Apparatus for ventilating liquid containers on aircraft

Claim 2

Apparatus for ventilating a liquid tank in aircraft during hazardous pressure rises for all aircraft attitudes, comprising: a plurality of ventilation pipes, at least one of said ventilation pipes having an orifice above the liquid level of said tank and at least one of said ventilation pipes having an orifice below said liquid level; two separate chambers sealed off from the interior of said tank and connected to said ventilation pipes; a rotary slide valve associated with said chambers and having a weight for controlling said rotary slide valve according to flight attitude; said rotary slide valve having control slots offset so that flow via said ventilation pipe below said liquid level is blocked during free flow via said ventilation pipe above said liquid level.

Claim 3

Apparatus as defined in claim 1 including rotary slide means; a housing connected to said tank and pivotally mounting said rotary slide means; said housing having two stops for maximum displacement of said weight connected to said rotary slide means.

Claim 4

Apparatus as defined in claim 2 including insert means connected to said housing for forming two adjacent separate annular channels between said housing and said rotary slide means, said annular channels corresponding to two separate housing openings; a base plate with further openings connected to said housing openings, said housing openings being connected to two said chambers through said further openings of said base plate, said rotary slide means having two cylindrical chambers separated by a wall, said cylindrical chambers being opened on the outer ends facing away from said wall and opening into a space enclosing said valve and being connected to a ventilation line, said insert means having slots at levels of both said annular channels, said channels being located in common lengthwise planes and being uniformly spaced in a peripheral direction, said rotary slide means having also control slots located at the level of either annular channel and being offset from their respective annular channels and chamber in a peripheral direction, so that depending on an end position of said rotary slide means either one annular channel is connected via slots of said insert means and said rotary slide means to one of said cylindrical chambers or the other annular channel is connected via other slots of said insert means and said slide means to the other cylindrical chamber.

Claim 5

Apparatus as defined in claim 3 wherein one of said cylindrical chambers is formed by a sleeve-shaped insert connected rigidly to said rotary slide means, said sleeve-shaped insert having flow slots aligned coincidentally with said control slots of said rotary slide means.

Claim 6

Apparatus as defined in claim 2 wherein said liquid tank has a plurality of separate chambers associated with a plurality of separate annular channels connectable through flow slots with respective separate chambers of said rotary slide means, a centered end position being selectable for said rotary slide means for tank ventilation in addition to two end positions of said rotary slide means restricted by said stops when three separate chambers are arranged within said tank.

Claim 7

Apparatus as defined in claim 2 wherein said rotary slide means has a longitudinal axis lying in a plane defined by the roll axis and pitch axis of the aircraft.

Claim 8

Apparatus as defined in claim 2 wherein said rotary slide means has a longitudinal axis inclined towards the plane defined by the roll axis and pitch axis of the aircraft.

Claim 9

Apparatus as defined in claim 2 wherein said rotary slide valve is arranged on said tank and has a variable position.