Title:
TURBOJET DRONE
Document Type and Number:
WIPO Patent Application WO/2018/097359
Kind Code:
A1
Abstract:
The present technique relates to a drone and, more specifically, to a drone which flies by jetting compressed gas. According to one embodiment, a turbojet drone is disclosed. The turbojet drone comprises an engine part for intaking and discharging external gas. A propulsion part, in which the gas discharged from the engine part is compressed and discharged to the outside, is included. A turbo propulsion part, in which the gas discharged from the engine part is compressed and selectively discharged to the outside, is included. The turbojet drone disclosed in the present specification receives additional propulsion power, different from that of the propulsion part, provided by the turbo propulsion part, thereby enabling flight power to be improved. In addition, the size of a turbo discharge part is adjusted by a turbo adjustment unit such that the strength of the additional propulsion power is controlled, thereby controlling the direction of the turbojet drone. In addition, a much stronger air can be discharged by the engine part comprising a turbojet fan in which one or more fans overlap, thereby further improving flight power.
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Inventors:
KIM KI TAE (KR)
Application Number:
PCT/KR2016/013682
Publication Date:
May 31, 2018
Filing Date:
November 25, 2016
Export Citation:
Assignee:
KIM KI TAE (KR)
International Classes:
B64D27/20; B64C39/02
Foreign References:
| KR101607816B1 | 2016-03-31 | |||
| KR20110123319A | 2011-11-15 | |||
| JP2008189043A | 2008-08-21 | |||
| KR101130203B1 | 2012-03-30 | |||
| US5170963A | 1992-12-15 |
Attorney, Agent or Firm:
SHIN, Jin Hyun (KR)
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