BRPI0819483A2 - Dispositivo para desacoplamento mecânico de um componente de uma aeronave sujeito a perfusão de gás quente - Google Patents

Dispositivo para desacoplamento mecânico de um componente de uma aeronave sujeito a perfusão de gás quente

Info

Publication number
BRPI0819483A2
BRPI0819483A2 BRPI0819483A BRPI0819483A2 BR PI0819483 A2 BRPI0819483 A2 BR PI0819483A2 BR PI0819483 A BRPI0819483 A BR PI0819483A BR PI0819483 A2 BRPI0819483 A2 BR PI0819483A2
Authority
BR
Brazil
Prior art keywords
hot gas
hot
aircraft component
holder
flange
Prior art date
Application number
Other languages
English (en)
Inventor
Markus Piesker
Original Assignee
Airbus Operations Gmbh
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 Airbus Operations Gmbh filed Critical Airbus Operations Gmbh
Publication of BRPI0819483A2 publication Critical patent/BRPI0819483A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00Power installations for auxiliary purposes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30Exhaust heads, chambers, or the like
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL-COMBUSTION ENGINES
    • F01N13/00Exhaust or silencing apparatus characterised by constructional features
    • F01N13/18Construction facilitating manufacture, assembly, or disassembly
    • F01N13/1805Fixing exhaust manifolds, exhaust pipes or pipe sections to each other, to engine or to vehicle body
    • F01N13/1811Fixing exhaust manifolds, exhaust pipes or pipe sections to each other, to engine or to vehicle body with means permitting relative movement, e.g. compensation of thermal expansion or vibration
    • F01N13/1816Fixing exhaust manifolds, exhaust pipes or pipe sections to each other, to engine or to vehicle body with means permitting relative movement, e.g. compensation of thermal expansion or vibration the pipe sections being joined together by flexible tubular elements only, e.g. using bellows or strip-wound pipes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/04Mounting of an exhaust cone in the jet pipe
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78Other construction of jet pipes
    • F02K1/80Couplings or connections
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L27/00Adjustable joints; Joints allowing movement
    • F16L27/10Adjustable joints; Joints allowing movement comprising a flexible connection only
    • F16L27/107Adjustable joints; Joints allowing movement comprising a flexible connection only the ends of the pipe being interconnected by a flexible sleeve
    • F16L27/11Adjustable joints; Joints allowing movement comprising a flexible connection only the ends of the pipe being interconnected by a flexible sleeve the sleeve having the form of a bellows with multiple corrugations
    • F16L27/111Adjustable joints; Joints allowing movement comprising a flexible connection only the ends of the pipe being interconnected by a flexible sleeve the sleeve having the form of a bellows with multiple corrugations the bellows being reinforced
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16LPIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L59/00Thermal insulation in general
    • F16L59/14Arrangements for the insulation of pipes or pipe systems
    • F16L59/16Arrangements specially adapted to local requirements at flanges, junctions, valves or the like
    • F16L59/21Arrangements specially adapted to local requirements at flanges, junctions, valves or the like adapted for expansion-compensation devices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/04Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • B64D2033/045Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes comprising infrared suppressors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D41/00Power installations for auxiliary purposes
    • B64D2041/002Mounting arrangements for auxiliary power units (APU's)
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/50Application for auxiliary power units (APU's)
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/53Means to assemble or disassemble

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Exhaust Silencers (AREA)
  • Joints Allowing Movement (AREA)
  • Diaphragms And Bellows (AREA)
  • Supports For Pipes And Cables (AREA)
  • Quick-Acting Or Multi-Walled Pipe Joints (AREA)
  • Air Bags (AREA)
BRPI0819483 2007-12-21 2008-11-10 Dispositivo para desacoplamento mecânico de um componente de uma aeronave sujeito a perfusão de gás quente BRPI0819483A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US1587007P 2007-12-21 2007-12-21
DE102007061995A DE102007061995B4 (de) 2007-12-21 2007-12-21 Vorrichtung zum mechanisch entkoppelten Befestigen einer von Heißgas durchströmten Flugzeugkomponente
PCT/EP2008/009462 WO2009083066A1 (de) 2007-12-21 2008-11-10 Vorrichtung zum mechanisch entkoppelten befestigen einer von heissgas durchströmten flugzeugkomponente

Publications (1)

Publication Number Publication Date
BRPI0819483A2 true BRPI0819483A2 (pt) 2015-05-05

Family

ID=40758319

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0819483 BRPI0819483A2 (pt) 2007-12-21 2008-11-10 Dispositivo para desacoplamento mecânico de um componente de uma aeronave sujeito a perfusão de gás quente

Country Status (10)

Country Link
US (1) US8844863B2 (pt)
EP (1) EP2153040B1 (pt)
JP (1) JP2011506184A (pt)
CN (1) CN101903625B (pt)
AT (1) ATE530442T1 (pt)
BR (1) BRPI0819483A2 (pt)
CA (1) CA2690287A1 (pt)
DE (1) DE102007061995B4 (pt)
RU (1) RU2010127340A (pt)
WO (1) WO2009083066A1 (pt)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140060004A1 (en) * 2011-09-20 2014-03-06 Bell Helicopter Textron Inc. Tiltrotor vectored exhaust system
CN103029840A (zh) * 2012-11-20 2013-04-10 中国商用飞机有限责任公司 飞机发动机系统及其风扇区机械接口的设计方法
WO2015050652A1 (en) 2013-10-01 2015-04-09 United Technologies Corporation Alignment system for exhaust installation
US10279924B2 (en) * 2017-05-12 2019-05-07 Bell Helicopter Textron Inc. Engine exhaust duct mounting assembly
FR3141681B1 (fr) * 2022-11-09 2025-03-21 Airbus Helicopters Aéronef muni d’un conduit d’échappement couplé à un système de stabilisation

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2339126A1 (fr) * 1976-01-22 1977-08-19 Semt Systeme de raccordement etanche entre deux elements de tuyauterie
US4121860A (en) * 1977-05-27 1978-10-24 Avco Corporation Bellows with rotational joints
US4659117A (en) * 1982-08-10 1987-04-21 Iwk Regler Und Kompensatoren Gmbh Flexible coupling for pipes in exhaust systems of motor vehicles
JPS61126026A (ja) * 1984-11-26 1986-06-13 Hiroyoshi Hidaka イソキノリンスルホン酸アミドを有効成分とする抗癌剤
US5159811A (en) * 1990-07-16 1992-11-03 Caterpillar Inc. Flexible coupling device for use in an engine manifold system
US5145215A (en) * 1991-04-26 1992-09-08 Senior Engineering Investments, B.V. Flexible coupler apparatus
US5238365A (en) * 1991-07-09 1993-08-24 General Electric Company Assembly for thermal shielding of low pressure turbine
DE19514020A1 (de) * 1995-04-13 1996-10-17 Daimler Benz Ag Abgassammelrohr, insbesondere für eine Brennkraftmaschine in einem Kraftfahrzeug, und Verfahren zu dessen Herstellung
EP0861974A4 (en) * 1996-02-02 2004-07-14 Calsonic Corp FLEXIBLE EXHAUST PIPE OF A MOTOR VEHICLE
FR2751054B1 (fr) * 1996-07-11 1998-09-18 Snecma Chambre de combustion anti-nox a injection de carburant de type annulaire
BR9806961A (pt) * 1997-01-17 2000-03-21 Senior Eng Investments Aparelho acoplador flexìvel.
US6464257B1 (en) * 1997-04-10 2002-10-15 Senior Investments Ag Vibration decoupler apparatus
US5957504A (en) * 1997-04-10 1999-09-28 Senior Engineering Investments Ag Exhaust manifold attachment apparatus
US6032463A (en) * 1998-07-22 2000-03-07 Caterpillar Inc Exhaust connector assembly and kit for a segmented exhaust manifold
DE10003728A1 (de) * 2000-01-28 2001-08-09 Siemens Ag Hitzeschildanordnung für eine Heißgas führende Komponente, insbesondere für Strukturteile von Gasturbinen
US6293098B1 (en) * 2000-08-29 2001-09-25 George J. Coates Method and apparatus for joining pressurized exhaust manifold sections
US6679045B2 (en) * 2001-12-18 2004-01-20 General Electric Company Flexibly coupled dual shell bearing housing
US6921112B2 (en) * 2002-11-26 2005-07-26 Josif Atansoski Exhaust vibration decoupling connector
US7040576B2 (en) * 2003-12-18 2006-05-09 Pratt & Whitney Canada Corp. Fire shield apparatus and method
US7011502B2 (en) * 2004-04-15 2006-03-14 General Electric Company Thermal shield turbine airfoil
US7350619B2 (en) * 2004-09-23 2008-04-01 Honeywell International, Inc. Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner
WO2006034461A1 (en) 2004-09-23 2006-03-30 Honeywell International Inc. Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner
DE202004019988U1 (de) * 2004-12-27 2005-03-03 Burgmann Industries Gmbh & Co. Kg Verbindungselement zur nicht starren Verbindung der Endbereiche von zwei Rohrleitungen
DE102006058006B4 (de) * 2006-12-08 2010-01-07 Airbus Deutschland Gmbh Anordnung und Verfahren zur Montage eines Bauelements in einem Flugzeug
US8196893B2 (en) * 2008-04-09 2012-06-12 Mks Instruments, Inc. Isolation valve with corrosion protected and heat transfer enhanced valve actuator and closure apparatus and method
US8042840B2 (en) * 2008-05-13 2011-10-25 Paul Chahine Sealed flexible coupling with torsion acceptance

Also Published As

Publication number Publication date
RU2010127340A (ru) 2012-01-27
US8844863B2 (en) 2014-09-30
US20100269328A1 (en) 2010-10-28
EP2153040B1 (de) 2011-10-26
CA2690287A1 (en) 2009-07-09
JP2011506184A (ja) 2011-03-03
CN101903625A (zh) 2010-12-01
ATE530442T1 (de) 2011-11-15
CN101903625B (zh) 2012-10-10
EP2153040A1 (de) 2010-02-17
WO2009083066A1 (de) 2009-07-09
DE102007061995A1 (de) 2009-07-16
DE102007061995B4 (de) 2012-03-01

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE AS 5A, 6A E 7A ANUIDADES.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2343 DE 01-12-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.