Vehicle-mounted device of unmanned rotorcraft for monitoring construction tunnel

Abstract

A vehicle-mounted device for monitoring a rotor unmanned aerial vehicle in a construction tunnel comprises a traveling chassis (1) used for transporting the monitoring rotor unmanned aerial vehicle, a box shell (2) arranged on the traveling chassis (1), a gripper assembly arranged on the box shell (2) and an air inflation bag (91) arranged on the box shell (2). The gripper assembly and the inflatable bag (91) are supported, the rotor unmanned aerial vehicle for monitoring the rotor unmanned aerial vehicle is clamped and supported through the gripper assembly, and monitoring equipment for monitoring the rotor unmanned aerial vehicle is supported through the inflatable bag (91). The monitoring rotor unmanned aerial vehicle in a transportation state is placed in an elastic and high-pressure gas composite interval, the technical problem that the rotor unmanned aerial vehicle and monitoring equipment are respectively brought to a tunnel construction site through a box is solved, and therefore the construction tunnel monitoring efficiency is improved.

Description

Technical Field

[0001] The utility model relates to a vehicle-mounted device, in particular to a vehicle-mounted device used for monitoring a rotary-wing unmanned aerial vehicle in a construction tunnel. Background Art

[0002] Tunnels are engineering structures buried in the ground and are a form of human use of underground space. Tunnels can be divided into traffic tunnels, hydraulic tunnels, municipal tunnels, mining tunnels, and military tunnels. In order to ensure the construction quality of tunnels, it is necessary to use monitoring rotor drones to inspect the interior of the tunnels. Therefore, a vehicle-mounted device for monitoring rotor drones in tunnels under construction is an important construction device. Among the existing vehicle-mounted devices for monitoring rotor drones in tunnels under construction, there is no vehicle-mounted device for monitoring rotor drones in tunnels under construction. Since cargo vehicles cannot meet the transportation performance requirements of monitoring rotor drones, the rotor drones and monitoring equipment are brought to the tunnel construction site separately in boxes, and then the rotor drones and monitoring equipment are assembled, which affects the monitoring efficiency of tunnels under construction.

[0003] The utility model uses the technical feature of placing the monitoring rotor drone in a transport state in a composite interval of elasticity and high-pressure gas to effectively explore and study the technical problem of bringing the rotor drone and monitoring equipment to the tunnel construction site separately in boxes. Summary of the Invention

[0004] The object of the utility model is a vehicle-mounted device for monitoring a rotary-wing UAV in a construction tunnel.

[0005] In order to overcome the above technical shortcomings, the purpose of the present utility model is to provide a vehicle-mounted device for monitoring a rotary-wing UAV in a construction tunnel, thereby improving the efficiency of monitoring the construction tunnel.

[0006] In order to achieve the above-mentioned purpose, the technical solution adopted by the present invention is: it includes a traveling chassis for transporting the monitoring rotor UAV, a box shell arranged on the traveling chassis, a clamp claw assembly arranged on the box shell, and an inflatable bag arranged on the box shell.

[0007] Due to the design of the traveling chassis, box shell, claw assembly and inflatable bag, the claw assembly and the inflatable bag are supported by the traveling chassis and box shell, the rotor drone of the monitoring rotor drone is clamped and supported by the claw assembly, and the monitoring equipment of the monitoring rotor drone is supported by the airbag body through the inflatable bag, so that the monitoring rotor drone in the transportation state is placed in the elastic and high-pressure gas composite interval, which solves the technical problem of bringing the rotor drone and the monitoring equipment to the tunnel construction site separately through boxes, thereby improving the monitoring efficiency of the tunnel under construction.

[0008] The utility model is designed to connect a traveling chassis, a box shell, a clamp claw assembly and an inflatable bag to each other in a manner that a monitoring rotor UAV in a transport state is placed in a composite interval of elasticity and high-pressure gas.

[0009] The utility model is designed to connect the clamp claw assembly with the driving chassis, the box shell and the inflatable bag in a manner of clamping and supporting the rotor UAV for monitoring the rotor UAV.

[0010] The utility model is designed to connect the inflatable bag with the driving chassis, the box shell and the clamp claw assembly in a manner of supporting the air bag body for monitoring the monitoring equipment of the monitoring rotor UAV.

[0011] The utility model is designed that the clamp claw assembly is arranged to include a movable seat, a clamping claw and a buffer spring.

[0012] The technical effects of the above five technical solutions are: highlighting the technical feature of placing the monitoring rotor drone in a transport state in a composite interval of elasticity and high-pressure gas, and introducing the application in the technical field of vehicle-mounted devices for monitoring rotor drones in construction tunnels.

[0013] The utility model is designed to further include a first accessory device, and the first accessory device is arranged between the clamp claw assembly and the box shell, and the first accessory device is arranged to push the telescopic cylinder.

[0014] The utility model is designed to further include a second accessory device, and the second accessory device is arranged between the box shell and the driving chassis. The second accessory device is arranged to include a box cover, a lifting and telescopic cylinder and a guide rod.

[0015] The utility model is designed to further include a third accessory device, and the third accessory device is arranged between the box shell and the driving chassis. The third accessory device is arranged to include a swing platform, a swing telescopic cylinder and a column.

[0016] The technical effects of the above three technical solutions are: realizing the integrated installation of other components and expanding the technical effects of the present utility model.

[0017] The utility model is designed as follows: a column is provided on the traveling chassis, a box shell is provided on the column and the traveling chassis, a swing platform is provided on the column, a swing telescopic cylinder is provided between the swing platform and the column, a box cover and a moving seat are provided on the box shell, a lifting telescopic cylinder is provided between the box cover and the traveling chassis, a guide rod is provided between the box cover and the box shell, a pushing telescopic cylinder is provided between the moving seat and the box shell, a clamping claw is provided on the moving seat, a buffer spring is provided between the clamping claw and the moving seat, and an air bag is provided between the clamping claw and the box shell.

[0018] The technical effect of the above technical scheme is that the basic technical scheme of the utility model is composed of the traveling chassis, box shell, box cover, lifting telescopic cylinder, guide rod, movable seat, pushing telescopic cylinder, clamping claw, buffer spring, inflatable bag, swinging platform, swinging telescopic cylinder and column, which solves the technical problem of the utility model.

[0019] The utility model is designed that the running chassis is arranged as a truck chassis, the middle part of the upper end surface of the running chassis is arranged to be connected with the box shell, and the rear side surface of the running chassis is arranged to be connected with the column.

[0020] The technical effect of the above technical solution is that: transportation is achieved using a truck chassis.

[0021] The utility model is designed, the box shell is configured to include a box portion, an edge strip portion, a support seat portion I, a vertical strip portion and a guide rail portion, and the upper portions of the front and rear side surfaces of the box portion are configured to be connected to the inner end face portion of the edge strip portion, the front side portion of the upper end face of the box portion is configured to be connected to the inner end face portion of the support seat portion I, and the rear side portion of the upper end face of the box portion is configured to be connected to the inner end face portion of the vertical strip portion, the middle rear portion of the upper end face of the box portion is configured to be connected to the inner end face portion of the guide rail portion, and the lower end face portion of the box portion is configured to be connected to the running chassis, and the upper end portion of the box portion is configured to be connected to the inner end face portion of the guide rail portion. It is arranged to be connected with the box cover in a through-type manner and the rear side surface of the box part is arranged to be distributed corresponding to the column, the upper end surface portion of the edge strip part is arranged to be connected with the box cover in a contact type manner and the rear side surface portion of the support seat part I is arranged to be connected with the push-telescopic cylinder, the guide rail part is arranged to be connected with the movable seat in a sunken manner and the front side surface portion of the vertical strip part and the rear side surface portion of the guide rail part are respectively arranged to be connected with the inflatable bag in a contact type manner, the box part is arranged to be connected with the inflatable bag in a accommodating type and the front and rear end portions of the upper end surface of the vertical strip part and the front angle portion of the upper end surface of the box part are respectively arranged to be connected with the guide rod.

[0022] The utility model is designed that the box portion is set as a box-shaped body with double-turn opening and closing doors on the side, the edge strip portion, the vertical strip portion and the guide rail portion are respectively set as rectangular bar-shaped bodies, and the support seat portion I is set as a block body.

[0023] The technical effects of the above two technical solutions are: achieving the support of the box and the installation of monitoring data processing equipment.

[0024] The utility model designs that the air inflation bag is arranged to include a bladder part, an air inflation pump part, a valve part I and a valve part II, and the input port part of the bladder part is arranged to be connected with the output port part of the air inflation pump part through the valve part I. The output port part of the bladder part is arranged to be connected with the inner port part of the valve part II, and the bladder part is arranged to be embeddedly connected with the box shell. The air inflation pump part, the valve part I and the valve part II are arranged to be built-in connected with the box shell, and the upper end face part of the bladder part is arranged to be contact-connected with the clamping claw.

[0025] The utility model designs that the bladder part is arranged as a rubber bag-shaped body, and the air inflation pump part is arranged as an air inflator. The valve part I and the valve part II are respectively arranged as electric valves.

[0026] The technical effects of the above two technical solutions are as follows: It realizes the high-pressure gas accommodation and support for the monitoring equipment of the monitored rotary-wing unmanned aerial vehicle.

[0027] The utility model designs that the moving seat is arranged as a block body with an L-shaped groove on the upper end face and a U-shaped groove on the lower end face. The front side face of the moving seat is arranged to be connected with the pushing telescopic cylinder. The inner and outer walls of the L-shaped groove of the moving seat are arranged to be connected with the clamping claw through a pin shaft, and the L-shaped groove of the moving seat is arranged to be connected with the buffer spring in an accommodating manner. The front wall of the L-shaped groove of the moving seat is arranged to be sleeved with the buffer spring, and the U-shaped groove of the moving seat is arranged to be connected with the box shell.

[0028] The utility model designs that the pushing telescopic cylinder is arranged as a two-stage telescopic cylinder, and the hydraulic port part of the pushing telescopic cylinder is arranged to be connected with the output port of the hydraulic device of the traveling chassis. One end face of the pushing telescopic cylinder is arranged to be connected with the box shell, and the other end face of the pushing telescopic cylinder is arranged to be connected with the moving seat.

[0029] The utility model designs that the clamping claw is arranged to include a clamping jaw part I, a clamping jaw part II and a shear telescopic cylinder part. The middle part of the clamping jaw part I is arranged to be connected with the end of the middle vertical part of the clamping jaw part II through a pin shaft. One end of the shear telescopic cylinder part is arranged to be connected with the rear side of the inner end of the clamping jaw part I through a pin shaft, and the other end of the shear telescopic cylinder part is arranged to be connected with the end of the rear horizontal part of the clamping jaw part II through a pin shaft. The inner end of the clamping jaw part I is arranged to be connected with the moving seat through a pin shaft, and the inner end of the clamping jaw part I is arranged to be contact-connected with the buffer spring. The outer end of the clamping jaw part I and the outer end of the clamping jaw part II are arranged to be contact-connected with the air inflation bag, and the hydraulic port part of the shear telescopic cylinder part is arranged to be connected with the output port of the hydraulic device of the traveling chassis.

[0030] The utility model is designed in that the jaw part I is configured as a Y-shaped rod-shaped body with a middle leakage hole body and the jaw part II is configured as a frame-shaped body with a Y-shaped rod at the outer end and an L-shaped rod at the inner end, the rear part of the middle leakage hole body of the jaw part I is configured to be connected to the vertical part of the L-shaped rod of the jaw part II and the front part of the middle leakage hole body of the jaw part I is configured to be connected to the shear telescopic cylinder part, and the shear telescopic cylinder part is configured to be a two-section telescopic cylinder.

[0031] The utility model is designed in that the buffer spring is configured as a torsion spring and the buffer spring is configured to be sleeve-connected to a pin shaft located between the clamping claw and the movable seat, one end of the buffer spring is configured to be through-connected to the movable seat and the other end of the buffer spring is configured to be contact-connected to the clamping claw.

[0032] The technical effect of the above five technical solutions is that the torsion spring buffer support of the rotor UAV for monitoring the rotor UAV is realized.

[0033] The utility model is designed in that the box cover is configured as a box-shaped body having a support seat portion II in the middle portion of the inner and outer end surfaces and a accommodating groove body in the outer portions of the front and rear inner walls, and the lower end open portion of the box cover is configured to be connected in a sleeve-type manner with the box shell, the end surface of the lower end open portion of the box cover is configured to be connected in a contact-type manner with the box shell, and the lower end surface portion of the support seat portion II is configured to be connected to the lifting and telescopic cylinder, the accommodating groove body is configured to be connected to the guide rod, and the box cover is respectively configured to be connected in an accommodating manner with the guide rod, the movable seat, the push telescopic cylinder, the clamping claw, the buffer spring and the inflatable bag.

[0034] The utility model is designed that the support seat part II is set as a rectangular block body and the accommodating groove body is set as a dovetail groove body.

[0035] The utility model is designed in that the lifting and telescopic cylinder is arranged as a two-section telescopic cylinder and the hydraulic port portion of the lifting and telescopic cylinder is arranged to be connected to the output port of the hydraulic device of the traveling chassis, one of the end surfaces of the lifting and telescopic cylinder is arranged to be connected to the traveling chassis and the other end surface portion of the lifting and telescopic cylinder is arranged to be connected to the box cover.

[0036] The utility model is designed that the guide rod is arranged as an L-shaped rod body with a dovetail block transverse portion, the vertical end portion of the guide rod is arranged to be connected with the box shell, and the transverse portion of the guide rod is arranged to be connected with the box cover in a sunken manner.

[0037] The technical effect of the above four technical solutions is that the upper cover of the monitoring rotor drone is sealed.

[0038] The utility model is designed that the swing platform is arranged as a plate-shaped body with an ear seat part I at the inner end face end portion and an ear seat part II at the middle portion of the inner and outer side faces; the ear seat part I is arranged to be connected to the column through a pin shaft, and the ear seat part II is arranged to be connected to the swing telescopic cylinder through a pin shaft.

[0039] The utility model is designed that the ear seat part I and the ear seat part II are respectively arranged as double-plate ear seats.

[0040] The utility model is designed in which the swing telescopic cylinder is arranged as a two-section telescopic cylinder and the hydraulic port portion of the swing telescopic cylinder is arranged to be connected to the output port of the hydraulic device of the traveling chassis, one end portion of the swing telescopic cylinder is arranged to be connected to the swing platform through a pin shaft and the other end portion of the swing telescopic cylinder is arranged to be connected to the column through a pin shaft.

[0041] The utility model is designed in such a way that the column is arranged as an L-shaped beam and the end surface portion of the horizontal portion of the column is arranged to be connected to the traveling chassis, the upper end portion of the vertical portion of the column is arranged to be connected to the swing platform through a pin shaft and the middle portion of the vertical portion of the column is arranged to be connected to the swing telescopic cylinder through a pin shaft, and the columns are arranged to be distributed corresponding to the box shell.

[0042] The technical effect of the above four technical solutions is to realize the take-off and landing platform support for the monitoring rotor UAV.

[0043] The utility model is designed in which the center lines of the traveling chassis, the box shell, the box cover, the movable seat, the push telescopic cylinder, the clamping claw, the air bag and the swinging platform are arranged on the same straight line, two lifting telescopic cylinders are arranged between the box cover and the traveling chassis, four guide rods are arranged between the box cover and the box shell, two buffer springs are arranged between the clamping claw and the moving seat, a swing telescopic cylinder and a column are arranged to form a group of beam components, two groups of beam components are arranged between the swinging platform and the traveling chassis, the bag part is respectively arranged to be connected with the vertical bar part and the guide rail part, the air pump part, the valve part I and the valve part II are respectively arranged to be connected with the box part, and the input pipe and the output pipe located on the bag part are respectively arranged to be through-connected with the rear side part of the upper wall of the box part.

[0044] In this technical solution, the running chassis, box shell and inflatable bag are basic components and are also necessary technical features of the utility model. The box cover, lifting telescopic cylinder, guide rod, movable seat, push telescopic cylinder, clamping claw, buffer spring, swing table, swing telescopic cylinder and column are functional components and are features for achieving other technical effects of the utility model. The design of these technical features, namely the box part, edge strip part, support seat part I, vertical strip part, guide rail part, support seat part II, accommodating trough body, clamp claw part I, clamp claw part II, shear telescopic cylinder part, bag part, air pump part, valve part I, valve part II, ear seat part I and ear seat part II, are technical features that comply with the Patent Law and its implementing rules.

[0045] In this technical solution, the monitoring rotor drone in the transport state is placed in the elastic and high-pressure gas composite interval by the claw assembly and the inflatable bag.

[0046] In this technical solution, the important technical features are the traveling chassis, box shell, claw assembly and inflatable bag that place the monitoring rotor drone in the transport state in the elastic and high-pressure gas composite interval. In the technical field of vehicle-mounted devices for monitoring rotor drones in construction tunnels, it has novelty, creativity and practicality. The terms in this technical solution can be explained and understood using the patent literature in this technical field. BRIEF DESCRIPTION OF THE DRAWINGS

[0047] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, the drawings described below are only some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying any creative work.

[0048] Figure 1 This is a schematic diagram of the utility model.

[0049] Driving chassis-1, box shell-2, box cover-3, lifting and telescopic cylinder-4, guide rod-5, moving seat-6, pushing and telescopic cylinder-7, clamping claw-8, buffer spring-9, inflation bag-91, swing table-92, swinging and telescopic cylinder-93, column-94, box part-21, edge strip part-22, support seat part I-23, vertical strip part-24, guide rail part-25, support seat part II-31, accommodating trough body-32, clamp claw part I-81, clamp claw part II-82, shearing and telescopic cylinder part-83, bag part-911, inflation pump part-912, valve part I-913, valve part II-914, ear seat part I-921, ear seat part II-922. DETAILED DESCRIPTION

[0050] According to the Examination Guidelines, terms such as “having”, “including” and “comprising” used in the present invention should be understood as not precluding the existence or addition of one or more other elements or their combinations.

[0051] In the description of this utility model, it should be noted that the terms "center," "upper," "lower," "left," "right," "vertical," "horizontal," "inner," and "outer," etc., indicating positions or relationships, are based on the positions or relationships shown in the accompanying drawings and are intended solely to facilitate the description of this utility model and simplify the description. They do not indicate or imply that the devices or components referred to must have a specific orientation, be constructed, or operate in a specific orientation. Therefore, they should not be construed as limitations on this utility model. Furthermore, the terms "first," "second," and "third" are used for descriptive purposes only and should not be construed as indicating or implying relative importance.

[0052] In the description of this utility model, it should be noted that, unless otherwise expressly specified or limited, the terms "mounted," "connected," and "connected" should be understood in a broad sense. For example, they can refer to fixed connections, detachable connections, or integral connections; mechanical connections, electrical connections; direct connections, indirect connections through an intermediate medium, and internal communication between two components. Those skilled in the art will understand the specific meanings of the above terms in this utility model based on the specific circumstances.

[0053] In addition, the technical features involved in the different embodiments of the present invention described below can be combined with each other as long as they do not conflict with each other. In addition, unless otherwise specified, the equipment and materials used in the following examples are commercially available. If the processing conditions are not clearly stated, please refer to the purchased product manual or follow the conventional methods in the field.

[0054] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0055] Figure 1 This is the first embodiment of the utility model, which is described in detail with reference to the accompanying drawings. It includes a traveling chassis 1, a box shell 2, a box cover 3, a lifting and telescopic cylinder 4, a guide rod 5, a movable seat 6, a push and telescopic cylinder 7, a clamping claw 8, a buffer spring 9, an air bag 91, a swing table 92, a swing and telescopic cylinder 93 and a column 94, and a column 94 is arranged on the traveling chassis 1, a box shell 2 is arranged on the column 94 and the traveling chassis 1, and a swing table 92 is arranged on the column 94, a swing and telescopic cylinder 93 is arranged between the swing table 92 and the column 94, and a box cover 3 and a movable seat 6 are arranged on the box shell 2, a lifting and telescopic cylinder 4 is arranged between the box cover 3 and the traveling chassis 1, and a guide rod 5 is arranged between the box cover 3 and the box shell 2, a push and telescopic cylinder 7 is arranged between the movable seat 6 and the box shell 2, and a clamping claw 8 is arranged on the movable seat 6, a buffer spring 9 is arranged between the clamping claw 8 and the movable seat 6, and an air bag 91 is arranged between the clamping claw 8 and the box shell 2.

[0056] In this embodiment, the running chassis 1 is configured as a truck chassis, and the middle portion of the upper end surface of the running chassis 1 is configured to be connected to the box shell 2 , and the rear side surface of the running chassis 1 is configured to be connected to the pillar 94 .

[0057] The traveling chassis 1 forms a supporting connection point for the box shell 2 and the column 94. The traveling chassis 1 realizes the connection with the box shell 2 and the column 94. Its technical purpose is to serve as a moving support carrier for the box shell 2 and the column 94.

[0058] In this embodiment, the box shell 2 is configured to include a box portion 21, an edge strip portion 22, a support seat portion I 23, a vertical strip portion 24 and a guide rail portion 25, and the upper portions of the front and rear side surfaces of the box portion 21 are configured to be connected to the inner end face portion of the edge strip portion 22, the front side portion of the upper end face of the box portion 21 is configured to be connected to the inner end face portion of the support seat portion I 23, and the rear side portion of the upper end face of the box portion 21 is configured to be connected to the inner end face portion of the vertical strip portion 24, the middle rear portion of the upper end face of the box portion 21 is configured to be connected to the inner end face portion of the guide rail portion 25, and the lower end face portion of the box portion 21 is configured to be connected to the running chassis 1, and the upper end portion of the box portion 21 It is arranged to be connected with the box cover 3 in a through-type manner and the rear side surface of the box part 21 is arranged to be distributed corresponding to the column 94, the upper end surface portion of the edge strip portion 22 is arranged to be connected with the box cover 3 in a contact type manner and the rear side surface portion of the support seat portion I23 is arranged to be connected with the push-telescopic cylinder 7, the guide rail portion 25 is arranged to be sunk into the moving seat 6 and the front side surface portion of the vertical strip portion 24 and the rear side surface portion of the guide rail portion 25 are respectively arranged to be connected with the inflatable bag 91, the box part 21 is arranged to be connected with the inflatable bag 91 in an accommodating manner and the front and rear end portions of the upper end surface of the vertical strip portion 24 and the front angle portion of the upper end surface of the box part 21 are respectively arranged to be connected with the guide rod 5.

[0059] Through the box shell 2, support connection points for the traveling chassis 1, box cover 3, guide rod 5, movable seat 6, telescopic cylinder 7, air bag 91 and column 94 are formed. The box part 21 realizes connection with the traveling chassis 1 and the column 94. The box part 21 and the edge strip part 22 realize connection with the box cover 3. The box part 21 and the vertical strip part 24 realize connection with the guide rod 5. The guide rail part 25 realizes connection with the movable seat 6. The support seat part I23 realizes connection with the telescopic cylinder 7. The vertical strip part 24 and the guide rail part 25 realize connection with the air bag 91. Its technical purpose is to serve as a moving support carrier for the box shell 2 and the column 94.

[0060] In this embodiment, the box portion 21 is configured as a box-shaped body with a double flip-opening and closing door on the side, the edge strip portion 22, the vertical strip portion 24 and the guide rail portion 25 are respectively configured as rectangular bar-shaped bodies and the support seat portion I 23 is configured as a block-shaped body.

[0061] The technical purpose is to realize the upper accommodation and storage of monitoring rotor UAVs and the lower accommodation and storage of monitoring data processing equipment.

[0062] In this embodiment, the box cover 3 is configured as a box-shaped body having a support seat portion Ⅱ31 in the middle part of the inner and outer end surfaces and a accommodating groove body 32 in the outer part of the front and rear inner walls, and the lower end open portion of the box cover 3 is configured to be connected in a sleeve-type manner with the box shell 2, the end face of the lower end open portion of the box cover 3 is configured to be connected in a contact-type manner with the box shell 2, and the lower end face portion of the support seat portion Ⅱ31 is configured to be connected to the lifting and telescopic cylinder 4, the accommodating groove body 32 is configured to be connected to the guide rod 5, and the box cover 3 is respectively configured to be accommodatingly connected to the guide rod 5, the moving seat 6, the pushing and telescopic cylinder 7, the clamping claw 8, the buffer spring 9 and the inflatable bag 91.

[0063] Through the box cover 3, support connection points are formed for the box shell 2, the lifting and telescopic cylinder 4, the guide rod 5, the movable seat 6, the pushing and telescopic cylinder 7, the clamping claw 8, the buffer spring 9 and the air bag 91. The box cover 3 realizes the connection with the box shell 2, the connection with the movable seat 6, the connection with the pushing and telescopic cylinder 7, the connection with the clamping claw 8, the connection with the buffer spring 9, and the connection with the air bag 91. The support seat part II 31 realizes the connection with the lifting and telescopic cylinder 4. The accommodating groove body 32 realizes the connection with the guide rod 5. Its technical purpose is to be used as a component to form an upper sealed storage area with the box shell 2.

[0064] In this embodiment, the support seat portion II 31 is configured as a rectangular block and the receiving groove 32 is configured as a dovetail groove.

[0065] Its technical purpose is to achieve connection with the lifting and telescopic cylinder 4 and the guide rod 5.

[0066] In this embodiment, the lifting and telescopic cylinder 4 is configured as a two-section telescopic cylinder and the hydraulic port portion of the lifting and telescopic cylinder 4 is configured to be connected to the hydraulic device output port of the traveling chassis 1, one of the end surface portions of the lifting and telescopic cylinder 4 is configured to be connected to the traveling chassis 1 and the other end surface portion of the lifting and telescopic cylinder 4 is configured to be connected to the box cover 3.

[0067] Through the lifting and telescopic cylinder 4, a supporting connection point is formed for the traveling chassis 1 and the box cover 3. The lifting and telescopic cylinder 4 realizes the connection with the traveling chassis 1 and the box cover 3. Its technical purpose is to serve as a component for driving the box cover 3 to rise and fall on the box shell 2.

[0068] In this embodiment, the guide rod 5 is configured as an L-shaped rod having a dovetail block transverse portion, and the vertical end portion of the guide rod 5 is configured to be connected to the box shell 2, and the transverse portion of the guide rod 5 is configured to be sunken in connection with the box cover 3.

[0069] Through the guide rod 5, support connection points for the box shell 2 and the box cover 3 are formed. By means of the guide rod 5, connection with the box shell 2 is achieved, and connection with the box cover 3 is achieved. Its technical purpose is: to be used as a guiding component for the lifting movement of the box cover 3 on the box shell 2.

[0070] In this embodiment, the moving seat 6 is set as a块状体 with an L-shaped groove on the upper end face and a U-shaped groove on the lower end face, and the front side face of the moving seat 6 is set to be connected to the pushing telescopic cylinder 7. The inner and outer walls of the L-shaped groove of the moving seat 6 are set to be connected to the clamping claws 8 through a pin shaft, and the L-shaped groove of the moving seat 6 is set to be connected to the buffer spring 9 in a receiving manner. The front wall of the L-shaped groove of the moving seat 6 is set to be sleeved with the buffer spring 9, and the U-shaped groove of the moving seat 6 is set to be connected to the box shell 2.

[0071] Through the moving seat 6, support connection points for the box shell 2, the pushing telescopic cylinder 7, the clamping claws 8, and the buffer spring 9 are formed. By means of the moving seat 6, connection with the box shell 2 is achieved, connection with the pushing telescopic cylinder 7 is achieved, connection with the clamping claws 8 is achieved, and connection with the buffer spring 9 is achieved. Its technical purpose is: to be used as a supporting carrier for the clamping claws 8.

[0072] In this embodiment, the pushing telescopic cylinder 7 is set as a two-stage telescopic cylinder, and the hydraulic port part of the pushing telescopic cylinder 7 is set to be connected to the output port of the hydraulic device of the traveling chassis 1. One end face of the pushing telescopic cylinder 7 is set to be connected to the box shell 2, and the other end face of the pushing telescopic cylinder 7 is set to be connected to the moving seat 6.

[0073] Through the pushing telescopic cylinder 7, support connection points for the traveling chassis 1, the box shell 2, and the moving seat 6 are formed. By means of the pushing telescopic cylinder 7, connection with the traveling chassis 1 is achieved, connection with the box shell 2 is achieved, and connection with the moving seat 6 is achieved. Its technical purpose is: to be used as a component for driving the moving seat 6 to move horizontally on the box shell 2.

[0074] In this embodiment, the clamping claws 8 are set to include a clamping jaw part I 81, a clamping jaw part II 82, and a shear telescopic cylinder part 83. The middle part of the clamping jaw part I 81 is set to be connected to the end of the middle vertical part of the clamping jaw part II 82 through a pin shaft. One end of the shear telescopic cylinder part 83 is set to be connected to the rear side of the inner end of the clamping jaw part I 81 through a pin shaft, and the other end of the shear telescopic cylinder part 83 is set to be connected to the end of the rear horizontal part of the clamping jaw part II 82 through a pin shaft. The inner end of the clamping jaw part I 81 is set to be connected to the moving seat 6 through a pin shaft, and the inner end of the clamping jaw part I 81 is set to be in contact connection with the buffer spring 9. The outer ends of the clamping jaw part I 81 and the clamping jaw part II 82 are set to be in contact connection with the air bag 91, and the hydraulic port part of the shear telescopic cylinder part 83 is set to be connected to the output port of the hydraulic device of the traveling chassis 1.

[0075] Through the clamping claw 8, a support connection point for the traveling chassis 1, the movable seat 6, the buffer spring 9 and the inflatable bag 91 is formed. The shearing telescopic cylinder part 83 realizes the connection with the traveling chassis 1. The clamping claw part I81 realizes the connection with the movable seat 6 and the buffer spring 9. The clamping claw part I81 and the clamping claw part II82 realize the connection with the inflatable bag 91. The shearing telescopic cylinder part 83 realizes the driving of the clamping claw part II82 to open and close on the clamping claw part I81. Its technical purpose is to be used as a component for supporting and fixing the monitoring rotor UAV.

[0076] In this embodiment, the jaw portion I81 is configured as a Y-shaped rod-shaped body with a middle leakage hole and the jaw portion II82 is configured as a frame-shaped body with a Y-shaped rod at the outer end and an L-shaped rod at the inner end. The rear part of the middle leakage hole of the jaw portion I81 is configured to be connected to the vertical part of the L-shaped rod of the jaw portion II82 and the front part of the middle leakage hole of the jaw portion I81 is configured to be connected to the shear telescopic cylinder portion 83. The shear telescopic cylinder portion 83 is configured as a two-section telescopic cylinder.

[0077] The technical purpose is to achieve clamping and supporting of the rotor UAV for monitoring the rotor UAV.

[0078] In this embodiment, the buffer spring 9 is configured as a torsion spring and the buffer spring 9 is configured to be sleeve-connected to a pin located between the clamping claw 8 and the movable seat 6, one end of the buffer spring 9 is configured to be through-connected to the movable seat 6 and the other end of the buffer spring 9 is configured to be contact-connected to the clamping claw 8.

[0079] A supporting connection point for the movable seat 6 and the clamping claw 8 is formed by the buffer spring 9. The buffer spring 9 realizes the connection with the movable seat 6 and the clamping claw 8. Its technical purpose is to serve as a component for buffering support between the clamping claw 8 and the movable seat 6.

[0080] In this embodiment, the inflatable bag 91 is configured to include a bag portion 911, an air pump portion 912, a valve portion I 913 and a valve portion II 914, and the input port portion of the bag portion 911 is configured to be connected to the output port portion of the air pump portion 912 through the valve portion I 913, the output port portion of the bag portion 911 is configured to be connected to the inner port portion of the valve portion II 914 and the bag portion 911 is configured to be embedded in the box shell 2, the air pump portion 912, the valve portion I 913 and the valve portion II 914 are configured to be built-in in the box shell 2 and the upper end surface portion of the bag portion 911 is configured to be contact-connected to the clamping claw 8.

[0081] The inflatable bag 91 forms a support connection point for the box shell 2 and the clamping claw 8. The bag part 911, the air pump part 912, the valve part I 913 and the valve part II 914 realize the connection with the box shell 2. The bag part 911 realizes the connection with the clamping claw 8. Its technical purpose is to be used as a component for soft support of monitoring rotor UAVs.

[0082] In this embodiment, the bag portion 911 is configured as a rubber bag-shaped body and the air pump portion 912 is configured as an inflator, and the valve portion I 913 and the valve portion II 914 are respectively configured as electric valves.

[0083] The technical purpose is to achieve airbag support for monitoring equipment of a monitoring rotor UAV.

[0084] In this embodiment, the swing platform 92 is configured as a plate-shaped body with an ear seat portion I 921 at the inner end face end portion and an ear seat portion II 922 at the middle portion of the inner and outer side faces, and the ear seat portion I 921 is configured to be connected to the column 94 through a pin shaft, and the ear seat portion II 922 is configured to be connected to the swing telescopic cylinder 93 through a pin shaft.

[0085] A support connection point for the swing telescopic cylinder 93 and the column 94 is formed through the swing platform 92. The connection with the swing telescopic cylinder 93 is realized by the ear seat part II 922, and the connection with the column 94 is realized by the ear seat part I 921. Its technical purpose is to be used as a component for planar support of the monitoring rotor drone.

[0086] In this embodiment, the ear seat portion I 921 and the ear seat portion II 922 are respectively configured as double-plate ear seats.

[0087] Its technical purpose is to achieve a rotational connection with the swing telescopic cylinder 93 and the column 94.

[0088] In this embodiment, the swing telescopic cylinder 93 is configured as a two-section telescopic cylinder and the hydraulic port portion of the swing telescopic cylinder 93 is configured to be connected to the hydraulic device output port of the traveling chassis 1, one end portion of the swing telescopic cylinder 93 is configured to be connected to the swing platform 92 through a pin shaft and the other end portion of the swing telescopic cylinder 93 is configured to be connected to the column 94 through a pin shaft.

[0089] Through the swing telescopic cylinder 93, a support connection point is formed for the traveling chassis 1, the swing platform 92 and the column 94. The swing telescopic cylinder 93 realizes the connection with the traveling chassis 1, the swing platform 92 and the column 94. Its technical purpose is to serve as a component for driving the swing platform 92 to swing on the column 94.

[0090] In this embodiment, the column 94 is configured to be an L-beam-shaped body and the transverse end surface of the column 94 is configured to be connected to the traveling chassis 1, the upper end of the vertical portion of the column 94 is configured to be connected to the swing platform 92 through a pin shaft and the middle of the vertical portion of the column 94 is configured to be connected to the swing telescopic cylinder 93 through a pin shaft, and the column 94 is configured to be distributed corresponding to the box shell 2.

[0091] Through the column 94, a support connection point is formed for the traveling chassis 1, the box shell 2, the swing platform 92 and the swing telescopic cylinder 93. The column 94 realizes the connection with the traveling chassis 1, the connection with the box shell 2, the swing platform 92 and the swing telescopic cylinder 93. Its technical purpose is to serve as a supporting carrier for the swing platform 92 and the swing telescopic cylinder 93.

[0092] In this embodiment, the center line of the traveling chassis 1, the center line of the box shell 2, the center line of the box cover 3, the center line of the movable seat 6, the center line of the push telescopic cylinder 7, the center line of the clamping claw 8, the center line of the inflation bag 91 and the center line of the swing platform 92 are arranged on the same straight line, two lifting telescopic cylinders 4 are arranged between the box cover 3 and the traveling chassis 1, four guide rods 5 are arranged between the box cover 3 and the box shell 2, two buffer springs 9 are arranged between the clamping claw 8 and the moving seat 6, a swing telescopic cylinder 93 and a column 94 are arranged to form a group of beam components, and the two groups of beam components are arranged between the swing platform 92 and the traveling chassis 1, the bag part 911 is respectively arranged to be connected with the vertical strip part 24 and the guide rail part 25, the inflation pump part 912, the valve part I913 and the valve part II914 are respectively arranged to be connected with the box part 21, and the input pipe and the output pipe located on the bag part 911 are respectively arranged to be through-connected with the rear side of the upper wall of the box part 21.

[0093] The method of using this embodiment is as follows: install the monitoring data processing equipment in the box part 21, make the lifting and telescopic cylinder 4 in an extended state, make the horizontal part of the guide rod 5 move downward in the accommodating groove body 32, separate the end face of the lower open part of the box cover 3 from the upper end face of the edge strip part 22, make the box cover 3 in a high position, make the shear telescopic cylinder part 83 in a retracted state, make the L-shaped rod vertical part of the clamp claw part II 82 rotate in the rear part of the middle leakage hole of the clamp claw part I 81, make the outer end head of the clamp claw part II 82 in a vertical state, make the clamp claw part II 82 and the clamp claw part I 81 in an expanded state, put the rotor UAV frame of the monitoring rotor UAV on the outer end head of the clamp claw part I 81, make the shear telescopic cylinder part 83 in an extended state, make the clamp claw part II 8 2 is reversely rotated in the rear of the middle leakage hole of the claw part I81, so that the outer end of the claw part II82 is in a horizontal state, and the claw part II82 and the claw part I81 are in a closed state. The outer end of the claw part II82 and the outer end of the claw part I81 clamp the rotor UAV frame of the monitoring rotor UAV, and the monitoring equipment for monitoring the rotor UAV is placed on the bag part 911, so that the valve part II914 is in a closed state, the valve part I913 is in an open state, the inflation pump part 912 is in a working state, and high-pressure gas is injected into the bag part 911. When the high-pressure gas is injected into the bag part 911, the inflation pump part 912 is in a non-working state, and the valve part I913 is in a closed state. The bag portion 911 in the state supports the monitoring equipment of the monitoring rotor UAV, so that the lifting and telescopic cylinder 4 is in a retracted state, and the horizontal part of the guide rod 5 moves upward in the accommodating groove body 32, so that the end face of the lower open part of the box cover 3 contacts the upper end face of the edge strip 22, so that the box cover 3 is in a low position, and the monitoring rotor UAV is sealed by the box cover 3. The monitoring rotor UAV is transported by the driving chassis 1 to the construction tunnel. When the monitoring rotor UAV is needed to monitor the construction tunnel, the double flip opening and closing doors of the box portion 21 are in an open state, and the box cover 3 is in a high position state through the lifting and telescopic cylinder 4, so that the valve part II 914 is in an open state, and the high-pressure gas in the bag portion 911 is emptied. When the bag portion 911 is completed After the medium and high pressure gas is exhausted, the swing telescopic cylinder 93 is in an extended state, the ear seat part I 921 swings on the column 94, the swing platform 92 is in a horizontal state, the push telescopic cylinder 7 is in an extended state, the movable seat 6 moves outward on the guide rail part 25, and the clamping claw 8 is located on the upper part of the swing platform 92. The monitoring rotor drone is moved from the upper end surface of the box part 21 to the swing platform 92 by the clamping claw 8. By shearing the telescopic cylinder part 83, the clamping claw part II 82 and the clamping claw part I 81 are in an expanded state, the monitoring rotor drone is moved out from the outer end of the clamping claw part I 81 and placed on the swing platform 92, the push telescopic cylinder 7 is in a contracted state, the movable seat 6 moves inward on the guide rail part 25, and the clamping claw 8 returns to its initial state.The monitoring rotor drone takes off from the swing platform 92 and monitors the construction tunnel. The monitoring data processing equipment in the box 21 stores and processes the detection data transmitted by the monitoring rotor drone. When the construction tunnel monitoring is completed, the monitoring rotor drone lands on the swing platform 92. By pushing the telescopic cylinder 7, the clamping claw 8 is positioned above the swing platform 92. The monitoring rotor drone is placed on the outer end of the clamping claw part I 81. By shearing the telescopic cylinder part 83, the clamping claw part II 82 and the clamping claw part I 81 are closed. The clamping claw 8 is then returned to its initial position, and the bag part 911 is expanded. The box cover 3 is lowered by raising and lowering the telescopic cylinder 4, and the double flip opening and closing door of the box 21 is closed. The swing platform 92 is then vertically adjusted by swinging the telescopic cylinder 93.

[0094] When verifying the present utility model, the inventor abandoned the existing technical feature of bringing the rotor UAV and the monitoring equipment to the tunnel construction site separately in boxes, and first proposed the technical feature of placing the monitoring rotor UAV in a transport state in a composite interval of elasticity and high-pressure gas, which obtained the first unexpected technical effect: the monitoring rotor UAV is transported as a whole, and the rotor UAV and the monitoring equipment are no longer frequently disassembled and installed, which improves the performance of the monitoring rotor UAV. The second unexpected technical effect is obtained: elastic buffer support is provided for the frame of the rotor UAV to prevent the rotor UAV from being subjected to transportation impact. By exerting force, the third unexpected technical effect was achieved: the monitoring equipment was wrapped and supported by a high-pressure gas bag to prevent the monitoring equipment from being subjected to transportation impact force. The fourth unexpected technical effect was achieved: the monitoring rotor UAV was able to take off and land on an external platform, thereby improving the safety performance of the monitoring rotor UAV. The fourth unexpected technical effect was achieved: the monitoring rotor UAV was able to be sealed and stored, thereby extending the service life of the monitoring rotor UAV. The fifth unexpected technical effect was achieved: the monitoring data processing equipment was able to be transported along with the monitoring rotor UAV, thereby improving the timeliness of the monitoring results of the construction tunnel.

[0095] In the second embodiment of the present invention, the traveling chassis 1, the box shell 2, the claw assembly and the inflatable bag 91 are connected to each other in such a way that the monitoring rotor UAV in the transport state is placed in the composite space of elasticity and high-pressure gas.

[0096] In this embodiment, the claw assembly is connected to the traveling chassis 1, the box shell 2 and the inflatable bag 91 in a manner of clamping and supporting the rotorcraft for monitoring the rotorcraft.

[0097] In this embodiment, the inflatable bag 91 is connected to the driving chassis 1, the box shell 2 and the claw assembly in a manner of supporting the airbag body of the monitoring equipment of the monitoring rotary-wing UAV.

[0098] In this embodiment, the clamp jaw assembly is configured to include a movable seat 6 , a clamping claw 8 and a buffer spring 9 .

[0099] In this embodiment, a first accessory device is further included and is arranged between the clamp jaw assembly and the box shell 2 . The first accessory device is configured to push the telescopic cylinder 7 .

[0100] In this embodiment, a second accessory device is further included and is arranged between the box shell 2 and the traveling chassis 1 . The second accessory device is configured to include a box cover 3 , a lifting and telescopic cylinder 4 and a guide rod 5 .

[0101] In this embodiment, a third accessory device is further included and is arranged between the box shell 2 and the traveling chassis 1 . The third accessory device is configured to include a swing platform 92 , a swing telescopic cylinder 93 and a column 94 .

[0102] The second embodiment of the present invention is based on the first embodiment.

[0103] The utility model has the following features:

[0104] 1. Due to the design of the traveling chassis 1, the box shell 2, the claw assembly and the inflatable bag 91, the traveling chassis 1 and the box shell 2 are used to support the claw assembly and the inflatable bag 91. The claw assembly is used to clamp and support the rotor drone of the monitoring rotor drone. The inflatable bag 91 is used to support the monitoring equipment of the monitoring rotor drone. The monitoring rotor drone in a transport state is placed in a composite interval of elasticity and high-pressure gas, which solves the technical problem of bringing the rotor drone and the monitoring equipment to the tunnel construction site separately in boxes, thereby improving the monitoring efficiency of the tunnel under construction.

[0105] 2. Due to the design of the movable seat 6, the clamping claw 8 and the buffer spring 9, elastic buffer support for the monitoring rotor UAV is achieved.

[0106] 3. Due to the design of the telescopic cylinder 7, the monitoring rotor UAV can be moved laterally.

[0107] 4. Due to the design of the box cover 3, the lifting and telescopic cylinder 4 and the guide rod 5, the monitoring rotor UAV is sealed.

[0108] 5. Due to the design of the swing platform 92, the swing telescopic cylinder 93 and the column 94, the platform body support for the monitoring rotor UAV is achieved.

[0109] 6. Since the design limits the numerical range of the structural shape, the numerical range is the technical feature in the technical solution of the utility model, and is not a technical feature calculated by formula or obtained through a limited number of tests. Tests have shown that the technical feature of this numerical range has achieved good technical effects.

[0110] 7. Due to the design of the technical features of the present invention, the effects of the individual and combined technical features have been shown through experiments to show that the performance indicators of the present invention are at least 1.7 times that of the existing performance indicators, and the evaluation shows that the present invention has a good market value.

[0111] There are other technical features that are connected to the traveling chassis 1, the box shell 2, the claw assembly and the inflatable bag 91 for placing the monitoring rotor UAV in a transport state in an elastic and high-pressure gas composite interval, which are all one of the embodiments of the present utility model, and the various technical features of the above-mentioned embodiments can be combined arbitrarily. In order to meet the requirements of the Patent Law, the Patent Implementation Rules and the Examination Guidelines, all possible combinations of the various technical features in the above-mentioned embodiments will no longer be described.

[0112] Therefore, in the technical field of vehicle-mounted devices for monitoring rotorcraft drones in construction tunnels, all technical contents including a traveling chassis 1 for transporting monitoring rotorcraft drones, a box shell 2 arranged on the traveling chassis 1, a claw assembly arranged on the box shell 2, and an inflatable bag 91 arranged on the box shell 2 are within the protection scope of this utility model.

Claims

1. A vehicle-mounted device for monitoring a rotary-wing drone in a tunnel under construction, characterized by: The invention comprises a traveling chassis (1) for transporting a monitoring rotor drone, a box shell (2) arranged on the traveling chassis (1), a clamping claw assembly arranged on the box shell (2), and an inflatable bag (91) arranged on the box shell (2). The clamp claw assembly is configured to include a movable seat (6), a clamping claw (8) and a buffer spring (9). It also includes a first accessory device and the first accessory device is arranged between the clamp claw assembly and the box shell (2), and the first accessory device is configured to push the telescopic cylinder (7). It also includes a second accessory device and is arranged between the box shell (2) and the travel chassis (1). The second accessory device is configured to include a box cover (3), a lifting and telescopic cylinder (4) and a guide rod (5). The third accessory device is also included and is arranged between the box shell (2) and the travel chassis (1). The third accessory device is configured to include a swing platform (92), a swing telescopic cylinder (93) and a column (94). A column (94) is provided on a traveling chassis (1), a box shell (2) is provided on the column (94) and the traveling chassis (1), and a swing platform (92) is provided on the column (94), a swing telescopic cylinder (93) is provided between the swing platform (92) and the column (94), and a box cover (3) and a movable seat (6) are provided on the box shell (2), a lifting telescopic cylinder (4) is provided between the box cover (3) and the traveling chassis (1), and a guide rod (5) is provided between the box cover (3) and the box shell (2), a push telescopic cylinder (7) is provided between the movable seat (6) and the box shell (2), and a clamping claw (8) is provided on the movable seat (6), a buffer spring (9) is provided between the clamping claw (8) and the movable seat (6), and an air bag (91) is provided between the clamping claw (8) and the box shell (2).

2. The vehicle-mounted device for monitoring a rotary-wing UAV in a tunnel under construction according to claim 1, characterized in that: The driving chassis (1), the box shell (2), the claw assembly and the inflatable bag (91) are connected to each other in such a way that the monitoring rotor drone in a transport state is placed in a composite space of elasticity and high-pressure gas.

3. The vehicle-mounted device for monitoring a rotary-wing UAV in a tunnel under construction according to claim 2, characterized in that: The clamp claw assembly is connected to the driving chassis (1), the box shell (2) and the inflatable bag (91) in a manner of clamping and supporting the rotor-wing UAV for monitoring the rotor-wing UAV.

4. The vehicle-mounted device for monitoring a rotary-wing UAV in a tunnel under construction according to claim 2, characterized in that: The inflatable bag (91) is connected to the driving chassis (1), the box shell (2) and the clamp claw assembly in a manner of supporting the air bag body for monitoring equipment of the monitoring rotor UAV.

5. The vehicle-mounted device for monitoring a rotary-wing UAV in a tunnel under construction according to claim 1 is characterized by: The running chassis (1) is configured as a truck chassis, and the middle portion of the upper end surface of the running chassis (1) is configured to be connected to the box shell (2), and the rear side surface of the running chassis (1) is configured to be connected to the column (94). Alternatively, the box shell (2) is configured to include a box portion (21), an edge strip portion (22), a support seat portion I (23), a vertical strip portion (24) and a guide rail portion (25), and the upper portions of the front and rear side surfaces of the box portion (21) are configured to be connected to the inner end face portion of the edge strip portion (22), the front side portion of the upper end face of the box portion (21) is configured to be connected to the inner end face portion of the support seat portion I (23), and the rear side portion of the upper end face of the box portion (21) is configured to be connected to the inner end face portion of the vertical strip portion (24), the middle rear portion of the upper end face of the box portion (21) is configured to be connected to the inner end face portion of the guide rail portion (25), and the lower end face portion of the box portion (21) is configured to be connected to the running chassis (1), and the upper end portion of the box portion (21) is configured to be connected to the inner end face portion of the guide rail portion (25). The invention is characterized in that the box portion (21) is connected to the box cover (3) in a through-type manner and the rear side surface of the box portion (21) is arranged to be distributed correspondingly to the column (94), the upper end surface of the edge strip portion (22) is arranged to be connected to the box cover (3) in a contacting manner and the rear side surface of the support seat portion I (23) is arranged to be connected to the push telescopic cylinder (7), the guide rail portion (25) is arranged to be connected to the movable seat (6) in a sinking manner and the front side surface of the vertical strip portion (24) and the rear side surface of the guide rail portion (25) are respectively arranged to be connected to the inflatable bag (91), the box portion (21) is arranged to be connected to the inflatable bag (91) in a housing manner and the front and rear end portions of the upper end surface of the vertical strip portion (24) and the front angle portion of the upper end surface of the box portion (21) are respectively arranged to be connected to the guide rod (5). Alternatively, the box portion (21) is configured as a box-shaped body with a double-turn opening and closing door on the side, the edge strip portion (22), the vertical strip portion (24) and the guide rail portion (25) are configured as rectangular bar-shaped bodies, and the support seat portion I (23) is configured as a block-shaped body. Alternatively, the inflatable bag (91) is configured to include a bag portion (911), an air pump portion (912), a valve portion I (913) and a valve portion II (914), and the input port portion of the bag portion (911) is configured to be connected to the output port portion of the air pump portion (912) through the valve portion I (913), the output port portion of the bag portion (911) is configured to be connected to the inner port portion of the valve portion II (914), and the bag portion (911) is configured to be embedded in the box shell (2), the air pump portion (912), the valve portion I (913) and the valve portion II (914) are configured to be built-in in the box shell (2), and the upper end portion of the bag portion (911) is configured to be in contact with the clamping claw (8), Alternatively, the bag portion (911) is configured as a rubber bag-shaped body and the air pump portion (912) is configured as an inflator, and the valve portion I (913) and the valve portion II (914) are configured as electric valves, respectively.

6. The vehicle-mounted device for monitoring a rotary-wing UAV in a tunnel under construction according to claim 1, characterized in that: The moving seat (6) is set as a块状 body with an L-shaped groove on the upper end face and a U-shaped groove on the lower end face, and the front side face of the moving seat (6) is set to be connected to the pushing telescopic cylinder (7). The inner and outer walls of the L-shaped groove of the moving seat (6) are set to be connected to the clamping claw (8) through a pin shaft, and the L-shaped groove of the moving seat (6) is set to be connected to the buffer spring (9) in a receiving manner. The front wall of the L-shaped groove of the moving seat (6) is set to be connected to the buffer spring (9) in a sleeved manner, and the U-shaped groove of the moving seat (6) is set to be connected to the box shell (2). Or, the pushing telescopic cylinder (7) is set as a two-stage telescopic cylinder, and the hydraulic port part of the pushing telescopic cylinder (7) is set to be connected to the output port of the hydraulic device of the traveling chassis (1). One end face of the pushing telescopic cylinder (7) is set to be connected to the box shell (2), and the other end face of the pushing telescopic cylinder (7) is set to be connected to the moving seat (6). Or, the clamping claw (8) is set to include a clamping jaw part I (81), a clamping jaw part II (82), and a shear telescopic cylinder part (83). The middle part of the clamping jaw part I (81) is set to be connected to the end of the middle vertical part of the clamping jaw part II (82) through a pin shaft. One end of the shear telescopic cylinder part (83) is set to be connected to the rear side of the inner end of the clamping jaw part I (81) through a pin shaft, and the other end of the shear telescopic cylinder part (83) is set to be connected to the end of the rear horizontal part of the clamping jaw part II (82) through a pin shaft. The inner end of the clamping jaw part I (81) is set to be connected to the moving seat (6) through a pin shaft, and the inner end of the clamping jaw part I (81) is set to be in contact connection with the buffer spring (9). The outer ends of the clamping jaw part I (81) and the clamping jaw part II (82) are set to be in contact connection with the air-filled bag (91), and the hydraulic port part of the shear telescopic cylinder part (83) is set to be connected to the output port of the hydraulic device of the traveling chassis (1). Or, the clamping jaw part I (81) is set as a Y-shaped rod body with a middle through-hole body, and the clamping jaw part II (82) is set as a frame body with a Y-shaped rod at the outer end and an L-shaped rod at the inner end. The rear part of the middle through-hole body of the clamping jaw part I (81) is set to be connected to the vertical part of the L-shaped rod of the clamping jaw part II (82), and the front part of the middle through-hole body of the clamping jaw part I (81) is set to be connected to the shear telescopic cylinder part (83). The shear telescopic cylinder part (83) is set as a two-stage telescopic cylinder. Or, the buffer spring (9) is set as a torsion spring, and the buffer spring (9) is set to be sleeved on the pin shaft between the clamping claw (8) and the moving seat (6). One end of the buffer spring (9) is set to be connected to the moving seat (6) in a penetrating manner, and the other end of the buffer spring (9) is set to be in contact connection with the clamping claw (8).

7. The vehicle-mounted device for monitoring a rotary-wing UAV in a tunnel under construction according to claim 1, characterized in that: The box cover (3) is configured as a box-shaped body having a support seat portion II (31) in the middle of the inner and outer end surfaces and a receiving groove body (32) on the outer sides of the front and rear inner walls, and the lower end open portion of the box cover (3) is configured to be connected in a sleeve-type manner to the box shell (2), the end surface of the lower end open portion of the box cover (3) is configured to be connected in a contact-type manner to the box shell (2), and the lower end surface portion of the support seat portion II (31) is configured to be connected to the lifting and telescopic cylinder (4), the receiving groove body (32) is configured to be connected to the guide rod (5), and the box cover (3) is configured to be connected in a receiving-type manner to the guide rod (5), the moving seat (6), the pushing and telescopic cylinder (7), the clamping claw (8), the buffer spring (9) and the inflatable bag (91). Alternatively, the support seat II (31) is configured as a rectangular block and the receiving groove (32) is configured as a dovetail groove. Alternatively, the lifting and telescopic cylinder (4) is configured as a two-section telescopic cylinder and the hydraulic port portion of the lifting and telescopic cylinder (4) is configured to be connected to the output port of the hydraulic device of the traveling chassis (1), one end surface portion of the lifting and telescopic cylinder (4) is configured to be connected to the traveling chassis (1) and the other end surface portion of the lifting and telescopic cylinder (4) is configured to be connected to the box cover (3), Alternatively, the guide rod (5) is configured as an L-shaped rod having a dovetail block transverse portion, and the vertical end portion of the guide rod (5) is configured to be connected to the box shell (2), and the transverse portion of the guide rod (5) is configured to be sunken in connection with the box cover (3). Alternatively, the swing platform (92) is configured as a plate-shaped body having an ear seat portion I (921) at the inner end face end portion and an ear seat portion II (922) at the middle portion of the inner and outer side faces, and the ear seat portion I (921) is configured to be connected to the column (94) through a pin shaft, and the ear seat portion II (922) is configured to be connected to the swing telescopic cylinder (93) through a pin shaft, Alternatively, the ear seat portion I (921) and the ear seat portion II (922) are respectively configured as double-plate ear seats. Alternatively, the swing telescopic cylinder (93) is configured as a two-section telescopic cylinder and the hydraulic port portion of the swing telescopic cylinder (93) is configured to be connected to the output port of the hydraulic device of the travel chassis (1), one end of the swing telescopic cylinder (93) is configured to be connected to the swing platform (92) via a pin shaft, and the other end of the swing telescopic cylinder (93) is configured to be connected to the column (94) via a pin shaft, Alternatively, the column (94) is configured as an L-shaped beam and the transverse end portion of the column (94) is configured to be connected to the travel chassis (1), the upper end of the vertical portion of the column (94) is configured to be connected to the swing platform (92) via a pin shaft, and the middle of the vertical portion of the column (94) is configured to be connected to the swing telescopic cylinder (93) via a pin shaft, and the columns (94) are configured to be distributed corresponding to the box shell (2).

8. The vehicle-mounted device for monitoring a rotary-wing UAV in a tunnel under construction according to any one of claims 1 to 7, characterized in that: The center line of the traveling chassis (1), the center line of the box shell (2), the center line of the box cover (3), the center line of the movable seat (6), the center line of the push telescopic cylinder (7), the center line of the clamping claw (8), the center line of the inflatable bag (91) and the center line of the swing platform (92) are arranged on the same straight line, two lifting telescopic cylinders (4) are arranged between the box cover (3) and the traveling chassis (1), four guide rods (5) are arranged between the box cover (3) and the box shell (2), two buffer springs (9) are arranged between the clamping claw (8) and the movable seat (6 ), a swing telescopic cylinder (93) and a column (94) are arranged to form a group of beam components, and the two groups of beam components are arranged between the swing platform (92) and the travel chassis (1). The bag part (911) is respectively arranged to be connected to the vertical bar part (24) and the guide rail part (25), and the air pump part (912), the valve part I (913) and the valve part II (914) are respectively arranged to be connected to the box part (21). The input pipe and the output pipe located on the bag part (911) are respectively arranged to be connected to the rear side of the upper wall of the box part (21) in a through-type manner.

Images