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특허 상세정보

Combination rotating fluidized bed combustor and heat exchanger

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F02C-003/26    F23D-019/00   
미국특허분류(USC) 60/3935 ; 60/3946 ; S ; 60/3951 ; H ; 431/170
출원번호 US-0136654 (1979-10-15)
국제출원번호 PCT/US 79/00843
§371/§102 date 19791015 (19791015)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 24  인용 특허 : 6
초록이 없습니다.
대표
청구항

A combination rotatable fluidized bed heat exchanger (54) and rotatable fluidized bed combustor (26), said heat exchanger (54) comprising: a. a first elongated perforated wall (108); b. a second perforated wall (110) spaced apart and substantially co-extensive with said first perforated wall (108); c. enclosing walls (109) defining with said first and second perforated walls (108, 110) a first fluidization chamber (112); d. a first bed of pulverulent solid particles (114) in said first chamber (112); e. means (111) for rotating said first chamber (112) a...

이 특허를 인용한 특허 피인용횟수: 24

  1. Kesseli, James B.; Nash, James S.. Ceramic-to-metal turbine shaft attachment. USP2015069051873.
  2. Baldwin, Matthew Stephen. Ceramic-to-metal turbine volute attachment for a gas turbine engine. USP20181010094288.
  3. Kendrick, Donald W.. Combustion cavity layouts for fuel staging in trapped vortex combustors. USP2014048689562.
  4. Donnelly, Frank Wegner; Dewis, David William. Dispatchable power from a renewable energy facility. USP2014108866334.
  5. Isashi Takehara JP. Gas turbine apparatus with heat exchanger. USP2002126494031.
  6. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Upton, Timothy; Watson, John D.. Gas turbine energy storage and conversion system. USP2013088499874.
  7. Dewis, David William; Kesseli, James; Donnelly, Frank Wegner; Wolf, Thomas; Watson, John D.. Gas turbine energy storage and conversion system. USP2014048708083.
  8. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460343.
  9. Anatoly Rakhmailov RU. Gas turbine engine. USP2002106460324.
  10. Anatoly Rakhmailov RU. Gas turbine engine. USP2002046363708.
  11. Anatoly Rakhmailov RU. Gas turbine engine. USP2002096442945.
  12. Rakhmailov Anatoly,RUX. Gas turbine engine. USP2001106305157.
  13. Rakhmailov Anatoly,RUX ; Yaishnikov Valentin,UAX ; Kolotilenko Mikhail,UAX ; Rakhmailov Oleg,RUX ; Drozd Igor,RUX ; Kalin Martin. Gas turbine engine. USP2001026189311.
  14. Rakhmailov, Anatoly. Gas turbine engine. USP2003056557337.
  15. Donnelly, Frank Wegner; Dewis, David William. Gas turbine engine configurations. USP2014038669670.
  16. Rakhmailov Anatoly,RUX ; Yaishnikov Valentin,UAX ; Kolotilenko Mikhail,UAX ; Rakhmailov Oleg,RUX ; Drozd Igor,RUX. Gas turbine engine having a bladed disk. USP2001086272844.
  17. Rakhmailov Anatoly,RUX. Gas turbine engine having counter rotating turbines and a controller for controlling the load driven by one of the turbines. USP2000116145296.
  18. Anatoly Rakhmailov RU. Gas turbine engine with exhaust compressor having outlet tap control. USP2002066397576.
  19. Kesseli, James B.; Baldwin, Matthew Stephen. Metallic ceramic spool for a gas turbine engine. USP2015038984895.
  20. Mondjian, Pierre; Nguyen Dinh An, Christine; Delpech, Fran.cedilla.oise; Roux, Jean-Claude; Bourgeois, Sylvie; Steinbrunn, Alexis; Pichat, Pierre; Disdier, Jean; Mietton-Ceulemans, Estelle; Bouvier, . Method for purifying gaseous effluents by means of photocatalysis, installation for carrying out said method. USP2003016503447.
  21. Kendrick, Donald W.. Method of fuel staging in combustion apparatus. USP2013108549862.
  22. Rakhmailov Anatoly,RUX. Method of operation of a gas turbine engine and a gas turbine engine. USP2001046212871.
  23. Alink Aloysius J. W. O. (Zevenaar NLX). Process for the preparation of a combustible gaseous mixture. USP1985074529409.
  24. Kendrick, Donald W.. Vortex premixer for combustion apparatus. USP2014048689561.