FR1233323A - Dispositif d'actionnement pour tuyères à section variable d'avions à réaction - Google Patents

Dispositif d'actionnement pour tuyères à section variable d'avions à réaction

Info

Publication number
FR1233323A
FR1233323A FR802764A FR802764A FR1233323A FR 1233323 A FR1233323 A FR 1233323A FR 802764 A FR802764 A FR 802764A FR 802764 A FR802764 A FR 802764A FR 1233323 A FR1233323 A FR 1233323A
Authority
FR
France
Prior art keywords
actuator
variable area
area nozzles
jet airplanes
airplanes
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
FR802764A
Other languages
English (en)
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.)
MAJESTE LA REINE DE DROIT DU C
Original Assignee
MAJESTE LA REINE DE DROIT DU C
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 MAJESTE LA REINE DE DROIT DU C filed Critical MAJESTE LA REINE DE DROIT DU C
Application granted granted Critical
Publication of FR1233323A publication Critical patent/FR1233323A/fr
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
    • F02K1/1223—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series
    • 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
    • F02K1/1269—Varying effective area of jet pipe or nozzle by means of pivoted flaps of three series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the internal downstream series having its flaps hinged at their downstream ends on the downstream ends of the flaps of the external downstream series hinged on a fixed structure at their upstream ends
    • Y—GENERAL 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/20—Control lever and linkage systems
    • Y10T74/20576—Elements
    • Y10T74/20582—Levers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
FR802764A 1958-08-25 1959-08-13 Dispositif d'actionnement pour tuyères à section variable d'avions à réaction Expired FR1233323A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US756933A US2926491A (en) 1958-08-25 1958-08-25 Actuating means for variable nozzles

Publications (1)

Publication Number Publication Date
FR1233323A true FR1233323A (fr) 1960-10-12

Family

ID=25045666

Family Applications (1)

Application Number Title Priority Date Filing Date
FR802764A Expired FR1233323A (fr) 1958-08-25 1959-08-13 Dispositif d'actionnement pour tuyères à section variable d'avions à réaction

Country Status (2)

Country Link
US (1) US2926491A (fr)
FR (1) FR1233323A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1214942B (de) * 1960-11-28 1966-04-21 Rolls Royce Schubduesenanordnung fuer Flugzeugstrahltrieb-werke
DE1245646B (de) * 1961-07-28 1967-07-27 Rolls Royce Schubduesenanordnung fuer Strahltriebwerke

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3062003A (en) * 1959-04-06 1962-11-06 United Aircraft Corp Variable area exhaust nozzle
US3095695A (en) * 1959-11-23 1963-07-02 Gen Motors Corp Convergent-divergent jet nozzle
US3032982A (en) * 1960-10-04 1962-05-08 Gen Motors Corp Tilting jet nozzle
US3214904A (en) * 1960-11-28 1965-11-02 Gen Electric Variable area convergent-divergent nozzle and actuation system therefor
US3214905A (en) * 1960-11-28 1965-11-02 Gen Electric Variable area convergent-divergent nozzle
US3229457A (en) * 1962-10-15 1966-01-18 James R Rowe Variable area ratio rocket nozzle
US3243126A (en) * 1963-09-18 1966-03-29 United Aircraft Corp Variable area exhaust nozzle
GB1073278A (en) * 1965-03-15 1967-06-21 Rolls Royce Improvements in or relating to propulsion nozzles
US3367579A (en) * 1965-12-08 1968-02-06 Air Force Usa Supersonic convergent-divergent jet exhaust nozzle
US3398896A (en) * 1965-12-30 1968-08-27 Air Force Usa Supersionic convergent-divergent jet exhaust nozzles
US3467312A (en) * 1966-02-10 1969-09-16 Gen Electric Ejector nozzle
US3426974A (en) * 1967-04-07 1969-02-11 United Aircraft Corp Variable area nozzle synchronous hinge
US3519207A (en) * 1968-09-20 1970-07-07 United Aircraft Corp Nozzle actuation system
US3527409A (en) * 1968-10-11 1970-09-08 United Aircraft Corp Ejector shroud system
US4176792A (en) * 1977-07-11 1979-12-04 General Electric Company Variable area exhaust nozzle
US4245787A (en) * 1978-12-01 1981-01-20 General Electric Company Variable area nozzle system
US5235808A (en) * 1990-02-12 1993-08-17 General Electric Company Exhaust nozzle including idle thrust spoiling
US5140809A (en) * 1990-02-12 1992-08-25 General Electric Company Exhaust nozzle idle thrust spoiling method
US5120005A (en) * 1990-09-14 1992-06-09 General Electric Company Exhaust flap speedbrake
US5150839A (en) * 1991-03-14 1992-09-29 General Electric Company Nozzle load management
FR2924411B1 (fr) * 2007-11-29 2010-02-12 Astrium Sas Dispositif d'arriere corps d'engin spatial

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB782494A (en) * 1954-03-26 1957-09-11 Rolls Royce Improvements in or relating to jet propulsion nozzle arrangements
GB774592A (en) * 1954-05-18 1957-05-15 Havilland Engine Co Ltd Adjustable propulsion nozzles

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1214942B (de) * 1960-11-28 1966-04-21 Rolls Royce Schubduesenanordnung fuer Flugzeugstrahltrieb-werke
DE1245646B (de) * 1961-07-28 1967-07-27 Rolls Royce Schubduesenanordnung fuer Strahltriebwerke

Also Published As

Publication number Publication date
US2926491A (en) 1960-03-01

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