FR3017111B1 - Dispositif d'assemblage de tuyaux carburant double peau d'un aeronef. - Google Patents

Dispositif d'assemblage de tuyaux carburant double peau d'un aeronef.

Info

Publication number
FR3017111B1
FR3017111B1 FR1450881A FR1450881A FR3017111B1 FR 3017111 B1 FR3017111 B1 FR 3017111B1 FR 1450881 A FR1450881 A FR 1450881A FR 1450881 A FR1450881 A FR 1450881A FR 3017111 B1 FR3017111 B1 FR 3017111B1
Authority
FR
France
Prior art keywords
aircraft
double skin
fuel pipes
assembling double
skin fuel
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.)
Active
Application number
FR1450881A
Other languages
English (en)
Other versions
FR3017111A1 (fr
Inventor
Thierry Gagnaire
Damien Fraysse
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR1450881A priority Critical patent/FR3017111B1/fr
Priority to US14/598,336 priority patent/US9546623B2/en
Publication of FR3017111A1 publication Critical patent/FR3017111A1/fr
Application granted granted Critical
Publication of FR3017111B1 publication Critical patent/FR3017111B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M37/00—Apparatus or systems for feeding liquid fuel from storage containers to carburettors or fuel-injection apparatus; Arrangements for purifying liquid fuel specially adapted for, or arranged on, internal-combustion engines
    • F02M37/0011—Constructional details; Manufacturing or assembly of elements of fuel systems; Materials therefor
    • F02M37/0017—Constructional details; Manufacturing or assembly of elements of fuel systems; Materials therefor related to fuel pipes or their connections, e.g. joints or sealings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L39/00—Joints or fittings for double-walled or multi-channel pipes or pipe assemblies
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L39/00—Joints or fittings for double-walled or multi-channel pipes or pipe assemblies
    • F16L39/005—Joints or fittings for double-walled or multi-channel pipes or pipe assemblies for concentric pipes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/02—Tanks
    • B64D37/14—Filling or emptying
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/32—Safety measures not otherwise provided for, e.g. preventing explosive conditions
FR1450881A 2014-02-05 2014-02-05 Dispositif d'assemblage de tuyaux carburant double peau d'un aeronef. Active FR3017111B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1450881A FR3017111B1 (fr) 2014-02-05 2014-02-05 Dispositif d'assemblage de tuyaux carburant double peau d'un aeronef.
US14/598,336 US9546623B2 (en) 2014-02-05 2015-01-16 Assembly device for double-skinned aircraft fuel pipes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1450881A FR3017111B1 (fr) 2014-02-05 2014-02-05 Dispositif d'assemblage de tuyaux carburant double peau d'un aeronef.

Publications (2)

Publication Number Publication Date
FR3017111A1 FR3017111A1 (fr) 2015-08-07
FR3017111B1 true FR3017111B1 (fr) 2016-01-22

Family

ID=50549130

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1450881A Active FR3017111B1 (fr) 2014-02-05 2014-02-05 Dispositif d'assemblage de tuyaux carburant double peau d'un aeronef.

Country Status (2)

Country Link
US (1) US9546623B2 (fr)
FR (1) FR3017111B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104040239A (zh) * 2011-10-07 2014-09-10 伊顿公司 双壁管适配器和接头
FR3120603A1 (fr) * 2021-03-11 2022-09-16 Airbus Operations (S.A.S.) Mât d’aéronef comprenant une structure primaire tubulaire intégrant au moins une canalisation à double peau et aéronef comportant au moins un tel mât
CN113775843B (zh) * 2021-07-27 2023-04-07 上海外高桥造船海洋工程有限公司 Lng船燃气双壁管连接装置

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3080180A (en) * 1958-06-30 1963-03-05 Rector Well Equipment Company Tubing hangers
US3072420A (en) * 1958-12-08 1963-01-08 Fmc Corp Tubing hanger assembly
US5351727A (en) * 1994-01-18 1994-10-04 Dayco Products Inc. Fuel dispensing system, hose assembly therefor and methods of making the same
US6971682B2 (en) * 2003-04-15 2005-12-06 Adel Wiggins Group, Transdigm, Inc. Coupling assembly
GB0523573D0 (en) * 2005-11-18 2005-12-28 Airbus Uk Ltd Aircraft fuel pipe coupling
US7942452B2 (en) * 2007-11-20 2011-05-17 The Boeing Company Flange fitting with leak sensor port
FR2948254B1 (fr) * 2009-07-16 2011-12-30 Airbus Operations Sas Dispositif de protection de tuyauteries contre la foudre
FR2978521B1 (fr) * 2011-07-29 2014-08-22 Airbus Operations Sas Dispositif de raccordement de deux tuyaux
CN104040239A (zh) * 2011-10-07 2014-09-10 伊顿公司 双壁管适配器和接头

Also Published As

Publication number Publication date
FR3017111A1 (fr) 2015-08-07
US9546623B2 (en) 2017-01-17
US20150219048A1 (en) 2015-08-06

Similar Documents

Publication Publication Date Title
EP3150918A4 (fr) Dispositif de combustion pour turbine à gaz
FR3038882B1 (fr) Aeronef combine muni d'un dispositif anticouple complementaire
EP3239499A4 (fr) Dispositif de moteur d'avion
GB201407743D0 (en) Gas turbine engine fuel system
GB201418685D0 (en) Gas turbine engine fuel system
PL3123009T3 (pl) Urządzenie wspomagające dla maszyny wirowej z turbiną swobodną statku powietrznego
FR3024707B1 (fr) Dispositif d'assistance rapide pour une turbomachine a turbine libre d'un aeronef
EP3246546A4 (fr) Dispositif de moteur d'avion
GB201420989D0 (en) Aircraft engine fuel system
GB201405704D0 (en) Gas turbine engine
GB201420175D0 (en) Gas turbine engine
EP2949883B8 (fr) Système de lubrification de moteur de turbine à gaz
GB2524320B (en) Gas turbine engine
DK3247893T3 (da) Forbrændingsmotor, forbrændingssystemer og relaterede fremgangsmåder samt styringsfremgangsmåder og -systemer
GB2558071B (en) Turbine for turbine engine
GB2524229B (en) Gas turbine engine
FR3023872B1 (fr) Dispositif de protection contre survitesse d'un moteur d'aeronef
FR3021954B1 (fr) Ensemble de manutention d'un moteur d'aeronef
GB201416764D0 (en) Gas turbine engine
GB201416505D0 (en) Gas turbine engine
FR3017111B1 (fr) Dispositif d'assemblage de tuyaux carburant double peau d'un aeronef.
PL3149309T3 (pl) Silnik spalinowy
GB201414071D0 (en) Gas turbine engine
GB201420010D0 (en) Gas turbine engine
GB201420011D0 (en) Gas turbine engine

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 5

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11