UNMANNED AERIAL VEHICLE AND INSPECTION METHOD
An unmanned aerial vehicle is an unmanned aerial vehicle configured to fly in a closed space, which includes an airframe, a thrust generating means configured to generate a thrust for the airframe to fly in air, and a length measuring means mounted on the airframe. The length measuring means includes a transmission unit configured to transmit a measurement wave, a reception unit configured to receive reflected waves of the measurement wave, and a distance calculation unit configured to calculate a distance between the unmanned aerial vehicle and a stationary object present in the closed space based on the reflected waves of the measurement wave transmitted from the transmission unit which are received a plurality of times by the reception unit.
1 . An unmanned aerial vehicle configured to fly in a closed space, comprising:
an airframe;
a thrust generating means configured to generate a thrust for the airframe to fly in air; and
a length measuring means mounted on the airframe,
wherein the length measuring means includes:
a transmission unit configured to transmit a measurement wave;
a reception unit configured to receive reflected waves of the measurement wave; and
a distance calculation unit configured to calculate a distance between the unmanned aerial vehicle and a stationary object present in the closed space based on the reflected waves of the measurement wave transmitted from the transmission unit which are received a plurality of times by the reception unit.
2 . The unmanned aerial vehicle according to claim 1 ,
wherein the length measuring means measures at least a distance to the stationary object in a horizontal direction.
3 . The unmanned aerial vehicle according to claim 1 ,
wherein the thrust generating means includes a propeller,
wherein the transmission unit includes a horizontal transmission unit configured to transmit the measurement wave in a horizontal direction,
wherein the reception unit includes a horizontal reception unit configured to receive the reflected waves of the measurement wave transmitted from the horizontal transmission unit, and
wherein the horizontal transmission unit and the horizontal reception unit are installed above the propeller.
4 . The unmanned aerial vehicle according to claim 1 ,
wherein the transmission unit includes a vertical transmission unit configured to transmit the measurement wave downward in a vertical direction, and
wherein the reception unit includes a vertical reception unit configured to receive the reflected waves of the measurement wave transmitted from the vertical transmission unit.
5 . The unmanned aerial vehicle according to claim 4 ,
wherein the thrust generating means includes a propeller, and
wherein the vertical transmission unit and the vertical reception unit are installed below the propeller.
6 . The unmanned aerial vehicle according to claim 1 , further comprising an imaging means mounted on the airframe.
7 . The unmanned aerial vehicle according to claim 1 , further comprising a position calculation unit configured to calculate a position of the unmanned aerial vehicle based on the distance.
8 . The unmanned aerial vehicle according to claim 1 ,
wherein the stationary object is a wall forming the closed space which is an interior space of a combustion furnace.
9 . An inspection method using an unmanned aerial vehicle configured to fly in a closed space, the method comprising:
a flight step of flying the unmanned aerial vehicle in the closed space; and
a length measurement step of measuring a distance between the unmanned aerial vehicle and a stationary object present in the closed space, during the flight of the unmanned aerial vehicle,
wherein the length measurement step includes:
a transmission step of transmitting a measurement wave;
a reception step of receiving reflected waves of the measurement wave; and
a distance calculation step of calculating the distance between the unmanned aerial vehicle and the stationary object based on the reflected waves of the measurement wave transmitted in the transmission step which are received a plurality of times in the reception step.
10 . The inspection method according to claim 9 , further comprising a shooting step of shooting at least one portion of an inspection target present in the closed space.
11 . The inspection method according to claim 9 , further comprising a position calculation step of calculating a position of the unmanned aerial vehicle based on the distance between the unmanned aerial vehicle and the stationary object present in the closed space.