CN217731268U - Engineering investigation unmanned aerial vehicle's conveyer - Google Patents

Abstract

The utility model provides an engineering investigation unmanned aerial vehicle's conveyer, belong to the unmanned air vehicle technique field, this engineering investigation unmanned aerial vehicle's conveyer includes the base, fixed connection is at the box of base upper surface and articulates the chamber door in the box front side through the hinge, the lower part sliding connection of box inside wall has the backup pad, the left and right sides of backup pad is provided with first buffering subassembly, fixedly connected with supporting seat in the backup pad, the downside of supporting seat links to each other through the interior diapire of second buffering subassembly with the box, two standing grooves of bilateral symmetry are seted up to the upside of supporting seat. This engineering investigation unmanned aerial vehicle's conveyer, in the unmanned aerial vehicle transportation, when taking place to jolt the collision, through the cooperation of first buffering subassembly and second buffering subassembly, the backup pad drives unmanned aerial vehicle through the supporting seat and reciprocates, can effectual reduction in the impact vibrations that vertical direction caused, improved the buffering effect greatly, and then guarantee unmanned aerial vehicle inner structure's safety and stability.

Description

Engineering reconnaissance unmanned aerial vehicle's conveyer

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to engineering investigation unmanned aerial vehicle's conveyer.

Background

Along with the development of unmanned aerial vehicle technique, also improve gradually unmanned aerial vehicle's transportation requirement, current unmanned aerial vehicle equipment transportation usually is mainly with direct vanning, but unmanned aerial vehicle structure is complicated, in the transportation, if receive the striking of jolting, can influence unmanned aerial vehicle's inner structure, leads to unmanned aerial vehicle's damage.

The retrieval discovery discloses an unmanned aerial vehicle transportation device in a Chinese patent with an authorization publication number of CN202020974609.X, which comprises a box body, wherein a box cover is hinged to the top of the box body, a placing table is arranged in the box body, placing openings are formed in the left side and the right side of the top of the placing table, a lead screw is rotatably connected in the placing table, a rotating rod is rotatably connected to the right side of the top of the placing table, a rotating disc is fixedly connected to the top end of the rotating rod, the bottom end of the rotating rod extends into the placing table and is sleeved with a first bevel gear, a second bevel gear is sleeved at the left end of the lead screw and is meshed with the first bevel gear, moving blocks are connected to the outer sides of the two ends of the lead screw in a threaded manner, and clamping plates are fixedly connected to the tops of the two moving blocks. The utility model discloses a, solved that the unmanned aerial vehicle structure is complicated in the transportation, if receive the striking, can influence unmanned aerial vehicle's inner structure, lead to the problem of unmanned aerial vehicle damage.

However, above-mentioned technical scheme still has following defect, in the vanning transportation, because unmanned aerial vehicle realizes the holistic fixed of unmanned aerial vehicle through fixed landing leg, under inertial effect, the horizontal direction's that unmanned aerial vehicle received impact force need offset through the landing leg, offsets the wearing and tearing aggravation that the impact force leads to landing leg and junction for a long time, damages the landing leg even easily, seriously influences subsequent safe in utilizationly.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an engineering reconnaissance unmanned aerial vehicle's conveyer aims at solving the fragile problem of horizontal impact force aggravation landing leg wearing and tearing among the prior art.

In order to achieve the above purpose, the utility model provides a following technical scheme: the utility model provides an engineering investigation unmanned aerial vehicle's conveyer, includes base, fixed connection at the box of base upper surface and articulates the chamber door in the box front side through the hinge, the lower part sliding connection of box inside wall has the backup pad, the left and right sides of backup pad is provided with first buffering subassembly, fixedly connected with supporting seat in the backup pad, the downside of supporting seat links to each other with the inner bottom wall of box through second buffering subassembly, two standing grooves of bilateral symmetry are seted up to the upside of supporting seat, two the spacing groove has all been seted up to the opposite side of standing groove, sliding connection has the gag lever post, two in the spacing groove the looks remote site of gag lever post all is provided with adjusting part, the equal fixedly connected with erection column in the left and right sides of backup pad, can dismantle in the erection column and be connected with the mounting bracket, the installation pipe that two symmetries of the interior roof fixedly connected with of mounting bracket set up, sliding connection has the rack, two in the installation pipe the equal fixedly connected with L type splint of the looks back end of rack, the middle part of mounting bracket is provided with drive assembly.

In order to make this engineering reconnaissance unmanned aerial vehicle's conveyer reach the effect of being convenient for to access spare part, as the utility model relates to a preferred, the symmetry is provided with two storing boxes in the base, one side of diapire has the lid through hinge joint in the storing box, the surface of lid is provided with the handle.

In order to make this engineering reconnaissance unmanned aerial vehicle's conveyer reach the effect of guarantee backup pad mobility stability, as the utility model relates to an it is preferred, first buffering subassembly is including the fixed plate that the symmetry set up in the backup pad left and right sides respectively, the equal fixedly connected with buffering box in both sides of box corresponding fixed plate, fixed plate sliding connection is at the inside wall of buffering box, the upper and lower both sides of fixed plate all link to each other with the buffering box through first spring.

In order to make this engineering investigation unmanned aerial vehicle's conveyer reach the effect that can effectively cushion, conduct the utility model relates to an it is preferred, second buffering subassembly includes the telescopic link of fixed connection at the supporting seat lower surface, the bottom fixed connection of telescopic link is at the interior diapire of box, the surface cover of telescopic link is equipped with the second spring.

In order to make this engineering reconnaissance unmanned aerial vehicle's conveyer reach the effect of being convenient for adjust the use, as the utility model relates to an it is preferred, adjusting part includes the branch of fixed connection at two gag lever post looks remote sites, the front side that the supporting seat corresponds the spacing groove open be equipped with the groove of stepping down of spacing groove intercommunication, the one end of branch is through the outside that the groove extended to the supporting seat of stepping down, two the equal fixedly connected with third spring of opposite side of branch, the other end fixed connection of third spring is on the inside wall that corresponds the groove of stepping down.

In order to make this engineering reconnaissance unmanned aerial vehicle's conveyer reach the effect that improves and use the flexibility, as the utility model relates to an it is preferred, the both ends of mounting bracket can sliding connection at the inside wall that corresponds the erection column, set up the mounting hole along vertical direction equipartition on the erection column, set up the locating hole with mounting hole looks adaptation on the mounting bracket, it has the bolt to peg graft in mounting hole and the locating hole that corresponds.

In order to make this engineering reconnaissance unmanned aerial vehicle's conveyer reach the effect of the operation of being convenient for, as the utility model relates to an it is preferred, drive assembly is including the T type dwang that runs through the mounting bracket middle part, the bottom fixedly connected with gear of T type dwang, two the connector has all been seted up to one side that the installation pipe corresponds the gear, the gear is connected with the rack toothing who corresponds respectively through two connectors.

In order to make this engineering reconnaissance unmanned aerial vehicle's conveyer reach the effect that improves transportation security, as the utility model relates to an it is preferred, the upside of supporting seat all is provided with first rubber pad, two with the downside of gag lever post the opposite side of L type splint all is provided with the second rubber pad.

Compared with the prior art, the beneficial effects of the utility model are that:

1. this engineering reconnaissance unmanned aerial vehicle's conveyer, in the unmanned aerial vehicle transportation, when taking place to jolt the collision, cooperation through first buffering subassembly and second buffering subassembly, the backup pad drives unmanned aerial vehicle through the supporting seat and reciprocates, can effectual reduction the impact vibrations that cause in vertical direction, the buffering effect has been improved greatly, and then the safety and stability of guarantee unmanned aerial vehicle inner structure, and simultaneously, through the erection column, the cooperation of mounting bracket and L type splint, hold unmanned aerial vehicle with the holding through two L type splint and fix on the supporting seat, unmanned aerial vehicle follows supporting seat synchronous motion, effectually avoided the wearing and tearing that cause the unmanned aerial vehicle landing leg because of the horizontal direction impact force, guarantee the transportation safety of unmanned aerial vehicle landing leg, thereby guarantee the fail safe nature of follow-up use, the practicality of conveyer transportation unmanned aerial vehicle has been improved greatly.

2. This engineering investigation unmanned aerial vehicle's conveyer, cooperation through standing groove and gag lever post, can be firm fix the unmanned aerial vehicle landing leg in the standing groove, it is simple more high-efficient to control the gag lever post through adjusting part simultaneously, be convenient for unmanned aerial vehicle's loading and unloading, through the cooperation through erection column and mounting bracket, can adjust the height that L splint were placed in a flexible way, thereby guarantee safe effectual fixed unmanned aerial vehicle that holds with, cooperation through installation pipe and rack, drive two rack synchronous motion through drive assembly, it is more convenient high-efficient to control the regulation, be favorable to improving operator's work efficiency, it is higher to use nimble adaptability.

3. This engineering reconnaissance unmanned aerial vehicle's conveyer, store the box through setting up two in the base, with unmanned aerial vehicle detachable spare part, like paddle and camera etc. and the instrument that uses leaves respectively in two storing boxes, access simple and convenient when the guarantee is deposited safety, the effectual spare part that causes when having avoided the whole transportation of unmanned aerial vehicle damages, thereby guarantee unmanned aerial vehicle's normal use, can also be convenient for change maintenance spare part simultaneously.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention. In the drawings:

fig. 1 is a front isometric view of the present invention;

FIG. 2 is a front cut-away view of the present invention;

FIG. 3 is a right sectional plan view of the present invention;

FIG. 4 is a sectional plan view of the buffer box, the supporting seat and the box body of the present invention;

fig. 5 is a top sectional plan view of the present invention;

fig. 6 is a cut-away view of the rack, the gear and the L-shaped clamp plate of the present invention.

In the figure: 1. a base; 2. a box body; 3. a box door; 4. a support plate; 5. a supporting seat; 6. a placement groove; 7. a limiting groove; 8. a limiting rod; 9. mounting a column; 10. a mounting frame; 11. installing a pipe; 12. a rack; 13. an L-shaped splint; 14. a storage box; 15. a fixing plate; 16. a buffer box; 17. a first spring; 18. a telescopic rod; 19. a second spring; 20. a strut; 21. a third spring; 22. mounting holes; 23. positioning holes; 24. a bolt; 25. a T-shaped rotating rod; 26. a gear; 27. a first rubber pad; 28. a second rubber cushion.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.

Referring to fig. 1-6, the present invention provides the following technical solutions: the utility model provides an engineering reconnaissance unmanned aerial vehicle's conveyer, the on-line screen storage device comprises a base 1, fixed connection is at the box 2 of 1 upper surface of base and articulates the chamber door 3 in box 2 front side through the hinge, the lower part sliding connection of the 2 inside walls of box has backup pad 4, the left and right sides of backup pad 4 is provided with first buffering subassembly, fixedly connected with supporting seat 5 on the backup pad 4, the downside of supporting seat 5 links to each other with the inner bottom wall of box 2 through second buffering subassembly, bilateral symmetry's two standing grooves 6 have been seted up to the upside of supporting seat 5, spacing groove 7 has all been seted up to the opposite side of two standing grooves 6, sliding connection has gag lever post 8 in the gag lever post 7, the looks remote site of two gag lever posts 8 all is provided with adjusting part, the equal fixedly connected with erection column 9 in the left and right sides of backup pad 4, can dismantle in the erection column 9 and be connected with mounting bracket 10, the installation pipe 11 that two symmetries of the interior roof fixedly connected with of mounting bracket 10 set up, sliding connection has rack 12 in installation pipe 11, the equal fixedly connected with L type splint 13 of the looks back end of two rack 12, the middle part of mounting bracket 10 is provided with drive assembly.

The utility model discloses an in the embodiment, during transportation unmanned aerial vehicle, open chamber door 3 and place unmanned aerial vehicle's landing leg in standing groove 6 on supporting seat 5, drive two gag lever post 8 at spacing inslot 7 synchronous motion through adjusting part simultaneously, thereby fix the unmanned aerial vehicle landing leg in standing groove 6, then place the height according to unmanned aerial vehicle, cooperation through erection column 9 and mounting bracket 10, adjust the fixed height of mounting bracket 10, thereby adjust the height that two L type splint 13 were placed, guarantee that two L type splint 13 can be safe effectual fixed unmanned aerial vehicle of centre gripping, then drive two rack 12 synchronous motion in the installation pipe 11 through drive assembly, it is fixed with the unmanned aerial vehicle centre gripping. In the transportation, cooperation through first buffering subassembly and second buffering subassembly, when taking place the collision of jolting, backup pad 4 drives supporting seat 5 and reciprocates, thereby effectual reduction is because of the impact vibrations that the collision of jolting caused at vertical direction, improve the buffering effect in the transportation greatly, guarantee unmanned aerial vehicle inner structure's safety and stability, fix unmanned aerial vehicle with holding through two L type splint 13 simultaneously on supporting seat 5, the stability that unmanned aerial vehicle placed has been improved greatly, because of the wearing and tearing that the horizontal direction impact force caused the unmanned aerial vehicle landing leg when can effectually avoiding the collision of jolting, guarantee the transportation safety of unmanned aerial vehicle landing leg, thereby guarantee the security in the follow-up use of unmanned aerial vehicle, the practicality is stronger.

Specifically, base 1 internal symmetry is provided with two storing boxes 14, and one side of diapire has the lid through hinge joint in the storing box 14, and the surface of lid is provided with the handle. Open and close the lid through the handle, then with unmanned aerial vehicle detachable spare part, like paddle and camera etc to and the instrument of using leaves respectively in two storing boxes 14, the safety of depositing in the guarantee transportation, access simple and convenient, the effectual spare part damage that causes when having avoided unmanned aerial vehicle whole transportation.

Specifically, first buffering subassembly is including the fixed plate 15 that the symmetry set up respectively in the 4 left and right sides of backup pad, and the equal fixedly connected with buffering box 16 in both sides that box 2 corresponds fixed plate 15, and fixed plate 15 sliding connection is at the inside wall of buffering box 16, and the upper and lower both sides of fixed plate 15 all link to each other with buffering box 16 through first spring 17. Through the cooperation of fixed plate 15 and buffering box 16, reciprocate the in-process at backup pad 4 and can provide good direction supporting role, the first spring 17 of both sides about the fixed plate 15 of cooperation simultaneously can play good buffering effect to the stability that support plate 4 removed is ensured.

Specifically, the second buffering subassembly includes telescopic link 18 of fixed connection at the supporting seat 5 lower surface, and the bottom fixed connection of telescopic link 18 is at the interior diapire of box 2, and the surface cover of telescopic link 18 is equipped with second spring 19. Telescopic link 18 is established by a section of body of rod and is constituteed on another section of body of rod, through telescopic link 18 and 19 cooperation of second spring, under the effect of 19 elasticity of second spring, supporting seat 5 reciprocates the in-process and can effectual buffering impact force to ensure unmanned aerial vehicle inner structure's safety.

Concretely, the adjusting part includes branch 20 of fixed connection at two 8 looks remote ends of gag lever post, and support seat 5 opens the front side that corresponds spacing groove 7 and is equipped with the groove of stepping down that communicates with spacing groove 7, and branch 20's one end extends to the outside of support seat 5 through the groove of stepping down, the equal fixedly connected with third spring 21 of opposite side of two branch 20, and the other end fixed connection of third spring 21 is on the inside wall that corresponds the groove of stepping down. Promote two branch 20, drive two gag lever post 8 relative movement in the spacing groove 7 that corresponds, then put into the unmanned aerial vehicle landing leg standing groove 6, under the effect of third spring 21 elasticity, gag lever post 8 automatic re-setting to fixed the unmanned aerial vehicle landing leg, the stability of placing is ensured, places and takes out unmanned aerial vehicle simple and convenient, the operator's of being convenient for regulation is used.

Specifically, both ends of the mounting frame 10 can be slidably connected to the inner side wall of the corresponding mounting column 9, mounting holes 22 uniformly distributed along the vertical direction are formed in the mounting column 9, positioning holes 23 matched with the mounting holes 22 are formed in the mounting frame 10, and a bolt 24 is inserted into each of the mounting holes 22 and the corresponding positioning holes 23. Through the cooperation of mounting hole 22 and locating hole 23, after mounting bracket 10 removed suitable height in erection column 9, insert corresponding mounting hole 22 and locating hole 23 through bolt 24 in, accomplish mounting bracket 10's fixed, can adjust mounting bracket 10 fixed height in a flexible way to satisfy the user demand that not co-altitude unmanned aerial vehicle placed, the effectual nimble adaptability that improves the use.

Specifically, the driving assembly comprises a T-shaped rotating rod 25 penetrating through the middle of the mounting frame 10, a gear 26 is fixedly connected to the bottom end of the T-shaped rotating rod 25, connectors are respectively formed on one sides of the two mounting pipes 11 corresponding to the gear 26, and the gear 26 is respectively meshed with the corresponding racks 12 through the two connectors. Through the cooperation of gear 26 and two racks 12, drive gear 26 forward or antiport through T type dwang 25, then drive two relative or mutually opposite directions removals of rack 12, centre gripping that can be quick or dismantle unmanned aerial vehicle, the operation is convenient high efficiency more.

Specifically, the upper side of the supporting seat 5 and the lower side of the limiting rod 8 are both provided with a first rubber pad 27, and the opposite sides of the two L-shaped clamping plates 13 are both provided with a second rubber pad 28. Through first rubber pad 27 and second rubber pad 28, wearing and tearing in can effectual reduction unmanned aerial vehicle transportation improve the protection effect.

In the description of the present invention, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, e.g., as being fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.

Claims (8)

1. The utility model provides an engineering investigation unmanned aerial vehicle's conveyer, includes base, fixed connection at the box of base upper surface and articulates the chamber door in the box front side through the hinge, its characterized in that: the lower part sliding connection of box inside wall has the backup pad, the left and right sides of backup pad is provided with first buffering subassembly, fixedly connected with supporting seat in the backup pad, the downside of supporting seat links to each other through the inner bottom wall of second buffering subassembly with the box, two standing grooves of bilateral symmetry are seted up to the upside of supporting seat, two the spacing groove has all been seted up to the opposite side of standing groove, sliding connection has the gag lever post in the spacing groove, two the looks remote site of gag lever post all is provided with adjusting part, the equal fixedly connected with erection column in the left and right sides of backup pad, can dismantle in the erection column and be connected with the mounting bracket, the installation pipe that two symmetries of interior roof fixedly connected with of mounting bracket set up, sliding connection has the rack in the installation pipe, two the equal fixedly connected with L type splint in the back of the looks end of rack, the middle part of mounting bracket is provided with drive assembly.

2. The transportation device of engineering investigation unmanned aerial vehicle of claim 1, characterized in that: the base is internally and symmetrically provided with two storage boxes, one side of the inner bottom wall of each storage box is hinged to a box cover through a hinge, and a handle is arranged on the outer surface of the box cover.

3. The transportation device of engineering investigation unmanned aerial vehicle of claim 1, characterized in that: first buffering subassembly is including the fixed plate that the symmetry set up in the backup pad left and right sides respectively, the equal fixedly connected with buffering box in both sides of the box corresponding fixed plate, fixed plate sliding connection is at the inside wall of buffering box, the upper and lower both sides of fixed plate all link to each other with the buffering box through first spring.

4. The transportation device of engineering investigation unmanned aerial vehicle of claim 1, characterized in that: the second buffering subassembly includes the telescopic link of fixed connection at the supporting seat lower surface, the bottom fixed connection of telescopic link is at the interior diapire of box, the surface cover of telescopic link is equipped with the second spring.

5. The transportation device of engineering investigation unmanned aerial vehicle of claim 1, characterized in that: the adjusting part includes the branch of fixed connection at two gag lever post looks remote ends, the front side that the supporting seat corresponds the spacing groove open be equipped with the groove of stepping down of spacing groove intercommunication, the one end of branch is through the outside that the groove extended to the supporting seat of stepping down, two the equal fixedly connected with third spring of opposite side of branch, the other end fixed connection of third spring is on the inside wall that corresponds the groove of stepping down.

6. The transportation device of engineering investigation unmanned aerial vehicle of claim 1, characterized in that: the utility model discloses a mounting bracket, including mounting bracket, locating hole, locating pin, mounting bracket, locating hole and corresponding locating hole, the both ends of mounting bracket can sliding connection at the inside wall that corresponds the erection column, set up the mounting hole along vertical direction equipartition on the erection column, set up the locating hole with mounting hole looks adaptation on the mounting bracket, it has the bolt to peg graft in mounting hole and the locating hole that corresponds.

7. The transportation device of engineering investigation unmanned aerial vehicle of claim 1, characterized in that: the drive assembly is including the T type dwang that runs through the mounting bracket middle part, the bottom fixedly connected with gear of T type dwang, two the connector has all been seted up to one side that the installation pipe corresponds the gear, the gear is connected with the rack toothing who corresponds respectively through two connectors.

8. The transportation device of an engineering exploration unmanned aerial vehicle as claimed in any one of claims 1-7, wherein: the upside of supporting seat all is provided with first rubber pad with the downside of gag lever post, two the opposite side of L type splint all is provided with the second rubber pad.

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