CONTROL DEVICE FOR ELECTRIC FLIGHT VEHICLE

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Inventor(s)

CONTROL DEVICE FOR ELECTRIC FLIGHT VEHICLE - A simplified explanation of the abstract

This abstract first appeared for US patent application 18679884 titled 'CONTROL DEVICE FOR ELECTRIC FLIGHT VEHICLE

The abstract describes a control device for an electric flight vehicle, which includes an electric drive device for the rotor blade and a cooling unit for the drive device. The control device has a temperature acquisition unit and a cooling determination unit to monitor and regulate the cooling of the drive device based on its temperature.

Electric flight vehicle control device
Monitors and regulates cooling of the drive device
Includes temperature acquisition unit and cooling determination unit
Ensures proper cooling of the drive device to prevent abnormalities
Enhances safety and efficiency of the electric flight vehicle

Potential Applications: - Electric aircraft industry - Drone technology - Aerospace engineering

Problems Solved: - Prevents overheating of the drive device - Ensures optimal performance of the electric flight vehicle - Enhances safety during flight operations

Benefits: - Improved efficiency and performance - Enhanced safety measures - Extended lifespan of the electric flight vehicle

Commercial Applications: Title: "Advanced Control Device for Electric Flight Vehicles" This technology can be utilized in the electric aircraft industry to enhance the safety and efficiency of electric flight vehicles. It can also be applied in drone technology and aerospace engineering for improved performance and reliability.

Questions about the technology: 1. How does the control device monitor the temperature of the drive device? - The control device uses a temperature acquisition unit to acquire the temperature of the drive device. 2. What are the potential benefits of using this control device in electric flight vehicles? - The control device can improve efficiency, enhance safety, and extend the lifespan of the electric flight vehicle.

Original Abstract Submitted

A control device is configured to control an electric flight vehicle. The electric flight vehicle includes an electric drive device configured to drive and rotate a rotor blade and a cooling unit configured to cool the drive device. The control device includes a temperature acquisition unit and a cooling determination unit. The temperature acquisition unit is configured to acquire temperature of the drive device as a device temperature. The cooling determination unit is configured to determine, according to the device temperature, whether a cooling-related abnormality has occurred as an abnormality related to cooling of the drive device by the cooling unit.