发明名称 Heat pipe cooled probe
摘要 The basic heat pipe principle is employed to provide a self-contained passively cooled probe that may be placed into a high temperature environment. The probe consists of an evaporator region 13 of a heat pipe 10 and a sensing instrument 17. Heat is absorbed as the working fluid 22 evaporates in the probe. The vapor is transported to the vapor space 14 of the condenser region 15. Heat is dissipated from the condenser region and fins 20 causing condensation of the working fluid, which returns to the probe by gravity and the capillary action of the wick 18. Working fluid, wick and condenser configurations and structure materials can be selected to maintain the probe within an acceptable temperature range.
申请公布号 US4485670(A) 申请公布日期 1984.12.04
申请号 US19810234222 申请日期 1981.02.13
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 CAMARDA, CHARLES J.;COUCH, LANA M.
分类号 F28D15/02;G01K1/12;G12B15/02;(IPC1-7):G01L19/04 主分类号 F28D15/02
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