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FR1283690A - Aircraft propulsion reactor - Google Patents

Aircraft propulsion reactor

Info

Publication number
FR1283690A
FR1283690A FR855638A FR855638A FR1283690A FR 1283690 A FR1283690 A FR 1283690A FR 855638 A FR855638 A FR 855638A FR 855638 A FR855638 A FR 855638A FR 1283690 A FR1283690 A FR 1283690A
Authority
FR
France
Prior art keywords
aircraft propulsion
propulsion reactor
reactor
aircraft
propulsion
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
FR855638A
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.)
B M W TRIEBWERKBAU GmbH
Original Assignee
B M W TRIEBWERKBAU GmbH
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 B M W TRIEBWERKBAU GmbH filed Critical B M W TRIEBWERKBAU GmbH
Priority to FR855638A priority Critical patent/FR1283690A/en
Application granted granted Critical
Publication of FR1283690A publication Critical patent/FR1283690A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR855638A 1961-03-15 1961-03-15 Aircraft propulsion reactor Expired FR1283690A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR855638A FR1283690A (en) 1961-03-15 1961-03-15 Aircraft propulsion reactor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR855638A FR1283690A (en) 1961-03-15 1961-03-15 Aircraft propulsion reactor

Publications (1)

Publication Number Publication Date
FR1283690A true FR1283690A (en) 1962-02-02

Family

ID=8750861

Family Applications (1)

Application Number Title Priority Date Filing Date
FR855638A Expired FR1283690A (en) 1961-03-15 1961-03-15 Aircraft propulsion reactor

Country Status (1)

Country Link
FR (1) FR1283690A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1245750B (en) * 1963-10-28 1967-07-27 Rolls Royce Twin-flow gas turbine jet engine with gas and air deflectors
US3833187A (en) * 1973-05-11 1974-09-03 Boeing Co Thrust control apparatus for pod mounted engine
FR2309728A1 (en) * 1975-04-28 1976-11-26 Gen Electric MANEUVERABLE IN-FLIGHT EJECTION TUBE FOR GAS TURBINE ENGINE
US4000610A (en) * 1975-04-28 1977-01-04 General Electric Company Flight maneuverable nozzle for gas turbine engines
US4587804A (en) * 1983-01-31 1986-05-13 Fuji Jukogyo Kabushiki Kaisha Device for increasing and deflecting thrust of jet-propulsion engine of V/STOL aircraft
RU2193680C2 (en) * 2001-01-03 2002-11-27 Открытое акционерное общество "Авиадвигатель" Adjustable flat nozzle for gas turbine engine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1245750B (en) * 1963-10-28 1967-07-27 Rolls Royce Twin-flow gas turbine jet engine with gas and air deflectors
US3833187A (en) * 1973-05-11 1974-09-03 Boeing Co Thrust control apparatus for pod mounted engine
FR2309728A1 (en) * 1975-04-28 1976-11-26 Gen Electric MANEUVERABLE IN-FLIGHT EJECTION TUBE FOR GAS TURBINE ENGINE
US4000610A (en) * 1975-04-28 1977-01-04 General Electric Company Flight maneuverable nozzle for gas turbine engines
US4587804A (en) * 1983-01-31 1986-05-13 Fuji Jukogyo Kabushiki Kaisha Device for increasing and deflecting thrust of jet-propulsion engine of V/STOL aircraft
RU2193680C2 (en) * 2001-01-03 2002-11-27 Открытое акционерное общество "Авиадвигатель" Adjustable flat nozzle for gas turbine engine

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