ES2105928B1 - Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas. - Google Patents

Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas.

Info

Publication number
ES2105928B1
ES2105928B1 ES09301991A ES9301991A ES2105928B1 ES 2105928 B1 ES2105928 B1 ES 2105928B1 ES 09301991 A ES09301991 A ES 09301991A ES 9301991 A ES9301991 A ES 9301991A ES 2105928 B1 ES2105928 B1 ES 2105928B1
Authority
ES
Spain
Prior art keywords
gas turbine
variable geometry
master petal
petal
divergent master
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
ES09301991A
Other languages
English (en)
Other versions
ES2105928A1 (es
Inventor
Urruela Jose Rivacoba
Mendia Jose Ignacio Ibarreche
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.)
Sener Ingenieria y Sistemas SA
Original Assignee
Sener Ingenieria y Sistemas 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 Sener Ingenieria y Sistemas SA filed Critical Sener Ingenieria y Sistemas SA
Priority to ES09301991A priority Critical patent/ES2105928B1/es
Priority to US08/232,706 priority patent/US5513799A/en
Priority to CA002122537A priority patent/CA2122537C/en
Priority to EP94500103A priority patent/EP0644325B1/en
Priority to DE69401254T priority patent/DE69401254T2/de
Publication of ES2105928A1 publication Critical patent/ES2105928A1/es
Application granted granted Critical
Publication of ES2105928B1 publication Critical patent/ES2105928B1/es
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
    • F02K1/78—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
    • F02K1/002—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
    • 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

Abstract

PETALO MAESTRO DIVERGENTE PARA TOBERAS ORIENTABLES DE GEOMETRIA VARIABLE DESTINADAS A PROPULSORES DE TURBINA DE GAS, QUE VA VINCULADO POR MEDIO DE ARTICULACIONES AL PETALO MAESTRO CONVERGENTE (4) Y A LA BARRA (12) QUE RELACIONA DICHO PETALO MAESTRO CON EL MECANISMO DE GOBIERNO. LA SUPERFICIE INTERIOR (5C) DEL PETALO MAESTRO DIVERGENTE (5), EN CONTACTO CON EL FLUJO DE GASES, ES DE FORMA VARIABLE ENTRE UNA SECCION TRANSVERSA PRACTICAMENTE RECTA, COINCIDENTE O PROXIMA AL BORDE TRANSVERSA EXTREMO AGUAS ARRIBA, Y UNA SECCION TRANSVERSAL CURVA, COINCIDENTE O PROXIMA A SU BORDE TRANSVERSAL EXTREMO AGUAS ABAJO, CON LA CONVEXIDAD DIRIGIDA HACIA EL INTERIOR DEL PROPULSOR.
ES09301991A 1993-09-21 1993-09-21 Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas. Expired - Fee Related ES2105928B1 (es)

Priority Applications (5)

Application Number Priority Date Filing Date Title
ES09301991A ES2105928B1 (es) 1993-09-21 1993-09-21 Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas.
US08/232,706 US5513799A (en) 1993-09-21 1994-04-25 Divergent master petal for orientable nozzles of variable geometry intended for gas turbine engines
CA002122537A CA2122537C (en) 1993-09-21 1994-04-29 Divergent master petal for orientable nozzles of variable geometry intended for gas turbine engines
EP94500103A EP0644325B1 (en) 1993-09-21 1994-06-08 Exhaust nozzle for a gas turbine
DE69401254T DE69401254T2 (de) 1993-09-21 1994-06-08 Abgasdüse für eine Gasturbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES09301991A ES2105928B1 (es) 1993-09-21 1993-09-21 Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas.

Publications (2)

Publication Number Publication Date
ES2105928A1 ES2105928A1 (es) 1997-10-16
ES2105928B1 true ES2105928B1 (es) 1998-05-01

Family

ID=8283098

Family Applications (1)

Application Number Title Priority Date Filing Date
ES09301991A Expired - Fee Related ES2105928B1 (es) 1993-09-21 1993-09-21 Petalo maestro divergente para toberas orientables de geometria variable destinadas a propulsores de turbina de gas.

Country Status (5)

Country Link
US (1) US5513799A (es)
EP (1) EP0644325B1 (es)
CA (1) CA2122537C (es)
DE (1) DE69401254T2 (es)
ES (1) ES2105928B1 (es)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69704479T2 (de) * 1997-01-17 2001-10-18 Turbo Propulsores Ind Dichtungsklappe für eine convergent-divergente Schubdüse
FR2796422B1 (fr) * 1999-07-12 2001-09-07 Snecma Tuyere d'ejection de turboreacteur axisymetrique, convergente divergente a deviation de jet
FR2857414B1 (fr) * 2003-07-08 2007-06-08 Snecma Moteurs Volet souple de tuyere a section variable de turbomachine
US7096661B2 (en) * 2004-03-26 2006-08-29 United Technologies Corporation Axial divergent section slot nozzle

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB557229A (en) * 1942-05-08 1943-11-10 Ibm Improvements in or relating to electrically-conductive inks
GB1466874A (en) * 1974-11-15 1977-03-09 Rolls Royce Gas rurbine engine variable area exhaust nozzle
US4022948A (en) * 1974-12-23 1977-05-10 United Technologies Corporation Resiliently coated metallic finger seals
DE2719439C2 (de) * 1977-04-30 1984-01-19 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Schwenkbare Schubdüse zur Vektorsteuerung
US4128208A (en) * 1977-07-11 1978-12-05 General Electric Company Exhaust nozzle flap seal arrangement
US4171093A (en) * 1977-08-19 1979-10-16 The United States Of America As Represented By The Secretary Of The Air Force Durability flap and seal liner assembly for exhaust nozzles
FR2470253A1 (fr) * 1979-11-23 1981-05-29 Snecma Tuyere orientable pour propulseur a reaction
FR2501786A1 (fr) * 1981-03-13 1982-09-17 Snecma Dispositif de roulement et de guidage d'une tuyere orientable de propulseur a reaction
US4544098A (en) * 1982-12-27 1985-10-01 United Technologies Corporation Cooled exhaust nozzle flaps
US4637550A (en) * 1985-10-01 1987-01-20 The United States Of America As Represented By The Secretary Of The Air Force Dual material exhaust nozzle flap
US5039014A (en) * 1989-04-11 1991-08-13 General Electric Company Axisymmetric vectoring exhaust nozzle seal
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
US5076496A (en) * 1990-02-05 1991-12-31 General Electric Company Exhaust nozzle flap seal
WO1992003649A1 (en) * 1990-08-23 1992-03-05 United Technologies Corporation Axisymmetric nozzle with gimbled unison ring
US5245823A (en) * 1991-09-23 1993-09-21 United Technologies Corporation External flap vectoring mechanism
ES2075782B1 (es) * 1992-02-20 1998-03-16 Sener Ing & Sist Tobera orientable de geometria variable para turbinas de gas.

Also Published As

Publication number Publication date
EP0644325B1 (en) 1996-12-27
DE69401254T2 (de) 1997-07-03
CA2122537C (en) 1999-06-29
CA2122537A1 (en) 1995-03-22
US5513799A (en) 1996-05-07
EP0644325A1 (en) 1995-03-22
ES2105928A1 (es) 1997-10-16
DE69401254D1 (de) 1997-02-06

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