IP Library › Granted Patent US 7,232,093
Granted Patent B2
US 7,232,093 · App. 11/271,600 · Granted Jun 19, 2007

Cooled insulation surface temperature control system

Assignee: The Boeing Company
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Quick Facts
Patent No.
US 7,232,093
App. No.
11/271,600
Granted
Jun 19, 2007
Kind
B2
Abstract

An apparatus and method for surface temperature control is provided. Surface temperature control is achieved by flowing coolant in and then out of a low strength porous layer attached to a structural plenum. A semi-permeable layer may be attached to the outer surface of the porous layer to prevent erosion of the porous layer and to facilitate surface film cooling.

Claims (27)

1. A method of cooling a surface comprising:

providing a structural plenum bounded by an inner structural member and an outer structural wall;

providing a porous layer attached to said outer structural wall exterior to said plenum;

providing a semi-permeable layer attached to said porous layer;

providing a plurality of openings in said semi-permeable layer;

providing openings in said outer structural wall to place said plenum in fluid communication with said porous layer; and

providing pressurized air within said plenum, wherein a majority of said pressurized air exits said porous layer through the plurality of openings in said semi-permeable layer, and wherein a portion of said pressurized air transpires through said semi-permeable layer in regions between said openings, said pressurized air that exits through said plurality of openings combines with said portion of pressurized air that transpires through said semi-permeable layer to form a cooling film adjacent to said surface being cooled.

2. The method of claim 1 , wherein said pressurized air generally flows through the thickness of said porous layer from said openings in said outer structural wall of said plenum to said semi-permeable layer with some spreading of flow in the plane of said porous layer.

3. A method of cooling a surface, the method comprising:

providing a porous layer beneath said surface;

providing a plenum beneath said porous layer;

providing a plurality of exit holes in said surface;

providing a semi-permeable layer in areas between said exit holes;

flowing coolant from said plenum into said porous layer and through said exit holes; and

transpiring coolant from said plenum into said porous layer and through said semi-permeable layer, wherein a majority of the coolant flows through said exit holes and a minority of coolant transpires through said semi-permeable layer.

4. The method of claim 3 , wherein said plenum is formed between an inner structural member and an outer structural wall.

5. The method of claim 4 , wherein at least one of said inner structural member and said outer structural wall is formed from a metallic material.

6. The method of claim 4 , wherein said porous layer is adhesively bonded to said outer structural wall.

7. The method of claim 6 , wherein coolant flows from said plenum through one or more entrance holes formed in said outer structural wall into said porous layer.

8. The method of claim 3 , wherein coolant spreads in the plane of said porous layer while traveling through the thickness of said porous layer.

9. A method of cooling a surface, the method comprising:

providing a porous layer beneath said surface;

providing a plenum beneath said porous layer;

providing a plurality of exit holes in said surface;

providing a semi-permeable layer in areas between said exit holes;

flowing coolant from said plenum into said porous layer and through said exit holes; and

transpiring coolant from said plenum into said porous layer and through said semi-permeable layer wherein coolant flow exiting through said surface exit holes combines with coolant transpiring through said semi-permeable layer forming a cooling film at said surface.

Continuity (2)
Division 1045520400 · Jun 5, 2003
Related Publication 20060060702A1 · Mar 23, 2006