ES2082224T3 - Una tobera axisimetrica con aro de control sincronizado suspendido. - Google Patents

Una tobera axisimetrica con aro de control sincronizado suspendido.

Info

Publication number
ES2082224T3
ES2082224T3 ES91915379T ES91915379T ES2082224T3 ES 2082224 T3 ES2082224 T3 ES 2082224T3 ES 91915379 T ES91915379 T ES 91915379T ES 91915379 T ES91915379 T ES 91915379T ES 2082224 T3 ES2082224 T3 ES 2082224T3
Authority
ES
Spain
Prior art keywords
nozzle
axisimetric
suspended
control ring
synchronized control
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
ES91915379T
Other languages
English (en)
Inventor
George H Mclafferty
Edward B Thayer
Jim D Stewart
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of ES2082224T3 publication Critical patent/ES2082224T3/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
    • F02K1/06—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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Exhaust Silencers (AREA)
  • Jet Pumps And Other Pumps (AREA)

Abstract

SE PRESENTA UNA TOBERA DE ESCAPE PARA DIRIGIR EL IMPULSO (10) QUE INCLUYE UNA PLURALIDAD DE ALETAS (16-22) Y OBTURADORES (2428) POSICIONADOS MEDIANTE UN ANILLO DE CONCORDANCIA (52) Y UNAS UNIONES DE ALETA (54-56)
ES91915379T 1990-08-23 1991-07-23 Una tobera axisimetrica con aro de control sincronizado suspendido. Expired - Lifetime ES2082224T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US57194890A 1990-08-23 1990-08-23

Publications (1)

Publication Number Publication Date
ES2082224T3 true ES2082224T3 (es) 1996-03-16

Family

ID=24285717

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91915379T Expired - Lifetime ES2082224T3 (es) 1990-08-23 1991-07-23 Una tobera axisimetrica con aro de control sincronizado suspendido.

Country Status (6)

Country Link
EP (1) EP0544764B1 (es)
KR (1) KR0167796B1 (es)
DK (1) DK0544764T3 (es)
ES (1) ES2082224T3 (es)
IL (1) IL99274A0 (es)
WO (1) WO1992003649A1 (es)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5215256A (en) * 1992-07-16 1993-06-01 Barcza W Kevin Flap hinge arrangement for a convergent/divergent nozzle
US5437411A (en) * 1992-12-14 1995-08-01 General Electric Company Vectoring exhaust nozzle flap and seal positioning apparatus
IL109085A (en) * 1993-04-05 1997-08-14 Gen Electric Nozzle seal assembly with removable baseplate
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.
RU2142571C1 (ru) * 1997-09-22 1999-12-10 Государственное унитарное предприятие "Завод им.В.Я.Климова" ВПК "Мапо" Регулируемое сопло авиационного двигателя с отклоняемым вектором тяги
US6109021A (en) * 1998-07-22 2000-08-29 General Electric Company Vectoring nozzle calibration
US6195981B1 (en) 1998-07-22 2001-03-06 General Electric Company Vectoring nozzle control system
FR2790792B1 (fr) * 1999-03-10 2003-11-14 Klimov Corp Tuyere vectorielle
FR2792367B1 (fr) * 1999-04-15 2002-04-26 Snecma Tuyere d'ejection axisymetrique, convergente divergente a orientation par un anneau guide
FR2792366B1 (fr) * 1999-04-15 2005-08-19 Snecma Tuyere d'ejection axisymetrique, convergente divergente et orientable
ES2224580T3 (es) * 1999-05-13 2005-03-01 Industria De Turbo Propulsores S.A. Mecanismo de control del area de salida en toberas convergente-divergentes.
FR2796422B1 (fr) 1999-07-12 2001-09-07 Snecma Tuyere d'ejection de turboreacteur axisymetrique, convergente divergente a deviation de jet
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
EP3008320B1 (en) * 2013-06-14 2020-07-29 Saab Ab Variable-geometry convergent-divergent exhaust nozzle for a jet engine and method for varying the nozzle
EP3008321B1 (en) * 2013-06-14 2018-11-14 Saab AB Variable exhaust nozzle for a jet engine and method for varying the nozzle
PL247813B1 (pl) * 2023-01-18 2025-09-01 Politechnika Swietokrzyska Układ napędowy bezzałogowego statku powietrznego

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3003312A (en) * 1957-08-19 1961-10-10 Thompson Ramo Wooldridge Inc Exhaust nozzle for jet engines
US3442455A (en) * 1967-07-07 1969-05-06 Gen Motors Corp Jet deflecting nozzle
US4128208A (en) * 1977-07-11 1978-12-05 General Electric Company Exhaust nozzle flap seal arrangement
US4994660A (en) * 1989-04-11 1991-02-19 Hitachi, Ltd. Axisymmetric vectoring exhaust nozzle

Also Published As

Publication number Publication date
KR930701689A (ko) 1993-06-12
EP0544764A1 (en) 1993-06-09
WO1992003649A1 (en) 1992-03-05
KR0167796B1 (ko) 1998-12-15
DK0544764T3 (da) 1995-12-11
IL99274A0 (en) 1992-07-15
EP0544764B1 (en) 1995-11-08

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