FR1173231A - Perfectionnements apportés aux installations avec turbine à gaz - Google Patents

Perfectionnements apportés aux installations avec turbine à gaz

Info

Publication number
FR1173231A
FR1173231A FR1173231DA FR1173231A FR 1173231 A FR1173231 A FR 1173231A FR 1173231D A FR1173231D A FR 1173231DA FR 1173231 A FR1173231 A FR 1173231A
Authority
FR
France
Prior art keywords
installations
improvements made
gas turbines
turbines
gas
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development Ltd
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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR1173231A publication Critical patent/FR1173231A/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
    • F02K3/02—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
    • F02K3/062—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 with aft fan
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1173231D 1956-02-27 1957-02-27 Perfectionnements apportés aux installations avec turbine à gaz Expired FR1173231A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2937495X 1956-02-27

Publications (1)

Publication Number Publication Date
FR1173231A true FR1173231A (fr) 1959-02-23

Family

ID=10918159

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1173231D Expired FR1173231A (fr) 1956-02-27 1957-02-27 Perfectionnements apportés aux installations avec turbine à gaz

Country Status (2)

Country Link
US (1) US2937495A (fr)
FR (1) FR1173231A (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3068646A (en) * 1959-01-28 1962-12-18 Rolls Royce Improvements in by-pass type gas turbine engines
US3070285A (en) * 1959-11-26 1962-12-25 Rolls Royce Gas turbine engine
US3303997A (en) * 1965-04-21 1967-02-14 United Aircraft Corp Compressor air seal
US3423048A (en) * 1966-11-18 1969-01-21 Bristol Siddeley Engines Ltd Gas turbine compound helicopter power plant
US4541775A (en) * 1983-03-30 1985-09-17 United Technologies Corporation Clearance control in turbine seals
GB2192237B (en) * 1986-07-02 1990-05-16 Rolls Royce Plc Gas turbine engine power turbine
FR3015570B1 (fr) * 2013-12-19 2016-02-05 Snecma Moyens de support radiaux comprenant un dispositif de decouplage axial entre un carter interne et un carter externe d'helice pour turbomachine a ensemble d'helices contrarotatives non carenees
US20170314509A1 (en) * 2016-04-27 2017-11-02 General Electric Company Turbofan assembly and method of assembling

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2505660A (en) * 1950-04-25 Augmentor fob jet propulsion hav
US2692724A (en) * 1942-07-02 1954-10-26 Power Jets Res & Dev Ltd Turbine rotor mounting
US2430399A (en) * 1942-11-05 1947-11-04 Armstrong Siddeley Motors Ltd Jet augmenter for combustion turbine propulsion plants
GB579775A (en) * 1943-10-23 1946-08-15 Armstrong Siddeley Motors Ltd Improvements relating to labyrinth packings for elastic fluid turbines
NL69078C (fr) * 1944-01-31
US2461242A (en) * 1944-08-23 1949-02-08 United Aircraft Corp Rotor construction for turbines
FR957061A (fr) * 1944-09-23 1950-02-14
US2614385A (en) * 1946-01-14 1952-10-21 Power Jets Res & Dev Ltd Supporting structure for gas turbine power plants
US2711631A (en) * 1949-06-21 1955-06-28 Hartford Nat Bank & Trust Co Gas turbine power plant

Also Published As

Publication number Publication date
US2937495A (en) 1960-05-24

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