FR1147262A - Jet control device of a jet thruster - Google Patents

Jet control device of a jet thruster

Info

Publication number
FR1147262A
FR1147262A FR1147262DA FR1147262A FR 1147262 A FR1147262 A FR 1147262A FR 1147262D A FR1147262D A FR 1147262DA FR 1147262 A FR1147262 A FR 1147262A
Authority
FR
France
Prior art keywords
jet
control device
thruster
jet control
jet thruster
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
Other languages
French (fr)
Inventor
Jacques-Louis Drouet
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1147262A publication Critical patent/FR1147262A/en
Expired 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
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
    • 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
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/008—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector in any rearward direction
FR1147262D 1955-04-05 1955-04-05 Jet control device of a jet thruster Expired FR1147262A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1147262T 1955-04-05

Publications (1)

Publication Number Publication Date
FR1147262A true FR1147262A (en) 1957-11-21

Family

ID=9645790

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1147262D Expired FR1147262A (en) 1955-04-05 1955-04-05 Jet control device of a jet thruster

Country Status (1)

Country Link
FR (1) FR1147262A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3016700A (en) * 1958-07-07 1962-01-16 Curtiss Wright Corp Thrust reverser for jet engines
US3039264A (en) * 1959-09-22 1962-06-19 Dale S Ernest Shrouded nozzle
FR2310471A1 (en) * 1976-04-12 1976-12-03 Rolls Royce TURBOMACHINE PIPE TRAINING
FR2537657A1 (en) * 1982-12-08 1984-06-15 Snecma TUYERE A VARIABLE SECTION FOR A TURBOJET ENGINE AND AIRCRAFT COMPRISING SUCH AN EQUIPMENT
EP1900909A2 (en) 2006-09-14 2008-03-19 Rolls-Royce plc Variable area nozzle in a gas turbine engine
WO2017064422A1 (en) * 2015-10-13 2017-04-20 Safran Nacelles Variable cross-section nozzle for an aircraft nacelle and nacelle for an aircraft turbojet engine comprising such a nozzle

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3016700A (en) * 1958-07-07 1962-01-16 Curtiss Wright Corp Thrust reverser for jet engines
US3039264A (en) * 1959-09-22 1962-06-19 Dale S Ernest Shrouded nozzle
FR2310471A1 (en) * 1976-04-12 1976-12-03 Rolls Royce TURBOMACHINE PIPE TRAINING
FR2537657A1 (en) * 1982-12-08 1984-06-15 Snecma TUYERE A VARIABLE SECTION FOR A TURBOJET ENGINE AND AIRCRAFT COMPRISING SUCH AN EQUIPMENT
EP0111436A1 (en) * 1982-12-08 1984-06-20 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Variable area nozzle for a turbo reactor, and aircraft comprising such an equipment
US4577814A (en) * 1982-12-08 1986-03-25 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Variable section nozzle for a turbo-jet engine and an aircraft comprising such equipment
EP1900909A2 (en) 2006-09-14 2008-03-19 Rolls-Royce plc Variable area nozzle in a gas turbine engine
EP1900909A3 (en) * 2006-09-14 2013-03-06 Rolls-Royce plc Variable area nozzle in a gas turbine engine
WO2017064422A1 (en) * 2015-10-13 2017-04-20 Safran Nacelles Variable cross-section nozzle for an aircraft nacelle and nacelle for an aircraft turbojet engine comprising such a nozzle
US20180230949A1 (en) * 2015-10-13 2018-08-16 Safran Nacelles Variable section nozzle for aircraft nacelle and nacelle for an aircraft turbojet engine including such a nozzle

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