US4706740A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Ventable survivable heat pipe vapor chamber spacecraft radiator
Assignee: United States Department of the Air Force
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Filing: 1987-03-11
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Granted: 1987-11-17
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Expires: 2007-03-11
Abstract
Abstract A system for radiating heat generated by a source of heat aboard a spacecraft or the like is described which comprises a pair of spaced heat pipes and a pair of spaced wall members having inner condensation surfaces and outer heat radiating surfaces bonded to the heat pipes and defining a vapor chamber, a rewet artery of capillary wicking material disposed within the vapor chamber between the heat pipes and extending substantially lengthwise of the vapor chamber, a source of expendable liquid heat exchange medium operatively connected to the rewet artery for maintaining an inventory of heat exchange medium within the vapor chamber, and a pressure relief valve on the vapor chamber for venting vapor overpressure. The condensation surfaces of the wall members include a multiplicity of capillary grooves extending between the rewet artery and the heat pipes to promote vapor condensation, to facilitate flow of condensate toward the heat pipes, and otherwise to maintain a liquid film inventory near the heat radiating surfaces of the wall members.
Inventors
- 👤 Edward T. Mahefkey
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 21:36
CPC Classifications
B; B64; B64G; B64G1/00; B64G1/22; B64G1/46; B64G1/50; B64G1/506; B64G1/503; F; F28; F28D; F28D15/00; F28D15/02; F28D15/0233; F28D15/0275; F28D15/04; Y; Y10; Y10S; Y10S165/00; Y10S165/911
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
259 words
A system for radiating heat generated by a source of heat aboard a spacecraft or the like, which comprises: (a) a pair of heat pipes, each heat pipe having an evaporator end for thermally interfacing said source of heat and an elongated condensor end, the respective condensor ends of said heat pipes being disposed in spaced relationship to each other; (b) a pair of spaced heat conducting wall members having first and second ends and being bonded to said heat pipes with said heat pipes therebetween, said wall members defining respective outer heat radiating surfaces and inner condensation surfaces, said condensation surfaces and said heat pipes defining therebetween a substantially closed vapor chamber of preselected size and configuration having an inlet at corresponding first ends of said wall members and an outlet at corresponding second ends of said wall members; (c) a rewet artery, including capillary wicking material having first and second ends, disposed within said vapor chamber between said condensor ends of said heat pipes, said first end of said rewet artery communicating with said inlet of said vapor chamber; (d) a source of liquid heat exchange medium operatively connected in liquid flow communication with said vapor chamber inlet; (e) means on said condensation surfaces of said wall members for promoting condensation of vaporous heat exchange medium and for facilitating flow of condensed heat exchange medium generally toward said heat pipes; and (f) a pressure relief valve disposed at said outlet of said vapor chamber for venting said vapor chamber when the pressure therein exceeds a preselected level.
Claim 2
Independent Claim
259 words
A system for radiating heat generated by a source of heat aboard a spacecraft or the like, which comprises: (a) a pair of heat pipes, each heat pipe having an evaporator end for thermally interfacing said source of heat and an elongated condensor end, the respective condensor ends of said heat pipes being disposed in spaced relationship to each other; (b) a pair of spaced heat conducting wall members having first and second ends and being bonded to said heat pipes with said heat pipes therebetween, said wall members defining respective outer heat radiating surfaces and inner condensation surfaces, said condensation surfaces and said heat pipes defining therebetween a substantially closed vapor chamber of preselected size and configuration having an inlet at corresponding first ends of said wall members and an outlet at corresponding second ends of said wall members; (c) a rewet artery, including capillary wicking material having first and second ends, disposed within said vapor chamber between said condensor ends of said heat pipes, said first end of said rewet artery communicating with said inlet of said vapor chamber; (d) a source of liquid heat exchange medium operatively connected in liquid flow communication with said vapor chamber inlet; (e) means on said condensation surfaces of said wall members for promoting condensation of vaporous heat exchange medium and for facilitating flow of condensed heat exchange medium generally toward said heat pipes; and (f) a pressure relief valve disposed at said outlet of said vapor chamber for venting said vapor chamber when the pressure therein exceeds a preselected level.
Claim 3
Dependent Claim
75 words
The system of claim 1 wherein said source of liquid heat exchange medium includes means defining a reservoir operatively connected to said inlet of said vapor chamber and communicating with said rewet artery for containing a reserve of said liquid heat exchange medium, and a wicking element disposed within said reservoir and operatively connected to said first end of said rewet artery for supplying liquid heat exchange medium to said rewet artery by capillary action.
Claim 4
Dependent Claim
38 words
The system of claim 2 wherein said rewet artery and said wicking element comprise a wicking material selected from the group consisting of rolled screen, a slotted tube, sintered metal foam, metal felt and porous polymer wetting material.
Claim 5
Dependent Claim
28 words
The system of claim 1 wherein said means on said condensation surfaces of said wall members for promoting condensation and facilitating flow comprises a multiplicity of capillary grooves.
Claim 6
Dependent Claim
28 words
The system of claim 1 wherein said first and second wall members comprise a material selected from the group consisting of aluminum, titanium, metal-graphite composite, steel and niobium.
Claim 7
Dependent Claim
25 words
The system of claim 1 wherein said liquid heat exchange medium comprises a material selected from the group consisting of water, ammonia, methanol and freon.
Claim 8
Dependent Claim
15 words
The system of claim 1 wherein said liquid heat exchange medium comprises a liquid metal.
Claim 9
Dependent Claim
21 words
The system of claim 7 wherein said liquid metal is selected from the group consisting of mercury, potassium, sodium and lithium.
Claim 10
Dependent Claim
26 words
The system of claim 7 wherein said liquid metal is a eutectic mixture of metals selected from the group consisting of mercury, potassium, sodium and lithium.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-11-16 | 1991-05-18 | 1991-11-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-11-16 | 1995-05-18 | 1995-11-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-11-16 | 1999-05-18 | 1999-11-17 | $7700.00 | Window Closed / Lapsed |