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DE60022707D1 - Hilfskraft- und Hilfsschubantrieb - Google Patents

Hilfskraft- und Hilfsschubantrieb

Info

Publication number
DE60022707D1
DE60022707D1 DE60022707T DE60022707T DE60022707D1 DE 60022707 D1 DE60022707 D1 DE 60022707D1 DE 60022707 T DE60022707 T DE 60022707T DE 60022707 T DE60022707 T DE 60022707T DE 60022707 D1 DE60022707 D1 DE 60022707D1
Authority
DE
Germany
Prior art keywords
auxiliary
push drive
drive
auxiliary push
push
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.)
Revoked
Application number
DE60022707T
Other languages
English (en)
Other versions
DE60022707T2 (de
Inventor
Gary D Reysa
Lynn A Swenson
Robert A Hutchinson
Kenny L Fung
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=23388721&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE60022707(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE60022707D1 publication Critical patent/DE60022707D1/de
Publication of DE60022707T2 publication Critical patent/DE60022707T2/de
Anticipated expiration legal-status Critical
Revoked 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
    • 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
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2220/00—Application
    • F05B2220/50—Application for auxiliary power units (APU's)

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE60022707T 1999-07-15 2000-07-13 Hilfskraft- und Hilfsschubantrieb Revoked DE60022707T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US353346 1999-07-15
US09/353,346 US6247668B1 (en) 1999-07-15 1999-07-15 Auxiliary power and thrust unit

Publications (2)

Publication Number Publication Date
DE60022707D1 true DE60022707D1 (de) 2005-10-27
DE60022707T2 DE60022707T2 (de) 2006-06-22

Family

ID=23388721

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60022707T Revoked DE60022707T2 (de) 1999-07-15 2000-07-13 Hilfskraft- und Hilfsschubantrieb

Country Status (3)

Country Link
US (1) US6247668B1 (de)
EP (1) EP1069044B1 (de)
DE (1) DE60022707T2 (de)

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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
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GB0523570D0 (en) * 2005-11-18 2005-12-28 Airbus Uk Ltd Aircraft cooling duct
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US7600714B2 (en) * 2006-04-20 2009-10-13 Honeywell International Inc. Diffusing air inlet door assembly
US20100236244A1 (en) * 2006-06-28 2010-09-23 Longardner Robert L Heat absorbing and reflecting shield for air breathing heat engine
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US8016234B2 (en) * 2006-09-12 2011-09-13 Airbus Deutschland Gmbh Airframe structure of an aircraft or spacecraft
US7484583B2 (en) * 2006-09-29 2009-02-03 Caterpillar Inc. Auxiliary power unit for moving a vehicle
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US20090072080A1 (en) * 2007-03-08 2009-03-19 Bhargava Brij B On board secondary propulsion system for an aircraft
US8109464B2 (en) 2007-03-08 2012-02-07 The Ashman Group, Llc Aircraft taxiing and secondary propulsion system
US20080217466A1 (en) * 2007-03-08 2008-09-11 Bhargava Brij B Auxiliary on board power system for an aircraft
US7980509B2 (en) * 2007-03-08 2011-07-19 The Ashman Group, Llc Aircraft taxiing systems
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ITTO20080142A1 (it) * 2008-02-28 2009-08-29 Alenia Aeronautica Spa Presa d'aria, in particolare per un espulsore di chaff per velivolo
FR2930760B1 (fr) * 2008-05-05 2010-09-10 Airbus France Dispositif annexe de deplacement au sol d'un vehicule aerien a turbine a air
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
DE102009010243A1 (de) 2009-02-24 2010-09-02 Airbus Deutschland Gmbh Leistungserzeugungs-Vorrichtung sowie Rumpf-Bauteil mit einer solchen Leistungserzeugungs-Vorrichtung
ES2350429B1 (es) * 2009-05-28 2011-11-18 Airbus Operations, S.L. Cono de cola de una aeronave con carena movil abatible
ES2394581B1 (es) * 2010-04-26 2013-12-12 Airbus Operation, S.L Cono de cola del fuselaje trasero de un avion con una unidad de potencia auxiliar
FR2964087B1 (fr) * 2010-08-25 2013-06-14 Turbomeca Procede d'optimisation de l'operabilite de motorisation d'un aeronef et groupe de puissance autonome de mise en oeuvre
US8519555B2 (en) 2010-11-29 2013-08-27 Pratt & Whitney Canada Corp. Combination low spool generator and ram air turbine generator
US8955335B2 (en) * 2010-12-30 2015-02-17 Rolls-Royce Corporation System, propulsion system and vehicle
EP2678226B1 (de) 2011-04-28 2015-01-21 Bell Helicopter Textron Inc. Selbstausrichtendes einlassplenumsystem für einen drehflügler
US8622342B2 (en) * 2011-06-17 2014-01-07 Embraer S.A. On-board aircraft auxiliary power systems having dual auxiliary power units
ES2398316B1 (es) * 2011-07-18 2014-04-29 Airbus Operations, S.L. Sistema versátil de potencia en aeronaves
US20130091850A1 (en) * 2011-10-13 2013-04-18 Hamilton Sundstrand Corporation Method and system for reducing hot soakback
US20130319003A1 (en) * 2012-05-30 2013-12-05 Jason Peel Auxiliary power unit mount with fire resistant shielding
US8864067B2 (en) * 2012-05-31 2014-10-21 Hamilton Sundstrand Corporation Auxiliary fire resistant mount system for an auxiliary power unit
FR2992630B1 (fr) 2012-06-29 2015-02-20 Turbomeca Procede et configuration d'apport d'energie propulsive et/ou non propulsive dans une architecture d'helicoptere par un moteur auxiliaire de puissance
FR3000025B1 (fr) * 2012-12-21 2016-12-09 Airbus Aeronef comprenant un poste de pilotage delocalise en dehors d'une partie superieure de la pointe avant
US9517843B2 (en) * 2013-03-13 2016-12-13 Rolls-Royce North American Technologies, Inc. Generator for flight vehicle
EP3055220B1 (de) * 2013-10-08 2019-05-15 United Technologies Corporation Akustisch gesteuertes einlasssystem für eisablenkungshilfsstromeinheit
FR3012422B1 (fr) * 2013-10-31 2016-12-09 Microturbo Procede et systeme de generation de puissance auxiliaire dans un aeronef
US9409653B2 (en) 2014-09-17 2016-08-09 The Boeing Company Auxilliary power and thrust unit drive system
FR3032419B1 (fr) * 2015-02-09 2018-06-08 Airbus Operations Pointe arriere d'aeronef
EP3056423B1 (de) * 2015-02-16 2017-12-13 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Flugzeug mit einem rumpf der mindestens einen innenbereich und einen bereich zur antriebsunterbringung definiert
JP6437347B2 (ja) 2015-02-27 2018-12-12 三菱重工業株式会社 推力発生装置及び航空機
US20170036773A1 (en) * 2015-08-07 2017-02-09 Pratt & Whitney Canada Corp. Inflight power management for aircraft
US20180327109A1 (en) * 2015-11-16 2018-11-15 Safran Aircraft Engines Propulsion unit comprising a main engine and an auxiliary engine
FR3043726B1 (fr) * 2015-11-16 2020-05-01 Safran Aircraft Engines Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire
FR3043728B1 (fr) * 2015-11-16 2020-05-01 Safran Aircraft Engines Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire
FR3043729B1 (fr) * 2015-11-16 2020-06-05 Safran Aircraft Engines Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire
FR3043725B1 (fr) * 2015-11-16 2017-11-17 Snecma Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire
FR3043727B1 (fr) * 2015-11-16 2017-11-10 Snecma Ensemble propulsif comprenant un moteur principal et un moteur auxiliaire
US10392120B2 (en) 2016-04-19 2019-08-27 General Electric Company Propulsion engine for an aircraft
US10836505B2 (en) 2016-06-23 2020-11-17 Raytheon Technologies Corporation Operating auxiliary power unit during off-nominal propulsion system operation
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US11415063B2 (en) 2016-09-15 2022-08-16 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US20180257788A1 (en) * 2017-03-09 2018-09-13 United Technologies Corporation Air intake assembly with horizontal door for an aircraft auxiliary power unit
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
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US11124310B2 (en) 2018-04-10 2021-09-21 DMS Aviation Services, LLC Pressure recovery device for an aircraft engine air intake
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Also Published As

Publication number Publication date
DE60022707T2 (de) 2006-06-22
EP1069044B1 (de) 2005-09-21
US6247668B1 (en) 2001-06-19
EP1069044A3 (de) 2003-11-19
EP1069044A2 (de) 2001-01-17

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8331 Complete revocation