Title:
MULTI-ROTOR UNMANNED AERIAL VEHICLE-BASED DUCT PROPULSION SYSTEM
Document Type and Number:
WIPO Patent Application WO/2019/047429
Kind Code:
A1
Abstract:
A multi-rotor unmanned aerial vehicle-based duct propulsion system, comprising a multi-rotor unmanned aerial vehicle (10), a first cradle head interface I (20), a duct buoyancy module (30) and a second cradle head interface II (40). The duct buoyancy module (30) and the multi-rotor unmanned aerial vehicle (10) are mutually independent modules; the multi-rotor unmanned aerial vehicle (10) and the first cradle head interface I (20) are rigidly connected, and the lower part of the first cradle head interface I (20) is rigidly connected to the duct buoyancy module (30); the upper part of the second cradle head interface II (40) is rigidly connected to the duct buoyancy module (30); and a reserved interface is disposed at the lower part of the second cradle head interface II (40) and may be connected to a cradle head or other equipment in which the same is carried. By using generic cradle head interfaces, rigid mechanical combination with various models of consumer stage multi-rotor unmanned aerial vehicles may be achieved, and different ducts or batteries may be carried according to different load bearing requirements so as to improve the maximum buoyancy.
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Inventors:
ZHANG WENLI (CN)
FENG HAO (CN)
WEI BOXIN (CN)
FENG HAO (CN)
WEI BOXIN (CN)
Application Number:
PCT/CN2017/118524
Publication Date:
March 14, 2019
Filing Date:
December 26, 2017
Export Citation:
Assignee:
UNIV BEIJING TECHNOLOGY (CN)
International Classes:
B64C27/08; B64C27/12
Domestic Patent References:
WO2016112124A2 | 2016-07-14 |
Foreign References:
CN107458593A | 2017-12-12 | |||
CN207157519U | 2018-03-30 | |||
CN105947201A | 2016-09-21 | |||
CN107042883A | 2017-08-15 | |||
CN103332293A | 2013-10-02 | |||
CN206243467U | 2017-06-13 |
Attorney, Agent or Firm:
BEIJING SIHAI TIANDA INTELLECTUAL PROPERTY AGENCY LTD. (CN)
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