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
Application number
DE8282900434T
Other languages
English (en)
Inventor
Siebold Vanderleest
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE3177189D1 publication Critical patent/DE3177189D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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)
DE8282900434T 1980-12-29 1981-12-14 Ablenkplatte und einlass fuer hilfskrafteinheit. Expired - Fee Related DE3177189D1 (de)

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)

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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
DE4008956A1 (de) * 1990-03-20 1991-09-26 Messerschmitt Boelkow Blohm Einlaufsystem fuer ueber- oder hyperschallflugzeuge
DE4008951A1 (de) * 1990-03-20 1991-09-26 Messerschmitt Boelkow Blohm Einlauframpe 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
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
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
EP3476741B1 (de) * 2017-10-30 2021-08-25 Airbus Operations, S.L. Flugzeug-tailcone mit einem ringförmigen apu-lufteinlass
US11584514B2 (en) * 2018-01-31 2023-02-21 Airbus Operations Gmbh Airfoil for flow control including a common inlet/outlet device connected to a porous section
US10266275B1 (en) * 2018-04-10 2019-04-23 DMS Aviation Services, LLC Pressure recovery device for an aircraft engine air intake
US11124310B2 (en) 2018-04-10 2021-09-21 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
ES2967158T3 (es) * 2018-06-22 2024-04-26 Airbus Operations Slu Sistema de admisión de aire
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)

* Cited by examiner, † Cited by third party
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
NL292033A (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

Also Published As

Publication number Publication date
US4418879A (en) 1983-12-06
EP0067847B1 (de) 1990-06-06
EP0067847A1 (de) 1982-12-29
EP0067847A4 (de) 1984-04-06
WO1982002181A1 (en) 1982-07-08

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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