Heater for aircraft potable water tank

Details Heater for aircraft potable water tank Heater for aircraft potable water tank

H - Electricity

05

B

H05B 3/18 (2006.01) B64D 11/00 (2006.01) F24H 1/18 (2006.01) H01C 1/08 (2006.01) H01C 3/00 (2006.01) H01C 3/06 (2006.01) H01C 3/20 (2006.01) H05B 3/36 (2006.01) H05B 3/46 (2006.01) H05B 3/58 (2006.01)

Patent

CA 2428530

A heater (10) for installation on a potable water tank (12). The heater (10) comprises a blanket (14) including an electrical resistance heating element (16) and a connection pad (18) for electrically connecting the heating element (16) to lead lines (20) to an aircraft power source (22). The water tank (12) is typically positioned under the cabin floor ar other locations on an aircraft which are susceptible to cold temperatures, moisture invasion, and pressure drops/rises caused by changing altitudes. The heater (10) maintains the tank (12) at an acceptable temperature range and prevents freezing of the water.

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