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특허 상세정보

Engine assembly with direct drive of generator

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F01D-015/10    F02C-006/00    H02K-007/18    H02P-009/04    B64D-041/00    F02C-003/10    F01C-011/00    F01C-001/22    F03G-007/00    B64D-013/06   
출원번호 US-0616187 (2017-06-07)
등록번호 US-9994332 (2018-06-12)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Norton Rose Fulbright Canada
인용정보 피인용 횟수 : 0  인용 특허 : 45
초록

An engine assembly for use as an aircraft auxiliary power unit, having internal combustion engine(s) in driving engagement with an engine shaft, a generator having a generator shaft directly engaged to the engine shaft such as to be rotatable at a same speed, a compressor having an outlet in communication with the internal combustion engine inlet, and a turbine having an inlet in communication with the internal combustion engine outlet. The turbine may be a first stage turbine, and the assembly may include a second stage turbine having an inlet in commun...

대표
청구항

1. An engine assembly for use as an auxiliary power unit for an aircraft, the engine assembly comprising: at least one internal combustion engine in driving engagement with an engine shaft;a generator having a generator shaft in driving engagement with the engine shaft to provide electrical power for the aircraft, the generator and engine shafts being directly engaged to one another such as to be rotatable at a same speed;a compressor having an outlet in fluid communication with an inlet of the at least one internal combustion engine; anda turbine having...

이 특허에 인용된 특허 (45)

  1. Whurr John (Derby GB2). Aircraft compound cycle propulsion engine. USP1997125692372.
  2. Miyajima Hidenobu (Fukuroi JPX). Apparatus for transmitting power obtained by converting the exhaust energy of an engine. USP1988084766729.
  3. Wurtele,Roger N.; McAndrew,Willard G.. Auxiliary power unit for a diesel powered transport vehicle. USP2007117291932.
  4. Schwarz, Frederick M.. Cabin air supercharged aircraft internal combustion engine. USP2013078480460.
  5. Roberts Richard W. (Lombard IL). Combined turbocharger and accessory drive. USP1979034145888.
  6. Ullyott, Richard. Compact compound engine package. USP2010027654087.
  7. Lamarre, Sylvain; Fontaine, Mike; Julien, Andre; Gaul, Michael; Thomassin, Jean; Mitrovic, Lazar. Compound engine assembly with cantilevered compressor and turbine. USP2018019869240.
  8. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves. Compound engine assembly with common inlet. USP2017109797297.
  9. Bergmann Horst (Esslingen DEX) Fischer Gnter (Stuttgart DEX) Bschel Wolfgang (Fellbach DEX). Compound turbo-drive for an internal-combustion engine. USP1992095142867.
  10. Rice Ivan G. (P.O. Box 233 Spring TX 77383). Compression intercooled gas turbine combined cycle. USP1990014896499.
  11. Ream Lloyd W. (N. Canton OH). Diesel engine catalytic combustor system. USP1984054449370.
  12. Striebich Helmut (Karlsruhe DEX). Drive assembly, especially for motor vehicles. USP1981104294074.
  13. Thorne Anthony R. ; Kaiser Fredrick ; Skinner ; Sr. Russell A.. Electrical generator employing rotary engine. USP2000016014015.
  14. Kapich Davorin (3111 Serrano Dr. Carlsbad CA 92009). Engine driven propulsion fan with turbochargers in series. USP1995125471834.
  15. Richards, Bryn. Engine induction system. USP2013118584459.
  16. Thomassin, Jean; Bolduc, Sebastien; Villeneuve, Bruno; Berube, Stephane; Fontaine, Mike; Gagnon-Martin, David; Julien, Andre; Cunningham, Mark; Lafortune, Serge; Legare, Pierre-Yves. Engine intake assembly with selector valve. USP2018019879591.
  17. Ward Michael S. (300 N. Main Excelsior Springs MO 64024). Exhaust gas turbine drive system for engine accessories. USP1994075329770.
  18. Horner Michael W.. Extracted, cooled, compressed/intercooled, cooling/combustion air for a gas turbine engine. USP1998035724806.
  19. Farrington Franklin D.. High efficiency environmental control systems and methods. USP1999105967461.
  20. Huber, David J. Hybrid gas turbine and internal combustion engine. USP2012038141360.
  21. Tadokoro Tomoo (Hiroshima JPX) Okimoto Haruo (Hiroshima JPX) Shiraishi Hideo (Hiroshima JPX) Akagi Toshimichi (Hiroshima JPX). Intake system for rotary piston engine. USP1986014562803.
  22. Zinsmeyer Herbert G. (Austin TX). Internal combustion engine having an exhaust gas turbine. USP1985084535592.
  23. Larson, Gerald L.; Cook, Anthony J.. Internal combustion engine with pressure boosted exhaust gas recirculation. USP2005106955162.
  24. Vuk, Carl T.. Low emission turbo compound engine system. USP2011057950231.
  25. Julien, André; Chèvrefils, André. Low volumetric compression ratio integrated turbo-compound rotary engine. USP2010087775044.
  26. Furman,Anthony Holmes; Primus,Roy James. Method and apparatus for actively turbocharging an engine. USP2006117137253.
  27. Curtil Remi (Montsoult FRX). Method of and system for power generation by supercharged internal combustion engine. USP1983094404805.
  28. Bonnaud Pierre L. (Carrieres sur Seine FRX). Method of recovering energy in a power generator and power generator for carrying out the said method. USP1985044513572.
  29. Mischler, James Robert; Loringer, Daniel Edward; Blythe, Neil Xavier; Henry, Luke; Malone, Matthew John; Polkus, Greg Thomas. Methods and system for controlling surge in a two-stage turbocharger. USP2017119822694.
  30. Halimi Edward M. ; Maloof Ralph P. ; Woollenweber William E.. Motor-assisted variable geometry turbocharging system. USP2001076256993.
  31. Niggeman Richard E.. Multiple mode environmental control system for pressurized aircraft cabin. USP1999095956960.
  32. Thomassin, Jean; Julien, Andre; Schulz, Edwin; Lanktree, Michael. Rotary internal combustion engine with variable volumetric compression ratio. USP2017019540992.
  33. Thompson Robert George. Secondary power integrated cabin energy system for a pressurized aircraft. USP2001096283410.
  34. Algrain, Marcelo C.. Stationary genset power system having turbo-compounding. USP2012038143732.
  35. Paillard, Jerome; Avons, Vincent-Pierre. Supercharged engine diagnostics method and associated engine. USP2016059328676.
  36. Hirabayashi Yuji (Zushi JPX) Noguchi Masato (Yokohama JPX) Hatanaka Keiji (Fujisawa JPX). Supercharger pressure control system for internal combustion engine with turbocharger. USP1987094691521.
  37. Bronicki Lucien Y. (Rehovot IL). Supercharger system for combustion engine. USP1976063961199.
  38. Rosson, Randy Scott; Wilkes, Kevin Wood. Systems involving multi-spool generators and variable speed electrical generators. USP2012048164208.
  39. Waterstripe, Robert F.; Hoffman, Gary P.; Willoughby, Richard L.. Thermodynamic power generation system. USP2013098522552.
  40. Wong, Alexander. Turbo recharger. USP2015129200556.
  41. Wong, Alexander. Turbo recharger. USP2016129518507.
  42. Denholm, Tim; Nishiyama, Toshihiko; Ryder, Owen Alistair. Turbo-compound turbocharged engine and method of operating turbo-compound turbocharged engine. USP2016029267442.
  43. Schwartzman Everett H. (2751 Toledo St. Torrance CA 90503). Turbocharger systems. USP1983014367626.
  44. Khair Magdi K.. Turbocharging systems for internal combustion engines. USP1998065771868.
  45. Woollenweber William E. ; Halimi Edward M.. Turbocharging systems for internal combustion engines. USP2000056062026.