Title:
マルチコプタの回転翼拘束器具
Document Type and Number:
Japanese Patent JP7025221
Kind Code:
B2
Abstract:
To restrain rotary wings of a multicopter from rotating with an instrument which has a simple structure.SOLUTION: The present invention relates to a rotary wing restraint instrument which restrains rotary wings 42, 50 of a multicopter having the rotary wings 42,50 provided on a rod-like support arm 18, extending horizontally, rotatably on an axis of rotation facing in a vertical direction. The rotary wing restraint instrument has a part 136 in a vertically-inverted U shape including one pair of leg members 132 and a bridge part 134 for coupling upper ends of both the leg members 132 to each other, and the part 136 in the U shape straddles the support arm 18 from above to sandwich the rotary wings 42, 50 from both sides in a rotating direction and then restrain the rotary wings 42, 50 from rotating with the rotary wings 42, 50 aligned with the support arm 18.SELECTED DRAWING: Figure 4
Inventors:
Masahiko Asanuma
Application Number:
JP2018006338A
Publication Date:
February 24, 2022
Filing Date:
January 18, 2018
Export Citation:
Assignee:
Honda motor industry stock company
International Classes:
B64F1/22; B64C27/08; B64F5/40
Domestic Patent References:
| JP2012111272A |
Foreign References:
| CN106394906A | ||||
| US6769644 | ||||
| US5211538 |
Attorney, Agent or Firm:
Patent Business Corporation Oshima Patent Office