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Patent Searching and Data


Title:
TAKEOFF METHOD FOR FIXED-WING UNMANNED AERIAL VEHICLE
Document Type and Number:
WIPO Patent Application WO/2019/080179
Kind Code:
A1
Abstract:
An unmanned aerial vehicle release mechanism, comprising: a servo motor (101), the servo motor (101) comprising an output shaft; a servo plate (102), one end of the servo plate (102) being fixedly connected to the output shaft; a transmission rod (20), one end of the transmission rod (20) being hingedly connected to the other end of the servo plate (102); a latch rod (30), one end of the latch rod (30) being hingedly connected to the other end of the transmission rod (20); and an installation block (40), the installation block (40) being fixedly installed on the servo motor (101), a groove (401) being provided in the middle of the installation block (40), a through hole (402) being provided along a horizontal direction of the installation block (40), the other end of the latch rod (30) passing through the through hole (402) and extending into the groove (401), the inner wall of the side of the groove (401) against the servo plate (102) abutting against the other end of the latch rod (30), and the servo motor (101) being capable of driving the latch rod (30) to move reciprocately in the through hole (402).

Inventors:
LUO WEI (CN)
Application Number:
PCT/CN2017/110238
Publication Date:
May 02, 2019
Filing Date:
November 09, 2017
Export Citation:
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Assignee:
LUO WEI (CN)
International Classes:
B64D5/00; B64C29/00; B64C27/08; B64D47/00
Foreign References:
CN107298178A2017-10-27
CN107813937A2018-03-20
CN107792372A2018-03-13
CN106005400A2016-10-12
CN205589484U2016-09-21
CN106428554A2017-02-22
CN106915452A2017-07-04
EP3127809A12017-02-08
Attorney, Agent or Firm:
HUIZHOU CHOYES INTELLECTUAL PROPERTY AGENCY (GERNAL PARTNERSHIP) (CN)
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