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FR1326989A - Improvements to turbojets - Google Patents

Improvements to turbojets

Info

Publication number
FR1326989A
FR1326989A FR902462A FR902462A FR1326989A FR 1326989 A FR1326989 A FR 1326989A FR 902462 A FR902462 A FR 902462A FR 902462 A FR902462 A FR 902462A FR 1326989 A FR1326989 A FR 1326989A
Authority
FR
France
Prior art keywords
turbojets
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
FR902462A
Other languages
French (fr)
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.)
Bristol Siddeley Engines Ltd
Original Assignee
De Havilland Engine Co 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 De Havilland Engine Co Ltd filed Critical De Havilland Engine Co Ltd
Priority to FR902462A priority Critical patent/FR1326989A/en
Application granted granted Critical
Publication of FR1326989A publication Critical patent/FR1326989A/en
Expired 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR902462A 1962-06-29 1962-06-29 Improvements to turbojets Expired FR1326989A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR902462A FR1326989A (en) 1962-06-29 1962-06-29 Improvements to turbojets

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR902462A FR1326989A (en) 1962-06-29 1962-06-29 Improvements to turbojets

Publications (1)

Publication Number Publication Date
FR1326989A true FR1326989A (en) 1963-05-10

Family

ID=8782167

Family Applications (1)

Application Number Title Priority Date Filing Date
FR902462A Expired FR1326989A (en) 1962-06-29 1962-06-29 Improvements to turbojets

Country Status (1)

Country Link
FR (1) FR1326989A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1227286B (en) * 1963-07-05 1966-10-20 Rolls Royce Engine, especially for hover vehicles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1227286B (en) * 1963-07-05 1966-10-20 Rolls Royce Engine, especially for hover vehicles

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