A hybrid heater system for an aircraft air data sensor includes a voltage source (46) and a first hybrid heater set (42). The first hybrid heater set includes a carbon nanotube (CNT) heater (28), a first positive temperature coefficient (PTC) heater disposed in parallel with the CNT heater (28) to form a parallel formation, and a second PTC heater disposed in series between the voltage source (46) and the parallel formation.
THIN FILM HEATER CONFIGURATION FOR AIR DATA PROBE
DÜNNSCHICHTHEIZUNGSKONFIGURATION FÜR EINE LUFTDATENSONDE
CONFIGURATION DE DISPOSITIF CHAUFFANT À FILM MINCE POUR SONDE DE DONNÉES D'AIR
2021-09-22
Patent
Electronic Resource
English
IPC: | G01P MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK , Messen der Linear- oder Winkelgeschwindigkeit, der Beschleunigung, der Verzögerung oder des Stoßes / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung |
AIR DATA PROBE INCLUDING SELF-REGULATING THIN FILM HEATER
European Patent Office | 2024
|NTRS | 1994
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