FR2265996A1 - Gas turbine jet with annular nozzle - gas flow diversion inside the nozzle produces an inclined nozzle outlet flow - Google Patents

Gas turbine jet with annular nozzle - gas flow diversion inside the nozzle produces an inclined nozzle outlet flow

Info

Publication number
FR2265996A1
FR2265996A1 FR7509137A FR7509137A FR2265996A1 FR 2265996 A1 FR2265996 A1 FR 2265996A1 FR 7509137 A FR7509137 A FR 7509137A FR 7509137 A FR7509137 A FR 7509137A FR 2265996 A1 FR2265996 A1 FR 2265996A1
Authority
FR
France
Prior art keywords
nozzle
flow
annular
produces
jet engine
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.)
Granted
Application number
FR7509137A
Other languages
English (en)
French (fr)
Other versions
FR2265996B3 (enrdf_load_stackoverflow
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/fr
Application granted granted Critical
Publication of FR2265996B3 publication Critical patent/FR2265996B3/fr
Granted 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
    • F02K3/06—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 front fan
    • 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
    • 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)
  • 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 true FR2265996A1 (en) 1975-10-24
FR2265996B3 FR2265996B3 (enrdf_load_stackoverflow) 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 (enrdf_load_stackoverflow)
DE (1) DE2512082A1 (enrdf_load_stackoverflow)
FR (1) FR2265996A1 (enrdf_load_stackoverflow)
IT (1) IT1037141B (enrdf_load_stackoverflow)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2477100A1 (fr) * 1980-03-03 1981-09-04 Gen Electric Systeme d'ejection d'air de dilution de moteur a turbosoufflante
FR2993861A1 (fr) * 2012-07-27 2014-01-31 Snecma Ensemble turboreacteur et capotage du pylone de fixation a la voilure d'un aeronef

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT325898B (de) * 1971-09-29 1975-11-10 List Hans Schalldammend gekapselte brennkraftmaschine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2477100A1 (fr) * 1980-03-03 1981-09-04 Gen Electric Systeme d'ejection d'air de dilution de moteur a turbosoufflante
FR2993861A1 (fr) * 2012-07-27 2014-01-31 Snecma Ensemble turboreacteur et capotage du pylone de fixation a la voilure d'un aeronef

Also Published As

Publication number Publication date
JPS50129813A (enrdf_load_stackoverflow) 1975-10-14
FR2265996B3 (enrdf_load_stackoverflow) 1977-11-25
IT1037141B (it) 1979-11-10
DE2512082A1 (de) 1975-10-09

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Legal Events

Date Code Title Description
ST Notification of lapse