ATE325947T1 - Axialsymmetrische konvergent-divergente schubdüse - Google Patents

Axialsymmetrische konvergent-divergente schubdüse

Info

Publication number
ATE325947T1
ATE325947T1 AT00402005T AT00402005T ATE325947T1 AT E325947 T1 ATE325947 T1 AT E325947T1 AT 00402005 T AT00402005 T AT 00402005T AT 00402005 T AT00402005 T AT 00402005T AT E325947 T1 ATE325947 T1 AT E325947T1
Authority
AT
Austria
Prior art keywords
divergent
ring
shutters
convergent
fixed structure
Prior art date
Application number
AT00402005T
Other languages
English (en)
Inventor
Didier Georges Feder
Bertrand Pierre Renau Monville
Daniel Kettler
Jacky Serge Naudet
Guy Jean-Louis Lapergue
Laurent Claude Patr Salperwick
Original Assignee
Snecma
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 Snecma filed Critical Snecma
Application granted granted Critical
Publication of ATE325947T1 publication Critical patent/ATE325947T1/de

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
    • F02K1/002—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
    • 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
    • F02K1/15—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/323—Arrangement of components according to their shape convergent
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/32—Arrangement of components according to their shape
    • F05D2250/324—Arrangement of components according to their shape divergent
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/33—Arrangement of components symmetrical

Landscapes

  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Control Of Turbines (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Supercharger (AREA)
  • Details Or Accessories Of Spraying Plant Or Apparatus (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)
  • Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
  • Earth Drilling (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
AT00402005T 1999-07-12 2000-07-12 Axialsymmetrische konvergent-divergente schubdüse ATE325947T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9908988A FR2796422B1 (fr) 1999-07-12 1999-07-12 Tuyere d'ejection de turboreacteur axisymetrique, convergente divergente a deviation de jet

Publications (1)

Publication Number Publication Date
ATE325947T1 true ATE325947T1 (de) 2006-06-15

Family

ID=9547981

Family Applications (1)

Application Number Title Priority Date Filing Date
AT00402005T ATE325947T1 (de) 1999-07-12 2000-07-12 Axialsymmetrische konvergent-divergente schubdüse

Country Status (10)

Country Link
US (1) US6349539B1 (de)
EP (1) EP1069302B1 (de)
JP (1) JP2001041104A (de)
AT (1) ATE325947T1 (de)
CA (1) CA2314169A1 (de)
DE (1) DE60027822T2 (de)
ES (1) ES2258959T3 (de)
FR (1) FR2796422B1 (de)
RU (1) RU2208693C2 (de)
WO (1) WO2001004484A1 (de)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6622472B2 (en) * 2001-10-17 2003-09-23 Gateway Space Transport, Inc. Apparatus and method for thrust vector control
RU2312244C1 (ru) * 2006-05-17 2007-12-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Способ регулирования сопла с управляемым вектором тяги авиационного газотурбинного двигателя
RU2445486C1 (ru) * 2010-11-26 2012-03-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Плоское сопло турбореактивного двигателя
RU2445487C1 (ru) * 2010-12-02 2012-03-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Плоское сопло турбореактивного двигателя
CN103334850B (zh) * 2013-06-26 2016-02-24 中国航空工业集团公司沈阳发动机设计研究所 一种连杆式二元喷管收敛段控制机构
CN104791131A (zh) * 2015-04-02 2015-07-22 中国航空工业集团公司沈阳发动机设计研究所 一种喉道面积可调的二元塞式喷管
CN104847530B (zh) * 2015-04-02 2017-04-19 中国航空工业集团公司沈阳发动机设计研究所 一种具有反推功能的喷管
CN104787285B (zh) * 2015-04-03 2016-11-30 山东大学（威海） 一种螺旋桨矢量推进装置
CN104963786B (zh) * 2015-07-07 2017-02-01 中国航空工业集团公司沈阳发动机设计研究所 一种收扩调节片的传动控制机构
CN104963787B (zh) * 2015-07-09 2017-04-19 中国航空工业集团公司沈阳发动机设计研究所 一种具有反推功能的二元喷管
CN105865742B (zh) * 2016-04-07 2017-05-31 中国空气动力研究与发展中心低速空气动力研究所 一种风洞试验航发推力矢量喷管转向系统
CN114810414B (zh) * 2022-04-19 2023-09-19 清华大学 矢量调节喷管和自适应变循环发动机

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1562941A (de) * 1968-01-19 1969-04-11
DE2711936C2 (de) * 1977-03-18 1986-02-06 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Schubdüse für Gasturbinenstrahltriebwerke mit variablem Kreisprozeß
FR2501786A1 (fr) * 1981-03-13 1982-09-17 Snecma Dispositif de roulement et de guidage d'une tuyere orientable de propulseur a reaction
RU1563310C (ru) * 1988-04-19 1994-05-15 Акционерное общество "Авиадвигатель" Реверсивное устройство наружного контура турбореактивного двухконтурного двигателя
US5082182A (en) * 1990-08-23 1992-01-21 United Technologies Corporation Thrust vectoring exhaust nozzle
ES2082224T3 (es) 1990-08-23 1996-03-16 United Technologies Corp Una tobera axisimetrica con aro de control sincronizado suspendido.
US5174502A (en) * 1991-05-10 1992-12-29 General Electric Company Support for a translating nozzle vectoring ring
US5239815A (en) 1991-09-23 1993-08-31 United Technologies Corporation Sync-ring assembly for a gas turbine engine exhaust nozzle
ES2105928B1 (es) * 1993-09-21 1998-05-01 Sener Ing & Sist Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas.
ES2136475B1 (es) * 1994-05-20 2000-05-16 Sener Ing & Sist Perfeccionamientos en toberas axisimetricas de geometria variable y orientacion del flujo destinadas a propulsores de turbina de gas.
FR2748778B1 (fr) * 1996-05-15 1998-06-19 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes associees a un panneau amont
ES2136528B1 (es) * 1996-12-26 2000-05-01 Sener Ing & Sist Perfeccionamientos en toberas axisimetricas de geometria variable y orientacion del flujo destinadasa propulsores de turbina de gas
US6212877B1 (en) * 1998-09-04 2001-04-10 General Electric Company Vectoring ring support and actuation mechanism for axisymmetric vectoring nozzle with a universal joint

Also Published As

Publication number Publication date
DE60027822T2 (de) 2006-11-30
FR2796422A1 (fr) 2001-01-19
FR2796422B1 (fr) 2001-09-07
US6349539B1 (en) 2002-02-26
EP1069302B1 (de) 2006-05-10
RU2208693C2 (ru) 2003-07-20
WO2001004484A1 (fr) 2001-01-18
CA2314169A1 (fr) 2001-01-12
ES2258959T3 (es) 2006-09-16
EP1069302A1 (de) 2001-01-17
JP2001041104A (ja) 2001-02-13
DE60027822D1 (de) 2006-06-14

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Legal Events

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