BR112015018741A2 - retentor de tanque em uma aeronave - Google Patents

retentor de tanque em uma aeronave

Info

Publication number
BR112015018741A2
BR112015018741A2 BR112015018741A BR112015018741A BR112015018741A2 BR 112015018741 A2 BR112015018741 A2 BR 112015018741A2 BR 112015018741 A BR112015018741 A BR 112015018741A BR 112015018741 A BR112015018741 A BR 112015018741A BR 112015018741 A2 BR112015018741 A2 BR 112015018741A2
Authority
BR
Brazil
Prior art keywords
aircraft
tank
retaining
retainer
fuselage
Prior art date
Application number
BR112015018741A
Other languages
English (en)
Inventor
Santerre Angélique
Faure Benjamin
Bertrand Jérôme
Mezieres Pascal
Abadie-Lahaille Robert
Chevrollier Samuel
Coraboeuf Yohann
Original Assignee
Airbus Defence & Space Sas
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 Defence & Space Sas filed Critical Airbus Defence & Space Sas
Publication of BR112015018741A2 publication Critical patent/BR112015018741A2/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/04Arrangement thereof in or on aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/02Tanks
    • B64D37/06Constructional adaptations thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00Arrangements in connection with fuel supply for power plant
    • B64D37/30Fuel systems for specific fuels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40Arrangements or adaptations of propulsion systems
    • B64G1/402Propellant tanks; Feeding propellants
    • 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
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C11/00Pivots; Pivotal connections
    • F16C11/04Pivotal connections
    • F16C11/06Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
    • F16C11/0695Mounting of ball-joints, e.g. fixing them to a connecting rod
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2205/00Vessel construction, in particular mounting arrangements, attachments or identifications means
    • F17C2205/01Mounting arrangements
    • F17C2205/0153Details of mounting arrangements
    • F17C2205/0192Details of mounting arrangements with external bearing means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/08Ergols, e.g. hydrazine
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/01Applications for fluid transport or storage
    • F17C2270/0186Applications for fluid transport or storage in the air or in space
    • F17C2270/0197Rockets

Abstract

resumo retentor de tanque em uma aeronave a invenção refere-se a um retentor de tanque (100) para reter um tanque na fuselagem de uma aeronave que compreende, entre o tanque e um quadro (12) rigidamente conectada a uma fuselagem da aeronave, um meio de retenção giratório (4) e uma haste de fixação (20) em que o dito meio de retenção giratório é montado. vantajosamente, o meio de retenção giratório é pretendido para ser conectado a uma extremidade traseira (102) do tanque e a haste de fixação (20) é adequada para ser montada em um quadro (12) rigidamente conectada a fuselagem da aeronave e, preferivelmente, o meio de retenção giratório compreende uma junta de esfera (4).
BR112015018741A 2013-02-05 2014-02-04 retentor de tanque em uma aeronave BR112015018741A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1350987A FR3001713B1 (fr) 2013-02-05 2013-02-05 Dispositif de retenue d'un reservoir dans un aeronef
PCT/EP2014/052144 WO2014122127A1 (fr) 2013-02-05 2014-02-04 Dispositif de retenue d'un réservoir dans un aéronef

Publications (1)

Publication Number Publication Date
BR112015018741A2 true BR112015018741A2 (pt) 2017-07-18

Family

ID=48170719

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015018741A BR112015018741A2 (pt) 2013-02-05 2014-02-04 retentor de tanque em uma aeronave

Country Status (9)

Country Link
US (1) US20150360791A1 (pt)
EP (1) EP2953856B1 (pt)
JP (1) JP6499974B2 (pt)
CN (1) CN104968567B (pt)
BR (1) BR112015018741A2 (pt)
FR (1) FR3001713B1 (pt)
RU (1) RU2015137826A (pt)
SG (1) SG11201505830YA (pt)
WO (1) WO2014122127A1 (pt)

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FR3001714B1 (fr) * 2013-02-05 2016-08-26 Astrium Sas Dispositif de support et de maintien de reservoirs cryogeniques
CN104315928B (zh) * 2014-10-27 2015-12-09 中国运载火箭技术研究院 一种大推力运载火箭低温末级贮箱连接支撑结构设计方法
US10306984B2 (en) * 2016-08-30 2019-06-04 The Boeing Company Toroidal support structures
CN107140217A (zh) * 2017-06-12 2017-09-08 江苏美龙振华科技有限公司 一种运输类飞机的液化天然气油箱结构
CN108945486A (zh) * 2018-08-04 2018-12-07 江苏东翼通用航空科技有限公司 一种无人直升机及其工作方法
FR3107739B1 (fr) * 2020-03-02 2023-02-10 Etablissements Magyar Dispositif de maintien d’un réservoir intérieur d’une citerne de transport de liquide cryogénique
FR3123050A1 (fr) * 2021-05-20 2022-11-25 Airbus Sas Système de réservoir comportant un châssis, un réservoir de dihydrogène et des moyens de fixation du réservoir au châssis
RU207326U1 (ru) * 2021-07-15 2021-10-22 Акционерное общество "Рузаевский завод химического машиностроения" (АО "Рузхиммаш") Контейнер-цистерна
RU2762445C1 (ru) * 2021-08-03 2021-12-21 Акционерное общество "Рузаевский завод химического машиностроения" (АО "Рузхиммаш") Контейнер-цистерна (Варианты)
US20230037638A1 (en) * 2021-08-03 2023-02-09 The Boeing Company Load coupling attachment systems and methods

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Also Published As

Publication number Publication date
SG11201505830YA (en) 2015-08-28
WO2014122127A1 (fr) 2014-08-14
RU2015137826A (ru) 2017-03-13
CN104968567B (zh) 2018-06-01
FR3001713B1 (fr) 2016-07-15
JP2016507419A (ja) 2016-03-10
CN104968567A (zh) 2015-10-07
FR3001713A1 (fr) 2014-08-08
JP6499974B2 (ja) 2019-04-10
US20150360791A1 (en) 2015-12-17
EP2953856B1 (fr) 2017-06-14
EP2953856A1 (fr) 2015-12-16

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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]