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
Links
- 230000004888 barrier function Effects 0.000 title 1
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)
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)
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 |
-
1992
- 1992-09-28 FR FR9211518A patent/FR2696212B3/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
FR2696212A1 (en) | 1994-04-01 |
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