CN215884107U

CN215884107U - Engineering monitoring is with unmanned aerial vehicle fixed bolster for supervisory equipment that has shock-absorbing function

Info

Publication number: CN215884107U
Application number: CN202122630381.XU
Authority: CN
Inventors: 诸葛政桦; 沈磊; 蒋金霞; 石晶; 谭清清; 顾红生
Original assignee: Zhejiang Jiangnan Engineering Management Co ltd
Current assignee: Zhejiang Jiangnan Engineering Management Co ltd
Priority date: 2021-10-29
Filing date: 2021-10-29
Publication date: 2022-02-22
Anticipated expiration: 2031-10-29

Abstract

The utility model discloses a fixed support for unmanned aerial vehicle monitoring equipment with a damping function for engineering monitoring, which comprises a fixed base, wherein a first fixed rod is movably installed on the outer side of the fixed base, a filtering and vibrating frame is movably installed at one end of the first fixed rod, a second fixed rod is movably installed on one side of the filtering and vibrating frame, an arc-shaped fixed plate is movably installed at one end of the second fixed rod, a rubber pad is movably installed on the inner side of the arc-shaped fixed plate, and lantern rings are fixedly installed on the outer side surfaces of the fixed base and the arc-shaped fixed plate. The fixing support for the unmanned aerial vehicle monitoring equipment with the shock absorption function for engineering monitoring can filter the shock generated by the operation of the unmanned aerial vehicle, improve the shooting stability of the monitoring equipment, and change the connection mode between the fixing support and the unmanned aerial vehicle so that the fixing support can be fixed with the support legs of the unmanned aerial vehicles with different diameters, thereby enabling one monitoring equipment to be used on unmanned aerial vehicles with different models.

Description

Engineering monitoring is with unmanned aerial vehicle fixed bolster for supervisory equipment that has shock-absorbing function

Technical Field

The utility model relates to the field of fixed supports, in particular to a fixed support for unmanned aerial vehicle monitoring equipment with a damping function for engineering monitoring.

Background

The engineering monitoring is that in the construction process of building structures, the technical means of monitoring various control indexes of key parts by adopting a monitoring instrument can check and ensure the safety and the reasonability of engineering construction, and the pilotless aircraft is called an unmanned aerial vehicle for short, is an unmanned aerial vehicle operated by utilizing radio remote control equipment and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, and is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster rescue, wild animal observation, monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like, so that the use of the unmanned aerial vehicle is greatly expanded, and developed countries also actively expand the industrial application and develop the unmanned aerial vehicle technology; there is certain drawback in the use of fixed bolster for unmanned aerial vehicle monitoring facilities of current engineering monitoring usefulness, directly adopt the bolt-up in the unmanned aerial vehicle below, when monitoring the picture, can be influenced by the vibrations that unmanned aerial vehicle operation produced, the picture that makes the shooting is unstable, can not clearly carry out the picture monitoring to building site, and the construction site of difference, unmanned aerial vehicle's model is also different, single unmanned aerial vehicle can only be connected with model assorted shooting device unable adjustment base, the unable adjustment base that makes the shooting device is applicable to multiple unmanned aerial vehicle.

SUMMERY OF THE UTILITY MODEL

The utility model mainly aims to provide a fixing support for unmanned aerial vehicle monitoring equipment with a damping function for engineering monitoring, which can effectively solve the problems in the background technology.

In order to achieve the purpose, the utility model adopts the technical scheme that:

the utility model provides an engineering monitoring is with fixed bolster for unmanned aerial vehicle monitoring facilities that has shock-absorbing function, includes unable adjustment base, unable adjustment base outside movable mounting has the dead lever No. one, No. one dead lever one end movable mounting strains the shake frame, strain shake frame one side movable mounting have the dead lever No. two, No. two dead lever one end movable mounting has the arc fixed plate, the inboard movable mounting of arc fixed plate has the rubber pad, unable adjustment base with the equal fixed mounting in arc fixed plate outside surface has the lantern ring, lantern ring one side surface activity embedding installs the screw thread inserted bar.

Preferably, a position of one side surface of the lantern ring, one side surface of the first fixing rod and one side surface of the second fixing rod close to one end is provided with a limiting groove, and the threaded insertion rod is movably inserted into the limiting groove.

Preferably, the surface of the outer side of the threaded inserted rod is fixedly provided with a limiting strip, the threaded inserted rod passes through the limiting strip and the limiting groove is movably connected, and the surface of the outer side of the threaded inserted rod is close to one end and is movably provided with a nut.

Preferably, strain and shake frame side surface movable embedding and install the connecting block, strain the inside fixed surface of shake frame and install the buffer block, the buffer block with connecting block fixed connection, strain the inside movable mounting of shake frame and have return spring, the equal fixed mounting in return spring both ends has rubber base, return spring passes through rubber base respectively with strain shake frame with connecting block fixed connection.

Preferably, strain and shake the frame with equal fixed mounting in connecting block one end surface has the carriage, the through-hole has all been seted up to carriage, dead lever No. one and No. two dead lever opposite side surfaces, a dead lever passes through the carriage with strain and shake frame swing joint, No. two dead levers pass through the carriage with connecting block swing joint, the inside activity of through-hole alternates there is a fastener.

Preferably, the outer side surface of the arc-shaped fixing plate is fixedly provided with a second lantern ring, a second fastener is movably inserted into the surface of one side of the second lantern ring, the inner side surface of the arc-shaped fixing plate is provided with a sliding groove, the outer side surface of the rubber pad is fixedly provided with a sliding strip, and the rubber pad is movably connected with the sliding groove through the sliding strip.

Compared with the prior art, the utility model has the following beneficial effects:

in the utility model, monitoring equipment is fixed on the lower surface of a fixed base, two arc-shaped fixed plates are clamped on the surface of a support leg of an unmanned aerial vehicle, a second fastener is inserted into a second sleeve ring to fix the second sleeve ring by the second fastener, one end of a second fixed rod is clamped between the two sleeve rings, the angle between the sleeve ring and the second fixed rod is adjusted, a threaded inserted rod is inserted into a limiting groove, a nut is screwed on the surface of the threaded inserted rod, the second fixed rod and the sleeve ring are fixed by the matching of a limiting strip and the limiting groove, and the first fixed rod and the sleeve ring are fixed in the same way, when the device is used, vibration generated by the unmanned aerial vehicle is buffered by a rubber pad and then transmitted to the second fixed rod and a connecting block by the arc-shaped fixed plates, a return spring enables the connecting block to slightly move, the contact between the connecting block and a filtering and vibrating frame is reduced, and the vibration of the connecting block is further absorbed by a rubber base and a buffer block, the vibrations that make the connecting block are straining the inside elimination of shake frame, thereby the vibrations that produce when can avoiding unmanned aerial vehicle flight drive monitoring facilities vibrations together, reduce unmanned aerial vehicle to monitoring facilities's influence, make the picture of shooting stable, improve monitoring facilities's shooting stability, swing joint through draw runner and spout, make the rubber pad dismantle fast and the installation, then change the rubber pad of different thickness, it can be fixed with the unmanned aerial vehicle stabilizer blade of different diameters to make a monitoring facilities can use on the unmanned aerial vehicle of different models.

Drawings

Fig. 1 is a schematic overall structure diagram of a fixing bracket for an unmanned aerial vehicle monitoring device with a damping function for engineering monitoring, according to the present invention;

fig. 2 is a view of a fixing bracket for an unmanned aerial vehicle monitoring device with a damping function for engineering monitoring according to the present invention;

fig. 3 is a view of a fixing bracket for an unmanned aerial vehicle monitoring device with a damping function for engineering monitoring according to the present invention;

fig. 4 is a view of a fixing bracket for an unmanned aerial vehicle monitoring device with a damping function for engineering monitoring according to the present invention.

In the figure: 1. a fixed base; 101. a collar; 102. a limiting groove; 2. a first fixing rod; 201. a second fixing rod; 202. a through hole; 203. a fastener number one; 3. a vibration filtering frame; 301. a connecting frame; 302. a rubber base; 303. a buffer block; 304. connecting blocks; 305. a return spring; 4. an arc-shaped fixing plate; 401. a chute; 402. a second lantern ring; 403. a fastener number two; 5. a rubber pad; 501. a slide bar; 6. a threaded bayonet; 601. a limiting strip; 602. and a nut.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the utility model easy to understand, the utility model is further described with the specific embodiments.

As shown in fig. 1-4, a fixed bracket for an unmanned aerial vehicle monitoring device with a shock absorption function for engineering monitoring comprises a fixed base 1, wherein a first fixed rod 2 is movably installed on the outer side of the fixed base 1, a first filtering and vibrating frame 3 is movably installed at one end of the first fixed rod 2, a second fixed rod 201 is movably installed on one side of the filtering and vibrating frame 3, an arc-shaped fixed plate 4 is movably installed at one end of the second fixed rod 201, a rubber pad 5 is movably installed on the inner side of the arc-shaped fixed plate 4, lantern rings 101 are fixedly installed on the outer side surfaces of the fixed base 1 and the arc-shaped fixed plate 4, and threaded insertion rods 6 are movably embedded into the surface of one side of the lantern rings 101;

limiting grooves 102 are formed in the surfaces of one side of the lantern ring 101, one side of the first fixing rod 2 and one side of the second fixing rod 201 close to one end, and the threaded insertion rod 6 is movably inserted into the limiting grooves 102; the outer side surface of the threaded insert rod 6 is fixedly provided with a limiting strip 601, the threaded insert rod 6 is movably connected with the limiting groove 102 through the limiting strip 601, and a nut 602 is movably arranged at one end, close to the outer side surface of the threaded insert rod 6; the connecting block 304 is movably embedded in the surface of one side of the filtering and vibrating frame 3, the buffer block 303 is fixedly installed on the surface inside the filtering and vibrating frame 3, the buffer block 303 is fixedly connected with the connecting block 304, the return spring 305 is movably installed inside the filtering and vibrating frame 3, the rubber bases 302 are fixedly installed at two ends of the return spring 305, and the return spring 305 is fixedly connected with the filtering and vibrating frame 3 and the connecting block 304 through the rubber bases 302 respectively, so that the monitoring equipment is prevented from being driven to vibrate together by vibration generated during flying of the unmanned aerial vehicle, the influence of the unmanned aerial vehicle on the monitoring equipment is reduced, and the shot picture is stable; a connecting frame 301 is fixedly arranged on one end surface of each of the filtering and vibrating frame 3 and the connecting block 304, through holes 202 are formed in the other side surfaces of the connecting frame 301, the first fixing rod 2 and the second fixing rod 201, the first fixing rod 2 is movably connected with the filtering and vibrating frame 3 through the connecting frame 301, the second fixing rod 201 is movably connected with the connecting block 304 through the connecting frame 301, and a first fastener 203 is movably inserted in each through hole 202; 4 outside fixed surfaces of arc fixed plate have No. two lantern rings 402, No. two lantern rings 402 side surface activity interlude has No. two fasteners 403, spout 401 has been seted up to 4 inside surfaces of arc fixed plate, 5 outside fixed surfaces of rubber pad have draw runner 501, rubber pad 5 passes through draw runner 501 and spout 401 swing joint, change the rubber pad 5 of different thickness, it can be fixed with the unmanned aerial vehicle stabilizer blade of different diameters to make unable adjustment base 1, thereby make a monitoring facilities can use on the unmanned aerial vehicle of different models.

The utility model is a fixing bracket for unmanned aerial vehicle monitoring equipment with shock absorption function for engineering monitoring, when in installation, the monitoring equipment is fixed on the lower surface of a fixing base 1, two arc-shaped fixing plates 4 are clamped on the surface of a support leg of an unmanned aerial vehicle, a second fastening piece 403 is inserted into a second sleeve ring 402, the second fastening piece 403 fixes the second sleeve ring 402, one end of a second fixing rod 201 is clamped between the two sleeve rings 101, the angle between the sleeve ring 101 and the second fixing rod 201 is adjusted, a threaded inserted rod 6 is inserted into a limiting groove 102, a nut 602 is screwed on the surface of the threaded inserted rod 6, the second fixing rod 201 and the sleeve ring 101 are fixed through the fit of a limiting strip 601 and the limiting groove 102, and similarly, a first fixing rod 2 and the sleeve ring 101 are fixed, when in use, the shock generated by the unmanned aerial vehicle is buffered by a rubber pad 5 and then transmitted to the second fixing rod 201 and a connecting block 304 through the arc-shaped fixing plate 4, return spring 305 makes connecting block 304 can slightly remove, reduce connecting block 304 and strain the contact between the shake frame 3, simultaneously reduce the vibrations of connecting block 304, the further absorption of rethread rubber base 302 and buffer block 303, make the vibrations of connecting block 304 strain the inside elimination of shake frame 3, thereby the vibrations that produce when can avoiding unmanned aerial vehicle to fly drive monitoring facilities vibrations together, reduce unmanned aerial vehicle to monitoring facilities's influence, make the picture of shooing stable, improve monitoring facilities's shooting stability, swing joint through draw runner 501 and spout 401, make rubber pad 5 dismantle fast and install, then change rubber pad 5 of different thickness, it can be fixed with the unmanned aerial vehicle stabilizer blade of different diameters to make a monitoring facilities can use on the unmanned aerial vehicle of different models.

The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides an engineering monitoring is with unmanned aerial vehicle fixed bolster for supervisory equipment that has shock-absorbing function, its characterized in that: including unable adjustment base (1), unable adjustment base (1) outside movable mounting has dead lever (2) No. one, dead lever (2) one end movable mounting strains and shakes frame (3), strain and shake frame (3) one side movable mounting and have dead lever (201) No. two, No. two dead lever (201) one end movable mounting has arc fixed plate (4), arc fixed plate (4) inboard movable mounting has rubber pad (5), unable adjustment base (1) with arc fixed plate (4) outside surface equal fixed mounting has lantern ring (101), screw thread inserted bar (6) are installed in the embedding of lantern ring (101) one side surface activity.

2. The engineering monitoring is with fixed bolster for unmanned aerial vehicle supervisory equipment that has shock-absorbing function of claim 1, characterized in that: limiting grooves (102) are formed in the positions, close to one end, of one side surface of the lantern ring (101), one side surface of the first fixing rod (2) and one side surface of the second fixing rod (201), and the threaded insertion rod (6) is movably inserted into the limiting grooves (102).

3. The engineering monitoring is with fixed bolster for unmanned aerial vehicle supervisory equipment that has shock-absorbing function of claim 2, characterized in that: the utility model discloses a nut, including screw thread inserted bar (6), spacing strip (601) is installed to screw thread inserted bar (6) outside fixed surface, screw thread inserted bar (6) pass through spacing strip (601) with spacing groove (102) swing joint, screw thread inserted bar (6) outside surface is close one end department movable mounting and is had nut (602).

4. The engineering monitoring is with fixed bolster for unmanned aerial vehicle supervisory equipment that has shock-absorbing function of claim 3, characterized in that: strain and shake frame (3) one side surface activity embedding and install connecting block (304), strain and shake frame (3) inside fixed surface and install buffer block (303), buffer block (303) with connecting block 304 fixed connection, strain and shake frame (3) inside movable mounting have return spring (305), the equal fixed mounting in return spring (305) both ends has rubber base (302), return spring (305) pass through rubber base (302) respectively with strain shake frame (3) with connecting block (304) fixed connection.

5. The engineering monitoring is with fixed bolster for unmanned aerial vehicle monitoring equipment that has shock-absorbing function of claim 4, characterized in that: strain shake frame (3) with equal fixed mounting in connecting block (304) one end surface has connecting frame (301), dead lever (2) and through-hole (202) have all been seted up to No. two dead lever (201) opposite side surfaces, dead lever (2) pass through connecting frame (301) with strain shake frame (3) swing joint, No. two dead lever (201) pass through connecting frame (301) with connecting block (304) swing joint, through-hole (202) inside activity is interlude has fastener (203).

6. The engineering monitoring is with fixed bolster for unmanned aerial vehicle monitoring equipment that has shock-absorbing function of claim 5, characterized in that: arc fixed plate (4) outside fixed surface installs No. two lantern rings (402), No. two lantern rings (402) one side surface activity interlude has No. two fasteners (403), spout (401) have been seted up to arc fixed plate (4) inside surface, rubber pad (5) outside fixed surface installs draw runner (501), rubber pad (5) pass through draw runner (501) with spout (401) swing joint.