FR1066903A - Perfectionnements aux moteurs à turbine à gaz - Google Patents

Perfectionnements aux moteurs à turbine à gaz

Info

Publication number
FR1066903A
FR1066903A FR1066903DA FR1066903A FR 1066903 A FR1066903 A FR 1066903A FR 1066903D A FR1066903D A FR 1066903DA FR 1066903 A FR1066903 A FR 1066903A
Authority
FR
France
Prior art keywords
gas turbine
turbine engine
engine improvements
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)
Inventor
Donald Hamilton Mattinson
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 FR1066903A publication Critical patent/FR1066903A/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
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
    • 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)
FR1066903D 1952-07-22 1952-07-31 Perfectionnements aux moteurs à turbine à gaz Expired FR1066903A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB18370/51A GB712633A (en) 1952-07-22 1952-07-22 Improvements relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
FR1066903A true FR1066903A (fr) 1954-06-10

Family

ID=32011990

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1066903D Expired FR1066903A (fr) 1952-07-22 1952-07-31 Perfectionnements aux moteurs à turbine à gaz

Country Status (3)

Country Link
CH (1) CH304500A (fr)
FR (1) FR1066903A (fr)
GB (1) GB712633A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1043721B (de) * 1955-10-05 1958-11-13 Power Jets Res & Dev Ltd Strahltriebwerk
FR2313566A1 (fr) * 1975-06-02 1976-12-31 Gen Electric Moteur a turbine a gaz a cycle variable
FR2369429A1 (fr) * 1976-11-01 1978-05-26 Gen Electric Melangeur hybride pour turbo-moteur dilue et moteur ainsi obtenu
FR2713749A1 (fr) * 1993-12-15 1995-06-16 Snecma Chambre de post combustion de turbine à gaz.

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1276969B (de) * 1962-10-30 1968-09-05 Bristol Siddeley Engines Ltd Gasturbinenstrahltriebwerk

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1043721B (de) * 1955-10-05 1958-11-13 Power Jets Res & Dev Ltd Strahltriebwerk
FR2313566A1 (fr) * 1975-06-02 1976-12-31 Gen Electric Moteur a turbine a gaz a cycle variable
FR2369429A1 (fr) * 1976-11-01 1978-05-26 Gen Electric Melangeur hybride pour turbo-moteur dilue et moteur ainsi obtenu
FR2713749A1 (fr) * 1993-12-15 1995-06-16 Snecma Chambre de post combustion de turbine à gaz.

Also Published As

Publication number Publication date
GB712633A (en) 1954-07-28
CH304500A (de) 1955-01-15

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