ATE284348T1 - Lufteinlasswirbeldämpfer und eisschutzvorrichtung für hilfstriebwerke - Google Patents
Lufteinlasswirbeldämpfer und eisschutzvorrichtung für hilfstriebwerkeInfo
- Publication number
- ATE284348T1 ATE284348T1 AT01911137T AT01911137T ATE284348T1 AT E284348 T1 ATE284348 T1 AT E284348T1 AT 01911137 T AT01911137 T AT 01911137T AT 01911137 T AT01911137 T AT 01911137T AT E284348 T1 ATE284348 T1 AT E284348T1
- Authority
- AT
- Austria
- Prior art keywords
- door
- intake
- side walls
- air inlet
- protection device
- Prior art date
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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/32—Inducing air flow by fluid jet, e.g. ejector action
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0213—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for auxiliary power units (APU's)
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
- B64D2041/002—Mounting arrangements for auxiliary power units (APU's)
-
- 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
- F05D2220/00—Application
- F05D2220/40—Application in turbochargers
-
- 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
- F05D2260/60—Fluid transfer
- F05D2260/601—Fluid transfer using an ejector or a jet pump
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Air-Flow Control Members (AREA)
- Exhaust Gas After Treatment (AREA)
- Exhaust-Gas Circulating Devices (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Superstructure Of Vehicle (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/514,203 US6264137B1 (en) | 2000-02-25 | 2000-02-25 | Inlet vortex bustor and ice protector for auxiliary power units |
| PCT/US2001/005838 WO2001062592A2 (en) | 2000-02-25 | 2001-02-21 | Inlet vortex bustor and ice protector for auxiliary power units |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE284348T1 true ATE284348T1 (de) | 2004-12-15 |
Family
ID=24046212
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT01911137T ATE284348T1 (de) | 2000-02-25 | 2001-02-21 | Lufteinlasswirbeldämpfer und eisschutzvorrichtung für hilfstriebwerke |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US6264137B1 (de) |
| EP (1) | EP1257468B1 (de) |
| AT (1) | ATE284348T1 (de) |
| CA (1) | CA2401649C (de) |
| DE (1) | DE60107658T2 (de) |
| WO (1) | WO2001062592A2 (de) |
Families Citing this family (66)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6520738B2 (en) | 2001-03-15 | 2003-02-18 | Honeywell International, Inc. | Plenum entry bulk swirl generator |
| US6651929B2 (en) * | 2001-10-29 | 2003-11-25 | Pratt & Whitney Canada Corp. | Passive cooling system for auxiliary power unit installation |
| DE10200459A1 (de) * | 2002-01-09 | 2003-07-24 | Airbus Gmbh | Lufteinlauf für ein Hilfstriebwerk in einem Flugzeug |
| US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
| US6896003B1 (en) * | 2002-11-12 | 2005-05-24 | The United States Of America As Represented By The Secretary Of The Navy | High efficiency low actuation force inlet door |
| US7093666B2 (en) * | 2003-02-20 | 2006-08-22 | Pratt & Whitney Canada Corp. | Apparatus and method for providing fireproofing to an aircraft auxiliary power unit |
| US6883751B2 (en) * | 2003-05-02 | 2005-04-26 | The Boeing Company | Apparatus and method for preventing foreign object damage to an aircraft |
| US7014144B2 (en) * | 2003-07-22 | 2006-03-21 | Honeywell International, Inc. | Dual action inlet door and method for use thereof |
| US7040576B2 (en) * | 2003-12-18 | 2006-05-09 | Pratt & Whitney Canada Corp. | Fire shield apparatus and method |
| US20060061107A1 (en) * | 2004-03-24 | 2006-03-23 | Paul Cadaret | Energy scavenging methods and apparatus |
| US7192462B2 (en) * | 2004-04-14 | 2007-03-20 | Aerospace Filtration Systems, Inc. | Engine air filter and sealing system |
| US7137240B2 (en) * | 2004-08-18 | 2006-11-21 | Hamilton Sundstrand Corporation | Inlet muff anti-icing system for an auxiliary power unit |
| US7364116B2 (en) * | 2004-09-27 | 2008-04-29 | The Boeing Company | Automatic control systems for aircraft auxiliary power units, and associated methods |
| US7790878B2 (en) * | 2004-10-22 | 2010-09-07 | Alnylam Pharmaceuticals, Inc. | RNAi modulation of RSV, PIV and other respiratory viruses and uses thereof |
| US7344107B2 (en) * | 2004-10-26 | 2008-03-18 | The Boeing Company | Dual flow APU inlet and associated systems and methods |
| US7513119B2 (en) * | 2005-02-03 | 2009-04-07 | The Boeing Company | Systems and methods for starting aircraft engines |
| US7600713B2 (en) * | 2005-03-04 | 2009-10-13 | Honeywell International Inc. | Pre-hung inlet door system |
| KR101211541B1 (ko) | 2005-05-04 | 2012-12-12 | 한국항공우주산업 주식회사 | 항공기용 스쿱의 자동개폐 구조 |
| US7540142B2 (en) * | 2006-02-21 | 2009-06-02 | Honeywell International Inc. | Multiple auxiliary power unit system inlet ducts controlled by a single actuator |
| WO2007108787A2 (en) * | 2006-03-13 | 2007-09-27 | Honeywell International Inc. | Pre-hung inlet door system |
| US7600714B2 (en) * | 2006-04-20 | 2009-10-13 | Honeywell International Inc. | Diffusing air inlet door assembly |
| US20080203218A1 (en) * | 2007-02-26 | 2008-08-28 | Honeywell International, Inc. | Systems And Methods For Reducing Pressure Loss Of Air Flowing From A First Area To A Second Area |
| US8657567B2 (en) * | 2007-05-29 | 2014-02-25 | United Technologies Corporation | Nacelle compartment plenum for bleed air flow delivery system |
| US7708230B2 (en) * | 2007-05-29 | 2010-05-04 | United Technologies Corporation | Flow distribution system for inlet flow control |
| DE102008009274B4 (de) * | 2008-02-15 | 2011-06-01 | Airbus Operations Gmbh | System und Verfahren zur Belüftung eines Bereichs, insbesondere eines explosionsgefährdeten Bereichs eines Luftfahrzeugs |
| US8240126B2 (en) * | 2008-03-22 | 2012-08-14 | Pratt & Whitney Rocketdyne, Inc. | Valve system for a gas turbine engine |
| US8141816B2 (en) * | 2008-04-30 | 2012-03-27 | Honeywell International Inc. | AFT inlet duct mounted door actuator |
| DE102008002205A1 (de) * | 2008-06-04 | 2009-12-17 | Airbus Deutschland Gmbh | Lufteinlassventil für ein Flugzeug und Herstellungsverfahren für ein Lufteinlassventil |
| US8079550B2 (en) * | 2008-07-18 | 2011-12-20 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet door actuation mechanism |
| US8113767B2 (en) * | 2008-09-15 | 2012-02-14 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet duct with acoustic silencing |
| US8141818B2 (en) * | 2009-07-02 | 2012-03-27 | Honeywell International Inc. | Ram door assemblies |
| US8657227B1 (en) | 2009-09-11 | 2014-02-25 | The Boeing Company | Independent power generation in aircraft |
| EP2472067B1 (de) * | 2010-12-31 | 2013-09-25 | Techspace Aero S.A. | Einbau eines Oberflächenwärmetauschers mit reguliertem Luftdurchsatz in einen Flugzeugmotor |
| US8738268B2 (en) | 2011-03-10 | 2014-05-27 | The Boeing Company | Vehicle electrical power management and distribution |
| DE102011015126B4 (de) * | 2011-03-25 | 2014-09-25 | Airbus Operations Gmbh | Flugzeugheckbereich mit einem in dem Flugzeugheckbereich installierten Kühlsystem |
| US8444083B2 (en) * | 2011-06-30 | 2013-05-21 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet |
| ES2401015B1 (es) * | 2011-09-29 | 2014-03-13 | Airbus Operations, S.L. | Toma de aire con doble compuerta |
| US9957060B2 (en) * | 2012-03-21 | 2018-05-01 | Hamilton Sundstrand Corporation | Deployable inlet scoop for an inboard ram air turbine |
| EP2743178B1 (de) * | 2012-12-11 | 2016-08-17 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Lufteinlass mit einer Kombination einer Filter- und einer Bypass-Vorrichtung zur Verwendung mit einem Turbomotor |
| CN104118566A (zh) * | 2013-04-24 | 2014-10-29 | 哈尔滨飞机工业集团有限责任公司 | 一种飞机惯性分离器 |
| US9611050B2 (en) | 2013-07-26 | 2017-04-04 | The Boeing Company | Auxiliary power unit inlet apparatus and methods |
| EP3055220B1 (de) * | 2013-10-08 | 2019-05-15 | United Technologies Corporation | Akustisch gesteuertes einlasssystem für eisablenkungshilfsstromeinheit |
| US9145214B2 (en) * | 2013-10-25 | 2015-09-29 | Honeywell International Inc. | Auxiliary power unit inlet door having openings formed therein |
| EP2889466A1 (de) | 2013-12-31 | 2015-07-01 | Rolls-Royce Deutschland Ltd & Co KG | Strömungsführungssystem, Turbomaschine mit einem Strömungsführungssystem und Verfahren zur Herstellung eines Strömungsführungssystems |
| US9719352B2 (en) | 2014-12-17 | 2017-08-01 | Honeywell International Inc. | Compartment based inlet particle separator system |
| PL232261B1 (pl) | 2015-11-02 | 2019-05-31 | Gen Electric | Zespół silnika turbowentylatorowego i układ do zmniejszania rezonansu w komorze |
| US10023296B2 (en) * | 2016-08-09 | 2018-07-17 | Bell Helicopter Textron Inc. | Inlet duct selector for tiltrotor barrier filter |
| US10513344B2 (en) * | 2016-10-14 | 2019-12-24 | Pratt & Whitney Canada Corp. | Auxiliary power unit assembly with removable inlet filter |
| US10508628B2 (en) | 2016-10-14 | 2019-12-17 | Pratt & Whitney Canada Corp. | Auxiliary power unit inlet assembly with particle separator |
| US10508626B2 (en) * | 2016-10-14 | 2019-12-17 | Pratt & Whitney Canada Corp. | Auxiliary power unit inlet assembly with filter |
| US10322621B2 (en) * | 2017-02-15 | 2019-06-18 | Hamilton Sundstrand Corporation | Inertial particle separator for air cycle machine |
| US20180257788A1 (en) * | 2017-03-09 | 2018-09-13 | United Technologies Corporation | Air intake assembly with horizontal door for an aircraft auxiliary power unit |
| US10668486B2 (en) | 2017-07-12 | 2020-06-02 | Hamilton Sundstrand Corporation | Water extractor |
| ES2890374T3 (es) * | 2017-10-30 | 2022-01-18 | Airbus Operations Sl | Cono de cola de aeronave que incorpora una APU con admisión de aire anular |
| US11111024B2 (en) | 2018-01-12 | 2021-09-07 | Honeywell International Inc. | Foldable RAM air inlet filter |
| US10279920B1 (en) * | 2018-02-27 | 2019-05-07 | Brant Farrell | Foreign object debris barrier filter apparatus for an aircraft intake system |
| CN110513162B (zh) | 2018-05-22 | 2022-06-14 | 通用电气公司 | 斗式入口 |
| ES2967158T3 (es) * | 2018-06-22 | 2024-04-26 | Airbus Operations Slu | Sistema de admisión de aire |
| CN109465791B (zh) * | 2018-11-14 | 2020-11-03 | 中国直升机设计研究所 | 一种直升机进气道组件装配型架 |
| CN112960123B (zh) * | 2021-03-26 | 2023-11-07 | 中国商用飞机有限责任公司 | 飞机辅助动力单元的进气门装置 |
| CN113772106B (zh) * | 2021-09-15 | 2024-03-19 | 中国航空工业集团公司西安飞机设计研究所 | 一种组合式辅助动力进气装置 |
| US11999500B2 (en) * | 2021-10-20 | 2024-06-04 | General Electric Company | Deployable inlet assembly for aerial vehicle |
| GB2615834A (en) | 2022-02-15 | 2023-08-23 | Bae Systems Plc | Cavity acoustic tones suppression |
| EP4282765B1 (de) | 2022-05-27 | 2025-07-02 | Airbus Operations, S.L.U. | Hilfstriebwerkssystem eines flugzeugs |
| US12275533B2 (en) | 2023-06-02 | 2025-04-15 | Honeywell International Inc. | Inlet system for auxiliary power unit |
| CN119389442B (zh) * | 2024-12-12 | 2025-04-11 | 江苏晟楠电子科技股份有限公司 | 一种飞机辅助动力系统用的进气门组件 |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2694357A (en) | 1950-07-18 | 1954-11-16 | Chance Vought Aircraft Inc | Boundary layer energization for flush inlets |
| US2695074A (en) | 1951-09-14 | 1954-11-23 | Smith Morris Corp | Retractible screen for jet engines |
| US2944631A (en) * | 1956-01-06 | 1960-07-12 | Rolls Royce | Retractable guards for air intakes |
| US3109610A (en) | 1962-09-12 | 1963-11-05 | Boeing Co | Combined aircraft air intake scoop, foreign material ingestion inhibitor, and aerodynamic flap |
| US3421296A (en) | 1966-11-15 | 1969-01-14 | United Aircraft Corp | Engine inlet air particle separator |
| US3952972A (en) | 1974-12-24 | 1976-04-27 | United Aircraft Of Canada Limited | Inertial separator |
| US4174083A (en) | 1977-04-29 | 1979-11-13 | The Boeing Company | Flow deflector for fluid inlet |
| CA1116418A (en) | 1979-07-18 | 1982-01-19 | Pratt & Whitney Aircraft Of Canada Limited | Vane fairing for inertial separator |
| US4418879A (en) | 1980-12-29 | 1983-12-06 | The Boeing Company | Scoop and inlet for auxiliary power units and method |
| US4397431A (en) | 1981-11-02 | 1983-08-09 | Avco Corporation | Fail-safe, anti-icing system for aircraft engines |
| US4899958A (en) * | 1988-12-05 | 1990-02-13 | Mitsubishi Jukogyo Kabushiki Kaisha | Air intake system of an aircraft |
| US5694763A (en) | 1990-04-11 | 1997-12-09 | United Technologies Corporation | Low observable engine inlet system |
| US5697394A (en) | 1993-03-02 | 1997-12-16 | United Technologies Corporation | Low observable engine air inlet system |
| US5655359A (en) | 1995-05-15 | 1997-08-12 | The Boeing Company | Passive cooling device and method for cooling an auxiliary power unit on an airplane |
-
2000
- 2000-02-25 US US09/514,203 patent/US6264137B1/en not_active Expired - Fee Related
-
2001
- 2001-02-21 WO PCT/US2001/005838 patent/WO2001062592A2/en not_active Ceased
- 2001-02-21 EP EP01911137A patent/EP1257468B1/de not_active Expired - Lifetime
- 2001-02-21 AT AT01911137T patent/ATE284348T1/de not_active IP Right Cessation
- 2001-02-21 CA CA002401649A patent/CA2401649C/en not_active Expired - Fee Related
- 2001-02-21 DE DE60107658T patent/DE60107658T2/de not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| WO2001062592A3 (en) | 2002-03-28 |
| EP1257468B1 (de) | 2004-12-08 |
| CA2401649C (en) | 2007-05-15 |
| WO2001062592A2 (en) | 2001-08-30 |
| US6264137B1 (en) | 2001-07-24 |
| CA2401649A1 (en) | 2001-08-30 |
| DE60107658D1 (de) | 2005-01-13 |
| DE60107658T2 (de) | 2006-03-16 |
| EP1257468A2 (de) | 2002-11-20 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |