Four-light composite pod for unmanned aerial vehicle reconnaissance

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, and discloses an unmanned aerial vehicle-mounted reconnaissance four-light composite pod which comprises a mounting base and a rotating frame rotationally connected to the bottom of the mounting base, and further comprises a pod body detachably arranged on the rotating frame, a first motor is fixedly connected to the interior of the mounting base, and the rotating frame is provided with a dismounting mechanism. And the dismounting mechanism is used for facilitating workers to take down the pod body and comprises mounting grooves formed in the left side and the right side of the rotating frame. Through the arrangement of the rotary knob, the supporting arm, the connecting groove and the threaded rod, the function that a user can conveniently take down the pod body from the rotating frame for maintenance is achieved, the use efficiency is improved, and the problem that when an existing unmanned aerial vehicle pod is used, fixing is generally conducted through a screw fixing mode, and the use cost of the unmanned aerial vehicle pod is lowered is solved. And when the unmanned aerial vehicle pod fails, maintenance operation is inconvenient, and the working efficiency is greatly influenced.

Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field, concretely is a kind of four light composite pod for unmanned aerial vehicle reconnaissance. BACKGROUND

[0002] The unmanned aerial vehicle pod is a device installed under the fuselage of unmanned aerial vehicle, usually used for aerial photography, reconnaissance, monitoring and rescue tasks, the unmanned aerial vehicle pod usually includes sensors, cameras, laser radars, infrared cameras, digital signal processors, communication devices and stabilizers and other components, these pods are stably suspended in the air to provide high-quality image and data collection, and support various industries and tasks, but the existing composite pod still has some problems in actual use.

[0003] For example, the application number CN201621030936.X discloses a kind of unmanned aerial vehicle pod system, it includes pod and the detection equipment being arranged in its inside, further include damping device and mounting disc, the damping device is detachably installed on pod, the mounting disc is equipped with a plurality of installation holes required to be connected with unmanned aerial vehicle and is equipped with a plurality of positioning holes required to be connected with damping device, with the characteristics of strengthening the stability of pod operation, the existing unmanned aerial vehicle pod is generally fixed by screw fixing mode when in use, when unmanned aerial vehicle pod fails, it is not convenient to maintain operation, greatly influence work efficiency.

[0004] To solve the above problems, a kind of four light composite pod for unmanned aerial vehicle reconnaissance is provided. UTILITY MODEL CONTENT

[0005] The utility model aims at providing a kind of four light composite pod for unmanned aerial vehicle reconnaissance, using the device to work, to solve the problem that the existing unmanned aerial vehicle pod is generally fixed by screw fixing mode when in use, when unmanned aerial vehicle pod fails, it is not convenient to maintain operation, greatly influence work efficiency.

[0006] To achieve the above object, the utility model provides the following technical scheme: a kind of four light composite pod for unmanned aerial vehicle reconnaissance, including mounting seat and rotating frame being rotatably connected at the bottom of mounting seat, further including detachably setting the pod body on rotating frame, the inside fixed connection of mounting seat has motor one, the rotating frame is provided with dismounting mechanism, the dismounting mechanism is used to facilitate staff to take down pod body, the dismounting mechanism includes the installation groove being opened in the left and right sides of rotating frame, the inside detachable of installation groove is provided with support arm, the support arm is provided with two groups.

[0007] Preferably, the output end of the motor one is fixedly connected with a rotating disc, the bottom of the rotating disc is fixedly connected with a limiting block one, and the side of the rotating frame is rotatably connected with a knob.

[0008] By the arrangement of the rotating disc, the pod body can rotate in the horizontal direction, and the use effect is improved.

[0009] Preferably, one end of the knob extends to the inside of the rotating frame and is fixedly connected with a threaded rod, the threaded rod is threadedly connected with a sliding plate, and the sliding plate is slidingly connected in the inside of the rotating frame.

[0010] By the connecting relationship that the sliding plate is slidingly connected, the sliding plate will not deviate from the moving track during movement.

[0011] Preferably, one side of the sliding plate is fixedly connected with a connecting block, the connecting block is provided in two groups, one side of the supporting arm is provided with a connecting groove, and the connecting groove is provided in two groups.

[0012] By the arrangement of the supporting arm, related devices can be connected to the supporting arm, and the space utilization of the device is improved.

[0013] Preferably, the connecting groove and the connecting block are slidingly matched, the inside of the supporting arm is fixedly connected with a second motor, the first motor and the second motor are both speed-reducing motors, and the output end of the second motor is fixedly connected with a bevel gear one.

[0014] By the arrangement of the connecting groove and the connecting block, the user can conveniently take down the pod body from the rotating frame for maintenance.

[0015] Preferably, one side of the bevel gear one is meshingly connected with a bevel gear two, one side of the bevel gear two is fixedly connected with a limiting block two, and the left and right sides of the pod body are both provided with a limiting groove.

[0016] By the arrangement of the bevel gear one and the bevel gear two, the transmission direction of the second motor is changed, and the work process is promoted.

[0017] Preferably, the limiting groove and the limiting block two are slidingly matched, the top of the pod body is fixedly connected with a clamping block, and the clamping block and the limiting block one are slidingly matched.

[0018] By the arrangement of the clamping block and the limiting block one, the pod body can rotate in the vertical direction, and the convenience is improved.

[0019] Compared with the prior art, the utility model has the advantages of the following:

[0020] 1、The present application is through the setting of knob, support arm, connecting groove and threaded rod, realizes the function that the user can take down the pod body from the rotating frame for maintenance, improves the use efficiency, solves the problem that the existing unmanned aerial vehicle pod is generally fixed by screw when using, when the unmanned aerial vehicle pod fails, it is inconvenient to maintain, greatly affects the work efficiency.

[0021] 2、The present application is through the setting of motor two, motor one, limit groove and bevel gear one, realizes the function that the user can adjust the angle of view, improves the use effect of the device, solves the problem that the existing unmanned aerial vehicle pod is generally fixed, when the observation angle needs to be adjusted to observe the surrounding environment, it is inconvenient to operate, affects the use effect of the device. BRIEF DESCRIPTION OF DRAWINGS

[0022] Figure 1 It is the overall structure schematic diagram of the utility model;

[0023] Figure 2 It is the motor one and the clamping block structure diagram of the utility model;

[0024] Figure 3 It is the knob and support arm structure diagram of the utility model;

[0025] Figure 4 It is the connecting groove and limit block two structure diagram of the utility model;

[0026] Figure 5 It is the motor two and limit groove structure diagram of the utility model.

[0027] In the drawing: 1, mounting seat; 11, motor one; 111, rotating disc; 112, limit block one; 2, rotating frame; 21, installation groove; 211, knob; 212, threaded rod; 213, sliding plate; 214, connecting block; 22, support arm; 221, connecting groove; 23, motor two; 231, bevel gear one; 232, bevel gear two; 233, limit block two; 3, pod body; 31, limit groove; 32, clamping block. DETAILED DESCRIPTION

[0028] The technical scheme in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only part of the embodiments of the present application, not all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative labor fall within the scope of the present application.

[0029] In order to further understand the content of the present application, the present application will be described in detail with reference to the drawings.

[0030] In combination Figures 1-3 The utility model provides a unmanned aerial reconnaissance four light composite pod, including mounting seat 1 and the rotary frame 2 of rotary connection in mounting seat 1 bottom, still including detachably setting on the pod body 3 of rotary frame 2, the inside fixed connection of mounting seat 1 has motor no. 11, rotary frame 2 is provided with the dismounting mechanism, and the dismounting mechanism is used for facilitating staff to take down pod body 3, and the dismounting mechanism includes the installation groove 21 of opening in the left and right sides of rotary frame 2, and the inside detachably of installation groove 21 is provided with support arm 22, and support arm 22 is provided with two groups.

[0031] The utility model will be further described below in combination with the embodiment.

[0032] Embodiment 1:

[0033] To solve the existing unmanned aerial vehicle pod when using, generally all through the screw fixed mode fixed, when unmanned aerial vehicle pod failure, it is inconvenient to maintain operation, greatly influenced the work efficiency problem, the embodiment discloses the following technical scheme, specifically like Figures 1-4As shown, the bottom of the rotating disc 111 is fixedly connected with a limiting block one 112, one side of the rotating frame 2 is rotatably connected with a knob 211, one end of the knob 211 extends to the inside of the rotating frame 2 and is fixedly connected with a threaded rod 212, the threaded rod 212 is threadedly connected with a sliding plate 213, the sliding plate 213 is slidably connected in the inside of the rotating frame 2, one side of the sliding plate 213 is fixedly connected with a connecting block 214, the connecting block 214 is provided with two groups, one side of the supporting arm 22 is provided with a connecting groove 221, and the connecting groove 221 is provided with two groups, the connecting groove 221 and the connecting block 214 are in sliding fit, the left and right sides of the pod body 3 are both provided with a limiting groove 31, the limiting groove 31 and the limiting block two 233 are in sliding fit, the top of the pod body 3 is fixedly connected with a clamping block 32, the clamping block 32 and the limiting block one 112 are in sliding fit, when used, the mounting seat 1 can be installed at the bottom of the unmanned aerial vehicle, and the pod body 3 can be used, when the pod body 3 fails and needs to be maintained, the knob 211 on the rotating frame 2 can be rotated, the knob 211 drives the threaded rod 212 to rotate, and then the sliding plate 213 moves, the sliding plate 213 drives the two groups of connecting blocks 214 to come out of the inside of the connecting groove 221, and then the supporting arm 22 can be moved, so that the limiting block two 233 and the limiting groove 31 are separated, and then the pod body 3 can be taken off from the rotating frame 2, when the maintenance is completed and the pod body 3 needs to be installed, the clamping block 32 at the top of the pod body 3 is butted against the limiting block one 112 at the bottom of the rotating disc 111, the supporting arm 22 is moved, so that the supporting arm 22 is reset, finally the knob 211 is rotated, the knob 211 drives the connecting block 214 to move, and then the connecting block 214 moves to the inside of the connecting groove 221, and then the installation of the supporting arm 22 is completed, the function that the user can conveniently take the pod body 3 off from the rotating frame 2 for maintenance is realized, and the use efficiency is improved.

[0034] Embodiment 2:

[0035] To solve the problem that the existing unmanned aerial vehicle pod is often fixedly arranged, and when it is necessary to adjust the observation angle to observe the surrounding environment, it is inconvenient to operate and affects the use effect of the device, the technical scheme is disclosed as follows, specifically as Figure 2 、 Figure 3 and Figure 5As shown, the output end of the motor 11 is fixedly connected with a rotating disc 111, the inside of the support arm 22 is fixedly connected with a motor 23, the motor 11 and the motor 23 are all reduction motors, the output end of the motor 23 is fixedly connected with a bevel gear 231, one side of the bevel gear 231 is meshingly connected with a bevel gear 232, one side of the bevel gear 232 is fixedly connected with a limiting block 233, when it is needed to adjust the rotating angle of the pod body 3, at this time, the motor 11 can be started, the motor 11 drives the rotating disc 111 to rotate, thereby making the rotating frame 2 rotate, the rotating frame 2 drives the pod body 3 to rotate, thereby realizing the horizontal direction visual angle adjustment, the motor 23 can also be started, the motor 23 drives the bevel gear 231 to rotate, thereby making the bevel gear 232 rotate, the bevel gear 232 and the limiting groove 31 cooperate to make the pod body 3 rotate in the vertical direction, thereby multi-direction adjustment can be carried out, the function that the user can conveniently adjust the visual angle is realized, and the use effect of the device is improved.

[0036] It should be noted that the above-mentioned electrical elements are provided with power supplies, and their control modes are prior art, in order to avoid tedious description, which are uniformly described herein; and the present application is mainly used to protect mechanical equipment, so the control mode and circuit connection are not explained in detail in the text, in the text, relationship terms such as first and second are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any such actual relationship or order between the entities or operations. Moreover, the terms "include", "contain" or any other variant thereof are intended to cover non-exclusive inclusion, so that the process, method, article or device including a series of elements includes not only those elements, but also other elements not explicitly listed, or further includes elements inherent to such process, method, article or device.

[0037] Although the embodiments of the present application have been shown and described, it can be understood by those skilled in the art that various changes, modifications, replacements and variations can be made to the embodiments without departing from the principles and spirits of the present application, the scope of the present application is defined by the appended claims and their equivalents.

Claims

1. A four-light composite pod for unmanned aerial reconnaissance, comprising a mounting seat (1) and a rotating frame (2) rotatably connected to the bottom of the mounting seat (1), and further comprising a pod body (3) detachably arranged on the rotating frame (2), characterized in that: The inside of mounting seat (1) is fixedly connected with motor one (11), the rotating frame (2) is provided with dismounting mechanism, the dismounting mechanism is used for facilitating staff to take down the pod body (3), the dismounting mechanism includes the installation groove (21) being opened in the left and right sides of rotating frame (2), the inside of installation groove (21) is detachably provided with support arm (22), support arm (22) is provided with two groups.

2. The four-light composite pod for unmanned airborne reconnaissance according to claim 1, characterized in that: The output end of motor one (11) is fixedly connected with rotating disc (111), the bottom of rotating disc (111) is fixedly connected with limit block one (112), one side of rotating frame (2) is rotatably connected with knob (211).

3. The four-light composite pod for unmanned airborne reconnaissance according to claim 2, characterized in that: One end of knob (211) extends to the inside of rotating frame (2) and is fixedly connected with threaded rod (212), threaded rod (212) is threadedly connected with sliding plate (213), sliding plate (213) is slidably connected in the inside of rotating frame (2).

4. The four-light composite pod for unmanned airborne reconnaissance according to claim 3, characterized in that: One side of sliding plate (213) is fixedly connected with connecting block (214), connecting block (214) is provided with two groups, one side of support arm (22) is provided with connecting groove (221), and connecting groove (221) is provided with two groups.

5. The four-light composite pod for unmanned airborne reconnaissance according to claim 4, characterized in that: Connecting groove (221) and connecting block (214) are slidably matched, the inside of support arm (22) is fixedly connected with motor two (23), motor one (11) and motor two (23) are all reduction motors, the output end of motor two (23) is fixedly connected with bevel gear one (231).

6. The four-light composite pod for unmanned airborne reconnaissance according to claim 5, characterized in that: One side of bevel gear one (231) is meshedly connected with bevel gear two (232), one side of bevel gear two (232) is fixedly connected with limit block two (233), the left and right sides of pod body (3) are both provided with limit slot (31).

7. The four-light composite pod for unmanned airborne reconnaissance according to claim 6, characterized in that: Limit slot (31) and limit block two (233) are slidably matched, the top of pod body (3) is fixedly connected with clamping block (32), clamping block (32) and limit block one (112) are slidably matched.

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