An electric temperature control system for unpressurized aircraft and methods for operating are disclosed. The electric temperature control system may be electrically powered and used on all-electric aircraft or hybrid aircraft. The electric temperature control system may comprise a vapor cycle cooling system for cooling air and an electric heater for heating air. The electric heater may be a PTC electric heater with individually-controllable heating elements. Various input devices may be disposed in the aircraft allowing an operator to set a compartment temperature, an air source, and a fan speed. A controller controls operations of the electric temperature control system based on feedback received from a plurality of feedback devices and the operator inputs.
ELECTRIC TEMPERATURE CONTROL SYSTEM FOR UNPRESSURIZED AIRCRAFT
2023-11-23
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Electric temperature control system for unpressurized aircraft
European Patent Office | 2024
|Electric Temperature Control System for Unpressurized Aircraft
European Patent Office | 2024
|Heating control system and method for unpressurized aircraft
European Patent Office | 2024
|Heating Control System and Method for Unpressurized Aircraft
European Patent Office | 2023
|ICC - The Unpressurized Cargo Carrier Family
AIAA | 2003
|