BR112019021861A2 - Vedações e métodos para tubulação de escape de unidade de alimentação auxiliar de aeronave - Google Patents

Vedações e métodos para tubulação de escape de unidade de alimentação auxiliar de aeronave Download PDF

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Publication number
BR112019021861A2
BR112019021861A2 BR112019021861-0A BR112019021861A BR112019021861A2 BR 112019021861 A2 BR112019021861 A2 BR 112019021861A2 BR 112019021861 A BR112019021861 A BR 112019021861A BR 112019021861 A2 BR112019021861 A2 BR 112019021861A2
Authority
BR
Brazil
Prior art keywords
seal
auxiliary power
seals
methods
power supply
Prior art date
Application number
BR112019021861-0A
Other languages
English (en)
Inventor
David Sandiford A.
Original Assignee
Itt Manufacturing Enterprises Llc
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 Itt Manufacturing Enterprises Llc filed Critical Itt Manufacturing Enterprises Llc
Publication of BR112019021861A2 publication Critical patent/BR112019021861A2/pt

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
    • F02C7/28—Arrangement of seals
    • 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
    • B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
    • 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
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/40—Maintaining or repairing aircraft
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005—Sealing means between non relatively rotating elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/30—Exhaust heads, chambers, or the like
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/80—Couplings or connections
    • F02K1/805—Sealing devices therefor, e.g. for movable parts of jet pipes or nozzle flaps
    • 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)

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Gasket Seals (AREA)

Abstract

a presente invenção refere-se a várias vedações para vedar ao redor de tubulações de escape, como a tubulação de escape de uma unidade de alimentação auxiliar de aeronave. a vedação pode incluir uma porção de colar que delimita uma abertura que é configurada para receber a tubulação de escape. a vedação pode incluir uma porção de tubo longo conectada à porção de colar e que se estende radialmente para fora dela. a vedação pode ser configurada para inflar e/ou esvaziar para facilitar a instalação e/ou remoção da vedação da tubulação de escape.
BR112019021861-0A 2017-04-18 2018-04-17 Vedações e métodos para tubulação de escape de unidade de alimentação auxiliar de aeronave BR112019021861A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201762486704P 2017-04-18 2017-04-18
US62/486,704 2017-04-18
PCT/US2018/028033 WO2018195122A1 (en) 2017-04-18 2018-04-17 Aircraft auxiliary power unit exhaust pipe seals and methods

Publications (1)

Publication Number Publication Date
BR112019021861A2 true BR112019021861A2 (pt) 2020-05-26

Family

ID=62116616

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112019021861-0A BR112019021861A2 (pt) 2017-04-18 2018-04-17 Vedações e métodos para tubulação de escape de unidade de alimentação auxiliar de aeronave

Country Status (6)

Country Link
US (1) US20180298826A1 (pt)
EP (1) EP3612446A1 (pt)
CN (1) CN110740935A (pt)
BR (1) BR112019021861A2 (pt)
CA (1) CA3060252A1 (pt)
WO (1) WO2018195122A1 (pt)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10787922B2 (en) * 2018-05-02 2020-09-29 Rohr, Inc. Tubular seal with wavy shroud for an aircraft propulsion system
US11174948B2 (en) 2019-07-26 2021-11-16 Raytheon Technologies Corporation Slider seal with non-circular puck geometry

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1751550C3 (de) * 1968-06-18 1975-04-17 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Dichtung zwischen dem Einlauf eines Strahltriebwerkes und einem zellenfesten Aufnahmering des Einlaufgehäuses
GB1474030A (en) * 1973-09-22 1977-05-18 Rolls Royce Fire seal
FR2670177B1 (fr) * 1990-12-05 1993-01-22 Snecma Joint d'etancheite entre l'arriere du fuselage d'un avion et les volets exterieurs de son turboreacteur.
US6039287A (en) * 1996-08-02 2000-03-21 Alliedsignal Inc. Detachable integral aircraft tailcone and power assembly
US7350619B2 (en) * 2004-09-23 2008-04-01 Honeywell International, Inc. Auxiliary power unit exhaust duct with muffler incorporating an externally replaceable acoustic liner
US8079809B2 (en) * 2008-06-26 2011-12-20 Honeywell International Inc. Inflatable seal assembly between an engine inlet and a vehicle
GB201007327D0 (en) * 2010-05-04 2010-06-16 Rolls Royce Plc A fireseal
CN102022222B (zh) * 2010-12-08 2013-05-29 中国商用飞机有限责任公司 消声器
US10077669B2 (en) * 2014-11-26 2018-09-18 United Technologies Corporation Non-metallic engine case inlet compression seal for a gas turbine engine
CN205858247U (zh) * 2016-06-27 2017-01-04 中石化石油工程技术服务有限公司 干法固井用井口环空密封装置

Also Published As

Publication number Publication date
CA3060252A1 (en) 2018-10-25
WO2018195122A1 (en) 2018-10-25
CN110740935A (zh) 2020-01-31
US20180298826A1 (en) 2018-10-18
EP3612446A1 (en) 2020-02-26

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Legal Events

Date Code Title Description
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]
B350 Update of information on the portal [chapter 15.35 patent gazette]