DE602005008796D1 - Lufteinlass-Struktur für ein Flugzeugtriebwerk - Google Patents
Lufteinlass-Struktur für ein FlugzeugtriebwerkInfo
- Publication number
- DE602005008796D1 DE602005008796D1 DE200560008796 DE602005008796T DE602005008796D1 DE 602005008796 D1 DE602005008796 D1 DE 602005008796D1 DE 200560008796 DE200560008796 DE 200560008796 DE 602005008796 T DE602005008796 T DE 602005008796T DE 602005008796 D1 DE602005008796 D1 DE 602005008796D1
- Authority
- DE
- Germany
- Prior art keywords
- aircraft engine
- air intake
- intake structure
- frame
- end portion
- 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.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
-
- 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
-
- 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
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/07—Inlet and outlet
-
- 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
- Y10T137/00—Fluid handling
- Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Characterised By The Charging Evacuation (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0450612A FR2868123B1 (fr) | 2004-03-29 | 2004-03-29 | Structure d'entree d'air pour moteur d'aeronef |
Publications (1)
Publication Number | Publication Date |
---|---|
DE602005008796D1 true DE602005008796D1 (de) | 2008-09-25 |
Family
ID=34878494
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE200560008796 Active DE602005008796D1 (de) | 2004-03-29 | 2005-03-23 | Lufteinlass-Struktur für ein Flugzeugtriebwerk |
Country Status (6)
Country | Link |
---|---|
US (1) | US7506838B2 (de) |
EP (1) | EP1582701B1 (de) |
AT (1) | ATE404776T1 (de) |
CA (1) | CA2500957C (de) |
DE (1) | DE602005008796D1 (de) |
FR (1) | FR2868123B1 (de) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2868124B1 (fr) * | 2004-03-29 | 2006-06-23 | Airbus France Sas | Structure d'entree d'air pour moteur d'aeronef |
US7721525B2 (en) * | 2006-07-19 | 2010-05-25 | Rohr, Inc. | Aircraft engine inlet having zone of deformation |
FR2904604B1 (fr) * | 2006-08-04 | 2009-02-27 | Airbus France Sas | Element de structure d'un aeronef |
EP2075194B1 (de) * | 2007-12-27 | 2017-08-16 | Techspace Aero | Luft-Öl-Wärmetauscher für ein Turbostrahltriebwerk, zugehöriges Turbostrahltriebwerk und Benutzung dieses Wärmetauschers |
ITMI20080886A1 (it) * | 2008-05-15 | 2009-11-16 | Alenia Aermacchi Spa | Giunto per indurre elevate cadute di temperatura tra parti collegate su un velivolo |
DE102008035823A1 (de) * | 2008-07-31 | 2010-02-25 | Airbus Deutschland Gmbh | Wärmeübertrager für die Außenhaut eines Flugzeugs |
FR2936776A1 (fr) * | 2008-10-08 | 2010-04-09 | Aircelle Sa | Structure d'entree d'air de nacelle |
FR2938238B1 (fr) * | 2008-11-13 | 2010-11-12 | Aircelle Sa | Structure d'entree d'air de nacelle |
US8152461B2 (en) * | 2008-11-19 | 2012-04-10 | Mra Systems, Inc. | Integrated inlet design |
FR2943624B1 (fr) * | 2009-03-27 | 2011-04-15 | Airbus France | Nacelle d'aeronef comportant une paroi exterieure renforcee |
US8197191B2 (en) * | 2009-04-14 | 2012-06-12 | Rohr, Inc. | Inlet section of an aircraft engine nacelle |
GB0907582D0 (en) * | 2009-05-05 | 2009-06-10 | Rolls Royce Plc | A duct wall for a fan of a gas turbine engine |
FR2960856B1 (fr) * | 2010-06-07 | 2012-06-22 | Airbus Operations Sas | Cadre arriere d'une nacelle d'aeronef |
FR2966126B1 (fr) * | 2010-10-15 | 2013-06-28 | Airbus Operations Sas | Nacelle d'aeronef incorporant un cadre arriere incline vers l'arriere |
FR2966128B1 (fr) * | 2010-10-15 | 2013-06-14 | Airbus Operations Sas | Nacelle d'aeronef incorporant une zone de jonction continue entre une paroi exterieure et un cadre avant et/ou un cadre arriere |
FR2976556B1 (fr) * | 2011-06-17 | 2013-12-27 | Airbus Operations Sas | Entree d'air d'une nacelle d'aeronef incorporant une levre renforcee avec un systeme de degivrage par effet joule |
US8887486B2 (en) * | 2011-10-24 | 2014-11-18 | Hamilton Sundstrand Corporation | Ram air fan inlet housing |
US9663238B2 (en) * | 2013-11-11 | 2017-05-30 | The Boeing Company | Nacelle inlet lip skin with pad-up defining a developable surface having parallel ruling lines |
FR3016159B1 (fr) | 2014-01-03 | 2016-01-01 | Airbus Operations Sas | Nacelle de turboreacteur d'aeronef comprenant un ensemble d'entree d'air a rigidite augmentee |
US20160356180A1 (en) * | 2015-06-03 | 2016-12-08 | The Boeing Company | Nacelle inlet having an angle or curved aft bulkhead |
FR3041937B1 (fr) * | 2015-10-05 | 2017-10-20 | Airbus Operations Sas | Structure compartimentee pour le traitement acoustique et le degivrage d'une nacelle d'aeronef et nacelle d'aeronef incorporant ladite structure |
US10189572B2 (en) * | 2016-05-02 | 2019-01-29 | The Boeing Company | Systems and methods for preventing ice formation on portions of an aircraft |
FR3092871B1 (fr) * | 2019-02-15 | 2022-02-25 | Airbus Operations Sas | Procede d’assemblage d’une entree d’air d’un turboreacteur d’aeronef |
FR3115223B1 (fr) * | 2020-10-21 | 2023-05-12 | Safran Nacelles | Fabrication d’une lèvre d’entrée d’air ou d’un secteur annulaire de lèvre d’entrée d’air intégrant des ouvertures à bord rentré |
CN114109536A (zh) * | 2021-11-15 | 2022-03-01 | 江苏迈信林航空科技股份有限公司 | 一种发动机叶轮罩及其加工工艺 |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1427339A (en) * | 1972-11-15 | 1976-03-10 | Rolls Royce | Gas turbine engine |
FR2771776B1 (fr) * | 1997-12-02 | 2000-01-28 | Aerospatiale | Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage |
US6027078A (en) * | 1998-02-27 | 2000-02-22 | The Boeing Company | Method and apparatus using localized heating for laminar flow |
FR2787509B1 (fr) * | 1998-12-21 | 2001-03-30 | Aerospatiale | Structure d'entree d'air pour moteur d'aeronef |
-
2004
- 2004-03-29 FR FR0450612A patent/FR2868123B1/fr not_active Expired - Fee Related
-
2005
- 2005-03-23 DE DE200560008796 patent/DE602005008796D1/de active Active
- 2005-03-23 US US11/086,380 patent/US7506838B2/en not_active Expired - Fee Related
- 2005-03-23 AT AT05102353T patent/ATE404776T1/de not_active IP Right Cessation
- 2005-03-23 EP EP20050102353 patent/EP1582701B1/de not_active Not-in-force
- 2005-03-24 CA CA2500957A patent/CA2500957C/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US7506838B2 (en) | 2009-03-24 |
EP1582701A1 (de) | 2005-10-05 |
FR2868123B1 (fr) | 2006-06-23 |
CA2500957A1 (fr) | 2005-09-29 |
CA2500957C (fr) | 2012-07-31 |
FR2868123A1 (fr) | 2005-09-30 |
US20050269443A1 (en) | 2005-12-08 |
ATE404776T1 (de) | 2008-08-15 |
EP1582701B1 (de) | 2008-08-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
R082 | Change of representative |
Ref document number: 1582701 Country of ref document: EP Representative=s name: HENKEL, BREUER & PARTNER, 80333 MUENCHEN, DE |