogging of the starting injector reaches the level resulting in an impossibility of starting said turbine engine. 7. A system for monitoring an operating state of a starting injector of a turbine engine comprising: a combustion chamber, into which a starting injector supplied with fuel leads, said starting injector being suitable for initiating a combustion in said combustion chamber by igniting the fuel,a turbine, rotated by gases resulting from the combustion of the fuel in the combustion chamber,a temperature sensor of gases at an outlet of the turbine, anda processing unit, comprising a memory and a processor configured to process temperature measurements and establishing a change over time of said temperature measurements for a determination of a degree of clogging of the starting injector,wherein the processing unit is further configured to: detect a phase of a fall of the temperature during a phase of rise of said temperature, an absence of detecting said fall corresponding to an absence of clogging of the starting injector, andmeasure an amplitude of said fall. 8. The system for monitoring according to claim 7, further comprising a sensor of speed of rotation of the turbine, wherein the processing unit is further configured to process measurements of speed of rotation of the turbine, for the determination of the degree of clogging of the starting injector. 9. The system for monitoring according to claim 7, wherein the temperature sensor is suitable for carrying out measurements at a frequency greater than or equal to 1 Hz. 10. A turbine engine comprising a system for monitoring according to claim 7. 11. An aircraft comprising: a system for monitoring according to claim 7.
Gilbert Kendall E. (Schenectady NY) Johnson Daniel (Rexford NY) Macier Robert Raymond (Saratoga Springs NY), Gas turbine temperature sensor validation apparatus and method.
Plimpton,Jonathon; Jubinville,Leo; Duckless,Edward, Method and apparatus for detecting the presence of flame in the exhaust path of a gas turbine engine.
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