发明名称 小型無人機
摘要 PROBLEM TO BE SOLVED: To solve a problem in a conventional small unmanned aircraft, wherein a flight operation for long hours is difficult, although having superior flight performance peculiar to a rotor craft.SOLUTION: In a small unmanned aircraft V, drive parts 1 generating upward thrust are arranged at four positions from the center of an aircraft body B. Each drive part 1 coaxially includes a rotated and driven rotor 2 at an inner side and a rotatably held ring body 3 at an outer side, wherein a rotation center line CL is inclined so that a portion of the ring body 3 is brought into contact relative to a horizontal surface. By means of a structure provided with a clutch mechanism 5 for connecting and disconnecting power transmission from a rotary drive shaft 4 to the ring body 3 between the rotary drive shaft 4 of the rotor 2 and the ring body 3, both flight performance and travel performance are provided to achieve operation for long hours.
申请公布号 JP5812849(B2) 申请公布日期 2015.11.17
申请号 JP20110279843 申请日期 2011.12.21
申请人 株式会社IHIエアロスペース 发明人 小林 研吾;岡本 伸也
分类号 B64C29/00;B60F5/02;B64C39/02 主分类号 B64C29/00
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