Draining apparatus for draining liquids from a vehicle, aircraft having a draining apparatus and method for draining liquids from a vehicle

Patent metadata

Field	Value
Publication number	US-9428271-B2
Application number	US-201314101532-A
Country	US
Kind code	B2
Filing date	Dec 10, 2013
Priority date	Dec 12, 2012
Publication date	Aug 30, 2016
Grant date	Aug 30, 2016

Abstract

A draining apparatus for draining liquids from a vehicle includes a containment; a drain mast having an outlet opening and an inlet; and an actuator. The containment is adapted for being coupled with a structure of the vehicle, wherein the actuator is coupled with the drain mast and adapted for moving the drain mast into a retracted position and at least one extracted position relative to the containment, and wherein the containment is further adapted for accommodating the drain mast in the retracted position at least partially. The drainage apparatus has clear advantages regarding the parasitic drag compared to known drainage masts as it is only deployed into the flow when it is absolutely necessary.

First claim

The invention claimed is:

1. A draining apparatus for draining liquids from a vehicle, comprising:
a containment;
a drain mast having an outlet opening and an inlet; and
an actuator;
wherein the containment is adapted for being coupled with a structure of the vehicle,
wherein the actuator is coupled with the drain mast and adapted for moving the drain mast into a retracted position and at least one extracted position relative to the containment,
wherein the containment is further adapted for accommodating the drain mast in the retracted position at least partially,
wherein the drain mast is rotatably supported around a rotational axis, wherein the drain mast extends over a coupling surface facing away from the containment at least in an extended position of the drain mast, and
wherein the drain mast comprises a longitudinal component having a main extension direction and further having a projected covering surface extending along substantially the whole extension of the longitudinal component for covering a cut-out in the skin of the vehicle in a retracted position of the drain mast.

2. The apparatus according to claim 1 , wherein the containment comprises a coupling surface adapted for coupling the containment with a skin component of the vehicle.

3. The apparatus according to claim 1 , wherein the drain mast comprises a first end and a second end,
wherein the rotational axis is arranged at the first end, and
wherein the drainage opening is arranged at the second end.

4. The apparatus according to claim 1 , wherein the drain mast is movable between a retracted position and an outermost extended position, which positions are distanced by an angle of 50°.

5. The apparatus according to claim 1 , wherein the drain mast is supported for conducting a translational motion relative to the containment, wherein the actuator is an axial actuator.

6. The apparatus according to claim 1 , further comprising a flexible liquid line connected to the inlet of the drain mast and a fluid interface with a fixed installation position relative to the containment.

7. The apparatus according to claim 1 , further comprising a heating apparatus at least on the drain mast connected to an electric interface with a spatially fixed installation position relative to the containment.

8. The apparatus according to claim 1 , further comprising a level switch connectable to a liquid containing component upstream of the drain mast,
wherein the level switch is couplable to the actuator in order to extend the drain mast when the level switch detects the presence of a liquid to be discharged.

9. The apparatus according to claim 1 , further comprising a buffer tank upstream of the drain mast, in which buffer tank the liquids to be discharged are collected to be discharged.

10. The apparatus according to claim 1 , further comprising a valve upstream of the inlet of the drain mast for preventing liquid flow to the outlet of the drain mast.

11. An aircraft, comprising a fuselage having a skin and at least one apparatus , the apparatus comprising:
a containment;
a drain mast having an outlet opening and an inlet; and
an actuator;
wherein the containment is adapted for being coupled with a structure of the vehicle;
wherein the actuator is coupled with the drain mast and adapted for moving the drain mast into a retracted position and at least one extracted position relative to the containment;
wherein the containment is further adapted for accommodating the drain mast in the retracted position at least partially;
wherein the apparatus is attached to an inner side of the aircraft skin and wherein the containment is positioned above a cut-out of the fuselage skin;
wherein the drain mast is rotatably supported around a rotational axis, wherein the drain mast extends over a coupling surface facing away from the containment at least in an extended position of the drain mast, and
wherein the drain mast comprises a longitudinal component having a main extension direction and further having a projected covering surface extending along substantially the whole extension of the longitudinal component for covering a cut-out in the skin of the vehicle in a retracted position of the drain mast.

Assignees

• Airbus Operations Gmbh

Inventors

• Becks Ralf
• Lucas Raymond

Classifications

• Y10T137/6906

  Aerial or water-supported [e.g., airplane or ship, etc.] · CPC title

• Y10T137/0318

  Processes · CPC title

• B64C1/1453 Primary

  Drain masts · CPC title

• B64D1/16 Primary

  Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting (jettisoning fuel B64D37/26) · CPC title