FR1122800A - Perfectionnements apportés aux moteurs à turbine à gaz - Google Patents

Perfectionnements apportés aux moteurs à turbine à gaz

Info

Publication number
FR1122800A
FR1122800A FR1122800DA FR1122800A FR 1122800 A FR1122800 A FR 1122800A FR 1122800D A FR1122800D A FR 1122800DA FR 1122800 A FR1122800 A FR 1122800A
Authority
FR
France
Prior art keywords
gas turbine
turbine engines
engines
gas
turbine
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
Other languages
English (en)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1122800A publication Critical patent/FR1122800A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow
    • F02K1/30—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow for varying effective area of jet pipe or nozzle
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1122800D 1954-04-27 1955-04-19 Perfectionnements apportés aux moteurs à turbine à gaz Expired FR1122800A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB12244/54A GB795651A (en) 1954-04-27 1954-04-27 Improvements in or relating to aircraft power plant installations incorporating gas-turbine engines

Publications (1)

Publication Number Publication Date
FR1122800A true FR1122800A (fr) 1956-09-12

Family

ID=10001020

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1122800D Expired FR1122800A (fr) 1954-04-27 1955-04-19 Perfectionnements apportés aux moteurs à turbine à gaz

Country Status (3)

Country Link
BE (1) BE537620A (fr)
FR (1) FR1122800A (fr)
GB (1) GB795651A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1121413B (de) * 1957-07-17 1962-01-04 Havilland Engine Co Ltd De Schubduese fuer Strahltriebwerke
US3641766A (en) * 1969-11-26 1972-02-15 Gen Electric Gas turbine engine constant speed thrust modulation

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3044258A (en) * 1958-11-25 1962-07-17 Gen Electric Adjustable converging-diverging nozzle
FR1391927A (fr) * 1964-01-29 1965-03-12 Monsieur Le Ministre Des Armee Chambre de combustion avec tuyère pour moteurs fusées à liquides
US3463404A (en) * 1966-12-21 1969-08-26 United Aircraft Corp Gas boundary layer variable area orifice
GB2192229B (en) * 1986-07-04 1990-05-02 Rolls Royce Plc A compressor and air bleed system
US6442941B1 (en) * 2000-09-11 2002-09-03 General Electric Company Compressor discharge bleed air circuit in gas turbine plants and related method
US7353647B2 (en) * 2004-05-13 2008-04-08 General Electric Company Methods and apparatus for assembling gas turbine engines
US8480350B2 (en) 2006-10-12 2013-07-09 United Technologies Corporation Turbofan engine with variable bypass nozzle exit area and method of operation

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1121413B (de) * 1957-07-17 1962-01-04 Havilland Engine Co Ltd De Schubduese fuer Strahltriebwerke
US3641766A (en) * 1969-11-26 1972-02-15 Gen Electric Gas turbine engine constant speed thrust modulation

Also Published As

Publication number Publication date
BE537620A (fr)
GB795651A (en) 1958-05-28

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