ES2176928T3 - Sistema de admision de aire en un conducto de gases de una turbomaquina. - Google Patents

Sistema de admision de aire en un conducto de gases de una turbomaquina.

Info

Publication number
ES2176928T3
ES2176928T3 ES98401107T ES98401107T ES2176928T3 ES 2176928 T3 ES2176928 T3 ES 2176928T3 ES 98401107 T ES98401107 T ES 98401107T ES 98401107 T ES98401107 T ES 98401107T ES 2176928 T3 ES2176928 T3 ES 2176928T3
Authority
ES
Spain
Prior art keywords
doors
air admission
ramps
turbomachine
admission system
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
ES98401107T
Other languages
English (en)
Inventor
Thierry Pascal Bardagi
Gerard Ernest Andre Jourdain
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 ES2176928T3 publication Critical patent/ES2176928T3/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
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry

Abstract

EL SISTEMA DE ADMISION (13) DE AIRE EXTERIOR (12) EN UN CHORRO (11) DE UN TURBOMOTOR A TRAVES DE UNA CUBIERTA (10) DEL CHORRO SE CARACTERIZA POR LA COMBINACION DE PUERTAS QUE SE DESLIZAN HACIA DELANTE (RAMPAS) (15) CON PUERTAS GIRATORIAS (14). LAS RAMPAS (15) VAN PROVISTAS DE UNOS BRAZOS LATERALES ACANALADOS (30) EN LOS QUE GIRAN RODILLOS MONTADOS SOBRE LAS PUERTAS (14). CUANDO LLEGAN A UNA PARTE ASCENDENTE (33) DE LAS RANURAS (31) TRAS UN DESPLAZAMIENTO SUFICIENTE HACIA DELANTE DE LAS RAMPAS (15), SE ELEVAN, LO QUE ABRE LAS PUERTAS (14). ESTE SISTEMA PUEDE EMPLEARSE EN TURBOMOTORES DE DOBLE FLUJO PARA AERONAVES SUPERSONICAS.
ES98401107T 1997-05-07 1998-05-07 Sistema de admision de aire en un conducto de gases de una turbomaquina. Expired - Lifetime ES2176928T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9705619A FR2763098B1 (fr) 1997-05-07 1997-05-07 Systeme d'admission d'air dans une veine de turbomachine

Publications (1)

Publication Number Publication Date
ES2176928T3 true ES2176928T3 (es) 2002-12-01

Family

ID=9506661

Family Applications (1)

Application Number Title Priority Date Filing Date
ES98401107T Expired - Lifetime ES2176928T3 (es) 1997-05-07 1998-05-07 Sistema de admision de aire en un conducto de gases de una turbomaquina.

Country Status (6)

Country Link
US (1) US6082669A (es)
EP (1) EP0877155B1 (es)
JP (1) JP3732336B2 (es)
DE (1) DE69806540T2 (es)
ES (1) ES2176928T3 (es)
FR (1) FR2763098B1 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6272838B1 (en) * 1999-02-25 2001-08-14 Alliedsignal, Inc. Method and apparatus for controlling the inlet duct leading to an auxiliary power unit
US7014144B2 (en) * 2003-07-22 2006-03-21 Honeywell International, Inc. Dual action inlet door and method for use thereof
DE10361722B4 (de) * 2003-12-30 2009-06-10 Airbus Deutschland Gmbh Stauluftkanal zur Umgebungsluftzufuhr in einem Flugzeug
US7790878B2 (en) * 2004-10-22 2010-09-07 Alnylam Pharmaceuticals, Inc. RNAi modulation of RSV, PIV and other respiratory viruses and uses thereof
GB0523570D0 (en) * 2005-11-18 2005-12-28 Airbus Uk Ltd Aircraft cooling duct
US7600714B2 (en) * 2006-04-20 2009-10-13 Honeywell International Inc. Diffusing air inlet door assembly
US7837142B2 (en) * 2006-10-12 2010-11-23 Aerion Corporation Supersonic aircraft jet engine
FR2915461B1 (fr) * 2007-04-24 2009-06-05 Airbus France Sas Agencement d'entree d'air pour vehicule, notamment un aeronef.
DE102008030399B4 (de) * 2008-06-26 2019-03-21 Airbus Operations Gmbh Luftkanal zur Umgebungsluftzufuhr in einem Flugzeug
FR2936778B1 (fr) * 2008-10-07 2011-06-10 Airbus France Agencement d'entree d'air pour aeronef
US8141818B2 (en) * 2009-07-02 2012-03-27 Honeywell International Inc. Ram door assemblies
CN107740730B (zh) * 2017-09-15 2019-06-28 江西洪都航空工业集团有限责任公司 一种超音速下颌进气道前堵盖
US10829199B2 (en) * 2018-08-20 2020-11-10 Bell Helicopter Textron Inc. Active airflow management for tiltrotor hub thermal ventilation
US20240092495A1 (en) * 2022-09-15 2024-03-21 Rohr, Inc. Aircraft propulsion system with variable area inlet

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL63747C (es) * 1943-07-02
FR966975A (fr) * 1948-05-21 1950-10-23 Snecma Buse d'entrée d'air pour appareils moteurs à turbine à gaz
US3503211A (en) * 1968-04-10 1970-03-31 Rohr Corp Thrust reverser
US3511055A (en) * 1968-05-29 1970-05-12 Rohr Corp Thrust reverser
DE1944472A1 (de) * 1969-09-02 1971-03-18 Messerschmitt Boelkow Blohm Doppelwandige Verschlussklappe fuer eine Hilfseinlaufoeffnung eines Strahltriebwerkes
US3659424A (en) * 1970-10-07 1972-05-02 Us Navy Stowable air scoop
US3915413A (en) * 1974-03-25 1975-10-28 Gen Electric Variable air inlet system for a gas turbine engine
US4022948A (en) * 1974-12-23 1977-05-10 United Technologies Corporation Resiliently coated metallic finger seals
DE2511468C3 (de) * 1975-03-15 1980-11-13 Vereinigte Flugtechnische Werke- Fokker Gmbh, 2800 Bremen Triebwerkseinlauf mit einer Hilfseinlaufklappe
GB1534583A (en) * 1976-06-08 1978-12-06 Short Bros Ltd Reversal of thrust in gas turbine engines
US4278220A (en) * 1979-03-30 1981-07-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thrust reverser for a long duct fan engine
US4371132A (en) * 1980-01-11 1983-02-01 Rolls Royce Limited Reversible thrust ducted fan propulsion unit
IL62132A0 (en) * 1980-02-26 1981-03-31 Gen Electric Inlet cowl for a two-dimensional inlet
US4418879A (en) * 1980-12-29 1983-12-06 The Boeing Company Scoop and inlet for auxiliary power units and method
DE3942323C2 (de) * 1989-12-21 1993-11-25 Mtu Muenchen Gmbh Einlaufkonfiguration für ein kombiniertes Turbo-Staustrahltriebwerk

Also Published As

Publication number Publication date
US6082669A (en) 2000-07-04
DE69806540T2 (de) 2003-02-27
FR2763098A1 (fr) 1998-11-13
EP0877155B1 (fr) 2002-07-17
EP0877155A1 (fr) 1998-11-11
JP3732336B2 (ja) 2006-01-05
FR2763098B1 (fr) 1999-06-11
JPH10325362A (ja) 1998-12-08
DE69806540D1 (de) 2002-08-22

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