$\require{mediawiki-texvc}$
  • 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
검색연산자 기능 검색시 예
() 우선순위가 가장 높은 연산자 예1) (나노 (기계 | machine))
공백 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 예1) (나노 기계)
예2) 나노 장영실
| 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 예1) (줄기세포 | 면역)
예2) 줄기세포 | 장영실
! NOT 이후에 있는 검색어가 포함된 문서는 제외 예1) (황금 !백금)
예2) !image
* 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 예) semi*
"" 따옴표 내의 구문과 완전히 일치하는 문서만 검색 예) "Transform and Quantization"

과학기술 지식인프라 ScienceON

상세검색 다국어 입력
도움말도움말

특허 상세정보

MyON담기
내보내기

Bleed valve control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-009/18   
미국특허분류(USC) 60/3902 ; 60/3929
출원번호 US-0155640 (1993-11-22)
우선권정보 GB-0025977 (1992-12-12)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 22  인용 특허 : 0
초록
▼

A method and means are provided for operating a bleed to counter surge in the compressor of a gas turbine. A number of engine condition parameters which are precursors to a change of engine running conditions are monitored to detect changes outside predetermined limits. The method includes deriving a measure of heat soakage effects as an engine condition parameter by monitoring a gas flow value such as compressor outlet pressure, and deriving a further engine condition parameter by evaluating changes of engine power-setting by comparing instantaneous pow...

대표
청구항
▼

A method of controlling a compressor bleed valve in a gas turbine engine for a flow of gas from a high pressure region of the compressor to counter compressor surge, said method comprising monitoring one or more properties of the gas flow as an engine condition parameter to obtain a measure of heat soakage effects produced in the compressor by adjustment of relative temperatures between the gas flow and the compressor parts during deceleration of the engine, and the detection of values of said parameter outside a predetermined limit causing said bleed va...

이 특허를 인용한 특허 피인용횟수: 22

  1. Oliverio, Fabrizio. Bleed valve override schedule on off-load transients. USP2016019228501.
  2. Kendrick, Donald W.. Combustion cavity layouts for fuel staging in trapped vortex combustors. USP2014048689562.
  3. Kawai, Keisuke. Control apparatus for a gas-turbine aeroengine. USP20180910077720.
  4. Krukoski Leon ; Laudadio Nicola ; Doherty ; Jr. Stephen P. ; Kratz Merrill L.. Control system for modulating bleed in response to engine usage. USP2000116141951.
  5. Khalid Syed J.. Control system for preventing compressor stall. USP2001056231306.
  6. Irwin Craig W. ; Khalid Syed J.. Controlling stall margin in a gas turbine engine during acceleration. USP2000126164902.
  7. Giove, Fabio; Tondolo, Flavio; Mastrovito, Marco. Dead time reducer for piston actuator. USP2017049611857.
  8. Price, Brian John; Demers, Louis. Dynamic control of a gas turbine engine compressor during rapid transients. USP2012118302405.
  9. King, Dennis M. Gas turbine engine with a plurality of bleed valves. USP2009097591183.
  10. Anatoly Rakhmailov RU. Gas turbine engine with exhaust compressor having outlet tap control. USP2002066397576.
  11. Prasad, Jonnalagadda V. R.; Neumeier, Yedidia; Krichene, Assaad; Dhingra, Manuj. Method and apparatus for active control of surge in compressors. USP2004096793455.
  12. Hillel, Malcolm; Moes, Thierry; Stieger, Rory Douglas. Method and apparatus for controlling a compressor of a gas turbine engine. USP2017109797314.
  13. Andrew Philip Lynn ; Stampfli John David ; Nava Pierluigi,ITX ; Mazzoni Marco,ITX. Method for ascertaining surge pressure ratio in compressors for turbines. USP2001046220086.
  14. Witt, Klaus Leonard. Method for determining a functioning of a gas bleed valve. USP2013028381583.
  15. Kendrick, Donald W.. Method of fuel staging in combustion apparatus. USP2013108549862.
  16. Khalid, Syed Jalaluddin; Gritton, Mark J.. Modulated cooling flow scheduling for both SFC improvement and stall margin increase. USP2016119482236.
  17. Srivastava, Sachin; Pistner, Alexander James; Varadhan, Raghavan; Moore, Matthew Everett. Predicting a surge event in a compressor of a turbomachine. USP20180810047757.
  18. Gregory J. Chapman. Smart surge bleed valve system and method. USP2002116481210.
  19. Lundquist Joseph E.. Soot filter. USP2000116152978.
  20. Xiong, Yufei; Faymon, Dave; Rushinsky, John. Surge bleed valve fault detection. USP2003056557400.
  21. Timothy J. Keller ; Daniel Burns ; Mohamad Hanif Vhora ; Patrick O'Brien ; Coung Van Nguyen. Valve control logic for gas turbine recuperator. USP2002106463730.
  22. Kendrick, Donald W.. Vortex premixer for combustion apparatus. USP2014048689561.

IPC 상위 출원인