HEAT PIPES
Assignee
Filed
Jun 15, 1978
Granted
Aug 8, 1995
Location
IE
Abstract
A heat pipe, which may for instance be in the form of an aerofoil blade for a gas turbine engine, is provided with capillary means which is in two different forms. One form is constituted by a porous material and the other constituted by grooves formed in the surface of the internal wall of the heat pipe.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Jun 24, 1982
Rescinded
Nov 29, 1994
Duration
12 years, 5 months
Inventor
- 1DAVID WILLIAM ARTT
Record Details
- Patent number
- US 5439351
- Application
- 00591727
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
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