An in-line heater system on board an aircraft includes a heater element positioned within a tubing, at least one sensor positioned within the tubing configured to monitor the temperature within the tubing, and an inline heater controller configured to receive information regarding the heater element via the at least one sensor. The inline heater controller is positioned at a location spaced away from the heater element and the tubing. The inline heater controller includes a printed circuit board configured to receive the information regarding the heater element via the at least one sensor, and an aerospace connector configured to transmit the information regarding the heater element via the at least one sensor to the aircraft.
INLINE HEATER CONTROLLER
2018-10-11
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |