GB1293868A - An arrangement for controlling and supporting a variable-geometry duct - Google Patents

An arrangement for controlling and supporting a variable-geometry duct

Info

Publication number
GB1293868A
GB1293868A GB31562/70A GB3156270A GB1293868A GB 1293868 A GB1293868 A GB 1293868A GB 31562/70 A GB31562/70 A GB 31562/70A GB 3156270 A GB3156270 A GB 3156270A GB 1293868 A GB1293868 A GB 1293868A
Authority
GB
United Kingdom
Prior art keywords
flaps
pivotally connected
nozzle
links
casing
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
GB31562/70A
Other languages
English (en)
Inventor
Andre Alphonse Med Camboulives
Jean-Claude Lucien Delonge
Roger Alfred Jul Vandenbroucke
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
Publication of GB1293868A publication Critical patent/GB1293868A/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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Nozzles (AREA)
  • Supercharger (AREA)
GB31562/70A 1969-07-03 1970-06-30 An arrangement for controlling and supporting a variable-geometry duct Expired GB1293868A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR6922624A FR2030532A5 (enExample) 1969-07-03 1969-07-03

Publications (1)

Publication Number Publication Date
GB1293868A true GB1293868A (en) 1972-10-25

Family

ID=9036896

Family Applications (1)

Application Number Title Priority Date Filing Date
GB31562/70A Expired GB1293868A (en) 1969-07-03 1970-06-30 An arrangement for controlling and supporting a variable-geometry duct

Country Status (3)

Country Link
US (1) US3612106A (enExample)
FR (1) FR2030532A5 (enExample)
GB (1) GB1293868A (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2168047C1 (ru) * 1999-10-11 2001-05-27 Государственное унитарное предприятие "Завод имени В.Я. Климова" - дочернее предприятие государственного унитарного предприятия Военно-промышленный комплекс "МАПО" Сопло с отклоняемым вектором тяги
RU2378522C2 (ru) * 2004-10-29 2010-01-10 Снекма Сопло переменного сечения турбомашины и турбомашина, содержащая такое сопло
RU2773171C1 (ru) * 2021-07-20 2022-05-31 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Регулируемое сопло турбореактивного двигателя

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA961652A (en) * 1971-12-20 1975-01-28 Richard E. Teagle Balanced flap converging/diverging nozzle
FR2202234B2 (enExample) * 1972-10-06 1976-03-26 Snecma
FR2244917B2 (enExample) * 1973-09-21 1978-01-13 Snecma
US4030687A (en) * 1976-02-23 1977-06-21 The Boeing Company Articulated nozzle for upper surface blown aircraft
FR2474592A1 (fr) * 1980-01-25 1981-07-31 Snecma Dispositif de tuyere de turboreacteur
US4398415A (en) * 1981-12-10 1983-08-16 The United States Of America As Represented By The Secretary Of The Air Force Swing link flexible wind tunnel nozzle
FR2714422A1 (fr) * 1983-01-13 1995-06-30 Snecma Tuyère convergente-divergente, en particulier pour turboréacteur.
FR2732408A1 (fr) * 1983-03-16 1996-10-04 Snecma Tuyere, en particulier pour turboreacteur
FR2557211A1 (fr) * 1983-12-21 1985-06-28 Camboulives Andre Ensemble d'ejection, en particulier pour turboreacteur
FR2617910A1 (fr) * 1987-07-08 1989-01-13 Snecma Tuyere axisymetrique de turboreacteur convergente divergente
FR2723764B1 (fr) * 1994-08-18 1996-12-20 Snecma Etancheite entre volets suiveurs divergents et convergents d'une tuyere d'ejection de turboreacteur
ES2156350T3 (es) * 1997-01-17 2001-06-16 Turbo Propulsores Ind Disposicion de petalos divergentes para tobera convergente-divergente de motor de aviacion.
AU2001281223A1 (en) * 2000-08-10 2002-02-25 Halton Company, Inc. Flow-volume control device
US20110005507A9 (en) * 2001-01-23 2011-01-13 Rick Bagwell Real-time control of exhaust flow
CA2573955C (en) 2004-07-23 2013-12-17 Halton Company Improvements for control of exhaust systems
FR2875853B1 (fr) * 2004-09-29 2006-12-22 Snecma Moteurs Sa Turboreacteur avec une tuyere a section variable dont chaque volet pivote autour d'un axe, axes pour les volets
FR2877052B1 (fr) * 2004-10-26 2007-04-20 Snecma Moteurs Sa Tuyere a section variable de turbomachine a support de levier de commande monobloc
US7475548B2 (en) 2005-09-09 2009-01-13 General Electric Company Vectorable nozzle with pivotable triangular panels
EP1927745B1 (en) * 2006-11-29 2012-08-01 General Electric Company Vectorable nozzle with pivotable triangular panels
US20080274683A1 (en) 2007-05-04 2008-11-06 Current Energy Controls, Lp Autonomous Ventilation System
US20090061752A1 (en) 2007-08-28 2009-03-05 Current Energy Controls, Lp Autonomous Ventilation System
US9494324B2 (en) 2008-12-03 2016-11-15 Oy Halton Group Ltd. Exhaust flow control system and method
KR101842235B1 (ko) * 2012-02-09 2018-03-27 무그 인코포레이티드 액츄에이터 시스템 및 방법
US9086125B2 (en) * 2013-03-15 2015-07-21 Moog Inc. Rotary actuator
KR102680123B1 (ko) 2016-01-13 2024-07-02 무그 인코포레이티드 합산 및 결함 허용성 로터리 액추에이터 어셈블리
DE102017104043A1 (de) * 2017-02-27 2018-08-30 Rolls-Royce Deutschland Ltd & Co Kg Konvergent-divergente Schubdüse für ein Turbofan-Triebwerk eines Überschallflugzeugs und Verfahren zur Reduzierung des Heckwiderstands hinter einer solchen Schubdüse

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2779157A (en) * 1951-02-14 1957-01-29 Rohr Aircraft Corp Nozzle with variable discharge orifice
US2939274A (en) * 1954-01-04 1960-06-07 North American Aviation Inc Means for varying a jet engine orifice
US2972226A (en) * 1955-10-06 1961-02-21 United Aircraft Corp Variable area converging-diverging nozzle
FR1562941A (enExample) * 1968-01-19 1969-04-11

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2168047C1 (ru) * 1999-10-11 2001-05-27 Государственное унитарное предприятие "Завод имени В.Я. Климова" - дочернее предприятие государственного унитарного предприятия Военно-промышленный комплекс "МАПО" Сопло с отклоняемым вектором тяги
RU2378522C2 (ru) * 2004-10-29 2010-01-10 Снекма Сопло переменного сечения турбомашины и турбомашина, содержащая такое сопло
RU2774567C1 (ru) * 2021-07-02 2022-06-21 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Регулируемое сопло турбореактивного двигателя
RU2773171C1 (ru) * 2021-07-20 2022-05-31 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Регулируемое сопло турбореактивного двигателя

Also Published As

Publication number Publication date
US3612106A (en) 1971-10-12
DE2033114B2 (de) 1976-08-05
DE2033114A1 (de) 1971-02-11
FR2030532A5 (enExample) 1970-11-13

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee