DE3177189D1 - Ablenkplatte und einlass fuer hilfskrafteinheit. - Google Patents
Ablenkplatte und einlass fuer hilfskrafteinheit.Info
- Publication number
- DE3177189D1 DE3177189D1 DE8282900434T DE3177189T DE3177189D1 DE 3177189 D1 DE3177189 D1 DE 3177189D1 DE 8282900434 T DE8282900434 T DE 8282900434T DE 3177189 T DE3177189 T DE 3177189T DE 3177189 D1 DE3177189 D1 DE 3177189D1
- Authority
- DE
- Germany
- Prior art keywords
- deflector
- inlet
- auxiliary unit
- auxiliary
- unit
- 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
Links
Classifications
-
- 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0213—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for auxiliary power units (APU's)
-
- 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)
- Aviation & Aerospace Engineering (AREA)
- Mobile Radio Communication Systems (AREA)
- Body Structure For Vehicles (AREA)
- Seal Device For Vehicle (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/220,515 US4418879A (en) | 1980-12-29 | 1980-12-29 | Scoop and inlet for auxiliary power units and method |
PCT/US1981/001667 WO1982002181A1 (en) | 1980-12-29 | 1981-12-14 | Auxiliary power unit scoop and inlet |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3177189D1 true DE3177189D1 (de) | 1990-07-12 |
Family
ID=22823846
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8282900434T Expired - Fee Related DE3177189D1 (de) | 1980-12-29 | 1981-12-14 | Ablenkplatte und einlass fuer hilfskrafteinheit. |
Country Status (4)
Country | Link |
---|---|
US (1) | US4418879A (de) |
EP (1) | EP0067847B1 (de) |
DE (1) | DE3177189D1 (de) |
WO (1) | WO1982002181A1 (de) |
Families Citing this family (55)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3407137A1 (de) * | 1984-02-28 | 1985-08-29 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Einrichtung zur verbesserung der stroemungsverhaeltnisse am lufteinlauf fuer in flugzeugen eingebaute gasturbinentriebwerke |
DE4008951A1 (de) * | 1990-03-20 | 1991-09-26 | Messerschmitt Boelkow Blohm | Einlauframpe fuer ueber- oder hyperschallflugzeuge |
DE4008956A1 (de) * | 1990-03-20 | 1991-09-26 | Messerschmitt Boelkow Blohm | Einlaufsystem fuer ueber- oder hyperschallflugzeuge |
US5490644A (en) * | 1993-12-20 | 1996-02-13 | The Boeing Company | Ducted boundary layer diverter |
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 |
FR2763098B1 (fr) * | 1997-05-07 | 1999-06-11 | Snecma | Systeme d'admission d'air dans une veine de turbomachine |
US6050527A (en) * | 1997-12-19 | 2000-04-18 | The Boeing Company | Flow control device to eliminate cavity resonance |
US6142417A (en) * | 1998-10-26 | 2000-11-07 | Atlantic Research Corporation | Self-deploying air inlet for an air breathing missile |
US6272838B1 (en) * | 1999-02-25 | 2001-08-14 | Alliedsignal, Inc. | Method and apparatus for controlling the inlet duct leading to an auxiliary power unit |
US6247668B1 (en) | 1999-07-15 | 2001-06-19 | The Boeing Company | Auxiliary power and thrust unit |
US6264137B1 (en) | 2000-02-25 | 2001-07-24 | Honeywell International Inc. | Inlet vortex bustor and ice protector for auxiliary power units |
US6349899B1 (en) | 2000-04-04 | 2002-02-26 | The Boeing Company | Aircraft auxiliary air intake with ram and flush opening door |
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 |
US6634597B2 (en) * | 2002-01-11 | 2003-10-21 | The Boeing Company | Method and apparatus for controlling aircraft airflow |
US7210653B2 (en) | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
US7093666B2 (en) * | 2003-02-20 | 2006-08-22 | Pratt & Whitney Canada Corp. | Apparatus and method for providing fireproofing to an aircraft auxiliary power unit |
GB0313456D0 (en) * | 2003-06-11 | 2003-07-16 | Rolls Royce Plc | Propulsion arrangement |
US7014144B2 (en) | 2003-07-22 | 2006-03-21 | Honeywell International, Inc. | Dual action inlet door and method for use thereof |
DE10335482B4 (de) | 2003-08-02 | 2008-04-03 | Airbus Deutschland Gmbh | Staulufteinlass eines Flugzeuges |
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 |
US7364116B2 (en) * | 2004-09-27 | 2008-04-29 | The Boeing Company | Automatic control systems for aircraft auxiliary power units, and associated methods |
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 |
US7540142B2 (en) * | 2006-02-21 | 2009-06-02 | Honeywell International Inc. | Multiple auxiliary power unit system inlet ducts controlled by a single actuator |
US7600714B2 (en) * | 2006-04-20 | 2009-10-13 | Honeywell International Inc. | Diffusing air inlet door assembly |
FR2915461B1 (fr) * | 2007-04-24 | 2009-06-05 | Airbus France Sas | Agencement d'entree d'air pour vehicule, notamment un aeronef. |
US8480460B2 (en) * | 2007-10-01 | 2013-07-09 | United Technologies Corporation | Cabin air supercharged aircraft internal combustion engine |
US8141816B2 (en) * | 2008-04-30 | 2012-03-27 | Honeywell International Inc. | AFT inlet duct mounted door actuator |
DE102008028799B4 (de) | 2008-06-17 | 2015-07-02 | Airbus Operations Gmbh | Druckausgleichs-Ventil zum Anordnen an einer Öffnung einer Rumpfschale eines Flugzeugs und Rumpfteil mit einem solchen Druckausgleichs-Ventil |
US8079550B2 (en) * | 2008-07-18 | 2011-12-20 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet door actuation mechanism |
US8245976B2 (en) | 2009-01-19 | 2012-08-21 | The Boeing Company | Door assembly for laminar flow control system |
US8128037B2 (en) * | 2009-01-19 | 2012-03-06 | The Boeing Company | Apparatus and method for passive purging of micro-perforated aerodynamic surfaces |
DE102009010243A1 (de) * | 2009-02-24 | 2010-09-02 | Airbus Deutschland Gmbh | Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung |
US8201535B2 (en) * | 2009-03-04 | 2012-06-19 | Honda Motor Company, Ltd. | Air intake device |
US8657227B1 (en) | 2009-09-11 | 2014-02-25 | The Boeing Company | Independent power generation in aircraft |
US8738268B2 (en) | 2011-03-10 | 2014-05-27 | The Boeing Company | Vehicle electrical power management and distribution |
FR2982588B1 (fr) * | 2011-11-10 | 2013-11-22 | Aircelle Sa | Panneau composite a ecope de prelevement integree |
US9957060B2 (en) * | 2012-03-21 | 2018-05-01 | Hamilton Sundstrand Corporation | Deployable inlet scoop for an inboard ram air turbine |
US9487288B2 (en) | 2013-06-04 | 2016-11-08 | The Boeing Company | Apparatus and methods for extending hybrid laminar flow control |
US9611050B2 (en) | 2013-07-26 | 2017-04-04 | The Boeing Company | Auxiliary power unit inlet apparatus and methods |
US9630723B2 (en) * | 2014-06-06 | 2017-04-25 | United Technologies Corporation | Acoustically diffusive auxilary power unit inlet doors |
DE102014217830A1 (de) * | 2014-09-05 | 2016-03-10 | Rolls-Royce Deutschland Ltd & Co Kg | Luftleitvorrichtung und Turbomaschine mit Luftleitvorrichtung |
FR3028289B1 (fr) * | 2014-11-06 | 2019-12-27 | Airbus Operations (S.A.S.) | Turbomachine d'aeronef comprenant un boitier d'admission d'air a profil aerodynamique variable |
US20180257788A1 (en) * | 2017-03-09 | 2018-09-13 | United Technologies Corporation | Air intake assembly with horizontal door for an aircraft auxiliary power unit |
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 |
CN111670141A (zh) * | 2018-01-31 | 2020-09-15 | 空中客车德国运营有限责任公司 | 用于流动控制的翼型件 |
US11124310B2 (en) | 2018-04-10 | 2021-09-21 | DMS Aviation Services, LLC | Pressure recovery device for an aircraft engine air intake |
US10266275B1 (en) * | 2018-04-10 | 2019-04-23 | DMS Aviation Services, LLC | Pressure recovery device for an aircraft engine air intake |
FR3080889B1 (fr) * | 2018-05-03 | 2020-08-07 | Airbus Operations Sas | Ensemble propulsif pour aeronef comprenant un dispositif de prise d'air froid a profil aerodynamique variable |
EP3587273B1 (de) * | 2018-06-22 | 2023-10-11 | Airbus Operations, S.L.U. | Lufteinlasssystem |
US11486306B2 (en) | 2020-06-18 | 2022-11-01 | The Boeing Company | Flush fluid inlet designs for aero-acoustic tone mitigation of aircraft |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR868609A (fr) * | 1939-10-13 | 1942-01-09 | B M W Flugmotorenbau G M B H | Dispositif pour influencer les conditions aérodynamiques sur le côté de courant d'impact de corps munis d'un revêtement, notamment de groupes propulseurs d'aéronefs |
US2477637A (en) * | 1941-11-14 | 1949-08-02 | Mercier Pierre Ernest | Aircraft |
NL73561C (de) * | 1947-04-22 | 1953-06-15 | ||
US2650752A (en) * | 1949-08-27 | 1953-09-01 | United Aircraft Corp | Boundary layer control in blowers |
US3027711A (en) * | 1950-02-07 | 1962-04-03 | Randolph S Rae | Scoop diffuser for use on ram jets for securing isentropic compression of a supersonic stream |
US2812980A (en) * | 1950-06-16 | 1957-11-12 | Snecma | Jet deflecting device |
US2694357A (en) * | 1950-07-18 | 1954-11-16 | Chance Vought Aircraft Inc | Boundary layer energization for flush inlets |
US3001740A (en) * | 1959-06-23 | 1961-09-26 | Short Brothers & Harland Ltd | Aeroplane with vertical lift engine intake structure |
US3099423A (en) * | 1961-10-02 | 1963-07-30 | Rolls Royce | Vtol aircraft engine inlet structure |
BE631638A (de) * | 1962-06-06 | 1900-01-01 | ||
US3109610A (en) * | 1962-09-12 | 1963-11-05 | Boeing Co | Combined aircraft air intake scoop, foreign material ingestion inhibitor, and aerodynamic flap |
US3129910A (en) * | 1962-12-18 | 1964-04-21 | Robert D Smith | Aircraft air scoop for inflatable air blanket safety equipment |
GB1026996A (en) * | 1964-08-05 | 1966-04-20 | Rolls Royce | Supersonic intake for a jet propulsion engine |
US3347496A (en) * | 1966-05-03 | 1967-10-17 | Ryan Aeronautical Co | Engine air inlet system for supersonic v/stol aircraft |
US3613704A (en) * | 1967-02-14 | 1971-10-19 | Technology Uk | Aircraft engine intake structures |
GB1212875A (en) * | 1967-12-21 | 1970-11-18 | Rolls Royce | Aircraft |
US3599429A (en) * | 1969-05-02 | 1971-08-17 | Boeing Co | Vortex preventing method and apparatus for aircraft jet engines |
US3659424A (en) * | 1970-10-07 | 1972-05-02 | Us Navy | Stowable air scoop |
US3717163A (en) * | 1970-10-08 | 1973-02-20 | Cci Aerospace Corp | Precompression shroud for inlets |
GB1452267A (en) * | 1972-10-14 | 1976-10-13 | Rolls Royce | Jet propulsion powerplant frames |
US3915413A (en) * | 1974-03-25 | 1975-10-28 | Gen Electric | Variable air inlet system for a gas turbine engine |
US4174083A (en) * | 1977-04-29 | 1979-11-13 | The Boeing Company | Flow deflector for fluid inlet |
US4121606A (en) * | 1977-10-25 | 1978-10-24 | General Dynamics Corporation | Inflatable air inlet duct |
US4203566A (en) * | 1978-08-21 | 1980-05-20 | United Aircraft Products, Inc. | Air inlet control for aircraft or the like |
-
1980
- 1980-12-29 US US06/220,515 patent/US4418879A/en not_active Expired - Lifetime
-
1981
- 1981-12-14 EP EP82900434A patent/EP0067847B1/de not_active Expired - Lifetime
- 1981-12-14 WO PCT/US1981/001667 patent/WO1982002181A1/en active IP Right Grant
- 1981-12-14 DE DE8282900434T patent/DE3177189D1/de not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US4418879A (en) | 1983-12-06 |
WO1982002181A1 (en) | 1982-07-08 |
EP0067847A1 (de) | 1982-12-29 |
EP0067847B1 (de) | 1990-06-06 |
EP0067847A4 (de) | 1984-04-06 |
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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 |