FR2696212B3 - Door thrust reverser assembly for aircraft engine incorporating a thermal barrier. - Google Patents

Door thrust reverser assembly for aircraft engine incorporating a thermal barrier.

Info

Publication number
FR2696212B3
FR2696212B3 FR9211518A FR9211518A FR2696212B3 FR 2696212 B3 FR2696212 B3 FR 2696212B3 FR 9211518 A FR9211518 A FR 9211518A FR 9211518 A FR9211518 A FR 9211518A FR 2696212 B3 FR2696212 B3 FR 2696212B3
Authority
FR
France
Prior art keywords
thermal barrier
aircraft engine
thrust reverser
engine incorporating
reverser assembly
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
FR9211518A
Other languages
French (fr)
Other versions
FR2696212A1 (en
Inventor
Alain Fournier
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.)
Societe de Construction des Avions Hurel Dubois
Original Assignee
Societe de Construction des Avions Hurel Dubois
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 Societe de Construction des Avions Hurel Dubois filed Critical Societe de Construction des Avions Hurel Dubois
Priority to FR9211518A priority Critical patent/FR2696212B3/en
Publication of FR2696212A1 publication Critical patent/FR2696212A1/en
Application granted granted Critical
Publication of FR2696212B3 publication Critical patent/FR2696212B3/en
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
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/64—Reversing fan flow
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/231—Preventing heat transfer
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/50—Intrinsic material properties or characteristics
    • 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)
  • Laminated Bodies (AREA)
FR9211518A 1992-09-28 1992-09-28 Door thrust reverser assembly for aircraft engine incorporating a thermal barrier. Expired - Lifetime FR2696212B3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9211518A FR2696212B3 (en) 1992-09-28 1992-09-28 Door thrust reverser assembly for aircraft engine incorporating a thermal barrier.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9211518A FR2696212B3 (en) 1992-09-28 1992-09-28 Door thrust reverser assembly for aircraft engine incorporating a thermal barrier.

Publications (2)

Publication Number Publication Date
FR2696212A1 FR2696212A1 (en) 1994-04-01
FR2696212B3 true FR2696212B3 (en) 1994-12-02

Family

ID=9433946

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9211518A Expired - Lifetime FR2696212B3 (en) 1992-09-28 1992-09-28 Door thrust reverser assembly for aircraft engine incorporating a thermal barrier.

Country Status (1)

Country Link
FR (1) FR2696212B3 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2764000B1 (en) * 1997-06-03 1999-08-13 Hurel Dubois Avions EJECTION STRUCTURE EQUIPPED WITH A PUSH-INVERTER WITH TWO REAR DOORS AND A FLAT OUTPUT SECTION
US6487845B1 (en) 2001-06-08 2002-12-03 The Nordam Group, Inc. Pivot fairing thrust reverser
US8739515B2 (en) * 2009-11-24 2014-06-03 United Technologies Corporation Variable area fan nozzle cowl airfoil

Also Published As

Publication number Publication date
FR2696212A1 (en) 1994-04-01

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