DE69100759D1 - Flexibler und druckdurchlässiger Wärmeschutz. - Google Patents

Flexibler und druckdurchlässiger Wärmeschutz.

Info

Publication number
DE69100759D1
DE69100759D1 DE91400284T DE69100759T DE69100759D1 DE 69100759 D1 DE69100759 D1 DE 69100759D1 DE 91400284 T DE91400284 T DE 91400284T DE 69100759 T DE69100759 T DE 69100759T DE 69100759 D1 DE69100759 D1 DE 69100759D1
Authority
DE
Germany
Prior art keywords
flexible
pressure
thermal protection
permeable thermal
permeable
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
DE91400284T
Other languages
English (en)
Other versions
DE69100759T2 (de
Inventor
Joel Heraud
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
Publication of DE69100759D1 publication Critical patent/DE69100759D1/de
Application granted granted Critical
Publication of DE69100759T2 publication Critical patent/DE69100759T2/de
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
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/84—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using movable nozzles
    • 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
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L59/00—Thermal insulation in general
    • F16L59/02—Shape or form of insulating materials, with or without coverings integral with the insulating materials
    • F16L59/029—Shape or form of insulating materials, with or without coverings integral with the insulating materials layered
    • 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
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L59/00—Thermal insulation in general
    • F16L59/14—Arrangements for the insulation of pipes or pipe systems
    • F16L59/16—Arrangements specially adapted to local requirements at flanges, junctions, valves or the like
    • F16L59/168—Flexible insulating material or covers for flanges, junctions, valves or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Critical Care (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Emergency Medicine (AREA)
  • General Health & Medical Sciences (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Thermal Insulation (AREA)
  • Exhaust Silencers (AREA)
  • Laminated Bodies (AREA)
DE91400284T 1990-02-09 1991-02-06 Flexibler und druckdurchlässiger Wärmeschutz. Expired - Fee Related DE69100759T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9001556A FR2658266B1 (fr) 1990-02-09 1990-02-09 Dispositif de protection thermique flexible et permeable a la pression.

Publications (2)

Publication Number Publication Date
DE69100759D1 true DE69100759D1 (de) 1994-01-27
DE69100759T2 DE69100759T2 (de) 1994-05-05

Family

ID=9393561

Family Applications (1)

Application Number Title Priority Date Filing Date
DE91400284T Expired - Fee Related DE69100759T2 (de) 1990-02-09 1991-02-06 Flexibler und druckdurchlässiger Wärmeschutz.

Country Status (8)

Country Link
US (1) US5156337A (de)
EP (1) EP0441703B1 (de)
JP (1) JPH0742898B2 (de)
DE (1) DE69100759T2 (de)
DK (1) DK0441703T3 (de)
ES (1) ES2047989T3 (de)
FR (1) FR2658266B1 (de)
IE (1) IE65831B1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2622181C1 (ru) * 2016-05-17 2017-06-13 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Тепловая защита негерметичного отсека двигательной установки летательного аппарата
FR3083827B1 (fr) * 2018-07-12 2022-07-29 Arianegroup Sas Protection thermique annulaire et procede de fabrication d'une telle protection
RU2705402C1 (ru) * 2018-11-29 2019-11-07 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ обеспечения теплового режима приборного отсека летательного аппарата
FR3096423B1 (fr) * 2019-05-21 2021-06-04 Arianegroup Sas Système d’amortissement non linéaire par lamelle pour moteur de lanceur spatial
FR3096426B1 (fr) * 2019-05-21 2021-06-04 Arianegroup Sas Système d’amortissement non linéaire pour moteur de lanceur spatial

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3203849A (en) * 1961-03-31 1965-08-31 Thiokol Chemical Corp Composite heat shield
FR1333603A (fr) * 1962-09-17 1963-07-26 Gen Motors Corp Bague d'étanchéité
US3346186A (en) * 1964-10-05 1967-10-10 North American Aviation Inc Extensible rocket nozzle comprised of a coated flexible mesh subsequently deployed and heated to become impermeable
US3507148A (en) * 1967-10-27 1970-04-21 Thiokol Chemical Corp Assembly for sealing thrust nozzle to exhaust diffuser
GB1376141A (en) * 1971-01-21 1974-12-04 Secr Defence Rocket motors having angularly movable exhaust nozzles
US3726480A (en) * 1971-02-24 1973-04-10 Us Navy Thrust vectoring control system for rocket nozzles
US3933310A (en) * 1974-07-11 1976-01-20 Thiokol Corporation Rocket nozzle construction and surfaces impervious to hot, high velocity gases
US4093157A (en) * 1976-12-16 1978-06-06 United Technologies Corporation Seal for variable plug two dimensional nozzle
US4110972A (en) * 1976-12-16 1978-09-05 United Technologies Corporation Seal means for a movable centerbody in a two dimensional nozzle
US4098076A (en) * 1976-12-16 1978-07-04 United Technologies Corporation Cooling air management system for a two-dimensional aircraft engine exhaust nozzle
NL7709903A (nl) * 1977-09-08 1979-03-12 Nederlandse Steenwolfabriek Nv Isolatiebekleding.
FR2422831A1 (fr) * 1978-02-03 1979-11-09 Aerospatiale Tuyere de propulseur a divergent deployable
US4477025A (en) * 1978-11-02 1984-10-16 Societe Nationale Industrielle Aerospatiale Hot nozzle
FR2455183A2 (fr) * 1979-04-24 1980-11-21 Aerospatiale Tuyere de propulseur a divergent deployable
FR2457390A1 (fr) * 1979-05-23 1980-12-19 Europ Propulsion Divergent deployable de tuyere pour propulseur fusee
JPS5685012U (de) * 1979-12-05 1981-07-08
US4324167A (en) * 1980-04-14 1982-04-13 General Dynamics, Pomona Division Flexible area launch tube rear cover
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
JPS5815644U (ja) * 1981-07-24 1983-01-31 愛知製鋼株式会社 長尺鋼材用連続加熱炉の炉内壁の形状
US4391865A (en) * 1981-10-05 1983-07-05 Constance Lillie B Thermal drapery construction
US4426038A (en) * 1982-01-11 1984-01-17 Thiokol Corporation Non-radiating extendible cloth exit cone for rocket nozzles
US4811529A (en) * 1982-07-01 1989-03-14 B&B Progessive Material & Technologies, Inc. Fire resistant flexible seal
US4525999A (en) * 1982-12-23 1985-07-02 Thiokol Corporation Actuator for deploying flexible bodies
US4649701A (en) * 1986-02-11 1987-03-17 The United States Of America As Represented By The Secretary Of The Navy Thrust nozzle with insulation
US4666084A (en) * 1986-06-09 1987-05-19 The United States Of America As Represented By The Secretary Of The Navy Nozzle assembly
JPS63117U (de) * 1986-06-19 1988-01-05
US4917302A (en) * 1988-12-30 1990-04-17 The United States Of America As Represented By The United States National Aeronautics And Space Administration High temperature flexible seal
US5014917A (en) * 1989-11-27 1991-05-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration High-temperature, flexible, thermal barrier seal

Also Published As

Publication number Publication date
FR2658266B1 (fr) 1992-06-12
DK0441703T3 (da) 1994-04-18
EP0441703A1 (de) 1991-08-14
ES2047989T3 (es) 1994-03-01
DE69100759T2 (de) 1994-05-05
EP0441703B1 (de) 1993-12-15
US5156337A (en) 1992-10-20
JPH04214954A (ja) 1992-08-05
IE65831B1 (en) 1995-11-29
IE910421A1 (en) 1991-08-14
JPH0742898B2 (ja) 1995-05-15
FR2658266A1 (fr) 1991-08-16

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee