$\require{mediawiki-texvc}$
  • 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"
쳇봇 이모티콘
안녕하세요!
ScienceON 챗봇입니다.
궁금한 것은 저에게 물어봐주세요.

특허 상세정보

Plural engine power producing system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02B-073/00   
미국특허분류(USC) 60/718 ; 60/716
출원번호 US-0846150 (1992-03-05)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 17  인용 특허 : 0
초록

Two gas turbine engines are interconnected through a pneumatic, mechanical, hydraulic, or power link. This power link runs from the gas producer shaft of one engine to the gas producer shaft of the other engine either delivering or absorbing power directly to or from each other. The gas producer section of a gas turbine engine comprises a compressor directly coupled to a turbine which drives the compressor and a combustor positioned between the compressor and the turbine. The unit delivers hot gases to another turbine on a separate independent shaft whic...

대표
청구항

A system for producing power utilizing gas turbine engines comprising: a primary engine including a gas generator and a power turbine; a secondary engine including: a compressor; a combustor; and a turbine drivingly engaged with said compressor; drive means selectively coupling said gas generator of said primary engine and said secondary engine for augmenting the output power of the primary engine and for achieving improved fuel consumption of said system at low power levels.

이 특허를 인용한 특허 피인용횟수: 17

  1. Hamel,Jerry. Air conditioning system with secondary compressor drive. USP2006057040106.
  2. Albero, Jose; Bruno, Louis J.; Dussault, Richard; Lents, Charles E.; Thresher, Wayne A.; Sahm, Michael K.; Thompson, Robert G.. Aircraft system architecture. USP2003106634596.
  3. Ullyott, Richard. Compact compound engine package. USP2010027654087.
  4. Selfors Brian J. ; Heitmann Arnold M.. Cooling of turboalternator for hybrid motor vehicle. USP1998085789824.
  5. Nims Robert A.. Dual turbogenerator auxiliary power system. USP1998095799484.
  6. Akiyama Kazuho,JPX ; Uji Shigekazu,JPX ; Hirata Masaru,JPX. Gas turbine generator with dual steam-injected turbines. USP2000116141955.
  7. Huber, David J. Hybrid gas turbine and internal combustion engine. USP2012038141360.
  8. Ullyott,Richard. Integral cooling system for rotary engine. USP2008087412831.
  9. Weber Kent. Integrated emergency power and environmental control system. USP2001116316841.
  10. Dauriac, Pascal; Bedrine, Olivier; Marconi, Patrick; Rideau, Jean-Francois. Method and architecture for the optimized transfer of power between an auxiliary power motor and the main engines of a helicopter. USP20180810059460.
  11. Haillot, Jean-Michel. Method for optimizing the operability of an aircraft propulsive unit, and self-contained power unit for implementing same. USP2016089404419.
  12. Jones, Alan R.. Method of inhibiting ice accretion within a turbine engine and control system therefor. USP2016019239011.
  13. Dull, Sebastian; Fritzsche, Albert; Serden, Andreas; Waschilewski, G?nther. Mobile, self-sufficient operating assembly for providing electrical energy. USP2005106954003.
  14. Milde ; Jr. Karl F.. Personal air transport. USP2001016179247.
  15. Hawkins John M.. Propeller gearbox. USP2001076264138.
  16. Burnier, Timothy A.; Padgett, John D.. Shared power street sweeper. USP2015049010467.
  17. Selfors Brian J. ; Heitmann Arnold M.. Turboalternator for hybrid motor vehicle. USP1998115831341.