FR2321599A1 - Mecanisme d'entrainement de soufflante de moteur a turbine a gaz - Google Patents

Mecanisme d'entrainement de soufflante de moteur a turbine a gaz

Info

Publication number
FR2321599A1
FR2321599A1 FR7624534A FR7624534A FR2321599A1 FR 2321599 A1 FR2321599 A1 FR 2321599A1 FR 7624534 A FR7624534 A FR 7624534A FR 7624534 A FR7624534 A FR 7624534A FR 2321599 A1 FR2321599 A1 FR 2321599A1
Authority
FR
France
Prior art keywords
turbine
rotor
rotor driving
fan
reduction gear
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.)
Withdrawn
Application number
FR7624534A
Other languages
English (en)
Inventor
Geoffrey Light Wilde
James Alexander Petrie
John Bertram Holliday
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 FR2321599A1 publication Critical patent/FR2321599A1/fr
Withdrawn legal-status Critical Current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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7624534A 1975-08-21 1976-08-11 Mecanisme d'entrainement de soufflante de moteur a turbine a gaz Withdrawn FR2321599A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3473775 1975-08-21

Publications (1)

Publication Number Publication Date
FR2321599A1 true FR2321599A1 (fr) 1977-03-18

Family

ID=10369361

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7624534A Withdrawn FR2321599A1 (fr) 1975-08-21 1976-08-11 Mecanisme d'entrainement de soufflante de moteur a turbine a gaz

Country Status (3)

Country Link
JP (1) JPS5225918A (fr)
DE (1) DE2636338A1 (fr)
FR (1) FR2321599A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL8303401A (nl) * 1982-11-01 1984-06-01 Gen Electric Aandrijfturbine voor tegengesteld draaiende propellers.
FR2961260B1 (fr) * 2010-06-15 2014-05-02 Turbomeca Architecture de turbomoteur non lubrifie

Also Published As

Publication number Publication date
DE2636338A1 (de) 1977-02-24
JPS5225918A (en) 1977-02-26

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Legal Events

Date Code Title Description
ST Notification of lapse