DE2512082A1 - Gasturbinenstrahltriebwerk - Google Patents

Gasturbinenstrahltriebwerk

Info

Publication number
DE2512082A1
DE2512082A1 DE19752512082 DE2512082A DE2512082A1 DE 2512082 A1 DE2512082 A1 DE 2512082A1 DE 19752512082 DE19752512082 DE 19752512082 DE 2512082 A DE2512082 A DE 2512082A DE 2512082 A1 DE2512082 A1 DE 2512082A1
Authority
DE
Germany
Prior art keywords
nozzle
flow
fan
engine
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.)
Pending
Application number
DE19752512082
Other languages
German (de)
English (en)
Inventor
Norman Roberts
Fredrick William Stanhope
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 1971 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 Rolls Royce 1971 Ltd filed Critical Rolls Royce 1971 Ltd
Publication of DE2512082A1 publication Critical patent/DE2512082A1/de
Pending 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)
DE19752512082 1974-03-26 1975-03-19 Gasturbinenstrahltriebwerk Pending DE2512082A1 (de)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
DE2512082A1 true DE2512082A1 (de) 1975-10-09

Family

ID=10019199

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19752512082 Pending DE2512082A1 (de) 1974-03-26 1975-03-19 Gasturbinenstrahltriebwerk

Country Status (4)

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

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 (fr) * 2012-07-27 2015-07-31 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

Also Published As

Publication number Publication date
IT1037141B (it) 1979-11-10
FR2265996B3 (enrdf_load_html_response) 1977-11-25
FR2265996A1 (en) 1975-10-24
JPS50129813A (enrdf_load_html_response) 1975-10-14

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