FR2265996B3 - - Google Patents

Info

Publication number
FR2265996B3
FR2265996B3 FR7509137A FR7509137A FR2265996B3 FR 2265996 B3 FR2265996 B3 FR 2265996B3 FR 7509137 A FR7509137 A FR 7509137A FR 7509137 A FR7509137 A FR 7509137A FR 2265996 B3 FR2265996 B3 FR 2265996B3
Authority
FR
France
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
FR7509137A
Other languages
French (fr)
Other versions
FR2265996A1 (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
Publication of FR2265996A1 publication Critical patent/FR2265996A1/en
Application granted granted Critical
Publication of FR2265996B3 publication Critical patent/FR2265996B3/fr
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants 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
    • F02K3/04Plants 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
    • F02K3/06Plants 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 front fan
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Gas Burners (AREA)
FR7509137A 1974-03-26 1975-03-24 Gas turbine jet with annular nozzle - gas flow diversion inside the nozzle produces an inclined nozzle outlet flow Granted FR2265996A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1322974 1974-03-26

Publications (2)

Publication Number Publication Date
FR2265996A1 FR2265996A1 (en) 1975-10-24
FR2265996B3 true FR2265996B3 (en) 1977-11-25

Family

ID=10019199

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7509137A Granted FR2265996A1 (en) 1974-03-26 1975-03-24 Gas turbine jet with annular nozzle - gas flow diversion inside the nozzle produces an inclined nozzle outlet flow

Country Status (4)

Country Link
JP (1) JPS50129813A (en)
DE (1) DE2512082A1 (en)
FR (1) FR2265996A1 (en)
IT (1) IT1037141B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1185101A (en) * 1980-03-03 1985-04-09 Daniel J. Lahti Drag-reducing nacelle
FR2993861B1 (en) * 2012-07-27 2015-07-31 Snecma TURBOJET ASSEMBLY AND CAPOTAGE OF THE FIXING PYLON TO THE VESSEL OF AN AIRCRAFT

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT325898B (en) * 1971-09-29 1975-11-10 List Hans SILENT ENCLOSED COMBUSTION ENGINE

Also Published As

Publication number Publication date
JPS50129813A (en) 1975-10-14
IT1037141B (en) 1979-11-10
FR2265996A1 (en) 1975-10-24
DE2512082A1 (en) 1975-10-09

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Legal Events

Date Code Title Description
ST Notification of lapse