Title:
FIXED-WING UNMANNED AIRCRAFT CAPABLE OF BEING QUICKLY DISASSEMBLED AND INSTALLED
Document Type and Number:
WIPO Patent Application WO/2016/141742
Kind Code:
A1
Abstract:
Disclosed is a fixed-wing unmanned aircraft capable of being quickly disassembled and installed, comprising an aircraft body, and a wing and a tail installed on the aircraft body, wherein the tail comprises a tail wing and a tail rod fixed between the aircraft body and the tail wing; a tail rod channel is provided on the aircraft body; one end of the tail rod is installed within the tail rod channel; and the depth of the tail rod inserted into the tail rod channel is adjustable. With regard to the fixed-wing unmanned aircraft capable of being quickly disassembled and installed, during transportation, the tail rod can be forwardly inserted to reduce the space occupied.
Inventors:
YANG HUADONG (CN)
WU QICAI (CN)
ZHAO JIANG (CN)
WU QICAI (CN)
ZHAO JIANG (CN)
Application Number:
PCT/CN2015/097380
Publication Date:
September 15, 2016
Filing Date:
December 15, 2015
Export Citation:
Assignee:
YANG HUADONG (CN)
International Classes:
B64C3/00; B64C1/36
Foreign References:
| CN104709460A | 2015-06-17 | |||
| CN204527611U | 2015-08-05 | |||
| CN204527605U | 2015-08-05 | |||
| CN104691736A | 2015-06-10 | |||
| CN202574612U | 2012-12-05 | |||
| CN104015916A | 2014-09-03 | |||
| US8657226B1 | 2014-02-25 | |||
| EP0215017A1 | 1987-03-25 |
Attorney, Agent or Firm:
CHINA CHANGZHOU VEI PATENT OFFICE et al. (CN)
常州市维益专利事务所 (CN)
常州市维益专利事务所 (CN)
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