DE69403376T2 - Wärmeschutzvorrichtung, insbesondere für Raumfahrzeuge - Google Patents

Wärmeschutzvorrichtung, insbesondere für Raumfahrzeuge

Info

Publication number
DE69403376T2
DE69403376T2 DE69403376T DE69403376T DE69403376T2 DE 69403376 T2 DE69403376 T2 DE 69403376T2 DE 69403376 T DE69403376 T DE 69403376T DE 69403376 T DE69403376 T DE 69403376T DE 69403376 T2 DE69403376 T2 DE 69403376T2
Authority
DE
Germany
Prior art keywords
protection device
thermal protection
space vehicles
vehicles
space
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
DE69403376T
Other languages
English (en)
Other versions
DE69403376D1 (de
Inventor
Thibault Arnold
Alain Lacombe
Michel Tual
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
EUROPEENNE DE PROPULSION SURESNES FR Ste
Societe Europeenne de Propulsion SEP 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 EUROPEENNE DE PROPULSION SURESNES FR Ste, Societe Europeenne de Propulsion SEP SA filed Critical EUROPEENNE DE PROPULSION SURESNES FR Ste
Publication of DE69403376D1 publication Critical patent/DE69403376D1/de
Application granted granted Critical
Publication of DE69403376T2 publication Critical patent/DE69403376T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/06—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
    • F16C11/0685—Manufacture of ball-joints and parts thereof, e.g. assembly of ball-joints
    • F16C11/069—Manufacture of ball-joints and parts thereof, e.g. assembly of ball-joints with at least one separate part to retain the ball member in the socket; Quick-release systems
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00—Pivots; Pivotal connections
    • F16C11/04—Pivotal connections
    • F16C11/06—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2202/00—Solid materials defined by their properties
    • F16C2202/20—Thermal properties
    • F16C2202/24—Insulating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/47—Cosmonautic vehicles, i.e. bearings adapted for use in outer-space
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/70—Interfitted members
    • Y10T403/7018—Interfitted members including separably interposed key
    • Y10T403/7021—Axially extending
    • Y10T403/7022—Resilient
    • 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
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/75—Joints and connections having a joining piece extending through aligned openings in plural members

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Critical Care (AREA)
  • Emergency Medicine (AREA)
  • General Health & Medical Sciences (AREA)
  • Thermal Sciences (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Connection Of Plates (AREA)
  • Thermal Insulation (AREA)
DE69403376T 1993-04-01 1994-03-30 Wärmeschutzvorrichtung, insbesondere für Raumfahrzeuge Expired - Fee Related DE69403376T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9303830A FR2703323B1 (fr) 1993-04-01 1993-04-01 Dispositif de protection thermique, notamment pour engin aerospatial.

Publications (2)

Publication Number Publication Date
DE69403376D1 DE69403376D1 (de) 1997-07-03
DE69403376T2 true DE69403376T2 (de) 1998-01-02

Family

ID=9445632

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69403376T Expired - Fee Related DE69403376T2 (de) 1993-04-01 1994-03-30 Wärmeschutzvorrichtung, insbesondere für Raumfahrzeuge

Country Status (6)

Country Link
US (1) US5489074A (de)
EP (1) EP0618133B1 (de)
JP (1) JP3431263B2 (de)
CA (1) CA2120555C (de)
DE (1) DE69403376T2 (de)
FR (1) FR2703323B1 (de)

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GB2296288A (en) * 1994-12-16 1996-06-26 Kenex Mount for a radiation shield
US5772154A (en) * 1995-11-28 1998-06-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Leading edge heat shield for wings of spacecraft
US5803406A (en) * 1996-04-22 1998-09-08 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated thermal insulation system for spacecraft
US6007026A (en) * 1997-06-30 1999-12-28 The Boeing Company Quick installation-removal thermal insulation blanket for space craft
US5928752A (en) * 1997-06-30 1999-07-27 The Boeing Company Quick installation-removal thermal insulation blanket for space craft
DE19810067C1 (de) * 1998-03-09 1999-03-18 Man Technologie Gmbh Bewegbare Baukomponente für eine thermomechanisch belastete Bauanordnung sowie Verfahren zur Herstellung der Baukomponente
US6299106B1 (en) * 1999-03-09 2001-10-09 The Boeing Company Thermal insulation utilizing a low profile snap fastener
US6293496B1 (en) * 1999-08-06 2001-09-25 The B. F. Goodrich Company Strain compatible attachment for metallic thermal protection system for a space vehicle
US6489001B1 (en) 2000-03-27 2002-12-03 Northrop Grumman Corp. Protective impact-resistant thermal insulation structure
US6367740B1 (en) 2000-05-16 2002-04-09 The Boeing Company Air foil having a hybrid leading edge construction
EP1302723A1 (de) * 2001-10-15 2003-04-16 Siemens Aktiengesellschaft Auskleidung für Innenwände von Brennkammern
US6827312B2 (en) * 2001-11-27 2004-12-07 Coi Ceramics, Inc. Method and system of thermal protection
FR2842582B1 (fr) * 2002-07-22 2005-01-21 Snecma Propulsion Solide Pontet de fixation de panneaux de protection thermique
US7871716B2 (en) * 2003-04-25 2011-01-18 Siemens Energy, Inc. Damage tolerant gas turbine component
US7281688B1 (en) * 2006-04-27 2007-10-16 The Boeing Company Materials for self-transpiring hot skins for hypersonic vehicles or reusable space vehicles
MX2009008130A (es) * 2007-02-02 2009-10-20 Materiaux De Construction Oldc Pared con acabado decorativo.
US9206599B2 (en) 2007-02-02 2015-12-08 Les Materiaux De Construction Oldcastle Canada, Inc. Wall with decorative facing
US7998392B2 (en) * 2007-09-25 2011-08-16 The Boeing Company Method for manufacturing and attachment of wing fairings
US8128025B2 (en) * 2008-03-21 2012-03-06 The Boeing Company Providing skins for aircraft fuselages
US8413398B1 (en) * 2008-06-20 2013-04-09 3Form, Inc. Ball pivot assemblies and systems and methods incorporating the same
US8752350B2 (en) * 2009-01-12 2014-06-17 The Boeing Company Ceramic composite thermal protection system
US8056862B1 (en) * 2010-06-09 2011-11-15 Arrowhead Products Corporation Thermal protection systems for air and space vehicles having hidden fastener attachments
US9441342B2 (en) 2010-09-28 2016-09-13 Les Materiaux De Construction Oldcastle Canada, In Retaining wall
CA2806259C (en) 2010-09-28 2014-04-22 Les Materiaux De Construction Oldcastle Canada, Inc. Retaining wall
US9670640B2 (en) 2010-09-28 2017-06-06 Les Materiaux De Construction Oldcastle Canada, Inc. Retaining wall
FI2959065T3 (fi) 2013-02-25 2024-01-30 Les Materiaux De Construction Oldcastle Canada Inc Seinäkokoonpano
EP3099912A4 (de) * 2014-01-28 2017-02-01 United Technologies Corporation Keramisch beschichtete turbinenkomponenten
CN105644795B (zh) * 2014-11-15 2017-11-28 北京临近空间飞行器系统工程研究所 一种旋转式分插热防护装置
CN105644796B (zh) * 2014-11-15 2017-11-28 北京临近空间飞行器系统工程研究所 一种推拉式分插热防护装置
US10507940B2 (en) * 2017-03-28 2019-12-17 The Boeing Company Machine in-place tile thermal protection
US11873762B2 (en) 2020-06-16 2024-01-16 Rolls-Royce Corporation High temperature heat shield assemblies
CN112329148A (zh) * 2020-11-18 2021-02-05 西北工业大学 一种高超声速飞行器热防护结构优化方法及系统
CN114645274A (zh) * 2020-12-21 2022-06-21 上海陆亿新能源有限公司 绿色经济耐用的高强高温绝热复合膜层结构

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB530144A (en) * 1939-06-17 1940-12-05 Rene Tampier Improvements in or relating to ball joints
US4308309A (en) * 1980-05-07 1981-12-29 Nasa Adjustable high emittance gap filler
US4379382A (en) * 1980-06-02 1983-04-12 Sauder Industries, Inc. Method and apparatus for insulating a furnace having a corrosive atmosphere
DE3027513A1 (de) * 1980-07-19 1982-02-25 Hochtemperatur-Reaktorbau GmbH, 5000 Köln Abstuetzeinrichtung fuer den aus kugelfoermigen brennelementen aufgeschuetteten kern eines hochtemperaturreaktors
DE3030433A1 (de) * 1980-08-12 1982-03-11 Fritz Bauer + Söhne oHG, 8503 Altdorf Winkelgelenk
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
FR2586080B1 (fr) * 1985-08-12 1987-11-27 Centre Nat Etd Spatiales Element de protection thermique pour un engin soumis a des echauffements importants
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
JPS63297198A (ja) * 1987-05-28 1988-12-05 三菱重工業株式会社 壁体
US5014934A (en) * 1989-06-30 1991-05-14 The Boeing Company Removable seal for discontinuities in aircraft skin
JP2634255B2 (ja) * 1989-10-18 1997-07-23 宇宙開発事業団 宇宙往還機用の金属ｔｐｓの機体取付装置
FR2657675B1 (fr) * 1990-01-31 1992-07-03 Dassault Avions Systeme de protection thermique, notamment pour vehicules spatiaux.
JPH03243499A (ja) * 1990-02-19 1991-10-30 Nec Corp 断熱材
JPH04356300A (ja) * 1991-05-31 1992-12-09 Mitsubishi Heavy Ind Ltd 熱防護部材用ギャップフィラー
US5254837A (en) * 1991-07-15 1993-10-19 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Thermally activated retainer means utilizing shape memory alloy
US5314144A (en) * 1991-12-18 1994-05-24 Raytheon Company Thermally compensating insert fastener
JPH05203095A (ja) * 1992-01-24 1993-08-10 Natl Space Dev Agency Japan<Nasda> 熱防護システム
JPH05203096A (ja) * 1992-01-24 1993-08-10 Natl Space Dev Agency Japan<Nasda> 熱防護システム
US5275529A (en) * 1992-03-16 1994-01-04 General Electric Company Sandwich panel joint

Also Published As

Publication number Publication date
DE69403376D1 (de) 1997-07-03
FR2703323A1 (fr) 1994-10-07
CA2120555A1 (en) 1994-10-02
CA2120555C (en) 2001-03-06
FR2703323B1 (fr) 1995-06-30
EP0618133A1 (de) 1994-10-05
JPH06321199A (ja) 1994-11-22
JP3431263B2 (ja) 2003-07-28
US5489074A (en) 1996-02-06
EP0618133B1 (de) 1997-05-28

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SOCIETE NATIONALE D'ETUDE ET DE CONSTRUCTION DE MO

8339 Ceased/non-payment of the annual fee