CN220199578U

CN220199578U - Aviation mapping ware with buffer function falls to ground

Info

Publication number: CN220199578U
Application number: CN202321125383.6U
Authority: CN
Inventors: 张敏
Original assignee: Jiangsu Coal Geological Exploration Team 2
Current assignee: Jiangsu Coal Geological Exploration Team 2
Priority date: 2023-05-11
Filing date: 2023-05-11
Publication date: 2023-12-19
Anticipated expiration: 2033-05-11

Abstract

The utility model relates to the field of aviation mapping, in particular to an aviation mapping device with a floor buffering function. The utility model provides an aviation mapping device with a landing buffering function, and the purpose of buffering is achieved through the cooperation of a first elastic piece and a second elastic piece when the aviation mapping device lands. The utility model provides an aviation mapping device with a floor buffering function, which comprises a control console, a mounting rod, a propeller, a mounting plate and a servo motor, wherein the mounting rod is fixedly connected to the control console at uniform intervals, the propeller is rotatably arranged in the mounting rod, the mounting plate is fixedly connected to the top of the control console, and the servo motor is mounted on the mounting plate. Through supporting shoe and ground contact upward movement, extrusion slide bar upward movement makes second elastic component and first elastic component compressed and plays the cushioning effect, reduces the collision dynamics between supporting shoe and the ground, takes place to empty the phenomenon when preventing aviation mapping ware landing and receives the damage.

Description

Aviation mapping ware with buffer function falls to ground

Technical Field

The utility model relates to the field of aviation mapping, in particular to an aviation mapping device with a floor buffering function.

Background

Aerial surveying is a means of surveying to the ground with an aircraft in the atmosphere as a measurement carrier, the object of which is the positional relationship of the ground object, in order to map the geodetic coordinates by the data obtained by aerial photography surveying, and the method generally adopted is aerial photogrammetry.

Patent grant bulletin number is CN 215622756U's patent, discloses an aviation survey and drawing unmanned aerial vehicle, including unmanned aerial vehicle main part, installation head, fastener and camera module, the installation head is connected with the unmanned aerial vehicle main part. The fastener is equipped with the mounting hole, is provided with first locating part on the pore wall of mounting hole, and first locating part and fastener sliding fit are in order to adjust the length that first locating part is arranged in the mounting hole, and the fastener is connected with installation head detachably. Be equipped with the second locating part on the shell of camera module, camera module peg graft in the mounting hole, and between first locating part and the installation head was located to the second locating part, the second locating part can support with first locating part and hold to prevent that camera module from deviating from the mounting hole. The aeronautical survey unmanned aerial vehicle of above-mentioned patent when falling to the ground, can't alleviate the collision dynamics between shell and the ground, lead to the shell to bump the back with ground and appear empting the phenomenon easily, lead to the unmanned aerial vehicle main part to receive the damage.

Therefore, there is a particular need for an airborne survey instrument with a floor cushioning function, where the airborne survey instrument is cushioning by the cooperation of the first elastic member and the second elastic member when the airborne survey instrument is landed.

Disclosure of Invention

In order to overcome the defects that the collision force between the shell and the ground cannot be reduced when the unmanned aerial vehicle for aerial surveying and mapping in the prior patent falls to the ground, the shell is easy to topple over after colliding with the ground, and the unmanned aerial vehicle main body is damaged, the utility model aims to provide the aerial surveying and mapping device with the function of buffering in the falling to the ground, and the aim of buffering is achieved through the cooperation of the first elastic piece and the second elastic piece when the aerial surveying and mapping device falls to the ground.

The utility model is realized by the following technical approaches: the utility model provides an aviation mapping ware with buffering function falls to ground, including the control cabinet, the installation pole, the screw, the mounting panel, servo motor, first mount pad and mapping instrument body, even interval rigid coupling has the installation pole on the control cabinet, the inside rotation type of installation pole is provided with the screw, control cabinet top rigid coupling has the mounting panel, install servo motor on the mounting panel, the rigid coupling has first mount pad on servo motor's the output shaft, the rigid coupling has the mapping instrument body that is used for shooting mapping to ground object on the first mount pad, still including the second mount pad, the fixed sleeve, the slide bar, first elastic component, the slider, second elastic component and supporting shoe, control cabinet lower part rigid coupling has the second mount pad, the equal bilateral symmetry rigid coupling of second mount pad has the fixed sleeve, the inside slidingtype of fixed sleeve is provided with the slide bar, be connected with first elastic component between slide bar bottom rigid coupling has the slider, slider bottom embedded second elastic component that is provided with, second elastic component one end is connected with the supporting shoe.

As a further preferred scheme, the anti-collision device further comprises a protection frame, guide rods, anti-collision plates and third elastic pieces, wherein the protection frame is fixedly connected to the installation rod, three guide rods are fixedly connected to the protection frame at equal intervals, the anti-collision plates used for anti-collision are arranged on the guide rods in a sliding mode, two third elastic pieces are connected between the anti-collision plates and the protection frame, the third elastic pieces are sleeved on the guide rods, and two ends of each third elastic piece are connected with the protection frame and the anti-collision plates respectively.

As a further preferable scheme, the intelligent alarm device further comprises a button and an alarm, wherein the button is arranged on the protection frame in a sliding mode at uniform intervals, the alarm for alarming is arranged on the installation rod in an embedded mode, and the alarm is electrically connected with the button.

As a further preferred scheme, the protection device further comprises a protection seat, a clamping block, a protection cover and clamping blocks, wherein the protection seat is fixedly connected to the control console, two clamping blocks are arranged on the protection seat, the protection cover for protection is placed on the protection seat, two clamping blocks are rotatably arranged on the protection cover, and the clamping blocks are clamped with the clamping blocks.

As a further preferable scheme, the surveying instrument further comprises a transparent protective cover, and the surveying instrument body is fixedly connected with the transparent protective cover for protection.

As a further preferable scheme, the device further comprises a reinforcing rod, wherein the reinforcing rod for reinforcing is fixedly connected between the two vertically aligned fixing cylinders.

The design starting point, concept and advantages of the utility model are as follows, as can be seen from the above description of the structure of the utility model: 1. through supporting shoe and ground contact upward movement, extrusion slide bar upward movement makes second elastic component and first elastic component compressed and plays the cushioning effect, reduces the collision dynamics between supporting shoe and the ground, takes place to empty the phenomenon when preventing aviation mapping ware landing and receives the damage.

2. The third elastic piece is compressed to play a buffering role, so that collision force between birds and the anti-collision plate is reduced, the anti-collision plate is prevented from being excessively large in collision force, and the aviation mapping device is prevented from falling down from the air to be damaged.

3. The anti-collision plate is collided, the push button is moved inwards, the push button transmits information to the alarm, the alarm operates to give out alarm sound, birds are surprised to be far away from the aviation mapping device, and accordingly safety of the aviation mapping device in the mapping process is improved.

4. The protection casing plays the guard action, prevents impurity such as external foreign matter and gets into in the protection seat, causes the damage to the surveying instrument body, prolongs the life of surveying instrument body.

Drawings

Fig. 1 is a schematic perspective view of the present utility model.

Fig. 2 is a schematic perspective sectional structure of the console, the first elastic member and the slider of the present utility model.

Fig. 3 is a schematic perspective sectional view of the protection seat, the clamping block and the protection cover of the present utility model.

Fig. 4 is a schematic perspective sectional structure of the servo motor, the first mounting seat and the surveying instrument body of the present utility model.

FIG. 5 is a schematic perspective cross-sectional view of the mounting plate and transparent protective cover of the present utility model.

Fig. 6 is a schematic perspective view of the crash panel, the third elastic member and the button according to the present utility model.

In the above figures: 1-control desk, 2-installation rod, 3-screw, 301-installation plate, 4-servo motor, 5-first installation seat, 6-surveying instrument body, 7-second installation seat, 8-fixed sleeve, 9-slide bar, 10-first elastic piece, 11-slider, 12-second elastic piece, 13-supporting block, 14-protection frame, 15-guide rod, 16-crashproof board, 17-third elastic piece, 18-button, 19-alarm, 20-protection seat, 21-fixture block, 22-protection casing, 23-buckle, 24-transparent visor, 25-reinforcement rod.

Detailed Description

The utility model will be further illustrated by the following description of specific examples, which are given by the terms such as: setting, mounting, connecting are to be construed broadly, and may be, for example, fixed, removable, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.

Example 1

1-6, the aviation mapping ware with fall to ground buffer function, see fig. 1-6, including control cabinet 1, installation pole 2, screw 3, mounting panel 301, servo motor 4, first mount pad 5 and surveying instrument body 6, even interval is provided with installation pole 2 through welded mode on the control cabinet 1, the inside rotation of installation pole 2 is provided with screw 3, control cabinet 1 top is provided with mounting panel 301 through welded mode, be provided with servo motor 4 through bolted connection's mode on the mounting panel 301, be provided with first mount pad 5 through key connection's mode on servo motor 4's the output shaft, be provided with surveying instrument body 6 that is used for taking the survey and drawing to ground object through welded mode on the first mount pad 5, still include second mount pad 7, fixed sleeve 8, slide bar 9, first elastic component 10, slider 11, second elastic component 12 and supporting shoe 13, control cabinet 1 lower part is provided with second mount pad 7 through welded mode, both sides are provided with fixed sleeve 8 through welded mode, fixed sleeve 8 inside slip type 9 is provided with slider 9 and elastic component 12 is provided with through the first elastic component 11, slider 11 is provided with bottom connection elastic component 12, slider 11 is provided with elastic component 12.

When needs carry out aviation survey and drawing to ground object, the staff places aviation survey and drawing ware subaerial, afterwards the staff opens control cabinet 1 and surveying instrument body 6, the staff makes screw 3 rotate through controlling control cabinet 1, and then make control cabinet 1 fly to aerial, surveying instrument body 6 operation is shot the survey and drawing to the object on ground, the in-process of shooting survey and drawing, the staff controls control cabinet 1 and opens servo motor 4, servo motor 4's output shaft rotates and drives surveying instrument body 6 rotation, and then carry out comprehensive shooting survey and drawing to ground object, reach good shooting survey and drawing effect, after the completion of shooting survey and drawing, the staff controls control cabinet 1 and makes screw 3's rotation speed slow down, make aviation survey and drawing ware start to descend, make supporting shoe 13 and ground contact upward move, extrusion slide bar 9 upward movement simultaneously, second elastic component 12 and first elastic component 10 are compressed and play the cushioning effect thereupon, reduce the collision dynamics between supporting shoe 13 and the ground, take place the damage when preventing aviation survey and drawing ware falls to the ground, the back is taken up from subaerial to the ground with it, make supporting shoe 13 and break away from ground, first elastic component 12 and second elastic component 10 restore to the original state that the supporting shoe is reset to the slide bar 13.

Example 2

On the basis of embodiment 1, referring to fig. 1 and 6, the anti-collision device further comprises a protection frame 14, a guide rod 15, an anti-collision plate 16 and a third elastic piece 17, wherein the protection frame 14 is arranged on the installation rod 2 in a welding mode, three guide rods 15 are uniformly arranged on the protection frame 14 at intervals in a welding mode, an anti-collision plate 16 for anti-collision is slidably arranged on the guide rod 15, two third elastic pieces 17 are connected between the anti-collision plate 16 and the protection frame 14, the third elastic pieces 17 are sleeved on the guide rods 15, and two ends of each third elastic piece 17 are respectively connected with the protection frame 14 and the anti-collision plate 16.

In the process of shooting and mapping objects on the ground, the protection frame 14 plays a role in protection, so that flying birds in the air are prevented from striking the propeller 3 to damage the propeller, when the protection frame 14 is impacted by the birds, the anti-collision plate 16 is extruded to move inwards, the third elastic piece 17 is compressed to play a role in buffering, the impact force between the birds and the anti-collision plate 16 is reduced, the anti-collision force received by the anti-collision plate 16 is prevented from being too large, the air mapper is prevented from falling and damaging in the air, and after the external impact force disappears, the third elastic piece 17 is restored to the original state, so that the anti-collision plate 16 moves outwards to reset.

Referring to fig. 3 and 6, the safety protection device further comprises a button 18 and an alarm 19, the button 18 is arranged on the protection frame 14 in a sliding mode at uniform intervals, the alarm 19 for alarming is arranged on the mounting rod 2 in an embedded mode, and the alarm 19 is electrically connected with the button 18.

When the anti-collision plate 16 is collided and moves inwards to squeeze the button 18, the button 18 transmits information to the alarm 19, and the alarm 19 operates to give out an alarm sound, so that birds are surprised to be far away from the aerial mapper, and the safety of the aerial mapper in the shooting mapping process is improved.

Referring to fig. 1 and 3, the protection device further comprises a protection seat 20, clamping blocks 21, a protection cover 22 and a buckle 23, wherein the protection seat 20 is arranged on the console 1 in a welding mode, two clamping blocks 21 are arranged on the protection seat 20 in a bolt connection mode, a protection cover 22 for protection is placed on the protection seat 20, two buckles 23 are rotatably arranged on the protection cover 22, and the buckle 23 is in clamping connection with the clamping blocks 21.

Initially, buckle 23 and fixture block 21 joint are fixed protection casing 22 on protection seat 20, when needs shoot the survey and drawing to the object on ground, the staff upwards rotates buckle 23, make it break away from the joint with fixture block 21, then the staff takes off protection casing 22 from protection seat 20, the staff controls the survey and drawing to shoot the survey and drawing to the object on ground, the in-process of shooting survey and drawing, protection seat 20 plays the guard action, reduce the probability that surveying instrument body 6 received the damage, after the survey and drawing was accomplished, the staff controls control console 1 and makes aviation survey and drawing ware fall to the ground, when need not use aviation survey and drawing ware, the staff places protection casing 22 on protection seat 20, the staff rotates buckle 23 downwards, make it and fixture block 21 joint, and then fix protection casing 22 on protection seat 20 again, protection casing 22 plays the guard action, prevent impurity such as external foreign matter from getting into protection seat 20, cause the damage to surveying instrument body 6, the life of surveying instrument body 6 is prolonged.

Referring to fig. 5, the surveying instrument body 6 further comprises a transparent protective cover 24, and the transparent protective cover 24 for protection is arranged on the surveying instrument body 6 in a welding mode.

The transparent protective cover 24 plays a protective role to prevent the lens of the surveying instrument body 6 from being damaged when objects on the ground are photographed and mapped.

Referring to fig. 2, the fixing device further comprises a reinforcing rod 25, wherein the reinforcing rod 25 for reinforcing is arranged between the two vertically aligned fixing cylinders in a welding mode.

The reinforcing rod 25 plays a reinforcing role, increases the contact area between the two fixing sleeves 8 vertically aligned, and improves the stability of the fixing sleeves 8.

The foregoing is merely a preferred embodiment of the present utility model and it should be noted that modifications and adaptations to those skilled in the art may be made without departing from the principles of the present utility model, which are intended to be comprehended within the scope of the present utility model.

Claims

1. The utility model provides an aviation mapping ware with buffering function falls to ground, including control cabinet (1), installation pole (2), screw (3), mounting panel (301), servo motor (4), first mount pad (5) and surveying instrument body (6), even interval rigid coupling has installation pole (2) on control cabinet (1), inside rotation type is provided with screw (3) of installation pole (2), control cabinet (1) top rigid coupling has mounting panel (301), install servo motor (4) on mounting panel (301), rigid coupling has first mount pad (5) on the output shaft of servo motor (4), rigid coupling has surveying instrument body (6) on first mount pad (5), a serial communication port, still include second mount pad (7), fixed sleeve (8), slide bar (9), first elastic component (10), slider (11), second elastic component (12) and supporting shoe (13), control cabinet (1) lower part rigid coupling has second mount pad (7), second mount pad (7) both sides all front and back symmetry rigid coupling have fixed sleeve (8), fixed sleeve (8) inside sliding type (9) are provided with slide bar (9) and slide bar (10) are connected with between the slide bar (11), the bottom of the sliding block (11) is provided with a second elastic piece (12) in an embedded mode, and one end of the second elastic piece (12) is connected with a supporting block (13).

2. The aviation mapping device with the floor buffering function according to claim 1, further comprising a protection frame (14), guide rods (15), anti-collision plates (16) and third elastic pieces (17), wherein the protection frame (14) is fixedly connected to the mounting rod (2), three guide rods (15) are fixedly connected to the protection frame (14) at equal intervals, the anti-collision plates (16) are slidably arranged on the guide rods (15), two third elastic pieces (17) are connected between the anti-collision plates (16) and the protection frame (14), the third elastic pieces (17) are sleeved on the guide rods (15), and two ends of each third elastic piece (17) are respectively connected with the protection frame (14) and the anti-collision plates (16).

3. An aeronautical survey instrument with floor buffer function according to claim 2, characterized by further comprising a button (18) and an alarm (19), wherein the button (18) is arranged on the protective frame (14) at uniform intervals in a sliding manner, the alarm (19) is arranged on the mounting rod (2) in an embedded manner, and the alarm (19) is electrically connected with the button (18).

4. The aviation mapping device with the floor buffering function according to claim 3, further comprising a protection seat (20), clamping blocks (21), a protection cover (22) and clamping blocks (23), wherein the protection seat (20) is fixedly connected to the control console (1), two clamping blocks (21) are installed on the protection seat (20), a protection cover (22) is placed on the protection seat (20), two clamping blocks (23) are rotatably arranged on the protection cover (22), and the clamping blocks (21) are clamped with the clamping blocks (23).

5. The aerial survey instrument with the floor buffer function according to claim 4, further comprising a transparent protective cover (24), wherein the transparent protective cover (24) is fixedly connected to the survey instrument body (6).

6. The airborne survey and drawing instrument with the floor buffer function according to claim 5, further comprising a reinforcing rod (25), wherein the reinforcing rod (25) is fixedly connected between the two vertically aligned fixed cylinders.