IT979502B - Inserto di controllo dell area trasver ale atto a mantenere un uniformita del flusso d aria attorno alla camera di combustio ne di un turbomotore a gas - Google Patents

Inserto di controllo dell area trasver ale atto a mantenere un uniformita del flusso d aria attorno alla camera di combustio ne di un turbomotore a gas

Info

Publication number
IT979502B
IT979502B IT20890/73A IT2089073A IT979502B IT 979502 B IT979502 B IT 979502B IT 20890/73 A IT20890/73 A IT 20890/73A IT 2089073 A IT2089073 A IT 2089073A IT 979502 B IT979502 B IT 979502B
Authority
IT
Italy
Prior art keywords
turbomotor
transver
uniformity
maintaining
gas
Prior art date
Application number
IT20890/73A
Other languages
English (en)
Original Assignee
Gen Electric
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Application granted granted Critical
Publication of IT979502B publication Critical patent/IT979502B/it

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT20890/73A 1972-03-01 1973-02-27 Inserto di controllo dell area trasver ale atto a mantenere un uniformita del flusso d aria attorno alla camera di combustio ne di un turbomotore a gas IT979502B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US23083972A 1972-03-01 1972-03-01

Publications (1)

Publication Number Publication Date
IT979502B true IT979502B (it) 1974-09-30

Family

ID=22866779

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20890/73A IT979502B (it) 1972-03-01 1973-02-27 Inserto di controllo dell area trasver ale atto a mantenere un uniformita del flusso d aria attorno alla camera di combustio ne di un turbomotore a gas

Country Status (7)

Country Link
US (1) US3750397A (it)
JP (1) JPS48100515A (it)
BE (1) BE795867A (it)
CA (1) CA963675A (it)
DE (1) DE2309715A1 (it)
FR (1) FR2174069B3 (it)
IT (1) IT979502B (it)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4098074A (en) * 1976-06-01 1978-07-04 United Technologies Corporation Combustor diffuser for turbine type power plant and construction thereof
US4373327A (en) * 1979-07-04 1983-02-15 Rolls-Royce Limited Gas turbine engine combustion chambers
US4512158A (en) * 1983-06-16 1985-04-23 United Technologies Corporation High blockage diffuser with means for minimizing wakes
US5077967A (en) * 1990-11-09 1992-01-07 General Electric Company Profile matched diffuser
US5142871A (en) * 1991-01-22 1992-09-01 General Electric Company Combustor dome plate support having uniform thickness arcuate apex with circumferentially spaced coolant apertures
CA2070518C (en) * 1991-07-01 2001-10-02 Adrian Mark Ablett Combustor dome assembly
US5289687A (en) * 1992-03-30 1994-03-01 General Electric Company One-piece cowl for a double annular combustor
FR2706534B1 (fr) * 1993-06-10 1995-07-21 Snecma Diffuseur-séparateur multiflux avec redresseur intégré pour turboréacteur.
DE19539771B4 (de) * 1995-10-26 2006-10-05 Alstom Gasturbine
US6513330B1 (en) 2000-11-08 2003-02-04 Allison Advanced Development Company Diffuser for a gas turbine engine
US6401447B1 (en) 2000-11-08 2002-06-11 Allison Advanced Development Company Combustor apparatus for a gas turbine engine
GB2391297A (en) * 2002-07-24 2004-02-04 Rolls Royce Plc Gas supply assembly
US6952927B2 (en) * 2003-05-29 2005-10-11 General Electric Company Multiport dome baffle
US8500399B2 (en) * 2006-04-25 2013-08-06 Rolls-Royce Corporation Method and apparatus for enhancing compressor performance
GB0618991D0 (en) * 2006-09-27 2006-11-08 Rolls Royce Plc A component for a gas turbine engine
FR2920524B1 (fr) * 2007-08-30 2013-11-01 Snecma Turbomachine a chambre annulaire de combustion
US9046272B2 (en) * 2008-12-31 2015-06-02 Rolls-Royce Corporation Combustion liner assembly having a mount stake coupled to an upstream support
FR2943726B1 (fr) * 2009-03-31 2014-04-25 Snecma Capot d'entree tournant pour turbomachine, comprenant une extremite avant excentree
GB201001974D0 (en) * 2010-02-08 2010-03-24 Rolls Royce Plc An outlet guide vane structure
EP2410138B8 (en) * 2010-07-22 2017-07-19 Ansaldo Energia IP UK Limited Gas turbine engine flange arrangement and method for retrofitting same
FR2964725B1 (fr) * 2010-09-14 2012-10-12 Snecma Carenage aerodynamique pour fond de chambre de combustion
WO2014052737A1 (en) 2012-09-28 2014-04-03 United Technologies Corporation Inner diffuser case struts for a combustor of a gas turbine engine
US9938963B2 (en) * 2012-12-29 2018-04-10 Spar Energy Llc Power generation from atmospheric air pressure
US10190603B2 (en) 2012-12-29 2019-01-29 Spar Energy Llc Power generation from atmospheric air pressure

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049882A (en) * 1960-05-16 1962-08-21 Gen Electric Combustor construction with means for prevention of hot streaks
GB1040390A (en) * 1965-07-12 1966-08-24 Rolls Royce Gas turbine engine
US3364678A (en) * 1966-02-28 1968-01-23 Gen Electric Means for stabilizing fluid flow in diffuser-combustor systems in axial flow gas turbine engines
US3372542A (en) * 1966-11-25 1968-03-12 United Aircraft Corp Annular burner for a gas turbine
US3589127A (en) * 1969-02-04 1971-06-29 Gen Electric Combustion apparatus
US3581492A (en) * 1969-07-08 1971-06-01 Nasa Gas turbine combustor
US3631674A (en) * 1970-01-19 1972-01-04 Gen Electric Folded flow combustion chamber for a gas turbine engine

Also Published As

Publication number Publication date
DE2309715A1 (de) 1973-09-13
FR2174069A1 (it) 1973-10-12
FR2174069B3 (it) 1976-03-05
CA963675A (en) 1975-03-04
BE795867A (fr) 1973-06-18
JPS48100515A (it) 1973-12-19
US3750397A (en) 1973-08-07

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