US4671348A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Transverse flow edge heat pipe
Assignee: McDonnell Douglas Corp
•
Filing: 1985-05-21
•
Granted: 1987-06-09
•
Expires: 2005-05-21
Abstract
Abstract An edge situated in high speed flow of medium is cooled by a tubular heat pipe having a longitudinal axis situated parallel to the edge. The exterior surface of the evaporator section of the heat pipe forms the edge. The heat pipe contains a working fluid existing in both gaseous and liquefied states. Heat input along the edge evaporates working fluid in the liquid state located in the evaporator section, and the heat is transferred transversely across the longitudinal axis of the heat pipe by the flow of vapor to the condenser section. The vapor condenses in the condenser section and releases its latent heat of vaporization. The condensate flows to the evaporator section by means of wicks composed of capillary material. The heat released into the walls of the condenser section is transferred through the walls by conduction and into another heat transfer device, for example, an active cooling apparatus or the evaporator sections of abutting heat pipes of conventional tubular configuration.
Inventors
- 👤 Paul E. Bauer
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 22:44
CPC Classifications
B; B64; B64C; B64C3/00; B64C3/36; B64C1/00; B64C1/38
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
134 words
A leading edge heat pipe for a flight vehicle comprising: a closed tube; a working fluid enclosed in said tube and existing as both a liquid and a vapor; said tube having a warm region and a cool region, said warm region being warm relative to said cool region, and both said warm region and said cool region continuing for the longitudinal length of said closed tube; capillary material contained in said tube for conveying said liquid from said cool region to said warm region; a warm lateral tube wall included in said warm region and a cool lateral tube wall included in said cool region; secondary heat transfer means for transferring heat away from said cool lateral tube wall; and said warm lateral tube wall forming a leading edge on a flight vehicle.
Claim 2
Dependent Claim
134 words
A leading edge heat pipe for a flight vehicle comprising: a closed tube; a working fluid enclosed in said tube and existing as both a liquid and a vapor; said tube having a warm region and a cool region, said warm region being warm relative to said cool region, and both said warm region and said cool region continuing for the longitudinal length of said closed tube; capillary material contained in said tube for conveying said liquid from said cool region to said warm region; a warm lateral tube wall included in said warm region and a cool lateral tube wall included in said cool region; secondary heat transfer means for transferring heat away from said cool lateral tube wall; and said warm lateral tube wall forming a leading edge on a flight vehicle.
Claim 3
Dependent Claim
40 words
The leading edge heat pipe as defined in claim 1 further comprising: at least one partition dividing said closed tube into a plurality of longitudinally juxtaposed closed tubes; and said partition being thermally conductive and impermeable to said working fluid.
Claim 4
Dependent Claim
22 words
The leading edge heat pipe as defined in claim 2 wherein: said capillary material lines the inner surfaces of said closed tube.
Claim 5
Dependent Claim
41 words
The leading edge heat pipe as defined in claim 3 further comprising: an additional quantity of said capillary material extending in a planar fashion from said cool lateral tube wall to said warm lateral tube wall and defining vapor passageways therethrough.
Claim 6
Dependent Claim
22 words
The leading edge heat pipe as defined in claim 4 wherein: said leading edge is the foremost edge of an air foil.
Claim 7
Dependent Claim
18 words
The leading edge heat pipe as defined in claim 4 wherein: said leading edge is a fuselage chine.
Claim 8
Dependent Claim
21 words
The leading edge heat pipe as defined in claim 4 wherein: said leading edge forms the lip of an engine inlet.
Claim 9
Dependent Claim
79 words
The leading edge heat pipe as defined in claim 2 wherein said secondary heat transfer means is comprised of: at least one leg heat pipe; said leg heat pipe being tubular and having a warm leg heat pipe end and a cool leg heat pipe end, said warm leg heat pipe end being warm relative to said cool leg heat pipe end; and said warm leg heat pipe end being in thermal contact with said cool lateral tube wall.
Claim 10
Dependent Claim
22 words
The leading edge heat pipe as defined in claim 8 wherein: said cool leg heat pipe end rejects heat into free space.
Claim 11
Dependent Claim
32 words
The leading edge heat pipe as defined in claim 9 wherein: said at least one leg heat pipe has its longitudinal axis situated transverse to the longitudinal axis of said closed tube.
Claim 12
Dependent Claim
22 words
The leading edge heat pipe as defined in claim 10 wherein: said capillary material lines the inner surfaces of said closed tube.
Claim 13
Dependent Claim
41 words
The leading edge heat pipe as defined in claim 11 further comprising: an additional quantity of said capillary material extending in a planar fashion from said cool lateral tube wall to said warm lateral tube wall and defining vapor passageways therethrough.
Claim 14
Dependent Claim
21 words
The leading edge heat pipe as defined in claim 11 wherein: said leading edge is the foremost edge of an airfoil.
Claim 15
Dependent Claim
18 words
The leading edge heat pipe as defined in claim 11 wherein: said leading edge is a fuselage chine.
Claim 16
Dependent Claim
21 words
The leading edge heat pipe as defined in claim 12 wherein: said leading edge forms the lip of an engine inlet.
References Cited (Backward Citations)
US3369782A
Cited
US3450195A
Cited
DE1956361A1
Cited
US3749156A
Cited
US3837311A
Cited
US3929305A
Cited
US4207027A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-06-08 | 1990-12-08 | 1991-06-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-06-08 | 1994-12-08 | 1995-06-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-06-08 | 1998-12-08 | 1999-06-09 | $7700.00 | Window Closed / Lapsed |