Title:
PARACHUTE EQUIPPED AUTOGYRO AND MANUFACTURING METHOD
Document Type and Number:
WIPO Patent Application WO/2017/036080
Kind Code:
A1
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.
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Inventors:
TAO LIANG (CN)
SHEN SHOUJIAN (CN)
QIN LIXIN (CN)
SHEN SHOUJIAN (CN)
QIN LIXIN (CN)
Application Number:
PCT/CN2016/072100
Publication Date:
March 09, 2017
Filing Date:
January 26, 2016
Export Citation:
Assignee:
SUN HAWK (HENAN) AVIATION IND CO LTD (CN)
International Classes:
B64C27/02; B64D17/80
Foreign References:
CN105059534A | 2015-11-18 | |||
CN204956905U | 2016-01-13 | |||
DE102011053678A1 | 2013-03-21 | |||
CN104401487A | 2015-03-11 | |||
CN204210731U | 2015-03-18 | |||
JPS60174393A | 1985-09-07 |
Attorney, Agent or Firm:
BEIJING DINGJIADA INTELLECTUAL PROPERTY AGENCY FIRM (GENERAL PARTNER) (CN)
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