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公开(公告)号:US20170029097A1
公开(公告)日:2017-02-02
申请号:US15062871
申请日:2016-03-07
Inventor: Hiroyuki MATSUMOTO , Shigenori ICHIMURA , Tatsuya IYOBE , Mizuki TAKITA
CPC classification number: B64C27/006 , B64B1/14 , B64B1/26 , B64B1/40 , B64B1/58 , B64C27/20 , B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/101 , B64C2201/108 , B64C2201/127 , B64D47/04 , B64D47/08 , B64D2203/00
Abstract: An aircraft includes: a plurality of rotor units each including a propeller and a motor that drives the propeller; and a shock absorber covering the entire vertical length of lateral sides of the plurality of rotor units.
Abstract translation: 飞机包括:多个转子单元,每个转子单元包括驱动推进器的螺旋桨和马达; 以及覆盖所述多个转子单元的横向侧的整个垂直长度的减震器。
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公开(公告)号:US20190002093A1
公开(公告)日:2019-01-03
申请号:US15748934
申请日:2016-07-27
Inventor: Fumio MURAMATSU , Masayuki TOYAMA , Hiroyuki MATSUMOTO , Shigenori ICHIMURA , Tatsuya IYOBE , Mizuki TAKITA
Abstract: An aircraft includes: a plurality of rotor units each including propeller and motor that drives propeller; a shock absorber covering an entire vertical length of a lateral side of the plurality of rotor units; and a plurality of rudders each being disposed downstream of a corresponding one of the plurality of rotor units and rotating about axis of rotation that extends in a direction intersecting a flow direction of air current generated by the corresponding one of the plurality of rotor units.
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