The invention discloses a single-seat ultra-light aircraft cockpit layout method, and belongs to the field of ultra-light aircraft cockpit design. The cabin layout comprises a comprehensive display and control console, a throttle lever, a three-axis control lever, a high-strength carbon fiber racing car grade lightweight seat, a five-point safety belt, a pedal and an emergency complete machine parachute. In functional design, the single-seat electric multi-rotor ultra-light aircraft has an automatic driving capability and has a manual stability augmentation mode, a fixed height mode, a fixed point mode and an airline flight mode. The single-seat ultra-light aircraft cockpit serves as an interaction and bearing entity of a single-seat electric multi-rotor ultra-light aircraft and a driver and is used for achieving the basic flight control function of the driver while ensuring reasonable man-machine interaction space accessibility and reasonable space perception and flight experience view. The aircraft has the functions of air flight and reliable, stable and comfortable riding, and provides basic flight communication, navigation, identification and positioning information functions, emergency landing safety function and noise suppression function.
一种单座超轻型飞机座舱布局方法,属于超轻型飞机座舱设计领域。座舱布局包括综合显控台、油门杆、三轴操纵杆、高强度碳纤维赛车级轻量化座椅、五点式安全带、脚踏板和应急整机降落伞。在功能设计上,单座电动多旋翼超轻型飞机具备自动驾驶能力,具有手动增稳模式、定高模式、定点模式与航线飞行模式。单座超轻型飞机座舱作为单座电动多旋翼超轻型飞机与驾驶员交互与承载实体,用于在确保合理的人机交互空间可达性、合理的空间感知与飞行体验视野的同时,实现驾驶员基本飞行操纵控制功能,空中飞行与机体可靠稳固舒适乘坐功能,提供基本飞行通信、导航、识别定位信息功能,应急着陆安全功能,噪声抑制功能。
Single-seat ultra-light aircraft cockpit layout method
一种单座超轻型飞机座舱布局方法
2025-03-11
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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