ES2091583T3 - Dispositivo de proteccion termica de un objeto y estructura, en particular un escudo termal, asi obtenido. - Google Patents

Dispositivo de proteccion termica de un objeto y estructura, en particular un escudo termal, asi obtenido.

Info

Publication number
ES2091583T3
ES2091583T3 ES93450001T ES93450001T ES2091583T3 ES 2091583 T3 ES2091583 T3 ES 2091583T3 ES 93450001 T ES93450001 T ES 93450001T ES 93450001 T ES93450001 T ES 93450001T ES 2091583 T3 ES2091583 T3 ES 2091583T3
Authority
ES
Spain
Prior art keywords
thermal
thermal protection
constituted
fabric
protection
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
ES93450001T
Other languages
English (en)
Inventor
Pierre Parrot
Philippe Herman
Philippe Lalanne
Jean-Louis Tisne
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2091583T3 publication Critical patent/ES2091583T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/52—Protection, safety or emergency devices; Survival aids
    • B64G1/58—Thermal protection, e.g. heat shields
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00—Stock material or miscellaneous articles
    • Y10S428/92—Fire or heat protection feature

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Critical Care (AREA)
  • Emergency Medicine (AREA)
  • General Health & Medical Sciences (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Road Paving Structures (AREA)
  • Thermal Insulation (AREA)

Abstract

LA INVENCION CONCIERNE A UN DISPOSITIVO DE PROTECCION TERMICA DE UN OBJETO, EN PARTICULAR UN VEHICULO ESPACIAL, DEL TIPO QUE COMPRENDE UNA ESTRUCTURA PORTADORA (1) REVESTIDA POR UN MATERIAL TERMOAISLANTE, CARACTERIZADO EN QUE DICHO MATERIAL ESTA CONSTITUIDO POR UN AGREGADO DE FIBRAS CORTAS DE CARBONO O DE SILICIO UNIDAS POR UN LIGANTE FORMADO POR EL MISMO CONSTITUYENTE Y EVENTUALMENTE POR UNA RESINA APROPIADA, DICHO AGREGADO ES PUESTO EN OBRA BAJO LA FORMA DE AL MENOS UN ELEMENTO MONOBLOQUE (2, 2A), CONFORMADO Y DIMENSIONADO EN CONSECUENCIA Y APLICADO POR ENCOLADO SOBRE LA ESTRUCTURA PORTADORA (1). APLICACION A LA PROTECCION TERMICA EN ESPECIAL DE INGENIOS ESPACIALES.
ES93450001T 1992-04-23 1993-04-22 Dispositivo de proteccion termica de un objeto y estructura, en particular un escudo termal, asi obtenido. Expired - Lifetime ES2091583T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9205260A FR2690499B1 (fr) 1992-04-23 1992-04-23 Dispositif de protection thermique d'un objet et structure, notamment bouclier thermique, ainsi obtenue.

Publications (1)

Publication Number Publication Date
ES2091583T3 true ES2091583T3 (es) 1996-11-01

Family

ID=9429354

Family Applications (1)

Application Number Title Priority Date Filing Date
ES93450001T Expired - Lifetime ES2091583T3 (es) 1992-04-23 1993-04-22 Dispositivo de proteccion termica de un objeto y estructura, en particular un escudo termal, asi obtenido.

Country Status (7)

Country Link
US (1) US5511747A (es)
EP (1) EP0567417B1 (es)
JP (1) JPH0687499A (es)
CA (1) CA2094331A1 (es)
DE (1) DE69303420T2 (es)
ES (1) ES2091583T3 (es)
FR (1) FR2690499B1 (es)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2720503B1 (fr) * 1994-05-26 1996-06-21 Commissariat Energie Atomique Système de caractérisation thermomécanique de matériaux utilisant un dispositif de chauffage rapide par induction.
DE19513906C2 (de) * 1995-04-12 1998-10-01 Man Technologie Gmbh Keramisches Hitzeschild
US5928752A (en) * 1997-06-30 1999-07-27 The Boeing Company Quick installation-removal thermal insulation blanket for space craft
US6007026A (en) * 1997-06-30 1999-12-28 The Boeing Company Quick installation-removal thermal insulation blanket for space craft
US6224339B1 (en) 1998-07-08 2001-05-01 Allison Advanced Development Company High temperature airfoil
US6592981B1 (en) 1998-08-07 2003-07-15 Lockheed Martin Corporation Oxidation resistant insulating sandwich tiles
US6558785B1 (en) 1998-08-07 2003-05-06 Lockheed Martin Corporation Insulated reentry heat shield
US6299106B1 (en) * 1999-03-09 2001-10-09 The Boeing Company Thermal insulation utilizing a low profile snap fastener
WO2001006828A2 (en) * 1999-07-22 2001-02-01 Lockheed Martin Corporation Oxidation resistant insulating sandwich tiles
US6676077B1 (en) * 2000-11-01 2004-01-13 The Boeing Company High temperature resistant airfoil apparatus for a hypersonic space vehicle
US6555211B2 (en) 2001-01-10 2003-04-29 Albany International Techniweave, Inc. Carbon composites with silicon based resin to inhibit oxidation
US7682578B2 (en) 2005-11-07 2010-03-23 Geo2 Technologies, Inc. Device for catalytically reducing exhaust
US7682577B2 (en) 2005-11-07 2010-03-23 Geo2 Technologies, Inc. Catalytic exhaust device for simplified installation or replacement
US7722828B2 (en) 2005-12-30 2010-05-25 Geo2 Technologies, Inc. Catalytic fibrous exhaust system and method for catalyzing an exhaust gas
US7998392B2 (en) * 2007-09-25 2011-08-16 The Boeing Company Method for manufacturing and attachment of wing fairings
US8714491B2 (en) * 2007-09-28 2014-05-06 The Boeing Company Thermal protection system with staggered joints
US8152107B1 (en) * 2008-02-19 2012-04-10 The Boeing Company Applying sealant to narrow deep gaps in an ablative heat shield surface
DE102010048998A1 (de) * 2010-10-20 2012-04-26 Airbus Operations Gmbh Kondenswasserfreies Isolationssystem für Passagierflugzeuge
US8662448B2 (en) * 2011-06-06 2014-03-04 The Boeing Company System and method for insulating frame member
US9327848B2 (en) * 2012-06-11 2016-05-03 Bigelow Aerospace Method of deploying a spacecraft shield in space
US10023286B2 (en) * 2015-11-19 2018-07-17 The Boeing Company Aircraft bay blankets that provide enhanced drainage features
CN106005485B (zh) * 2016-06-28 2018-06-26 湖北航天技术研究院总体设计所 一种高速运载器保温层及其安装方法
CN106428644B (zh) * 2016-09-28 2020-06-12 湖北航天技术研究院总体设计所 一种运载器保温层及其制造方法
FR3058129B1 (fr) * 2016-11-02 2021-05-14 Airbus Safran Launchers Sas Panneau de protection thermique detachable pour vehicule spatial, monte serre contre un carter structural
US10507940B2 (en) * 2017-03-28 2019-12-17 The Boeing Company Machine in-place tile thermal protection
US10988230B2 (en) * 2017-06-19 2021-04-27 The Boeing Company Passive moisture management bladder in an aircraft
RU2724195C1 (ru) * 2019-08-27 2020-06-22 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Высокоскоростной летательный аппарат

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3769511A (en) * 1970-10-12 1973-10-30 Gen Dynamics Corp Spacecraft heat shield testing method
US4151800A (en) * 1977-04-15 1979-05-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermal insulation protection means
FR2489812A1 (fr) * 1980-09-05 1982-03-12 Aerospatiale Procede de fabrication d'un materiau de protection thermique, notamment pour elements d'engin et materiau ainsi obtenu
FR2493304A1 (fr) * 1980-10-30 1982-05-07 Europ Propulsion Procede d'assemblage de pieces refractaires
US4338368A (en) * 1980-12-17 1982-07-06 Lovelace Alan M Administrator Attachment system for silica tiles
US4358480A (en) * 1981-05-22 1982-11-09 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of repairing surface damage to porous refractory substrates
US4373003A (en) * 1982-04-06 1983-02-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration High temperature silicon carbide impregnated insulating fabrics
FR2525963A1 (fr) * 1982-04-29 1983-11-04 Aerospatiale Procede de fabrication d'un materiau de protection thermique a hautes performances, et materiau ainsi obtenu
US4439968A (en) * 1982-09-15 1984-04-03 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Pre-stressed thermal protection systems
US4456208A (en) * 1982-10-20 1984-06-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Shell tile thermal protection system
US4833030A (en) * 1984-05-18 1989-05-23 Hitco Polymer impregnated and carbonized carbon/carbon composite
US4515847A (en) * 1984-08-22 1985-05-07 The United States Of America As Represented By The Secretary Of The Air Force Erosion-resistant nosetip construction
JPS61166934A (ja) * 1985-01-17 1986-07-28 Toyota Motor Corp 複合材料製造用短繊維成形体及びその製造方法
US4686128A (en) * 1985-07-01 1987-08-11 Raytheon Company Laser hardened missile casing
US4706912A (en) * 1985-12-16 1987-11-17 The United States Of America As Represented By The Secretary Of The Army Structural external insulation for hypersonic missiles
US4713275A (en) * 1986-05-14 1987-12-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ceramic/ceramic shell tile thermal protection system and method thereof
FR2652036B1 (fr) * 1989-09-19 1991-12-27 Aerospatiale Revetement de protection thermique, un procede et une installation pour sa fabrication.
FR2657675B1 (fr) * 1990-01-31 1992-07-03 Dassault Avions Systeme de protection thermique, notamment pour vehicules spatiaux.
FR2660410B1 (fr) * 1990-03-30 1992-06-12 Commissariat Energie Atomique Bouclier thermique.

Also Published As

Publication number Publication date
JPH0687499A (ja) 1994-03-29
EP0567417B1 (fr) 1996-07-03
US5511747A (en) 1996-04-30
FR2690499A1 (fr) 1993-10-29
CA2094331A1 (fr) 1993-10-24
DE69303420T2 (de) 1997-02-27
FR2690499B1 (fr) 1995-06-30
DE69303420D1 (de) 1996-08-08
EP0567417A1 (fr) 1993-10-27

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