Indirectly heated aircraft probes and masts

Details Indirectly heated aircraft probes and masts Indirectly heated aircraft probes and masts

1979-11-23

1981-06-30

Woodiel, Donald O.

Measuring and testing

Volume or rate of flow

Using differential pressure

73182, 16510426, 219201, G01F 146

Patent

active

042756030

ABSTRACT:
Aircraft probe or mast including heat pipe for indirectly heating the probe or mast thereby providing deicing. Heat for the heat pipe configured probe or mast is supplied by remote location of a heat source. The heat source may include a replacement plug in electric heater or a remote heat source such as an engine airbleed duct.

REFERENCES:
patent: 2706408 (1955-04-01), Holbrook
patent: 2858698 (1958-11-01), Hickey
patent: 2870633 (1959-01-01), Harding et al.
patent: 2992313 (1961-07-01), Taylor
patent: 3664412 (1972-05-01), Zerkle
patent: 3735175 (1973-05-01), Blomgren

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