FR1108176A - Gas turbine engine improvements - Google Patents

Gas turbine engine improvements

Info

Publication number
FR1108176A
FR1108176A FR1108176DA FR1108176A FR 1108176 A FR1108176 A FR 1108176A FR 1108176D A FR1108176D A FR 1108176DA FR 1108176 A FR1108176 A FR 1108176A
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
French (fr)
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 FR1108176A publication Critical patent/FR1108176A/en
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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F02K1/16—Control or regulation conjointly with another control
    • 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)
FR1108176D 1953-07-16 1954-07-07 Gas turbine engine improvements Expired FR1108176A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1108176X 1953-07-16

Publications (1)

Publication Number Publication Date
FR1108176A true FR1108176A (en) 1956-01-10

Family

ID=10874591

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1108176D Expired FR1108176A (en) 1953-07-16 1954-07-07 Gas turbine engine improvements

Country Status (1)

Country Link
FR (1) FR1108176A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2984969A (en) * 1955-12-29 1961-05-23 United Aircraft Corp Afterburner control for a multispool gas turbine power plant
US3021668A (en) * 1957-01-11 1962-02-20 Bendix Corp Nozzle area control for turbojet engines
US3056256A (en) * 1956-05-07 1962-10-02 United Aircraft Corp Afterburner control for a multispool gas turbine power plant

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2984969A (en) * 1955-12-29 1961-05-23 United Aircraft Corp Afterburner control for a multispool gas turbine power plant
US3056256A (en) * 1956-05-07 1962-10-02 United Aircraft Corp Afterburner control for a multispool gas turbine power plant
US3021668A (en) * 1957-01-11 1962-02-20 Bendix Corp Nozzle area control for turbojet engines

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