阅读说明：本技术 无人飞行机 (Unmanned aerial vehicle ) 是由 菱田聪 清水俊彦 柿本将大 于 2020-02-20 设计创作，主要内容包括：本发明提供无人飞行机(1),其包括：具有用于在空中飞行的推力产生部(12)的主体(10)；具有吸附部(21)且安装于主体(10)的真空吸附装置(20)；和控制推力产生部(12)和真空吸附装置(20)的动作的控制装置,通过吸附部(21)的真空吸附能够将主体(10)固定于壁面,上述无人飞行机(1)具有检测吸附部(21)内的压力的压力传感器(40),控制装置在主体(10)相对壁面的吸附时和/或者脱离时,基于压力传感器(40)的检测控制推力产生部(12)的动作。(The invention provides an unmanned aircraft (1) comprising: a main body (10) having a thrust generating section (12) for flying in the air; a vacuum adsorption device (20) having an adsorption part (21) and mounted on the main body (10); and a control device for controlling the operations of the thrust generation unit (12) and the vacuum adsorption device (20), wherein the main body (10) can be fixed to the wall surface by vacuum adsorption of the adsorption unit (21), the unmanned aircraft (1) is provided with a pressure sensor (40) for detecting the pressure in the adsorption unit (21), and the control device controls the operation of the thrust generation unit (12) based on the detection of the pressure sensor (40) when the main body (10) is adsorbed to and/or separated from the wall surface.)

1. An unmanned aerial vehicle, comprising:

a body having a thrust producing portion for flying in the air; an adsorption device having an adsorption part and mounted on the main body; and a control device for controlling the operations of the thrust generation unit and the adsorption device,

the suction unit can suck a wall surface by operation of the suction device and can fix the body to the wall surface, and the unmanned aerial vehicle is characterized in that:

comprises an adsorption state detection part for detecting the adsorption state of the adsorption part,

the control device controls the operation of the thrust generation unit based on the detection of the suction state detection unit when the main body is sucked to and/or separated from the wall surface.

2. The unmanned aircraft according to claim 1, wherein:

the adsorption device is a vacuum adsorption device which can utilize the adsorption part to adsorb the wall surface in vacuum,

the adsorption state detection unit is a pressure sensor that detects a pressure in the adsorption unit.

3. The unmanned aircraft according to claim 1 or 2, wherein:

when the body is brought close to a wall surface during flight based on the operation of the thrust generation unit,

the control device detects, by the suction state detection unit, suction to the wall surface by the operation of the suction device, and stops the thrust generation unit.

4. The unmanned aircraft according to any one of claims 1 to 3, wherein:

a wall surface detection sensor for detecting the approach of the main body to the wall surface,

the control device starts the operation of the suction device based on the detection of the wall surface detection sensor.

5. The unmanned aircraft according to claim 4, wherein:

the wall surface detection sensor includes a plurality of distance sensors that detect distances to the wall surface.

6. The unmanned aircraft according to any one of claims 1 to 5, wherein:

when the suction device is operated to suck the suspension on the wall surface and the suspension is performed by the operation of the thrust generation unit,

the control device stops the suction device, and operates the thrust generation unit to separate the main body from the wall surface after the suction state detection unit detects that suction to the wall surface is released.

7. The unmanned aircraft according to claim 6, wherein:

comprising a contact force sensor for detecting a contact force of the body against a wall surface,

the control device stops the suction device and separates the body from the wall surface after detecting that the body is in a separable state by the contact force sensor.

8. The unmanned aircraft according to any one of claims 1 to 7, wherein:

the body is attracted to and/or detached from a wall surface by the thrust generation unit flying the body horizontally.

9. The unmanned aircraft according to any one of claims 1 to 8, wherein:

the control device may operate the thrust generation unit to maintain the posture of the main body when the suction state detection unit detects that suction is released during suction to the wall surface based on the operation of the suction device.

10. The unmanned aircraft according to any one of claims 1 to 9, wherein:

the main body supports a rope-like body to which a movable body is attached in a state of being attracted to a wall surface,

the rope-like body can be wound up by a winding machine to move the object.

11. The unmanned aircraft according to claim 10, wherein:

the movable body has a plurality of blowers, and the movable body can be maintained in a predetermined posture by controlling the operation of the blowers.

12. The unmanned aircraft according to claim 10, wherein:

the object to be moved is configured to be movable along a wall surface.

Technical Field

The present invention relates to an unmanned aircraft, and more particularly, to an unmanned aircraft that can be attached to a wall surface.

Background

As a conventional unmanned aircraft that can be attracted to a wall surface, an attracting unmanned aircraft disclosed in patent document 1 is known. The sorption unmanned aircraft comprises: an aircraft body having a propeller; and a vacuum adsorption device having an adsorption part, wherein when the adsorption part adsorbs the adsorbed object, the rotation of the propeller is stopped, and the vacuum adsorption device can perform a predetermined operation. The suction unit is provided with a pressure sensor, and the rotation speed of a suction fan of the vacuum suction device is controlled based on the measurement value of the pressure sensor.

Documents of the prior art

Patent document

Patent document 1: japanese patent laid-open publication No. 2017-193330

Disclosure of Invention

Technical problem to be solved by the invention

Vacuum suction of the unmanned aerial vehicle against the wall surface is relatively easy to stably maintain the suction force in a stable state during suction, and when the unmanned aerial vehicle moves closer to a stable state from a flying state and moves away from the stable state to the flying state, the operation and posture of the unmanned aerial vehicle are likely to become unstable, and there is a possibility that collision or falling with the wall surface occurs.

The conventional suction unmanned aircraft described above can maintain the suction force by controlling the rotation speed of the suction fan based on the detection of the pressure sensor, but the problems of the approach and the separation to and from the wall surface have not been sufficiently studied, and there is room for improvement in this respect.

Accordingly, an object of the present invention is to provide an unmanned aircraft capable of easily and reliably performing suction and/or detachment with respect to a wall surface.

Means for solving the problems

The above object of the present invention is achieved by an unmanned aircraft including: a body having a thrust producing portion for flying in the air; an adsorption device having an adsorption part and mounted on the main body; and a control device for controlling the operations of the thrust generation unit and the suction device, wherein the suction unit sucks a wall surface by the operation of the suction device, and can fix the main body to the wall surface, and the control device includes a suction state detection unit for detecting a suction state of the suction unit, and controls the operation of the thrust generation unit based on the detection of the suction state detection unit when the main body is sucked to and/or removed from the wall surface. In the unmanned aircraft, the suction device is preferably a vacuum suction device capable of vacuum-sucking a wall surface by the suction portion, and the suction state detection portion is preferably a pressure sensor that detects a pressure in the suction portion.

Preferably, the control device detects, by the suction state detection unit, suction to the wall surface by the operation of the suction device and stops the thrust generation unit when the unmanned aircraft makes the main body approach the wall surface while flying by the operation of the thrust generation unit. In this configuration, it is preferable that a wall surface detection sensor for detecting that the main body is close to the wall surface is provided, and the control device starts the operation of the suction device based on the detection of the wall surface detection sensor. Preferably, the wall surface detection sensor includes a plurality of distance sensors for detecting a distance to the wall surface.

Preferably, the control device stops the suction device when the unmanned aircraft is suspended by the operation of the thrust generation unit during suction to the wall surface by the operation of the suction device, and operates the thrust generation unit to detach the main body from the wall surface after the suction state detection unit detects release of suction to the wall surface. In this configuration, it is preferable that the suction device includes a contact force sensor for detecting a contact force of the body with respect to the wall surface, and the control device stops the suction device and separates the body from the wall surface after the contact force sensor detects that the body is in a detachable state.

Preferably, the suction and/or separation of the body with respect to the wall surface is performed by horizontally flying the body by the thrust generation unit.

Preferably, the control device operates the thrust generation unit to maintain the posture of the main body when the suction state detection unit detects the release of suction during the suction to the wall surface by the operation of the suction device.

The body can support a rope-like body to which a moving object is attached in a state of being attracted to a wall surface, and can wind up the rope-like body by a hoisting machine to move the moving object. The movable body may include a plurality of blowers, and the movable body may be maintained in a predetermined posture by controlling operations of the blowers. Alternatively, the movable body may be configured to be movable along a wall surface.

Effects of the invention

According to the present invention, it is possible to provide an unmanned aircraft capable of easily and reliably performing suction and/or detachment with respect to a wall surface.

Drawings

Fig. 1 is a perspective view of an unmanned aerial vehicle according to an embodiment of the present invention.

Fig. 2 is a block diagram showing a functional structure of the unmanned aircraft shown in fig. 1.

Fig. 3 is a side view for explaining an operation of the unmanned aircraft shown in fig. 1 when the unmanned aircraft is attracted to a wall surface.

Fig. 4 is a side view for explaining an operation when the unmanned aircraft shown in fig. 1 is detached from a wall surface.

Figure 5 is a side view of an unmanned aircraft according to another embodiment of the present invention.

Fig. 6 is a side view of an unmanned aerial vehicle according to yet another embodiment of the present invention.

Fig. 7 is a side view of an unmanned aerial vehicle according to yet another embodiment of the present invention.

Fig. 8 is a side view of an unmanned aerial vehicle according to yet another embodiment of the present invention.

Fig. 9 is a side view of an unmanned aerial vehicle according to yet another embodiment of the present invention.

Fig. 10 is a side view of a main part for explaining the operation of the unmanned aerial vehicle shown in fig. 9.

Detailed Description

Hereinafter, embodiments of the present invention will be described with reference to the drawings. Fig. 1 is a perspective view of an unmanned aerial vehicle according to an embodiment of the present invention. As shown in fig. 1, the unmanned aerial vehicle 1 has a main body 10 and a vacuum adsorption device 20.

The main body 10 is configured by attaching a thrust generation unit 12, a housing (case) unit 15, and a leg unit 16 to a frame 11. The frame 11 is configured by connecting the distal ends of arms 11a radially extending from the center to each other in a regular hexagonal shape in plan view.

The thrust generation unit 12 includes: a plurality of propellers 13 attached to the arms 11a of the frame 11; and ducted fans 14 installed at left and right sides of a rear portion of the middle frame 11, respectively. The number of propellers 13 is 6 in the present embodiment, but is not particularly limited as long as they can generate flight thrust in any direction, and may be 3, 4, 8, or the like, for example. Each propeller 13 is disposed so that the rotation axis is perpendicular to the horizontal direction of the main body 10.

The ducted fan 14 is configured by having blades in a cylindrical pipe, and is disposed such that a rotation axis becomes horizontal in a state where the main body 10 is horizontal, thereby enabling the main body 10 to fly horizontally in a hovering state by the operation of the propeller 13. The ducted fan 14 is supported by a direction converter 14a formed of a servo motor so as to be rotatable about an axis orthogonal to the rotation axis, and can perform forward flight or backward flight by controlling the direction of the exhaust port.

The housing portion 15 has functions necessary for an operator who operates the unmanned aerial vehicle 1, such as a communication device, a GPS antenna, an acceleration sensor, and a battery, in addition to a control device such as a CPU or a memory, and is fixed to an upper portion of the frame 11. In fig. 1, the housing 15 is shown by a broken line in order to facilitate understanding of the structure of the unmanned aircraft 1.

The leg portions 16 are rod-shaped members supported so as to extend parallel to each other on both left and right sides below the frame 11, and support the unmanned aircraft 1 when grounded.

The vacuum suction apparatus 20 includes a suction unit 21 and a vacuum pump connected to the suction unit 21. The suction unit 21 is made of an elastic material such as resin or rubber, and a suction hole 23 is formed in the center of the suction surface 22 that can be sucked to the wall surface. The suction portions 21 are provided on both left and right sides of the front portion of the frame 11, respectively, and the suction surfaces 22 are arranged so as to face forward. The vacuum pump is housed in the housing 15 and is branched and connected to each of the suction units 21 by a pipe 25 indicated by a broken line. The number of the suction units 21 is 2 in the present embodiment, and if the suction can be performed reliably on the wall surface, the number of the suction units 21 may be one, or 3 or more suction units 21 may be provided, and may be set as appropriate in consideration of the necessary suction force, the state of the suction place, and the like.

In addition, the unmanned aircraft 1 includes a pressure sensor 40, a wall surface detection sensor 50, and a contact force sensor 60. The pressure sensors 40 are, for example, diaphragm pressure gauges, are attached to the respective adsorption portions 21 so as to face the adsorption holes 23, and detect the pressure in the respective adsorption portions 21.

The wall surface detection sensor 50 is a sensor that detects the approach of the unmanned aerial vehicle 1 to the wall surface, and in the present embodiment, a plurality of distance sensors 51 attached above the respective suction portions 21 are provided on both the left and right sides of the front portion of the frame 11. Each distance sensor 51 is configured by, for example, an ultrasonic sensor, an infrared sensor, a laser sensor, or the like, is arranged slightly behind the suction surface 22 so as not to interfere with suction with the wall surface by the suction surface 22, and detects a distance to the wall surface in front of the suction surface 22.

The contact force sensors 60 are, for example, piezoelectric elements, and are attached to the front portions of the left and right leg portions 16 so as to be in contact with the wall surface and detect the contact force when the unmanned aircraft 1 is attracted to the wall surface. The arrangement of the contact force sensor 60 and the leg portion 16 is not particularly limited, and for example, only 1 bar-shaped leg portion 16 may be provided at the center of the frame 11 so as not to interfere with the thrust of the thrust generating portion 12, and the contact force sensor 60 may be attached to the tip of the leg portion 16.

Fig. 2 is a block diagram showing a functional structure of the unmanned aircraft shown in fig. 1. As shown in fig. 1 and 2, the control device 30 housed in the housing 15 receives input signals from the pressure sensor 40, the wall surface detection sensor 50, and the contact force sensor 60 at the time of suction or detachment of the main body 10 to the wall surface, controls the operation of the vacuum pump 24 of the vacuum suction device 20, and controls the operation of the propeller 13 and the ducted fan 14 of the thrust generation unit 12.

Next, the operation of the unmanned aircraft 1 having the above-described configuration will be described. When the unmanned aircraft 1 is attracted to the wall surface, the unmanned aircraft 1 is caused to fly to the vicinity of the wall surface W extending in the vertical direction as shown in fig. 3(a) by manual operation or automatic operation of the launcher by the operator. When the wall surface detection sensor 50 detects that the distance to the wall surface W is equal to or less than the predetermined distance L, the control device 30 starts the operation of the vacuum pump 24, operates the ducted fan 14 while operating the propeller 13 in a hovering (airborne stop) state, and causes the main body 10 to fly in the horizontal direction indicated by the arrow toward the wall surface W. The flying speed of the body 10 during wall surface suction may be constant, but may be controlled so as to gradually decrease as the distance from the wall surface L detected by the wall surface detection sensor 50 becomes shorter.

Since the wall surface detection sensor 50 of the present embodiment includes the distance sensors 51 for detecting the distance from the wall surface W on the left and right sides of the front portion of the main body 10, the suction surfaces 22 can be reliably sucked in a state substantially parallel to the wall surface W by controlling the operation of the left and right ducted fans 14 so that the distances from the respective distance sensors 51 to the wall surface W are equal to each other. The installation position of the distance sensor 51 is not necessarily limited to the front of the main body 10, and may be the rear of the main body 10, for example. In addition, other sensors such as an air pressure sensor may be used in addition to the distance sensor 51 during horizontal flight.

As shown in fig. 3(b), when the suction surface 22 of the suction unit 21 is in close contact with the wall surface W, the vacuum suction unit 21 is evacuated by the vacuum pump 24, and the inside is depressurized. When the pressure sensor 40 detects that the inside of the suction unit 21 has reached a predetermined negative pressure, the control device 30 determines that the suction of the main body 10 to the wall surface W is completed, and stops the propeller 13 and the ducted fan 14. As a result, the unmanned aircraft 1 is inclined in the direction of the arrow by its own weight, and the contact force sensor 60 abuts against the wall surface W as shown in fig. 3 (c). The detection of completion of suction by the control device 30 can be performed by appropriately combining the detection value of the distance from the wall surface W by the distance sensor 51, the elapsed time from the detection of reduced pressure by the pressure sensor 40, and the like with the detection by the pressure sensor 40 described above.

While the unmanned aircraft 1 is attracted to the wall surface W by the operation of the vacuum pump 24, various working devices (not shown) such as an inspection device, a sprinkler device, a chemical agent spraying device, and a coating device mounted on the unmanned aircraft 1 can be operated, and predetermined work on the wall surface W or its vicinity can be performed. The pressure sensor 40 constantly monitors the pressure in the suction unit 21 during suction to the wall surface W, and when the pressure sensor 40 detects a predetermined decrease in negative pressure (a pressure change to the atmospheric pressure side), the control device 30 operates the propeller 13 so as to cause the main body 1 to hover or slowly descend, thereby maintaining the posture of the main body 10. In this way, the unmanned aircraft 1 can be reliably prevented from falling while being attracted. At this time, the control device 30 may transmit an abnormality signal indicating that the propeller 13 is to be operated urgently to a transmitter of the operator or the like.

When the unmanned aircraft 1 is detached from the wall surface W, as shown in fig. 4(a), a detachment signal from a transmitter, a work device, or the like is received, the control device 30 operates the propeller 13 to hover while maintaining the suction state by the operation of the vacuum pump 24, and also operates the direction conversion device 14a so that the direction of the ducted fan 14 can be retracted. Since the body 10 is in the horizontal posture by hovering, the contact force sensor 60 is separated from the wall surface W, and the detection value of the contact force sensor 60 is lowered. When detecting that the detection value of the contact force sensor 60 is equal to or less than the predetermined value, the control device 30 determines that the main body 10 can be detached and stops the operation of the vacuum pump 24. The hovering based on the operation of the propeller 13 may be performed by an operation of an operator, instead of being performed by control of the control device 30.

Then, when the pressure sensor 40 detects a decrease in the predetermined negative pressure in the suction unit 21, the ducted fan 14 is operated to fly the main body 10 in the horizontal direction indicated by the arrow as shown in fig. 4(b), and the unmanned aerial vehicle 1 can be detached from the wall surface W. In order to rapidly reduce the negative pressure in the suction unit 21, an exhaust valve may be provided in the suction unit 21, and the exhaust valve may be operated while the vacuum pump 24 is stopped to open the interior of the suction unit 21 to the atmosphere.

As described above, in the unmanned aerial vehicle 1 of the present embodiment, when the suction to the wall surface W is performed, the operation of the propeller 13 and the ducted fan 14 is stopped after the completion of the suction to the wall surface W is detected by the pressure sensor 40, and on the other hand, when the unmanned aerial vehicle is detached from the wall surface W, the operation of the ducted fan 14 is started after the release of the suction to the wall surface W is detected by the pressure sensor 40, so that the posture of the unmanned aerial vehicle 1 can be prevented from becoming unstable, and the suction to and the detachment from the wall surface can be performed easily and reliably.

Further, at the time of suction to the wall surface W, the operation of the vacuum suction apparatus 20 is started based on the detection of the distance sensor 51 constituting the wall surface detection sensor 50, so that the suction of the unmanned aircraft 1 can be performed more reliably. The distance sensor 51 may be provided at the rear, left and right, and up and down, in addition to the front of the body 10, and can maintain a distance from a peripheral object to prevent collision. The distance sensor 51 may be a single distance sensor capable of measuring distances to any of a plurality of distance measurement points by 2-dimensional scanning or 3-dimensional scanning.

On the other hand, when detaching from the wall surface W, the propeller 13 is operated to suspend the unmanned aircraft 1 during the suction to the wall surface W by the operation of the vacuum suction device 20, and after the contact force sensor 60 detects that the unmanned aircraft can detach from the wall surface W, the control device 30 stops the vacuum suction device 20 to detach the main body 10 from the wall surface W, so that the detachment of the unmanned aircraft 1 can be performed safely and smoothly.

While one embodiment of the present invention has been described in detail above, specific embodiments of the present invention are not limited to the above embodiment. For example, in the present embodiment, the wall surface detection sensor 50 that detects the approach of the main body 10 to the wall surface W is configured to include the plurality of distance sensors 51, but is not necessarily limited to a sensor that can measure the distance to the wall surface, and may be a camera, an infrared sensor, or the like that detects the presence of the wall surface W in a predetermined area. When a camera is used as the wall surface detection sensor 50, the suction state can be confirmed by continuing the image pickup after the suction onto the wall surface W. The wall surface detection sensor 50 is not essential in the present invention, and the vacuum adsorption device 20 can be manually operated by an operator or the like operating the transmitter by visually confirming that the unmanned aerial vehicle 1 approaches the wall surface W.

In the unmanned aerial vehicle 1 of the present embodiment, the thrust generation unit 12 is configured to include the plurality of propellers 13 and the plurality of ducted fans 14, and by disposing the plurality of propellers 13 with the rotation axis inclined with respect to the horizontal body 10, the body 10 can be flown horizontally with the horizontal attitude maintained without providing the ducted fans 14, and adsorption and/or separation with respect to the wall surface W can be performed. The inclination of the rotation axis of the propeller 13 may be realized by an inclination mechanism capable of adjusting the angle.

Further, although the suction portion 21 is fixed to the body 10 in the present embodiment, it may be rotatably attached to the body 10 via a universal joint or the like, and even when a deviation in the suction direction with respect to the wall surface W occurs, the deviation can be absorbed by the rotation of the suction portion 21.

When various operations are performed by the unmanned aircraft 1, the operation device is fixed to the main body 10 as in the present embodiment, and the unmanned aircraft 1 is moved to a desired position and is caused to adhere to the wall surface W, whereby the operation device can perform a predetermined operation at the adhering position. Alternatively, the main body 10 may be configured to support a rope-like body to which the movable body is attached in a state of being attracted to the wall surface W, and the rope-like body may be wound up by a winding machine to move the movable body, so that various operations can be performed by the operation device provided in the movable body.

For example, as shown in fig. 5, a hoist 70 may be fixed to the main body 10, and a movable body 72 may be attached to the tip of a rope-like body 71 such as a wire rope wound up by the hoist 70. According to this configuration, the unmanned aerial vehicle 1 is attracted to the wall surface W, the hoisting machine 70 winds up or unwinds (lowers/unwinds) the rope-like body 71, and the moved body 72 is moved to perform various operations (for example, inspection or painting of the wall surface W). The movement of the movable body 72 is not limited to the movement in the vertical direction directly below the hoist 70, and the movable body 72 may be moved so as to be dragged along the ground, the water surface, or the like by making the length of the rope-like body 71 sufficiently long.

The support of the rope-like body 72 by the main body 10 can be realized by the configurations shown in fig. 6 and 7 in addition to the configuration shown in fig. 5. The configuration shown in fig. 6 is configured such that one end side of the rope-like body 71 is attached to the main body 10, and the other end side of the rope-like body 71 can be wound or unwound by the winding machine 72. In this configuration, the object 72 can be moved by the operation of the hoist 70 by fixing the object 72 to the platen 73 or the like together with the hoist 70. The configuration shown in fig. 7 is a configuration in which a pulley 74 is provided on the main body 10, the object 72 to be moved is attached to one end of the rope-like body 71 hooked on the pulley 74, and the other end side of the rope-like body 71 is wound up or unwound by the hoisting machine 70 provided on the floor surface F or the like, whereby the object 72 to be moved can be moved.

The unmanned aircraft 1 according to each of the above embodiments is configured to control the operation of the thrust generation unit 12 based on the detection of the pressure sensor 40 at both the time of suction and the time of separation of the body 10 with respect to the wall surface W, but may be configured to control the operation of the thrust generation unit 12 based on the detection of the pressure sensor 40 only at either the time of suction or the time of separation. The wall surface W to which the unmanned aircraft 1 is attached is not necessarily limited to a wall surface extending in the vertical direction, and may be an inclined surface, a ceiling surface, or the like, and the unmanned aircraft 1 can also be attached by disposing the attaching portion 21 so as to be able to approach or separate from a desired wall surface in the orthogonal direction.

The unmanned aerial vehicle 1 according to each of the above embodiments uses the vacuum adsorption device 20 as an adsorption device for fixing the body 10 to the wall surface, but may use another adsorption device that operates to perform adsorption and desorption to and from the wall surface by an adsorption technique other than vacuum adsorption (for example, claws, adhesion, electromagnets, electrostatic adsorption, intermolecular force, and the like). In the present embodiment, the pressure sensor 40 is used as the suction state detection unit for detecting the suction state を of the suction unit 21, but when a suction device other than the vacuum suction device 20 is used, various sensors and the like corresponding to the suction technique of the suction device can be used as the suction state detection unit.

The movable body 72 shown in fig. 5 to 7 can be configured to stabilize the posture even in a state suspended and supported by the rope-like body 71. Fig. 8 is a side view showing an example of the unmanned aerial vehicle 1 having the moved body 72. The object 72 to be moved shown in fig. 8 is configured by attaching air blowers 72c to four corners of a rectangular base plate 72b supporting a basket-shaped object body 72 a. The blower 72c is constituted by various fans such as a ducted fan, and the rotation axis of the fan is disposed so as to be oriented in the vertical direction. The body 72a of the object to be moved accommodates not only a posture detection sensor such as a gyro sensor for detecting the posture of the object to be moved 72, a control device for controlling the posture of the object to be moved 72, but also an imaging camera for inspecting the wall surface W, an inspection device 72d such as an ultrasonic diagnostic device, and the like. The direction of the air blower 72c is not particularly limited as long as it can control the posture of the moved body 72, and a plurality of air blowers 72c can be appropriately arranged according to the size and shape of the moved body 72.

In the unmanned aerial vehicle 1 shown in fig. 8, when the mobile body 72 suspended and supported by the rope-like bodies 71 is shaken by wind, vibration, or the like, the posture of the mobile body 72 is detected in the mobile body 72a, and the operation of each air blower 72c is controlled, whereby the mobile body 72 can be maintained in a predetermined posture such as a horizontal posture, and therefore, the inspection of the wall surface W or the like by the inspection device 72d can be performed quickly and accurately. The main body 72a may be provided with a working device for performing various operations (e.g., drilling (drilling), welding, laser blasting, etc.) on the wall surface W, and in this case, the operations can be performed quickly and accurately. Since the blower 72c, the inspection device 72d, the working device, and the like can be supplied with electric power from a power supply, a generator, or the like (not shown) mounted on the main body 10 of the unmanned aircraft 1 via the rope-like body 71, the weight of the moved body 72 can be reduced, and high-power work can be handled.

The object 72 to be moved may be configured to be movable along the wall surface. Fig. 9 is a side view showing an example of the unmanned aerial vehicle 1 having the moved body 72. The object 72 to be moved shown in fig. 9 has a pair of leg portions 72f and 72g on both sides of a housing-shaped object body 72e to be moved. The pair of leg portions 72f and 72g have vacuum suction pads 72j, and are rotatably supported by the body 72e to be moved via the rotating shafts 72h and 72i, respectively. The body 72a to be moved accommodates: a motor for rotating the pair of leg portions 72f, 72 g; pressure sensors for detecting contact of the legs 72F and 72g with the floor surface F and the wall surface W; and a controller for controlling the operations of the vacuum suction pad 72j and the motor.

The unmanned aerial vehicle 1 shown in fig. 9 can move the body 72 along the ground surface F and the wall surface W standing from the ground surface F by sending the rope-like body 71 to ground the body 72 to the ground surface F.

Fig. 10 shows an example of the movement of the object 72 shown in fig. 9 along the floor surface F and the wall surface W. As shown in fig. 10(a), in a state where the vacuum suction pad 72j of one leg 72F is sucked to the floor surface F and the suction of the vacuum suction pad 72j of the other leg 72g is released, when the body 72e to be moved is rotated in the direction indicated by the arrow about the rotating shaft 72h and the other leg 72g is rotated in the direction indicated by the arrow about the rotating shaft 72i during the rotation of the body 72e to be moved, as shown in fig. 10(b), the vacuum suction pad 72j of the other leg 72g comes close to the wall surface W. When the other leg 72g comes into contact with the wall surface W, the vacuum suction pad 72j of the other leg 72g is sucked to the wall surface W in the body 72e to be moved, and as shown in fig. 10(c), the body 72e to be moved is rotated in the direction indicated by the arrow about the rotating shaft 72i, and during the rotation of the body 72e to be moved, the one leg 72f is rotated in the direction indicated by the arrow about the rotating shaft 72 h. In this way, the object 72 to be moved on the floor surface F can be smoothly moved to the wall surface W. As with the configuration shown in fig. 8, various inspection devices and work devices can be mounted on the body 72e to be moved, and inspection and work can be performed while moving on the wall surface W. Specific examples of the inspection and work include inspection of wall surfaces of tunnels, bridges, dams, buildings, power generation facilities, various plant facilities, and the like by imaging with a camera, inspection by a hammer with a hitting sound, inspection of a plate thickness with a probe, and the like.

The attraction of the object 72 to the floor surface F or the wall surface W can be performed by an electromagnet or the like other than the vacuum attraction. The structure for moving the object 72 along the floor surface F and the wall surface W is not limited to the above-described structure, and for example, wheels or crawler tracks having an adsorption portion on the whole in the circumferential direction, an inchworm motion principle, or the like may be used.

Description of reference numerals

1 unmanned aircraft

10 main body

12 thrust generating part

13 screw propeller

14 duct fan

20 vacuum adsorption device (adsorption device)

24 vacuum pump

21 adsorption part

30 control device

40 pressure sensor (adsorption state detector)

50 wall surface detection sensor

51 distance sensor

60 contact force sensor

70 windlass (capstan)

71 rope-like body

72 moved body

72c blower

The W wall.