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1. WO2013140156 - A VENT FOR AN AIRCRAFT WING FUEL TANK

Publication Number WO/2013/140156
Publication Date 26.09.2013
International Application No. PCT/GB2013/050709
International Filing Date 19.03.2013
IPC
B64C 3/34 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
3Wings
34Integrally-constructed tanks, e.g. for fuel
B64D 37/00 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
37Arrangements in connection with fuel supply for power plant
CPC
B64C 3/34
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
3Wings
34Integrally-constructed tanks, e.g. for fuel
B64D 37/00
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
37Arrangements in connection with fuel supply for power plant
B64D 37/005
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
37Arrangements in connection with fuel supply for power plant
005Accessories not provided for in the groups B64D37/02 - B64D37/28
Applicants
  • AIRBUS OPERATIONS LIMITED [GB]/[GB]
Inventors
  • JAMES, Dylan
Agents
  • SCOTT, Alistair
Priority Data
1204941.721.03.2012GB
Publication Language English (EN)
Filing Language English (EN)
Designated States
Title
(EN) A VENT FOR AN AIRCRAFT WING FUEL TANK
(FR) DISPOSITIF DE MISE À L'AIR LIBRE D'UN RÉSERVOIR DE CARBURANT D'AILE D'AVION
Abstract
(EN)
An aircraft fuel tank vent opening having a liquid separation nozzle, the liquid separation nozzle and the opening dimensioned such that migration across the liquid separation nozzle to the underside of a wing, of fuel escaping from the vent opening, is inhibited during normal operating conditions.
(FR)
La présente invention concerne une ouverture de mise à l'air libre d'un réservoir de carburant d'avion comportant une buse de séparation de liquide, la buse de séparation de liquide et l'ouverture étant dimensionnées de sorte que la migration à travers la buse de séparation de liquide vers la face inférieure d'une aile, de carburant s'échappant depuis l'ouverture de mise à l'air libre, soit interdite dans de conditions normales de fonctionnement.
Also published as
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