BRPI0412795A - conjunto de porta de entrada para redução de barulho a partir de uma unidade de força auxiliar(ufa) compreendida dentro de uma aeronave - Google Patents
conjunto de porta de entrada para redução de barulho a partir de uma unidade de força auxiliar(ufa) compreendida dentro de uma aeronaveInfo
- Publication number
- BRPI0412795A BRPI0412795A BRPI0412795-1A BRPI0412795A BRPI0412795A BR PI0412795 A BRPI0412795 A BR PI0412795A BR PI0412795 A BRPI0412795 A BR PI0412795A BR PI0412795 A BRPI0412795 A BR PI0412795A
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- apu
- door
- noise
- noise reduction
- 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
- 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
-
- 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
-
- 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
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
-
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
- F05D2220/50—Application 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
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
Landscapes
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)
- Main Body Construction Of Washing Machines And Laundry Dryers (AREA)
- Air-Conditioning For Vehicles (AREA)
- Motor Or Generator Frames (AREA)
- Air-Flow Control Members (AREA)
- Shielding Devices Or Components To Electric Or Magnetic Fields (AREA)
Abstract
"CONJUNTO DA PORTA DE ENTRADA PARA REDUZIR RUìDO DE UMA UNIDADE DE FORçA AUXILIAR (APU) CONTIDO DENTRO DE UMA AERONAVE". é fornecido um conjunto de porta de entrada e processo para redução de ruído a partir de uma unidade de força auxiliar (APU) contida dentro de um alojamento de aeronave. O conjunto de entrada inclui um duto de entrada, e uma porta. O duto de entrada é configurado, para se estender da unidade de força auxiliar ao alojamento de aeronave, e possui uma parede lateral que define uma passagem de fluxo, pela qual o ruído da APU se propaga. O atuador é disposto, pelo menos parcialmente, dentro do duto de entrada. A porta é acoplada ao atuador. O atuador é ainda configurado para girar seletivamente a porta entre pelo menos uma primeira posição, onde pelo menos uma parte da porta deflete o ruído da APU em uma primeira posição, e uma segunda posição, onde pelo menos uma parte da porta deflete o ruído da APU em uma segunda posição.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US48941203P | 2003-07-22 | 2003-07-22 | |
| US10/789,827 US7014144B2 (en) | 2003-07-22 | 2004-02-27 | Dual action inlet door and method for use thereof |
| PCT/US2004/023220 WO2005016748A2 (en) | 2003-07-22 | 2004-07-19 | Dual action inlet door and method for use thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI0412795A true BRPI0412795A (pt) | 2006-09-26 |
Family
ID=34197895
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI0412795-1A BRPI0412795A (pt) | 2003-07-22 | 2004-07-19 | conjunto de porta de entrada para redução de barulho a partir de uma unidade de força auxiliar(ufa) compreendida dentro de uma aeronave |
Country Status (6)
| Country | Link |
|---|---|
| US (4) | US7014144B2 (pt) |
| EP (1) | EP1646560B1 (pt) |
| BR (1) | BRPI0412795A (pt) |
| CA (1) | CA2533394C (pt) |
| DE (1) | DE602004005202T2 (pt) |
| WO (1) | WO2005016748A2 (pt) |
Families Citing this family (94)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7210653B2 (en) * | 2002-10-22 | 2007-05-01 | The Boeing Company | Electric-based secondary power system architectures for aircraft |
| US7150431B2 (en) * | 2004-01-14 | 2006-12-19 | Mjd Innovations, L.L.C. | Electrical generator fluid-flow-coolant filtration |
| US20060061107A1 (en) * | 2004-03-24 | 2006-03-23 | Paul Cadaret | Energy scavenging methods and apparatus |
| US20060032974A1 (en) * | 2004-08-16 | 2006-02-16 | Honeywell International Inc. | Modular installation kit for 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 |
| 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 |
| US7469545B2 (en) | 2005-09-27 | 2008-12-30 | Honeywell International Inc. | Auxiliary power unit inlet door position control system and method |
| DE102005053696B4 (de) * | 2005-11-10 | 2009-05-14 | Airbus Deutschland Gmbh | Notfall-Staulufteinlassklappe eines Flugzeuges |
| GB0523570D0 (en) * | 2005-11-18 | 2005-12-28 | Airbus Uk Ltd | Aircraft cooling duct |
| US7540142B2 (en) * | 2006-02-21 | 2009-06-02 | Honeywell International Inc. | Multiple auxiliary power unit system inlet ducts controlled by a single actuator |
| US7721989B2 (en) * | 2006-03-01 | 2010-05-25 | The Boeing Company | Multi-path inlet for aircraft engine |
| WO2007108787A2 (en) * | 2006-03-13 | 2007-09-27 | Honeywell International Inc. | Pre-hung inlet door system |
| CA2581827C (en) * | 2006-03-16 | 2014-05-27 | Hamilton Sundstrand Corporation | Low noise exhaust ducting system |
| ATE478800T1 (de) * | 2006-03-17 | 2010-09-15 | Honeywell Int Inc | Einlasstür |
| US7600714B2 (en) * | 2006-04-20 | 2009-10-13 | Honeywell International Inc. | Diffusing air inlet door assembly |
| EP2040818A2 (en) * | 2006-07-14 | 2009-04-01 | Aerospace Filtration Systems, Inc. | Aircraft engine inlet pivotable barrier filter |
| US7765784B2 (en) * | 2006-09-25 | 2010-08-03 | The Boeing Company | Thermally compliant APU exhaust duct arrangements and associated systems and methods |
| US7624944B2 (en) * | 2006-10-26 | 2009-12-01 | The Boeing Company | Tandem air inlet apparatus and method for an airborne mobile platform |
| US7861968B2 (en) | 2006-10-26 | 2011-01-04 | The Boeing Company | Air inlet and method for a highspeed mobile platform |
| US7618006B2 (en) * | 2006-11-13 | 2009-11-17 | The Boeing Company | Ram air inlets for use with aircraft environmental control systems and other aircraft and non-aircraft systems |
| FR2915461B1 (fr) * | 2007-04-24 | 2009-06-05 | Airbus France Sas | Agencement d'entree d'air pour vehicule, notamment un aeronef. |
| US7849702B2 (en) * | 2007-06-20 | 2010-12-14 | The Boeing Company | Combined cabin air and heat exchanger RAM air inlets for aircraft environmental control systems, and associated methods of use |
| US9194293B2 (en) * | 2007-09-18 | 2015-11-24 | Hamilton Sundstrand Corporation | Air inlet noise attenuation assembly |
| US8096498B2 (en) * | 2007-12-12 | 2012-01-17 | Hamilton Sundstrand Corporation | Rotating auxiliary power unit air inlet door |
| DE102007061588B4 (de) * | 2007-12-20 | 2011-07-21 | Airbus Operations GmbH, 21129 | Flugzeugkühlsystem |
| US8167540B2 (en) * | 2008-01-30 | 2012-05-01 | Hamilton Sundstrand Corporation | System for reducing compressor noise |
| ITTO20080142A1 (it) * | 2008-02-28 | 2009-08-29 | Alenia Aeronautica Spa | Presa d'aria, in particolare per un espulsore di chaff per velivolo |
| FR2928137B1 (fr) * | 2008-02-29 | 2010-08-20 | Airbus France | Systeme de propulsion arriere d'avion fixe par poutres et avion comportant un tel systeme. |
| FR2928135B1 (fr) * | 2008-02-29 | 2010-09-03 | Airbus France | Systeme de propulsion arriere d'avion a entrees d'air laterales escamotables et avion comportant un tel systeme. |
| US8141816B2 (en) * | 2008-04-30 | 2012-03-27 | Honeywell International Inc. | AFT inlet duct mounted door actuator |
| DE102008026117A1 (de) * | 2008-05-30 | 2009-12-10 | Airbus Deutschland Gmbh | Frischlufteinlass für ein Flugzeug |
| 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 |
| DE102008030399B4 (de) * | 2008-06-26 | 2019-03-21 | Airbus Operations Gmbh | Luftkanal zur Umgebungsluftzufuhr in einem Flugzeug |
| DE102008040184A1 (de) * | 2008-07-04 | 2010-01-14 | Airbus Deutschland Gmbh | Verfahren zum Steuern eines Innendrucks in einem Luftfahrzeug |
| US8079550B2 (en) * | 2008-07-18 | 2011-12-20 | Hamilton Sundstrand Corporation | Auxiliary power unit inlet door actuation mechanism |
| DE102008058451B4 (de) * | 2008-11-21 | 2010-11-18 | Airbus Deutschland Gmbh | Verfahren und System zur Notbelüftung einer Flugzeugkabine im Fall eines Lecks im Bereich eines Luftmischers |
| US8128037B2 (en) | 2009-01-19 | 2012-03-06 | The Boeing Company | Apparatus and method for passive purging of micro-perforated aerodynamic surfaces |
| US8245976B2 (en) * | 2009-01-19 | 2012-08-21 | The Boeing Company | Door assembly for laminar flow control system |
| DE102009010243A1 (de) * | 2009-02-24 | 2010-09-02 | Airbus Deutschland Gmbh | Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung |
| US8322981B2 (en) * | 2009-03-02 | 2012-12-04 | Hamilton Sundstrand Corporation | Aircraft fluid diversion inlet louver |
| US8201535B2 (en) * | 2009-03-04 | 2012-06-19 | Honda Motor Company, Ltd. | Air intake device |
| US8172511B2 (en) * | 2009-05-04 | 2012-05-08 | Hamilton Sunstrand Corporation | Radial compressor with blades decoupled and tuned at anti-nodes |
| US8172510B2 (en) * | 2009-05-04 | 2012-05-08 | Hamilton Sundstrand Corporation | Radial compressor of asymmetric cyclic sector with coupled blades tuned at anti-nodes |
| US8657227B1 (en) | 2009-09-11 | 2014-02-25 | The Boeing Company | Independent power generation in aircraft |
| DE102011011879A1 (de) * | 2011-02-21 | 2012-08-23 | Airbus Operations Gmbh | Kühllufteinlass, Triebwerkzapfluftsystem und Verfahren zum Betreiben eines Kühllufteinlasses |
| US8738268B2 (en) | 2011-03-10 | 2014-05-27 | The Boeing Company | Vehicle electrical power management and distribution |
| US8636051B2 (en) * | 2011-03-11 | 2014-01-28 | Raytheon Company | Free air stream heat exchanger design |
| ES2401015B1 (es) * | 2011-09-29 | 2014-03-13 | Airbus Operations, S.L. | Toma de aire con doble compuerta |
| US9045998B2 (en) | 2011-12-12 | 2015-06-02 | Honeywell International Inc. | System for directing air flow to a plurality of plena |
| US9051057B2 (en) * | 2011-12-28 | 2015-06-09 | Embraer S.A. | Aircraft air inlet diverter assemblies with improved aerodynamic characteristics |
| US9957060B2 (en) * | 2012-03-21 | 2018-05-01 | Hamilton Sundstrand Corporation | Deployable inlet scoop for an inboard ram air turbine |
| US9267390B2 (en) | 2012-03-22 | 2016-02-23 | Honeywell International Inc. | Bi-metallic actuator for selectively controlling air flow between plena in a gas turbine engine |
| EP2743178B1 (en) * | 2012-12-11 | 2016-08-17 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | An air inlet combining a filter and a bypass device for use with a turbine engine |
| US9593696B2 (en) | 2013-02-27 | 2017-03-14 | Woodward, Inc. | Rotary piston type actuator with hydraulic supply |
| US9476434B2 (en) | 2013-02-27 | 2016-10-25 | Woodward, Inc. | Rotary piston type actuator with modular housing |
| US9816537B2 (en) | 2013-02-27 | 2017-11-14 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US8955425B2 (en) | 2013-02-27 | 2015-02-17 | Woodward, Inc. | Rotary piston type actuator with pin retention features |
| US9631645B2 (en) | 2013-02-27 | 2017-04-25 | Woodward, Inc. | Rotary piston actuator anti-rotation configurations |
| US9234535B2 (en) | 2013-02-27 | 2016-01-12 | Woodward, Inc. | Rotary piston type actuator |
| US9163648B2 (en) | 2013-02-27 | 2015-10-20 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| US9487288B2 (en) | 2013-06-04 | 2016-11-08 | The Boeing Company | Apparatus and methods for extending hybrid laminar flow control |
| US9193436B2 (en) * | 2013-07-03 | 2015-11-24 | The Boeing Company | Flow control structure and associated method for controlling attachment with a control surface |
| US9611050B2 (en) | 2013-07-26 | 2017-04-04 | The Boeing Company | Auxiliary power unit inlet apparatus and methods |
| WO2015054334A1 (en) * | 2013-10-08 | 2015-04-16 | United Technologies Corporation | Acoustic controlled ice deflecting auxiliary power unit inlet system |
| EP2889466A1 (en) * | 2013-12-31 | 2015-07-01 | Rolls-Royce Deutschland Ltd & Co KG | Flow guiding system, turbo engine with a flow guiding system and method for manufacturing a flow guiding system |
| US9630723B2 (en) * | 2014-06-06 | 2017-04-25 | United Technologies Corporation | Acoustically diffusive auxilary power unit inlet doors |
| 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 |
| US9783306B2 (en) | 2015-10-13 | 2017-10-10 | Honeywell International Inc. | Bi-fold thrust recovery outflow valve with a ram air flap |
| US9840334B2 (en) * | 2015-12-21 | 2017-12-12 | Gulfstream Aerospace Corporation | Auxiliary power unit inlet duct assembly for mitigating noise |
| EP3184436A1 (en) * | 2015-12-23 | 2017-06-28 | Airbus Operations, S.L. | Door system for an exhaust gas duct of an auxiliary power unit of an aircraft |
| FR3055128A1 (fr) * | 2016-08-17 | 2018-02-23 | Zodiac Seats France | Agencement de sieges permettant d'augmenter l'intimite des passagers, notamment d'un avion |
| US10953997B2 (en) * | 2016-10-05 | 2021-03-23 | Safran Power Units | Translatable scoop for auxiliary power units air intake |
| US10465711B2 (en) * | 2016-10-18 | 2019-11-05 | The Boeing Company | Apparatus and methods to deploy a fluid flow channel |
| ES2897771T3 (es) * | 2017-02-08 | 2022-03-02 | Airbus Operations Sl | Sistema de apertura y cierre de seguridad para puertas de aeronaves |
| US20180257788A1 (en) * | 2017-03-09 | 2018-09-13 | United Technologies Corporation | Air intake assembly with horizontal door for an aircraft auxiliary power unit |
| US10309291B2 (en) | 2017-09-22 | 2019-06-04 | Denso International America, Inc. | Flapper door air guide |
| 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 |
| EP3746362B1 (en) * | 2018-01-31 | 2024-03-06 | Airbus Operations GmbH | Airfoil for flow control |
| FR3077777B1 (fr) * | 2018-02-13 | 2021-07-16 | Liebherr Aerospace Toulouse Sas | Bouche de prelevement d'air dynamique, dispositif de controle environnemental, moteur et vehicule equipes d'une telle bouche |
| 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 |
| ES2732306B2 (es) * | 2018-05-21 | 2021-06-18 | Alestis Aerospace S L | Metodo de fabricacion de un cono de cola |
| EP3581435B1 (en) * | 2018-06-13 | 2021-03-17 | Thule Sweden AB | Vehicle carrier box |
| ES2967158T3 (es) * | 2018-06-22 | 2024-04-26 | Airbus Operations Slu | Sistema de admisión de aire |
| US10960744B1 (en) * | 2018-11-19 | 2021-03-30 | Zoox, Inc. | Multi-directional vehicle roof cover system |
| US11199248B2 (en) | 2019-04-30 | 2021-12-14 | Woodward, Inc. | Compact linear to rotary actuator |
| US12179934B2 (en) | 2019-05-06 | 2024-12-31 | The Boeing Company | Method and apparatus for auxiliary power unit installation |
| WO2021207482A1 (en) | 2020-04-08 | 2021-10-14 | Woodward, Inc. | Rotary piston type actuator with a central actuation assembly |
| FR3117149B1 (fr) | 2020-12-03 | 2022-10-21 | Safran Aircraft Engines | Ecope pour une turbomachine d’aeronef |
| US11999500B2 (en) | 2021-10-20 | 2024-06-04 | General Electric Company | Deployable inlet assembly for aerial vehicle |
| EP4292924A1 (en) * | 2022-06-15 | 2023-12-20 | Airbus Operations GmbH | Sealing device for covering an aperture in a wing part |
| US12012217B2 (en) * | 2022-08-22 | 2024-06-18 | Gulfstream Aerospace Corporation | Auxiliary power unit air inlet door with specified acoustic reflecting and/or diffusing characteristics |
| US12275533B2 (en) * | 2023-06-02 | 2025-04-15 | Honeywell International Inc. | Inlet system for auxiliary power unit |
Family Cites Families (35)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2695074A (en) | 1951-09-14 | 1954-11-23 | Smith Morris Corp | Retractible screen for jet engines |
| US2947533A (en) * | 1954-12-13 | 1960-08-02 | Blackburn Group Ltd | Doors or closure members for bomb bays or like spaces in the fuselages or wings of aircraft |
| US2944631A (en) | 1956-01-06 | 1960-07-12 | Rolls Royce | Retractable guards for air intakes |
| US3232333A (en) * | 1963-03-28 | 1966-02-01 | Guy E Dixon | Foldable door with hollow double hinge |
| SE330335B (pt) * | 1967-04-20 | 1970-11-09 | Starfoenster Ab | |
| GB1212875A (en) * | 1967-12-21 | 1970-11-18 | Rolls Royce | Aircraft |
| GB1347690A (en) * | 1970-10-10 | 1974-02-27 | British Aircraft Corp Ltd | Doors |
| 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 |
| CA1116418A (en) | 1979-07-18 | 1982-01-19 | Pratt & Whitney Aircraft Of Canada Limited | Vane fairing for inertial separator |
| US4304094A (en) | 1979-11-16 | 1981-12-08 | United Technologies Corp. | Engine air particle separator for use with gas turbine engine |
| US4418879A (en) | 1980-12-29 | 1983-12-06 | The Boeing Company | Scoop and inlet for auxiliary power units and method |
| US4474344A (en) * | 1981-03-25 | 1984-10-02 | The Boeing Company | Compression-sealed nacelle inlet door assembly |
| US4397431A (en) | 1981-11-02 | 1983-08-09 | Avco Corporation | Fail-safe, anti-icing system for aircraft engines |
| 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 |
| 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 |
| DE4134499C2 (de) * | 1991-10-18 | 1994-09-22 | Deutsche Aerospace Airbus | Klappe zum Schließen einer Beladeöffnung |
| US5697394A (en) | 1993-03-02 | 1997-12-16 | United Technologies Corporation | Low observable engine air inlet system |
| DE9314977U1 (de) * | 1993-10-02 | 1993-11-25 | Huwil-Werke GmbH Möbelschloß- und Beschlagfabriken, 53809 Ruppichteroth | Stütze zum Halten eines Verschlußelementes |
| 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 |
| US6094907A (en) | 1996-06-05 | 2000-08-01 | The Boeing Company | Jet engine and method for reducing jet engine noise by reducing nacelle boundary layer thickness |
| US6106228A (en) | 1996-09-06 | 2000-08-22 | Siemens Electric Limited | Fan shroud air door assembly |
| FR2763098B1 (fr) | 1997-05-07 | 1999-06-11 | Snecma | Systeme d'admission d'air dans une veine de turbomachine |
| 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 |
| US6565035B1 (en) | 1999-11-11 | 2003-05-20 | The Boeing Company | Apparatus and method for forming an air curtain for use with an aircraft |
| US6257523B1 (en) * | 1999-12-09 | 2001-07-10 | The Boeing Company | Foldable partition with integral door |
| US6347484B1 (en) * | 2000-02-22 | 2002-02-19 | Specialty Manufacturing Co., Inc. | Ventilation unit for vehicles |
| 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 |
| US6634597B2 (en) * | 2002-01-11 | 2003-10-21 | The Boeing Company | Method and apparatus for controlling aircraft airflow |
| US7040576B2 (en) * | 2003-12-18 | 2006-05-09 | Pratt & Whitney Canada Corp. | Fire shield apparatus and method |
-
2004
- 2004-02-27 US US10/789,827 patent/US7014144B2/en not_active Expired - Fee Related
- 2004-07-19 DE DE602004005202T patent/DE602004005202T2/de not_active Expired - Lifetime
- 2004-07-19 CA CA2533394A patent/CA2533394C/en not_active Expired - Fee Related
- 2004-07-19 BR BRPI0412795-1A patent/BRPI0412795A/pt not_active Application Discontinuation
- 2004-07-19 WO PCT/US2004/023220 patent/WO2005016748A2/en not_active Ceased
- 2004-07-19 EP EP04786085A patent/EP1646560B1/en not_active Expired - Lifetime
-
2005
- 2005-12-08 US US11/299,116 patent/US7210652B2/en not_active Expired - Fee Related
- 2005-12-08 US US11/299,147 patent/US7461814B2/en not_active Expired - Fee Related
-
2007
- 2007-03-27 US US11/691,679 patent/US7665694B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| US7665694B2 (en) | 2010-02-23 |
| EP1646560B1 (en) | 2007-03-07 |
| WO2005016748A2 (en) | 2005-02-24 |
| US20060102781A1 (en) | 2006-05-18 |
| US7210652B2 (en) | 2007-05-01 |
| CA2533394C (en) | 2011-11-29 |
| US20090065297A1 (en) | 2009-03-12 |
| US7461814B2 (en) | 2008-12-09 |
| US7014144B2 (en) | 2006-03-21 |
| US20050224635A1 (en) | 2005-10-13 |
| WO2005016748A3 (en) | 2006-03-23 |
| DE602004005202T2 (de) | 2007-11-22 |
| CA2533394A1 (en) | 2005-02-24 |
| EP1646560A2 (en) | 2006-04-19 |
| DE602004005202D1 (de) | 2007-04-19 |
| US20060102776A1 (en) | 2006-05-18 |
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| B11A | Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing | ||
| B11Y | Definitive dismissal - extension of time limit for request of examination expired [chapter 11.1.1 patent gazette] |