Claims
- 1. In a heat pipe which includes at least one liquid return artery which extends into the evaporator region of the heat pipe, the improvement comprising an extension structure attached to at least one artery at the end of the artery most remote from the condenser region of the heat pipe, with the extension structure extending out of the evaporator region of the heat pipe and into a region which is not subjected to heat.
- 2. The heat pipe of claim 1 wherein the extension structure is constructed so that it acts as a capillary structure to pump liquid from within the extension structure to the evaporator of the heat pipe.
- 3. The heat pipe of claim 1 further including a cooling means acting upon the extension structure to aid in condensing vapor within the extension structure.
- 4. The heat pipe of claim 1 wherein the heat pipe includes a first wick structure with at least one artery located within the first wick structure and an artery within the first wick tructure attached to the artery extension structure.
- 5. The heat pipe of claim 4 further including a second wick structure located within the extension structure with the second wick structure connected to the first wick structure so that liquid can move between the wick structures.
SUMMARY OF THE INVENTION
The invention described herein was made in the performance of work under NASA contract NAS8-37261 and is subject to the provisions of Section 305 of the National Aeronautics and Space Act of 1958, Public Law 85-568 (72 Stat. 435; 42 USC 2457).
US Referenced Citations (4)