飞行器的控制系统、方法、装置、电子设备及存储介质
By integrating an electronic compressor and an electronic turbocharger into the aircraft control system, and combining the coordinated operation of the drive motor and the power battery pack, efficient power output and energy management are achieved in high-altitude, low-oxygen environments, solving the problem of poor power performance in existing technologies.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- GUANGZHOU AUTOMOBILE GROUP CO LTD
- Filing Date
- 2025-10-29
- Publication Date
- 2026-07-17
AI Technical Summary
Existing aircraft power systems struggle to maintain efficient and stable operation in high-altitude and low-oxygen environments. Hybrid power systems lack effective energy recovery and power demand balancing mechanisms, resulting in poor power performance.
It adopts an electronic compressor and an electronic turbocharger combined with the engine, and is coupled or disengaged through a clutch device. The drive motor and the power battery pack work together. The controller adjusts the working mode according to the real-time power and power, and optimizes energy management by combining an altitude recognition device.
It improves the power output efficiency and energy utilization of the aircraft in high-altitude, low-oxygen environments, enhances the system's power response speed and endurance, and ensures that power requirements are met in different flight phases.
Smart Images
Figure CN121106717B_ABST