Airbus Operations Gmbh

Parker-hannifin Corporation

Job Telford Kingdom Hutchings

Benjamin Richardson

Ted Dinh

Stuart Robert Fox

Michael Kevin Nolte

An aircraft fuel tank vent () having a first interface () for fluid communication with an aircraft fuel tank interior, and a second interface () for fluid communication with an aircraft fuel tank exterior, the vent comprising: a first flow path () between the first interface and the second interface, the fuel tank vent having a baffle () positioned in the first flow path, and, a second flow path () between the first interface and the second interface, the fuel tank vent having a overpressure device () positioned in the second flow path, wherein the first and second flow paths are common along at least a part of their length such that they are coincident at the second interface.

Aircraft fuel tank vent protector

The present application relates to a shaft locking device. The device has an locking element configured to be mounted on a shaft in a first position so that the locking element indicates the angular position of the shaft. The locking element is also configured to be mounted on a shaft in a second position so that the locking element is locatable against a stop to prevent rotation of the shaft. The present application also relates to a device for determining the angular position of a shaft, a valve assembly and an actuating unit for a valve.

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Bristol, United Kingdom

Job Telford Kingdom Hutchings