The invention discloses a vertical take-off and landing fixed-wing aircraft, and relates to the technical field of aircrafts. According to the invention, the conversion from a multi-rotor flight mode to a fixed-wing flight mode and from the fixed-wing flight mode to the multi-rotor flight mode can be easily realized. Due to the structural layout characteristics of the aircraft, the safety of the aircraft is guaranteed, and the aircraft can be safely and reliably landed according to the fault degree and urgency of the aircraft even if the aircraft breaks down seriously and only forced landing can be selected. Through multi-rotor-wing assisting control, the forced landing buffering function of the telescopic empennage assembly and the safety protection measure of a protection sponge lining in the manned cabin, various safety modes and measures such as an internal safety protection air bag, an external safety protection air bag and a forced landing parachute of the manned cabin can be selectively used according to the fault degree and urgency of the aircraft; and safe or low-damage forced landing of the aircraft is realized.
本发明公开了一种垂直起降固定翼飞行器,涉及飞行器技术领域。本发明,能够轻易实现从多旋翼飞行模式向固定翼飞行模式和从固定翼飞行模式向多旋翼模式的转换。因本飞行器的结构布局特性,保证了本飞行器的安全性,即使飞行器出现较严重故障只能选择迫降时,也可根据飞行器的故障程度和紧迫性,通过多旋翼协助控制、可伸缩尾翼组件迫降缓冲功能、载人舱内部防护海绵内衬本就具备的安全防护措施外,也可根据飞行器的故障程度和紧迫性,选择性使用载人舱内部安全防护气囊、外部安全防护气囊以及迫降伞等多种安全方式措施,实现飞行器的安全或低损伤迫降。
Vertical take-off and landing fixed-wing aircraft
一种垂直起降固定翼飞行器
2025-02-07
Patent
Electronic Resource
Chinese