BR112017022641A2 - arranjo de bomba de combustível de aeronave, sistema de abastecimento de aeronave, aeronave e tampa de entrada de inspeção para uma aeronave - Google Patents

arranjo de bomba de combustível de aeronave, sistema de abastecimento de aeronave, aeronave e tampa de entrada de inspeção para uma aeronave

Info

Publication number
BR112017022641A2
BR112017022641A2 BR112017022641A BR112017022641A BR112017022641A2 BR 112017022641 A2 BR112017022641 A2 BR 112017022641A2 BR 112017022641 A BR112017022641 A BR 112017022641A BR 112017022641 A BR112017022641 A BR 112017022641A BR 112017022641 A2 BR112017022641 A2 BR 112017022641A2
Authority
BR
Brazil
Prior art keywords
aircraft
supply system
fuel pump
pump arrangement
inlet cover
Prior art date
Application number
BR112017022641A
Other languages
English (en)
Other versions
BR112017022641B1 (pt
Inventor
Egner John
Bradshaw Nigel
Original Assignee
Eaton Ltd
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 Eaton Ltd filed Critical Eaton Ltd
Publication of BR112017022641A2 publication Critical patent/BR112017022641A2/pt
Publication of BR112017022641B1 publication Critical patent/BR112017022641B1/pt

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
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/02—Tanks
    • B64D37/06—Constructional adaptations thereof
    • 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
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/005—Accessories not provided for in the groups B64D37/02 - B64D37/28
    • 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
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/02—Tanks
    • B64D37/04—Arrangement thereof in or on aircraft
    • 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
    • F02C7/22—Fuel supply systems
    • 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
    • H—ELECTRICITY
    • H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00—Constructional details common to different types of electric apparatus
    • H05K7/20—Modifications to facilitate cooling, ventilating, or heating
    • H05K7/20845—Modifications to facilitate cooling, ventilating, or heating for automotive electronic casings
    • H05K7/20863—Forced ventilation, e.g. on heat dissipaters coupled to components
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Control Of Positive-Displacement Pumps (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

um arranjo de bomba de combustível da aeronave (30) compreende uma bomba (40), um recipiente (42) disposto para confinar a bomba e montar a bomba dentro de um tanque de combustível de aeronave (20, 22, 24). o arranjo também inclui uma unidade eletrônica separada (60) configurada para ser montada remotamente à bomba (40). o arranjo da bomba (30) pode ser provido dentro de um sistema de abastecimento de aeronave (10) de uma aeronave (1).
BR112017022641-3A 2015-04-22 2016-04-22 Sistema de abastecimento de aeronave e aeronave BR112017022641B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GBGB1506838.0A GB201506838D0 (en) 2015-04-22 2015-04-22 Aircraft fuel pump
GB1506838.0 2015-04-22
PCT/EP2016/059000 WO2016170108A1 (en) 2015-04-22 2016-04-22 Aircraft fuel pump

Publications (2)

Publication Number Publication Date
BR112017022641A2 true BR112017022641A2 (pt) 2018-07-24
BR112017022641B1 BR112017022641B1 (pt) 2023-01-17

Family

ID=53298996

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112017022641-3A BR112017022641B1 (pt) 2015-04-22 2016-04-22 Sistema de abastecimento de aeronave e aeronave

Country Status (9)

Country Link
US (1) US10745143B2 (pt)
EP (1) EP3286419B1 (pt)
CN (1) CN107531332B (pt)
BR (1) BR112017022641B1 (pt)
CA (1) CA2982525C (pt)
ES (1) ES2909523T3 (pt)
GB (1) GB201506838D0 (pt)
RU (1) RU2712143C2 (pt)
WO (1) WO2016170108A1 (pt)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110510131B (zh) * 2019-09-26 2022-11-22 中国航空工业集团公司沈阳飞机设计研究所 一种飞机燃油循环蓄冷装置
CN110768522A (zh) * 2019-10-25 2020-02-07 天津航空机电有限公司 一种应用于航空大功率变压整流器的液冷散热设备
DE102020216090A1 (de) 2020-12-16 2022-06-23 MTU Aero Engines AG Kühlsystem für ein Fluggerät, Fluggerät mit einem Kühlsystem und Verfahren zum Kühlen eines elektrischen Antriebssystems eines Fluggeräts
US20220410246A1 (en) * 2021-06-25 2022-12-29 Ultracell Llc Fuselage heat exchanger for cooling power source for unmanned aerial vehicles (uavs)

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB851428A (en) * 1957-08-28 1960-10-19 United Aircraft Corp Fuel supply system for use in aircraft
US3550678A (en) * 1969-04-01 1970-12-29 United Aircraft Prod Surface radiator
SU1108693A1 (ru) * 1983-03-31 1996-04-27 А.П. Белов Топливная система летательного аппарата
US4696442A (en) * 1986-07-14 1987-09-29 The Boeing Company Vortex generators for inlets
US6675778B1 (en) 2002-08-27 2004-01-13 Visteon Global Technologies, Inc. Fuel sender assembly
GB0526206D0 (en) * 2005-12-22 2006-02-01 Airbus Uk Ltd Aircraft fuel tank assembly
GB0608832D0 (en) * 2006-05-04 2006-06-14 Airbus Uk Ltd Aircraft wiring installation
DE102007051498A1 (de) * 2007-10-27 2009-04-30 Mtu Aero Engines Gmbh Kraftstoffzumesseinheit für ein Flugzeugtriebwerk
RU2364738C1 (ru) * 2008-01-21 2009-08-20 Открытое акционерное общество "Омское машиностроительное конструкторское бюро" Система топливопитания газотурбинного двигателя
US9296467B1 (en) * 2009-06-09 2016-03-29 The Boeing Company Pressure test door for use with a fuel tank
EP2572991B1 (en) * 2011-09-26 2014-06-18 Goodrich Lighting Systems GmbH Aircraft light
GB2501289A (en) * 2012-04-18 2013-10-23 Eaton Aerospace Ltd Aircraft fuel supply system
FR2992796B1 (fr) * 2012-07-02 2015-05-01 Snecma Dispositif de ventilation et d'alimentation electrique d'un calculateur de moteur d'aeronef
EP2938852A1 (en) 2012-12-28 2015-11-04 General Electric Company System for temperature and actuation control and method of controlling fluid temperatures in an aircraft
US10059435B2 (en) * 2014-12-04 2018-08-28 Parker-Hannifin Corporation Low drag skin heat exchanger

Also Published As

Publication number Publication date
EP3286419B1 (en) 2021-12-29
ES2909523T3 (es) 2022-05-06
RU2712143C2 (ru) 2020-01-24
EP3286419A1 (en) 2018-02-28
GB201506838D0 (en) 2015-06-03
US10745143B2 (en) 2020-08-18
CA2982525C (en) 2023-08-29
WO2016170108A1 (en) 2016-10-27
RU2017140402A (ru) 2019-05-22
BR112017022641B1 (pt) 2023-01-17
CN107531332B (zh) 2021-05-28
RU2017140402A3 (pt) 2019-08-02
US20180118365A1 (en) 2018-05-03
CN107531332A (zh) 2018-01-02
CA2982525A1 (en) 2016-10-27

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Legal Events

Date Code Title Description
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 22/04/2016, OBSERVADAS AS CONDICOES LEGAIS