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Patent Searching and Data


Title:
PROPELLER, POWER ASSEMBLY, AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2017/128744
Kind Code:
A1
Abstract:
A propeller, power assembly, and aircraft. The propeller comprises a blade fastener (1) and a blade (2) connected to the blade fastener (1). At a location having a distance of 55% of a radius of a propeller disc defined by the propeller from the center of the propeller disc, the blade (2) has a chord length of 16.7 mm ± 5 mm and an angle of attack of 14° ± 2.5°. At a location having a distance of 70% of the radius of the propeller disc from the center thereof, the blade (2) has a chord length of 14.4 mm ± 5 mm and an angle of attack of 11.7° ± 2.5°. At a location having a distance of 85% of the radius of the propeller disc from the center thereof, the blade (2) has a chord length of 12.2 mm ± 5 mm and an angle of attack of 9.3° ± 2.5°. The propeller, power assembly, and aircraft can effectively reduce the resistance on the propeller during rotation, thus improving the efficiency of mechanical power transmission.

Inventors:
LIU FENG (CN)
DENG TAO (CN)
JIANG BIN (CN)
WANG SHU (CN)
Application Number:
PCT/CN2016/099704
Publication Date:
August 03, 2017
Filing Date:
September 22, 2016
Export Citation:
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Assignee:
SZ DJI TECHNOLOGY CO LTD (CN)
International Classes:
B64C11/18
Foreign References:
CN205524939U2016-08-31
CN102963522A2013-03-13
CN202765286U2013-03-06
CN104139849A2014-11-12
US20070110582A12007-05-17
US20070158495A12007-07-12
JP2013184645A2013-09-19
JP2001233295A2001-08-28
Attorney, Agent or Firm:
SHENZHEN SCIENBIZIP INTELLECTUAL PROPERTY AGENCY CO.,LTD. (CN)
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