DE60012606D1 - Allseitig schwenkbare konvergente - divergente Schubdüse - Google Patents

Allseitig schwenkbare konvergente - divergente Schubdüse

Info

Publication number
DE60012606D1
DE60012606D1 DE60012606T DE60012606T DE60012606D1 DE 60012606 D1 DE60012606 D1 DE 60012606D1 DE 60012606 T DE60012606 T DE 60012606T DE 60012606 T DE60012606 T DE 60012606T DE 60012606 D1 DE60012606 D1 DE 60012606D1
Authority
DE
Germany
Prior art keywords
convergent
thrust nozzle
swiveling
round
divergent thrust
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 - Fee Related
Application number
DE60012606T
Other languages
English (en)
Other versions
DE60012606T2 (de
Inventor
Didier Georges Feder
Guy Jean-Louis Lapergue
Bertrand Pierre Renau Monville
Laurent Claude Patr Salperwyck
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
SNECMA Moteurs SA
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 Moteurs SA filed Critical SNECMA Moteurs SA
Application granted granted Critical
Publication of DE60012606D1 publication Critical patent/DE60012606D1/de
Publication of DE60012606T2 publication Critical patent/DE60012606T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K1/002—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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1292—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, the internal downstream series having its flaps hinged at their upstream ends on the downstream ends of the flaps of the upstream series and at their downstream ends on the downstream ends of the flaps of the external downstream series 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
    • F02K1/06—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)
  • Joints Allowing Movement (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Details Or Accessories Of Spraying Plant Or Apparatus (AREA)
DE60012606T 1999-04-15 2000-04-13 Allseitig schwenkbare konvergente - divergente Schubdüse Expired - Fee Related DE60012606T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9904709 1999-04-15
FR9904709A FR2792366B1 (fr) 1999-04-15 1999-04-15 Tuyere d'ejection axisymetrique, convergente divergente et orientable

Publications (2)

Publication Number Publication Date
DE60012606D1 true DE60012606D1 (de) 2004-09-09
DE60012606T2 DE60012606T2 (de) 2005-08-04

Family

ID=9544421

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60012606T Expired - Fee Related DE60012606T2 (de) 1999-04-15 2000-04-13 Allseitig schwenkbare konvergente - divergente Schubdüse

Country Status (8)

Country Link
US (1) US6375095B1 (de)
EP (1) EP1045129B1 (de)
JP (1) JP2000310159A (de)
CA (1) CA2305023A1 (de)
DE (1) DE60012606T2 (de)
ES (1) ES2222159T3 (de)
FR (1) FR2792366B1 (de)
RU (1) RU2184260C2 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4770086B2 (ja) * 2001-08-08 2011-09-07 株式会社Ｉｈｉ 排気ノズル駆動装置
US9650991B2 (en) * 2013-06-27 2017-05-16 The Boeing Company Pivoting ring petal actuation for variable area fan nozzle
GB201621331D0 (en) * 2016-12-15 2017-02-01 Rolls Royce Plc A Nozzle
CN108104974B (zh) * 2017-12-14 2020-03-17 中国航发沈阳发动机研究所 一种二元矢量喷管结构及具有其的飞机
GB2588651A (en) 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
GB2588653A (en) 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
GB2588652A (en) 2019-10-31 2021-05-05 Rolls Royce Plc An exhaust nozzle
CN114109648B (zh) * 2021-11-12 2023-02-28 中国航发沈阳发动机研究所 一种可调喷管外罩机构
CN114251188B (zh) * 2021-12-22 2023-04-07 北京航空航天大学 一种基于自适应变循环发动机的喷管结构及其操作方法
CN114893321B (zh) * 2022-03-31 2024-05-07 南京航空航天大学 一种自适应变循环发动机轴对称排气结构
CN117469698A (zh) 2022-07-21 2024-01-30 通用电气公司 燃烧衬里的性能因数

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1025827A (fr) * 1950-10-11 1953-04-20 Perfectionnement apporté aux engins aériens à réaction
GB1306588A (en) * 1969-12-23 1973-02-14 Messerschmitt Boelkow Blohm Nozzle assembly for jet propulsion engines
FR2501786A1 (fr) * 1981-03-13 1982-09-17 Snecma Dispositif de roulement et de guidage d'une tuyere orientable de propulseur a reaction
US4984741A (en) * 1987-02-26 1991-01-15 Rolls-Royce Inc. Vectorable variable flow area propulsion nozzle
ES2082224T3 (es) * 1990-08-23 1996-03-16 United Technologies Corp Una tobera axisimetrica con aro de control sincronizado suspendido.
US5150839A (en) * 1991-03-14 1992-09-29 General Electric Company Nozzle load management
US5239815A (en) * 1991-09-23 1993-08-31 United Technologies Corporation Sync-ring assembly for a gas turbine engine exhaust nozzle
ES2075782B1 (es) * 1992-02-20 1998-03-16 Sener Ing & Sist Tobera orientable de geometria variable para turbinas de gas.
US5511376A (en) 1993-08-31 1996-04-30 United Technologies Corporation Axisymmetric vectoring nozzle
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
US6199772B1 (en) * 1999-08-25 2001-03-13 General Electric Company Linear actuation and vectoring ring support mechanism for axisymmetric vectoring nozzle

Also Published As

Publication number Publication date
DE60012606T2 (de) 2005-08-04
CA2305023A1 (fr) 2000-10-15
FR2792366A1 (fr) 2000-10-20
FR2792366B1 (fr) 2005-08-19
ES2222159T3 (es) 2005-02-01
JP2000310159A (ja) 2000-11-07
US6375095B1 (en) 2002-04-23
EP1045129B1 (de) 2004-08-04
EP1045129A1 (de) 2000-10-18
RU2184260C2 (ru) 2002-06-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee