DE602006006628D1 - Konvergente-divergente Düse mit ineinander greifenden divergenten Klappen - Google Patents

Konvergente-divergente Düse mit ineinander greifenden divergenten Klappen

Info

Publication number
DE602006006628D1
DE602006006628D1 DE602006006628T DE602006006628T DE602006006628D1 DE 602006006628 D1 DE602006006628 D1 DE 602006006628D1 DE 602006006628 T DE602006006628 T DE 602006006628T DE 602006006628 T DE602006006628 T DE 602006006628T DE 602006006628 D1 DE602006006628 D1 DE 602006006628D1
Authority
DE
Germany
Prior art keywords
divergent
convergent
interlocking
flaps
nozzle
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.)
Active
Application number
DE602006006628T
Other languages
English (en)
Inventor
Donald William Peters
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.)
Raytheon Technologies 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
Publication of DE602006006628D1 publication Critical patent/DE602006006628D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Exhaust Silencers (AREA)
DE602006006628T 2005-09-20 2006-07-20 Konvergente-divergente Düse mit ineinander greifenden divergenten Klappen Active DE602006006628D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/231,067 US7624567B2 (en) 2005-09-20 2005-09-20 Convergent divergent nozzle with interlocking divergent flaps

Publications (1)

Publication Number Publication Date
DE602006006628D1 true DE602006006628D1 (de) 2009-06-18

Family

ID=37667354

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006006628T Active DE602006006628D1 (de) 2005-09-20 2006-07-20 Konvergente-divergente Düse mit ineinander greifenden divergenten Klappen

Country Status (4)

Country Link
US (1) US7624567B2 (de)
EP (1) EP1764498B1 (de)
JP (1) JP2007085335A (de)
DE (1) DE602006006628D1 (de)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7458221B1 (en) * 2003-10-23 2008-12-02 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Variable area nozzle including a plurality of convexly vanes with a crowned contour, in a vane to vane sealing arrangement and with nonuniform lengths
US20070062199A1 (en) * 2005-09-22 2007-03-22 United Technologies Corporation Turbine engine nozzle
US7624579B2 (en) 2006-02-15 2009-12-01 United Technologies Corporation Convergent divergent nozzle with supported divergent seals
US7721551B2 (en) * 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
GB2448320B (en) * 2007-04-10 2012-04-11 Pericles Pilidis Aircraft engine variable nozzle for silencing and performance enhancement
US7963099B2 (en) * 2007-05-21 2011-06-21 General Electric Company Fluted chevron exhaust nozzle
US7926285B2 (en) 2007-07-18 2011-04-19 General Electric Company Modular chevron exhaust nozzle
US7716932B2 (en) * 2008-07-24 2010-05-18 Spirit Aerosystems, Inc. Dilating fan duct nozzle
US8991191B2 (en) * 2009-11-24 2015-03-31 General Electric Company Thermally actuated passive gas turbine engine compartment venting
US9126374B2 (en) 2010-09-28 2015-09-08 Russell B. Hanson Iso-grid composite component
US8549834B2 (en) 2010-10-21 2013-10-08 United Technologies Corporation Gas turbine engine with variable area fan nozzle
JP5673405B2 (ja) * 2011-07-12 2015-02-18 株式会社Ihi ジェットエンジンの可変排気ノズル
US9810085B2 (en) 2011-08-22 2017-11-07 United Technologies Corporation Flap seal for gas turbine engine movable nozzle flap
US20130232949A1 (en) * 2012-03-09 2013-09-12 Gary J. Dillard Pressure balanced area control of high aspect ratio nozzle
US9163582B2 (en) 2012-05-30 2015-10-20 United Technologies Corporation Convergent-divergent gas turbine nozzle comprising movable flaps having a variable thickness in a lateral direction
US8695540B2 (en) 2012-06-18 2014-04-15 Aerojet Rocketdyne Of De, Inc. Fuel-cracking diesel engine system
US9689346B2 (en) * 2013-04-12 2017-06-27 United Technologies Corporation Gas turbine engine convergent/divergent exhaust nozzle divergent seal with dovetail interface
EP3097301B1 (de) 2014-01-24 2018-05-02 United Technologies Corporation Divergenzklappe
US9869190B2 (en) 2014-05-30 2018-01-16 General Electric Company Variable-pitch rotor with remote counterweights
US10072510B2 (en) 2014-11-21 2018-09-11 General Electric Company Variable pitch fan for gas turbine engine and method of assembling the same
US10100653B2 (en) 2015-10-08 2018-10-16 General Electric Company Variable pitch fan blade retention system
US11674435B2 (en) 2021-06-29 2023-06-13 General Electric Company Levered counterweight feathering system
US11795964B2 (en) 2021-07-16 2023-10-24 General Electric Company Levered counterweight feathering system
US11772809B2 (en) * 2021-11-27 2023-10-03 Airbus Defence and Space GmbH Fuselage for an aircraft with fuselage-integrated tailplane

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Publication number Priority date Publication date Assignee Title
US3972475A (en) * 1975-07-31 1976-08-03 United Technologies Corporation Nozzle construction providing for thermal growth
US4073441A (en) * 1976-10-04 1978-02-14 General Electric Company Gas turbine engine nozzle apparatus including a nozzle flap slot seal
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
US4643356A (en) * 1977-08-31 1987-02-17 United Technologies Corporation Cooling liner for convergent-divergent exhaust nozzle
US4718230A (en) * 1986-11-10 1988-01-12 United Technologies Corporation Augmentor liner construction
US4747542A (en) * 1987-04-14 1988-05-31 United Technologies Corporation Nozzle flap edge cooling
US4747543A (en) * 1987-04-14 1988-05-31 United Technologies Corporation Nozzle flap cooling liner
US5000386A (en) * 1989-07-03 1991-03-19 General Electric Company Exhaust flaps
US5076496A (en) * 1990-02-05 1991-12-31 General Electric Company Exhaust nozzle flap seal
US5067324A (en) * 1990-04-04 1991-11-26 United Technologies Corporation Engine nozzle liner retainer
US5060472A (en) * 1990-04-12 1991-10-29 The United States Of America As Represented By The Secretary Of The Air Force Insulated cooling liner
US5080284A (en) * 1990-06-25 1992-01-14 United Technologies Corporation Cooling system for the trailing edge of a liner
US5131222A (en) * 1990-11-28 1992-07-21 The United States Of Americas As Represented By The Secretary Of The Air Force Thermally valved cooling system for exhaust nozzle systems
US5239823A (en) * 1991-02-26 1993-08-31 United Technologies Corporation Multiple layer cooled nozzle liner
US5115979A (en) * 1991-05-28 1992-05-26 General Electric Company Conforming plunger seal assembly
US5188292A (en) * 1991-06-28 1993-02-23 The United States Of America As Represented By The Secretary Of The Air Force Thermal shields for rotating members in a gas flow path
US5239815A (en) * 1991-09-23 1993-08-31 United Technologies Corporation Sync-ring assembly for a gas turbine engine exhaust nozzle
US5209059A (en) * 1991-12-27 1993-05-11 The United States Of America As Represented By The Secretary Of The Air Force Active cooling apparatus for afterburners
US5215256A (en) * 1992-07-16 1993-06-01 Barcza W Kevin Flap hinge arrangement for a convergent/divergent nozzle
US5269467A (en) 1992-08-03 1993-12-14 General Electric Company Vectoring exhaust nozzle seal and flap retaining apparatus
US5249419A (en) * 1992-10-07 1993-10-05 The United States Of America As Represented By The Secretary Of The Air Force Nozzle liner for gas turbine engines
US5437411A (en) 1992-12-14 1995-08-01 General Electric Company Vectoring exhaust nozzle flap and seal positioning apparatus
US5323965A (en) * 1993-05-26 1994-06-28 The United States Of America As Represented By The Secretary Of The Air Force Hinge end seal
US5524438A (en) 1994-12-15 1996-06-11 United Technologies Corporation Segmented bulkhead liner for a gas turbine combustor
US5683034A (en) 1995-05-22 1997-11-04 United Technologies Corporation Engine exhaust nozzle seal
US5560198A (en) 1995-05-25 1996-10-01 United Technologies Corporation Cooled gas turbine engine augmentor fingerseal assembly
US5839663A (en) 1996-07-23 1998-11-24 United Technologies Corporation Gas turbine exhaust nozzle flap and flap seal apparatus
US5797544A (en) 1996-09-27 1998-08-25 United Technologies Corporation C/D nozzle with synchronizing ring link suspension
US5813611A (en) 1996-09-27 1998-09-29 United Technologies Corporation Compact pressure balanced fulcrum-link nozzle
US5842643A (en) * 1996-12-03 1998-12-01 General Electric Company Articulated exhaust nozzle fairing
US6398129B1 (en) 1999-12-29 2002-06-04 United Technologies Corporation Throat configuration for axisymmetric nozzle
US6658854B2 (en) * 2002-02-01 2003-12-09 General Electric Co. Methods and apparatus for retaining gas turbine engine nozzle basesheets
US6779336B2 (en) * 2002-07-05 2004-08-24 United Technologies Corporation Cooled variable geometry exhaust nozzle
FR2855559B1 (fr) * 2003-05-27 2005-07-15 Snecma Moteurs Systeme d'etancheite du flux secondaire a l'entree d'une tuyere d'une turbomachine avec chambre de post-combustion
US7225622B2 (en) 2003-07-21 2007-06-05 United Technologies Corporation Turbine engine nozzle
US7302793B2 (en) * 2003-10-29 2007-12-04 General Electric Company Methods and apparatus to reduce turbine engine nozzle basesheet stresses
US7178325B2 (en) * 2004-05-20 2007-02-20 United Technologies Corporation Divergent flap for a gas turbine engine
US7578133B2 (en) * 2005-03-28 2009-08-25 United Technologies Corporation Reduced radar cross section exhaust nozzle assembly

Also Published As

Publication number Publication date
US20070234728A1 (en) 2007-10-11
EP1764498B1 (de) 2009-05-06
US7624567B2 (en) 2009-12-01
EP1764498A3 (de) 2007-08-08
JP2007085335A (ja) 2007-04-05
EP1764498A2 (de) 2007-03-21

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition