ES2156350T3 - Disposicion de petalos divergentes para tobera convergente-divergente de motor de aviacion. - Google Patents

Disposicion de petalos divergentes para tobera convergente-divergente de motor de aviacion.

Info

Publication number
ES2156350T3
ES2156350T3 ES97500007T ES97500007T ES2156350T3 ES 2156350 T3 ES2156350 T3 ES 2156350T3 ES 97500007 T ES97500007 T ES 97500007T ES 97500007 T ES97500007 T ES 97500007T ES 2156350 T3 ES2156350 T3 ES 2156350T3
Authority
ES
Spain
Prior art keywords
divergent
metal plates
convergent
tower
provision
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 - Lifetime
Application number
ES97500007T
Other languages
English (en)
Inventor
Daniel Ikaza
Luis Martin
Dionisio Silvestre
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.)
Industria de Turbo Propulsores SA
Original Assignee
Industria de Turbo Propulsores 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 Industria de Turbo Propulsores SA filed Critical Industria de Turbo Propulsores SA
Application granted granted Critical
Publication of ES2156350T3 publication Critical patent/ES2156350T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle 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
    • 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
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Electron Sources, Ion Sources (AREA)
  • Toys (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

DISPOSITIVO DE PLACAS METALICAS DIVERGENTES PARA BOQUILLAS CONVERGENTES-DIVERGENTES APLICABLES A MOTORES DE AVION, EN EL QUE LA SECCION DIVERGENTE INCLUYE PLACAS METALICAS DIVERGENTES MAESTRAS (3) Y PLACAS METALICAS DIVERGENTES AUXILIARES (4), QUE INCLUYEN, ESTAS ULTIMAS, UNA SECCION TRANSVERSAL DOBLADA CON EL LADO CONCAVO FRENTE AL GAS, Y QUE PUEDE CONTAR CON UNA SERIE DE SOPORTES COLGANTES (7) COLOCADOS EN LAS PLACAS METALICAS DIVERGENTES AUXILIARES (4) Y GANCHOS (12) EN LOS EXTREMOS DE ESTOS SOPORTES (7), INTERACTUANDO ESTOS GANCHOS CON TOPES (5) DE SOPORTE DISPUESTOS EN LAS PLACAS METALICAS DIVERGENTES MAESTRAS (3), LIMITANDO ASI EL MOVIMIENTO DE LAS PLACAS METALICAS DIVERGENTES AUXILIARES (4).
ES97500007T 1997-01-17 1997-01-17 Disposicion de petalos divergentes para tobera convergente-divergente de motor de aviacion. Expired - Lifetime ES2156350T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP97500007A EP0854282B1 (en) 1997-01-17 1997-01-17 Divergent petal arrangement for a convergent-divergent nozzle

Publications (1)

Publication Number Publication Date
ES2156350T3 true ES2156350T3 (es) 2001-06-16

Family

ID=8230070

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97500007T Expired - Lifetime ES2156350T3 (es) 1997-01-17 1997-01-17 Disposicion de petalos divergentes para tobera convergente-divergente de motor de aviacion.

Country Status (5)

Country Link
US (1) US6148608A (es)
EP (1) EP0854282B1 (es)
CA (1) CA2224534C (es)
DE (1) DE69704479T2 (es)
ES (1) ES2156350T3 (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6935118B2 (en) * 2003-12-19 2005-08-30 General Electric Company Exhaust nozzle segmented basesheet and production method thereof
US7096661B2 (en) * 2004-03-26 2006-08-29 United Technologies Corporation Axial divergent section slot nozzle
FR2873757B1 (fr) * 2004-07-28 2006-09-29 Snecma Moteurs Sa Tuyere convergente de turboreacteur
US7721549B2 (en) * 2007-02-08 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system
US8122722B2 (en) * 2008-02-29 2012-02-28 General Electric Company Exhaust nozzle seal with segmented basesheet disposed between side rails
US8549834B2 (en) 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle
GB201621331D0 (en) * 2016-12-15 2017-02-01 Rolls Royce Plc A Nozzle
CN112682214A (zh) * 2020-12-28 2021-04-20 中国航发沈阳发动机研究所 一种轴对称可调收扩喷管内流道平衡协调结构
CN113530705A (zh) * 2021-08-18 2021-10-22 中国航发贵阳发动机设计研究所 一种航空发动机可调喷管外调节片收放限位装置

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1002116A (en) * 1964-04-24 1965-08-25 Rolls Royce Fluid flow control apparatus
FR2030532A5 (es) * 1969-07-03 1970-11-13 Snecma
GB1533986A (en) * 1976-04-12 1978-11-29 Rolls Royce Nozzles for gas turbine engines
US4128208A (en) * 1977-07-11 1978-12-05 General Electric Company Exhaust nozzle flap seal arrangement
US4544098A (en) * 1982-12-27 1985-10-01 United Technologies Corporation Cooled exhaust nozzle flaps
US5039014A (en) * 1989-04-11 1991-08-13 General Electric Company Axisymmetric vectoring exhaust nozzle seal
US4994660A (en) * 1989-04-11 1991-02-19 Hitachi, Ltd. Axisymmetric vectoring exhaust nozzle
CN1022433C (zh) * 1989-04-11 1993-10-13 通用电气公司 轴线对称转向排气喷口密封装置
US5269467A (en) * 1992-08-03 1993-12-14 General Electric Company Vectoring exhaust nozzle seal and flap retaining apparatus
US5232158A (en) * 1992-08-11 1993-08-03 United Technologies Corporation Convergent/divergent nozzle with seal centering
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.
US5484105A (en) * 1994-07-13 1996-01-16 General Electric Company Cooling system for a divergent section of a nozzle

Also Published As

Publication number Publication date
DE69704479T2 (de) 2001-10-18
EP0854282B1 (en) 2001-04-04
CA2224534C (en) 2005-09-13
CA2224534A1 (en) 1998-07-17
DE69704479D1 (de) 2001-05-10
US6148608A (en) 2000-11-21
EP0854282A1 (en) 1998-07-22

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