The invention discloses a safe landing system for an aircraft under extreme conditions, and relates to the technical field of aircrafts. Compared with a traditional parachute, the safe landing system for the aircraft under the extreme condition adopts the first helium air bag and the second helium air bag, the ejection speed is higher, the descending speed of the aircraft body can be slowed down in the first time, meanwhile, the generated impact force is small, the safety of the aircraft body and carried personnel can be effectively protected, and in addition, the safety of the aircraft is improved. The unmanned aerial vehicle further has excellent adaptability and can cope with various complex ground environments, stable support is provided for the aircraft body, the hang glider mechanism is further introduced to cope with the situation that the aircraft body loses the flying ability, and the hang glider mechanism can change the advancing direction and reduce the falling speed through swinging in the landing process; therefore, the landing safety is further improved, the safety of the aircraft body and carried personnel can be protected in emergency, and the application range of the aircraft can be expanded to a certain extent.
本发明公开了一种极端情况下飞行器安全降落系统,涉及飞行器技术领域。该种极端情况下飞行器安全降落系统,相比于传统的降落伞,采用第一氦气气囊和第二氦气气囊,弹出速度更快,能够在第一时间减缓飞行器本体的下降速度,同时,产生的冲击力较小,能够有效保护飞行器本体和所载人员的安全,此外,还具备优良的适应性,可以应对各种复杂的地面环境,为飞行器本体提供稳定的支撑,还引入了滑翔翼机构,以应对飞行器本体失去飞行能力的情况,滑翔翼机构能够在降落过程中通过摆动改变行进方向,降低下落速度,从而进一步提高降落的安全性,不仅能够在紧急情况下保护飞行器本体和所载人员的安全,还能在一定程度上拓展飞行器的应用范围。
Aircraft safe landing system under extreme conditions
一种极端情况下飞行器安全降落系统
2024-12-20
Patent
Electronic Resource
Chinese
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