The invention discloses a light electric aircraft parachute landing booster rocket system which comprises a booster rocket body, a guide cable, a complete machine parachute, an aircraft hatch cover protection mask, an aircraft parachute bay, an airborne 7.4 V power source and a control panel. The booster rocket body is connected with the complete machine parachute through the guide cable and placed in the aircraft parachute bay. The aircraft hatch cover protection mask is installed on an aircraft parachute bay. The device has a posture adjusting function and can automatically correct the ejection direction of the parachute of the whole machine according to the flight posture of the aircraft, so that the ejected parachute is always perpendicular to the ground, the parachute opening time is shortened, the landing process is optimized, and the safety and practicability of parachute landing of the whole machine are improved. According to the invention, the use efficiency and multifunctionality of the booster rocket with the whole parachute falling function can be greatly improved, and the use cost can be greatly reduced.
本发明公开了适用于轻型电动飞机伞降助推火箭系统,包括助推火箭本体、引导线缆、整机降落伞、飞机舱盖保护面罩、飞机降落伞伞舱、机载7.4V电源及控制板,所述助推火箭本体通过引导线缆与整机降落伞连接,并放置于飞机降落伞伞舱中,所述飞机舱盖保护面罩安装在飞机降落伞伞舱上;本发明具有调整姿态功能可根据飞机飞行姿态自动修正整机降落伞的弹出方向,使弹出的降落伞始终垂直于地面,进而缩短开伞时间,优化降落过程,提升整机伞降的安全性与实用性。通过本发明可大幅提高整机落伞的助推火箭的使用效率与多功能性,也可大幅度降低使用成本。
Parachute landing booster rocket system suitable for light electric aircraft
适用于轻型电动飞机伞降助推火箭系统
2024-06-04
Patent
Electronic Resource
Chinese
METHOD OF PARACHUTE LANDING DRONE AIRCRAFT AND PARACHUTE SYSTEM OF LANDING DRONE AIRCRAFT
European Patent Office | 2016
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