FR2681641B1 - Dispositif de refroidissement pour moteurs a reaction, notamment pour moteurs a reaction hypersoniques. - Google Patents

Dispositif de refroidissement pour moteurs a reaction, notamment pour moteurs a reaction hypersoniques.

Info

Publication number
FR2681641B1
FR2681641B1 FR929211394A FR9211394A FR2681641B1 FR 2681641 B1 FR2681641 B1 FR 2681641B1 FR 929211394 A FR929211394 A FR 929211394A FR 9211394 A FR9211394 A FR 9211394A FR 2681641 B1 FR2681641 B1 FR 2681641B1
Authority
FR
France
Prior art keywords
jet engines
cooling device
hypersonic
engines
jet
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
FR929211394A
Other languages
English (en)
Other versions
FR2681641A1 (fr
Inventor
Hubert Grieb Dr
Gerhard Pellischek
Grieb Dr Hubert
Pellischek Gerhard
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2681641A1 publication Critical patent/FR2681641A1/fr
Application granted granted Critical
Publication of FR2681641B1 publication Critical patent/FR2681641B1/fr
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
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D7/00—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall
    • F28D7/005—Heat-exchange apparatus having stationary tubular conduit assemblies for both heat-exchange media, the media being in contact with different sides of a conduit wall the conduits for only one medium being tubes having bent portions or being assembled from bent tubes or being tubes having a toroidal configuration
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
    • F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
    • F28D2021/0021—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for aircrafts or cosmonautics
    • 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)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
FR929211394A 1991-09-25 1992-09-24 Dispositif de refroidissement pour moteurs a reaction, notamment pour moteurs a reaction hypersoniques. Expired - Fee Related FR2681641B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE4131913A DE4131913A1 (de) 1991-09-25 1991-09-25 Kuehlvorrichtung fuer hyperschall-luftstrahltriebwerke

Publications (2)

Publication Number Publication Date
FR2681641A1 FR2681641A1 (fr) 1993-03-26
FR2681641B1 true FR2681641B1 (fr) 1994-09-30

Family

ID=6441462

Family Applications (1)

Application Number Title Priority Date Filing Date
FR929211394A Expired - Fee Related FR2681641B1 (fr) 1991-09-25 1992-09-24 Dispositif de refroidissement pour moteurs a reaction, notamment pour moteurs a reaction hypersoniques.

Country Status (4)

Country Link
US (1) US5272870A (fr)
DE (1) DE4131913A1 (fr)
FR (1) FR2681641B1 (fr)
GB (1) GB2260578B (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4226666B4 (de) * 1991-09-25 2005-12-01 Mtu Aero Engines Gmbh Wärmetauscher für die Kühlung eines heißen Gases
US5255505A (en) * 1992-02-21 1993-10-26 Westinghouse Electric Corp. System for capturing heat transferred from compressed cooling air in a gas turbine
DE4315256A1 (de) * 1993-05-07 1994-11-10 Mtu Muenchen Gmbh Einrichtung zur Verteilung sowie Zu- und Abführung eines Kühlmittels an einer Wand eines Turbo-, insbesondere Turbo-Staustrahltriebwerks
US6182435B1 (en) * 1997-06-05 2001-02-06 Hamilton Sundstrand Corporation Thermal and energy management method and apparatus for an aircraft
US6134880A (en) * 1997-12-31 2000-10-24 Concepts Eti, Inc. Turbine engine with intercooler in bypass air passage
GB2356671B (en) * 1999-11-27 2003-10-29 Abb Alstom Power Uk Ltd Gas turbine engine
US7013636B2 (en) * 2004-04-22 2006-03-21 The Boeing Company System and method for controlling the temperature and infrared signature of an engine
US7305816B2 (en) * 2004-08-13 2007-12-11 United Technologies Corporation Rocket augmentation for combined cycle turboaccelerator jet engine
US20060053801A1 (en) * 2004-09-15 2006-03-16 Orlando Robert J Cooling system for gas turbine engine having improved core system
US20090049794A1 (en) * 2007-08-23 2009-02-26 Barone Joseph C Heat exchanger panel and manufacturing method thereof using transient liquid phase bonding agent and vacuum compression brazing
US8127555B2 (en) * 2007-12-13 2012-03-06 Pratt & Whitney Rocketdyne, Inc. Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle
US9151180B2 (en) 2010-06-15 2015-10-06 Hamilton Sundstrand Corporation Lubrication driven gas turbine engine actuation system
US9403600B2 (en) 2012-05-01 2016-08-02 Lockheed Martin Corporation Integrated thermal protection and leakage reduction in a supersonic air intake system
US9416730B2 (en) * 2013-01-31 2016-08-16 The Boeing Company Bi-directional ventilation systems for use with aircraft and related methods
US20160010485A1 (en) * 2014-07-09 2016-01-14 Aerojet Rocketdyne, Inc. Combined cycle propulsion system
US11041463B1 (en) 2015-02-11 2021-06-22 Raytheon Technologies Corporation Turbine engine structure with oxidizer enhanced mode
CN105841193B (zh) * 2016-05-18 2018-07-20 葛明龙 两种航空航天涡扇发动机
GB2584094B (en) * 2019-05-20 2022-01-26 Rolls Royce Plc Engine
US11692479B2 (en) 2019-10-03 2023-07-04 General Electric Company Heat exchanger with active buffer layer
US11506124B2 (en) * 2020-03-27 2022-11-22 Raytheon Technologies Corporation Supercritical CO2 cycle for gas turbine engines having supplemental cooling
FR3110937B1 (fr) * 2020-05-28 2022-04-29 Safran Installation d’alimentation en carburant cryogénique de la chambre de combustion d’une turbomachine.
FR3110935B1 (fr) 2020-05-28 2022-04-29 Safran Installation d’alimentation en carburant cryogénique de la chambre de combustion d’une turbomachine.
FR3128738B1 (fr) 2021-10-29 2024-01-12 Safran Système de conditionnement de carburant pour alimenter une turbomachine d’aéronef, procédé d’alimentation d’une turbomachine

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB619964A (en) * 1945-05-25 1949-03-17 Rateau Sa Soc Improvements in or relating to the use in internal combustion plants of fuels which are normally gaseous but which are stored in liquid form
GB749684A (en) * 1952-12-12 1956-05-30 Rolls Royce Improvements in or relating to aircraft fuel systems
US2925712A (en) * 1952-12-12 1960-02-23 Rolls Royce Aircraft fuel system with fuel heating means
US2851863A (en) * 1953-07-07 1958-09-16 Sir George Godfrey And Partner Air conditioning apparatus for aircraft
GB763449A (en) * 1953-09-09 1956-12-12 Rolls Royce Improvements relating to gas turbine engine fuel systems
GB870265A (en) * 1957-08-09 1961-06-14 Garrett Corp Jet propulsion unit with cooling means
GB899312A (en) * 1959-09-22 1962-06-20 Napier & Son Ltd Gas turbine engines
GB912762A (en) * 1960-07-12 1962-12-12 Rolls Royce Heat exchange apparatus
US3747339A (en) * 1961-11-13 1973-07-24 Texaco Inc Reaction propulsion engine and method of operation
US3740949A (en) * 1963-11-20 1973-06-26 Texaco Inc Fuel cooled ram air reaction propulsion engine
US3733826A (en) * 1964-02-10 1973-05-22 Texaco Experiment Inc Fuel cooled ram air reaction propulsion engine
US4041697A (en) * 1975-07-17 1977-08-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Oil cooling system for a gas turbine engine
US4404793A (en) * 1980-03-20 1983-09-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for improving the fuel efficiency of a gas turbine engine
US4696156A (en) * 1986-06-03 1987-09-29 United Technologies Corporation Fuel and oil heat management system for a gas turbine engine
GB2240813B (en) * 1986-08-28 1991-11-27 Rolls Royce Plc Improvements in hypersonic and trans atmospheric propulsion
DE3635548C1 (de) * 1986-10-20 1988-03-03 Mtu Muenchen Gmbh Waermetauscher
GB2241537B (en) * 1988-03-23 1992-08-12 Rolls Royce Plc The prevention of icing in the intakes of aerospace propulsors.
GB8907788D0 (en) * 1989-04-06 1989-05-17 Rolls Royce Plc Management of heat generated by aircraft gas turbine installations
US5152146A (en) * 1989-04-06 1992-10-06 Rolls-Royce Plc Fuel control valve for an aircraft gas turbine engine fuel system
DE3942022A1 (de) * 1989-12-20 1991-06-27 Mtu Muenchen Gmbh Verfahren und vorrichtung zur kuehlung eines flugtriebwerkes

Also Published As

Publication number Publication date
DE4131913C2 (fr) 1993-07-15
FR2681641A1 (fr) 1993-03-26
US5272870A (en) 1993-12-28
GB2260578A (en) 1993-04-21
GB2260578B (en) 1995-01-18
DE4131913A1 (de) 1993-04-08
GB9220229D0 (en) 1992-11-04

Similar Documents

Publication Publication Date Title
FR2681641B1 (fr) Dispositif de refroidissement pour moteurs a reaction, notamment pour moteurs a reaction hypersoniques.
FR2682997B1 (fr) Dispositif de demarrage pour moteurs thermiques.
FR2703323B1 (fr) Dispositif de protection thermique, notamment pour engin aerospatial.
ITTO920490A1 (it) Dispositivo inversore di spinta per motori aeronautici a getto.
FR2735751B1 (fr) Dispositif antivol, notamment pour bouteille
FR2696502B1 (fr) Dispositif de post-combustion pour turbo réacteur double flux.
FR2662510B1 (fr) Dispositif de retenue d'un element annulaire.
FR2680329B3 (fr) Dispositif de verrouillage d'un outillage sur un support.
FR2788812B1 (fr) Dispositif de propulsion notamment pour fusee
FR2742479B1 (fr) Dispositif de refroidissement d'un turbomoteur sur aeronef
FR2609304B3 (fr) Dispositif de commande perfectionne, notamment pour automobiles
FR2699296B1 (fr) Dispositif de prise de vues triscopiques.
FR2769699B1 (fr) Dispositif de guidage d'un engin volant, notamment un missile
FR2719424B1 (fr) Dispositif de commande pour alternateur.
FR2672459B1 (fr) Dispositif de rechargement par plasma a orifice oblique.
FR2680386B1 (fr) Dispositif pour la commande du regime des moteurs d'un aeronef.
FR2686433B1 (fr) Dispositif d'actionnement pour un accelerateur.
FR2688411B1 (fr) Dispositif d'assemblage d'un accessoire sur un ski.
FR2697062B1 (fr) Dispositif de maintien d'une pluralité de vis, écrous ou analogues sur une pièce quelconque.
FR2694537B1 (fr) Dispositif d'accrochage d'une turbomachine sur une structure d'aéronef.
FR2714153B1 (fr) Dispositif d'injection, notamment dispositif d'injection pour un moteur à réacteur.
FR2688156B1 (fr) Dispositif de montage des segments sur une tete de piston.
FR2695904B1 (fr) Dispositif de sécurité pour navigateurs.
FR2723620B1 (fr) Dispositif de solidarisation par encliquetage d'un element sur un autre.
FR2709250B1 (fr) Dispositif pour sélectionner des spermatozoïdes.

Legal Events

Date Code Title Description
ST Notification of lapse