$\require{mediawiki-texvc}$
  • 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"

특허 상세정보

Apparatus for operating gas turbine engines

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-006/00   
미국특허분류(USC) 060/039.15; 060/224; 060/785
출원번호 US-0143246 (2005-06-02)
등록번호 US-7464533 (2008-12-16)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Andes,William Scott
인용정보 피인용 횟수 : 15  인용 특허 : 8
초록

A method facilitates assembling a gas turbine engine assembly. The method comprises providing at least one propelling gas turbine engine that includes a core engine including at least one turbine, coupling an auxiliary engine to the propelling gas turbine engine such that during operation of the propelling gas turbine engine, such that at least a portion of the airflow entering the propelling gas turbine engine is extracted from the propelling gas and channeled to the auxiliary engine for generating power, and coupling a modulating valve in flow communi...

대표
청구항

What is claimed is: 1. A gas turbine engine assembly comprising: at least one propelling gas turbine engine comprising a fan, a core engine downstream from the fan, and a plurality of extraction points; a modulating valve coupled in flow communication to said at least one propelling gas turbine engine; and an auxiliary engine used for generating electrical power, said auxiliary engine comprising at least one turbine and an inlet, said inlet coupled in flow communication with said modulating valve, such that a portion of airflow entering said at least on...

이 특허를 인용한 특허 피인용횟수: 15

  1. Ripley, David Lloyd. Accumulator assisted gas turbine engine start system and methods therefor. USP20190210208672.
  2. Way, Donald L.; Lantz, Joel. Active surge control. USP2013018342793.
  3. Kupratis, Daniel Bernard; Staubach, Joseph B.. Aerospace engine with augmenting turbojet. USP2015129222409.
  4. Kesseli, James B.; Nash, James S.. Ceramic-to-metal turbine shaft attachment. USP2015069051873.
  5. Baldwin, Matthew Stephen. Ceramic-to-metal turbine volute attachment for a gas turbine engine. USP20181010094288.
  6. Donnelly, Frank Wegner; Dewis, David William. Dispatchable power from a renewable energy facility. USP2014108866334.
  7. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Upton, Timothy; Watson, John D.. Gas turbine energy storage and conversion system. USP2013088499874.
  8. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Watson, John D.. Gas turbine energy storage and conversion system. USP2014048708083.
  9. Donnelly, Frank Wegner; Dewis, David William. Gas turbine engine configurations. USP2014038669670.
  10. Kesseli, James B.; Baldwin, Matthew Stephen. Metallic ceramic spool for a gas turbine engine. USP2015038984895.
  11. Rice, Edward C.. Propulsive force vectoring. USP2018059976514.
  12. Rice, Edward C.; Sumner, Bradley S.. Splayed inlet guide vanes. USP20181110125622.
  13. Rice, Edward C.. System and method for a fluidic barrier on the low pressure side of a fan blade. USP2018039915149.
  14. Rice, Edward C.. System and method for creating a fluidic barrier from the leading edge of a fan blade. USP20190310233869.
  15. Paulino, Jose R.. Variable bypass ratio augmented gas turbine engine. USP2014098844266.