Controllable parachute for aircraft

• Main Author: ZHU DEWU
• Format: Patent
• Language: Chinese; English
• Published: 19.01.2018
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The invention discloses a controllable parachute for an aircraft. The controllable parachute comprises a main parachute, and an auxiliary parachute is arranged on the upper portion of the main parachute. An even number of regulating mechanisms, an ejection device, a parachute bin and a control system are arranged on the lower portion of the main parachute and all located inside an aircraft cabin.The regulating mechanisms are symmetrically distributed on the two sides of the parachute bin. The ejection device is located on the outer side of the parachute bin, and the control system is arrangedon the lower portion of the parachute bin. The regulating mechanisms are used for regulating the moving direction of the aircraft to avoid secondary accidents. The passive safety of the aircraft is improved, the aircraft, a driver and passengers can be well protected, and the survival hope of the driver and the passengers is great. 本发明公开了种用于飞机的可控降落伞，包括主伞，所述主伞的上方设置有副伞，所述主伞的下方设置有调节机构、弹射装置、伞仓以及操控系统，且所述调节机构、弹射装置、伞仓以及所述操控系统均位于