| 摘要 |
The present invention relates to an integrated electronic operating device and, more specifically, to an electronic operating device including a driving motor rotating an output shaft protruding to the outside of a housing; at least one temperature sensor sensing an inner temperature of the housing; a control unit generating temperature compensating information by receiving information about the temperature sensed by the temperature sensor and controlling the operating device; and at least one temperature compensating body receiving the temperature compensating information from the control unit and controlling the inner temperature of the housing. Disclosed is the electronic operating device wherein an operation controlling method is applied in order to enable the normal operation even in an extremely-low temperature environment which is out of a normal operation possible range of a compartment. The electronic operating device for operating an aileron, a rudder, or a flaperon, and the like according to the present invention is capable of easily obtaining a space for mounting the operating device in an aircraft and minimizing a weight increase of the aircraft caused by the installation of the operating device as a structure of the electronic operating device is simpler and the weight of the electronic operating device is lighter than an operating device using a hydraulic device. In addition, the operating device enabling a normal flight of the aircraft even in the extremely-low temperature environment by increasing the inner temperature of the housing of the operating device or a temperature of the compartment which is out of normal operation possible range even though an ambient temperature is decreased when the aircraft flies at a high altitude. |
