Vent system for an aerospace vehicle
AssigneeThe Boeing Company
InventorsKurt E. Acheson, David S. Chambers, Brian S. Kornegay
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AssigneeThe Boeing Company
InventorsKurt E. Acheson, David S. Chambers, Brian S. Kornegay
Estimating the term…
An improved vent system for venting an internal cavity of an aerospace vehicle to an exterior surface of the aerospace vehicle generally includes a substantially concave vent inlet surface recessed with respect the exterior surface, and a duct opening formed therein. The vent inlet surface has a major axis substantially parallel to the local external flow direction. The upstream surface contour and the downstream surface contour of the vent inlet surface are substantially oblique to the local external flow direction. The placement and orientation of the duct opening, as well as the geometry of the vent inlet surface, may be selected to achieve a particular pressurization of the internal cavity with respect to the external environment under a variety of conditions.
An apparatus comprising:
A vent system for venting an internal cavity of an aerospace vehicle to an exterior surface of the aerospace vehicle, wherein the exterior surface has an associated local external flow direction, the vent system comprising:
A method for venting an interior cavity of an aerospace vehicle to an exterior surface of the aerospace vehicle, wherein the exterior surface has a local external flow direction, the method comprising:
Dependencies are inferred from the claim text.