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1. (WO2017036080) PARACHUTE EQUIPPED AUTOGYRO AND MANUFACTURING METHOD

Pub. No.:    WO/2017/036080    International Application No.:    PCT/CN2016/072100
Publication Date: Fri Mar 10 00:59:59 CET 2017 International Filing Date: Wed Jan 27 00:59:59 CET 2016
IPC: B64C 27/02
B64D 17/80
Applicants: SUN HAWK (HENAN) AVIATION INDUSTRY CO., LTD.
河南三和航空工业有限公司
Inventors: TAO, Liang
陶亮
SHEN, Shoujian
申守健
QIN, Lixin
秦立新
Title: PARACHUTE EQUIPPED AUTOGYRO AND MANUFACTURING METHOD
Abstract:
A parachute equipped autogyro comprises: a fuselage body (1), a rotor device (2), a propeller device (3), and a parachute device (4). The fuselage body (1) comprises a cockpit (5) and a tail rudder (6). A control system is arranged at a front part of the cockpit (5), an engine (8) is arranged at a back part of the cockpit (5), and a landing gear (9) is arranged underneath the fuselage body (1). The rotor device (2) is arranged at a top part of the fuselage body (1), and comprises a rotor hub (201) and rotor blades (202) arranged symmetrically about the rotor hub (201). The propeller device (3) is arranged at a tail part of the cockpit (5), and connected to the engine (8) via a gearbox. The parachute device (4) is arranged at above the rotor hub (201), and comprises a whole-airplane parachute (401), an accommodation cabinet (402) configured to accommodate the whole-airplane parachute (401) and a launcher configured to unfold the parachute. The parachute equipped autogyro accomplishes the following effects: high safety, a short inflation distance, high stability, high wind resistance, and a higher a high price-performance ratio.