Aircraft bleed system and method of controlling an aircraft bleed system
US-9207688-B2 · Dec 8, 2015 · US
US10160545B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10160545-B2 |
| Application number | US-201514886365-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 19, 2015 |
| Priority date | Oct 19, 2015 |
| Publication date | Dec 25, 2018 |
| Grant date | Dec 25, 2018 |
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A heat exchanger to exchange heat between a ram air flow and a liquid flow includes a plurality of ram air layers that direct air, wherein each ram air layer is a single pass layer including a plurality of ram air fins in fluid communication with the ram air flow, and a plurality of liquid pass layers, wherein each liquid pass layer is a five pass layer including a plurality of liquid pass fins in fluid communication with the liquid flow, and each of the plurality of liquid pass layers is disposed adjacent to at least one ram air layer of the plurality of ram air layers.
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What is claimed is: 1. A heat exchanger to exchange heat between a ram air flow and a liquid flow, comprising: a plurality of ram air layers that direct air, wherein each ram air layer is a single pass layer including a plurality of ram air fins in fluid communication with the ram air flow; and a plurality of liquid pass layers, wherein each liquid pass layer is a five pass layer including: a liquid inlet defined through a first end wall; a liquid outlet defined through a second end wall opposite the first end wall; a plurality of liquid pass fins in fluid communication with the liquid flow, and each of the plurality of liquid pass layers is disposed adjacent to at least one ram air layer of the plurality of ram air layers; first tent fins and second tent fins proximate to the first and second end walls, respectively, which are respectively interposed between sequential ones of the liquid pass fins and configured to direct the liquid flow from a first direction, to an intermediate direction and to a second direction opposite the first direction; and first closure bars and second closure bars proximate to the first and second end walls, respectively, which are interposed between adjacent tent fins of the first tent fins and the second tent fins and corresponding sections of the liquid flow in the first and second directions, wherein: the first tent fins and one of the first closure bars that is remote from the liquid inlet terminate at an interior plane of the first end wall, the second tent fins and one of the second closure bars that is remote from the liquid outlet terminate at an interior plane of the second end wall, the one of the first closure bars that is proximate to the liquid inlet terminates at an exterior plane of the first end wall, and the one of the second closure bars that is proximate to the liquid outlet terminates at an exterior plane of the second end wall. 2. The heat exchanger of claim 1 , wherein the plurality of liquid pass fins each have a liquid pass fin height of 0.058 inches. 3. The heat exchanger of claim 1 , wherein the plurality of liquid pass fins have a liquid pass fin density of between 10 to 14 fins per inch. 4. The heat exchanger of claim 1 , wherein the plurality of liquid pass fins each have a liquid pass fin thickness of between 0.002 to 0.004 inches. 5. The heat exchanger of claim 1 , wherein the plurality of ram air fins each have a ram air fin height of 0.500 inches. 6. The heat exchanger of claim 1 , wherein the plurality of ram air fins includes a plurality of ruffled ram air fins and a plurality of straight ram air fins. 7. The heat exchanger of claim 6 , wherein the plurality of ruffled ram air fins have a ruffled ram air fin density of between 22 to 26 fins per inch. 8. The heat exchanger of claim 6 , wherein the plurality of ruffled ram air fins have a ruffled ram air fin thickness of between 0.002 to 0.004 inches. 9. The heat exchanger of claim 6 , wherein the plurality of straight ram air fins have a straight ram air fin density of between 7 to 11 fins per inch. 10. The heat exchanger of claim 6 , wherein the plurality of straight ram air fins have a straight ram air fin thickness of between 0.011 to 0.013 inches. 11. The heat exchanger of claim 1 , wherein each ram air layer has a ram air flow length of 7.3 inches. 12. The heat exchanger of claim 1 , wherein each liquid pass layer has a total liquid flow length of 14.7 inches. 13. The heat exchanger of claim 1 , wherein the plurality of ram air layers is between 53 to 57 ram air layers. 14. The heat exchanger of claim 1 , wherein the plurality of liquid pass layers is between 52 to 56 liquid pass layers. 15. The heat exchanger of claim 1 , further comprising a plurality of parting sheets, wherein each parting sheet is disposed between each of the plurality of liquid pass layers and each of the plurality of ram air layers. 16. A power electronics cooling system, comprising: a heat exchanger to exchange heat between a ram air flow and a liquid flow, including: a plurality of ram air layers that direct air, wherein each ram air layer is a single pass layer including a plurality of ram air fins in fluid communication with the ram air flow; and a plurality of liquid pass layers, wherein each liquid pass layer is a five pass layer including: a liquid inlet defined through a first end wall; a liquid outlet defined through a second end wall opposite the first end wall; a plurality of liquid pass fins in fluid communication with the liquid flow, and each of the plurality of liquid pass layers is disposed adjacent to at least one ram air layer of the plurality of ram air layers; first tent fins and second tent fins proximate to the first and second end walls, respectively, which are respectively interposed between sequential ones of the liquid pass fins and configured to direct the liquid flow from a first direction, to an intermediate direction and to a second direction opposite the first direction; and first closure bars and second closure bars proximate to the first and second end walls, respectively, which are interposed between adjacent tent fins of the first tent fins and the second tent fins and corresponding sections of the liquid flow in the first and second directions, wherein: the first tent fins and one of the first closure bars that is remote from the liquid inlet terminate at an interior plane of the first end wall, the second tent fins and one of the second closure bars that is remote from the liquid outlet terminate at an interior plane of the second end wall, the one of the first closure bars that is proximate to the liquid inlet terminates at an exterior plane of the first end wall, and the one of the second closure bars that is proximate to the liquid outlet terminates at an exterior plane of the second end wall. 17. The heat exchanger of claim 1 , wherein the tent fins of the first tent fins and the second tent fins comprise opposite sides tapering from an end plane toward one another to form a point and a proximal one of the closure bars of the first closure bars and the second closure bars extends from the end plane to a plane of the point. 18. The heat exchanger of claim 17 , wherein the liquid flow in the first direction is directed to flow in the intermediate direction at one of the opposite sides of each of the first and second tent fins and is directed to flow in the second direction at the other of the opposite sides of each of the first and second tent fins. 19. The power electronics cooling system of claim 16 , wherein the tent fins of the first tent fins and the second tent fins comprise opposite sides tapering from an end plane toward one another to form a point and a proximal one of the closure bars of the first closure bars and the second closure bars extends from the end plane to a plane of the point.
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