Title:
PROPELLER, POWER ASSEMBLY AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2019/019332
Kind Code:
A1
Abstract:
Disclosed are a propeller, a power assembly and an aircraft.A propeller (100) comprises a propeller hub (10) and a propeller blade (20), the propeller blade (20) being connected on the propeller hub (10). At a distance of 40% of the radius of the propeller (100) from the centre of the propeller hub (10), the angle of attack of the propeller blade (20) is 16.98° ± 2.5°, and the chord length of the propeller blade (20) is 22.6 mm ± 5 mm. At a distance of 60% of the radius of the propeller (100) from the centre of the propeller hub (10), the angle of attack of the propeller blade (20) is 13.99° ± 2.5°, and the chord length of the propeller blade (20) is 17.59 mm ± 5 mm. At a distance of 80% of the radius of the propeller (100) from the centre of the propeller hub (10), the angle of attack of the propeller blade (20) is 11.78° ± 2.5°, and the chord length of the propeller blade (20) is 12.7 mm ± 5 mm. The present invention can optimise the structure of a propeller, increasing flight performance of an aircraft.
Inventors:
LIU YIHAN (CN)
JIANG BIN (CN)
WANG SHU (CN)
JIANG BIN (CN)
WANG SHU (CN)
Application Number:
PCT/CN2017/102968
Publication Date:
January 31, 2019
Filing Date:
September 22, 2017
Export Citation:
Assignee:
SZ DJI TECHNOLOGY CO LTD (CN)
International Classes:
B64C11/18
Domestic Patent References:
WO2009093491A1 | 2009-07-30 |
Foreign References:
CN205469778U | 2016-08-17 | |||
CN205366054U | 2016-07-06 | |||
CN206297727U | 2017-07-04 | |||
CN205554565U | 2016-09-07 |
Attorney, Agent or Firm:
SHENZHEN SCIENBIZIP INTELLECTUAL PROPERTY AGENCY CO., LTD. (CN)
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