The invention belongs to the field of helicopter special equipment, and particularly relates to a helicopter side door parachute landing system and a design method thereof, and the helicopter side door parachute landing system comprises a parachute opening pull rope device (10), a cabin door blocking device (20), a floor mooring ring (30) and a cabin door mooring ring (40); the parachute opening pull rope device is fixed to a bottom plate in a cabin through a floor mooring ring and used for being connected with a parachute opening structure of a parachute. The cabin door blocking device is installed at the side door through the cabin door mooring ring, located between the first structural frame and the second structural frame and used for being grabbed by parachute landing personnel to avoid accidental falling.
本发明属于直升机特种设备领域,具体涉及一种直升机侧门伞降系统及其设计方法,包括:开伞拉绳装置(10)、舱门阻拦装置(20)、地板系留环(30)、舱门系留环(40);开伞拉绳装置通过地板系留环固定在机舱内底板上,用于连接降落伞的开伞结构;舱门阻拦装置通过舱门系留环安装在侧门处且位于第一结构框和第二结构框之间,用于伞降人员抓握避免意外跌落。
Helicopter side door parachuting system and design method thereof
一种直升机侧门伞降系统及其设计方法
2025-01-03
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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