JP2019167110A5 - - Google Patents

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JP2019167110A5
JP2019167110A5 JP2019107582A JP2019107582A JP2019167110A5 JP 2019167110 A5 JP2019167110 A5 JP 2019167110A5 JP 2019107582 A JP2019107582 A JP 2019107582A JP 2019107582 A JP2019107582 A JP 2019107582A JP 2019167110 A5 JP2019167110 A5 JP 2019167110A5
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Japan
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unit
observation
flight
rotorcraft
rotor blades
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JP2019107582A
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Japanese (ja)
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JP6913912B2 (en
JP2019167110A (en
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Priority claimed from JP2018208509A external-priority patent/JP2019085104A/en
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Claims (2)

飛行部と観測部とを備える回転翼機であって、
前記飛行部は、複数の回転翼と、前記複数の回転翼を支持するアーム部と、前記観測部を着脱可能に保持する保持部とを備えており、
前記観測部は、前記回転翼機に着脱自在に取り付けられ、観測装置と当該観測装置を天井又は壁に固定するための磁石部を備えている、回転翼機。
It is a rotary wing aircraft equipped with a flight unit and an observation unit.
The flight unit includes a plurality of rotor blades, an arm unit that supports the plurality of rotor blades, and a holding unit that holds the observation unit detachably.
The observation unit is a rotorcraft that is detachably attached to the rotorcraft and includes an observation device and a magnet unit for fixing the observation device to the ceiling or a wall.
前記観測部は、前記飛行部を貫通するように互いに前記保持部により連結される、請求項1に記載の回転翼機。The rotary wing aircraft according to claim 1, wherein the observation unit is connected to each other by the holding unit so as to penetrate the flight unit.
JP2019107582A 2017-11-06 2019-06-10 Aircraft and control method of air vehicle Active JP6913912B2 (en)

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JP2017214142 2017-11-06
JP2017214142 2017-11-06
JP2018208509A JP2019085104A (en) 2017-11-06 2018-11-05 Flight unit and control method of flight unit

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JP2018208509A Division JP2019085104A (en) 2017-11-06 2018-11-05 Flight unit and control method of flight unit

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JP2019167110A JP2019167110A (en) 2019-10-03
JP2019167110A5 true JP2019167110A5 (en) 2021-04-15
JP6913912B2 JP6913912B2 (en) 2021-08-04

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