CN117566113A - Unmanned aerial vehicle loading platform shock mounting - Google Patents

Unmanned aerial vehicle loading platform shock mounting Download PDF

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Publication number
CN117566113A
CN117566113A CN202311727126.4A CN202311727126A CN117566113A CN 117566113 A CN117566113 A CN 117566113A CN 202311727126 A CN202311727126 A CN 202311727126A CN 117566113 A CN117566113 A CN 117566113A
Authority
CN
China
Prior art keywords
aerial vehicle
unmanned aerial
assembly
buffer
loading platform
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202311727126.4A
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Chinese (zh)
Inventor
谢余龙
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Yizhi Aviation Talent Technology Cooperation Wuhu Co ltd
Original Assignee
Yizhi Aviation Talent Technology Cooperation Wuhu Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Yizhi Aviation Talent Technology Cooperation Wuhu Co ltd filed Critical Yizhi Aviation Talent Technology Cooperation Wuhu Co ltd
Priority to CN202311727126.4A priority Critical patent/CN117566113A/en
Publication of CN117566113A publication Critical patent/CN117566113A/en
Pending legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00—Ground or aircraft-carrier-deck installations
    • B64F1/32—Ground or aircraft-carrier-deck installations for handling freight
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
    • F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
    • F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
    • F16F15/06—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with metal springs
    • F16F15/067—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with metal springs using only wound springs

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Acoustics & Sound (AREA)
  • Vibration Dampers (AREA)

Abstract

The invention discloses an unmanned aerial vehicle loading platform shockproof device, wherein a buffer assembly capable of buffering an unmanned aerial vehicle loaded with articles falling onto the loading platform is arranged on the inner side of the loading platform, a limiting clamping assembly capable of limiting the articles falling onto the buffer assembly is arranged on the inner side of the buffer assembly, a plurality of elastic supporting assemblies which are distributed along the circumferential direction of the buffer assembly and are used for buffering and resetting when the buffer assembly swings are respectively arranged on the outer side of the buffer assembly, and a transverse plate adjusting assembly capable of adjusting the transverse plate to avoid obstruction caused by swinging of the buffer assembly is arranged on the elastic supporting assembly. The invention solves the problems that the existing unmanned aerial vehicle can drive the articles to land on the loading and unloading platform, the unmanned aerial vehicle has higher speed, and the articles are easy to roll over under the action of inertia when the articles are driven to land on the loading and unloading platform, and the articles and the unmanned aerial vehicle are easy to be damaged, thereby greatly improving the whole operation cost.

Description

Unmanned aerial vehicle loading platform shock mounting
Technical Field
The invention relates to the technical field of unmanned aerial vehicle distribution, in particular to an unmanned aerial vehicle loading platform shockproof device.
Background
In recent years, unmanned aerial vehicle industry development is rapid, unmanned aerial vehicle application fields are more and more extensive, and most products are basically in the foot aerial photography and mass consumption market at present. Whereas the current logistics market faces the following problems: on one hand, the labor cost is continuously increased, the traffic congestion is increasingly aggravated, the logistics delivery cost is continuously aggravated, the timeliness is continuously prolonged, the waiting time of a user is influenced by holidays and the like, and the conflict between the user and an electronic commerce is increasingly aggravated due to frequent goods return caused by untimely delivery; on the other hand, when private articles are needed by both friends and the friends to be delivered, the delivery is finished by means of express delivery at present, the delivery is not smooth due to various restrictions of postal regulations, and the like.
The existing unmanned aerial vehicle drives articles to fall on a loading platform, because the unmanned aerial vehicle is faster, when the articles are driven to fall on the loading platform, side turning occurs under the action of inertia easily, so that damage is caused to the articles and the unmanned aerial vehicle easily, the overall operation cost is greatly improved, and meanwhile, the efficiency of unmanned aerial vehicle distribution is greatly reduced, and the practicality of unmanned aerial vehicle distribution is greatly reduced.
Disclosure of Invention
According to the unmanned aerial vehicle loading platform shock-proof device, the problem that the existing unmanned aerial vehicle drives objects to fall on the loading platform is solved, the unmanned aerial vehicle is fast, when the objects are driven to fall on the loading platform, the objects and the unmanned aerial vehicle are easy to damage due to the fact that the objects are easy to roll over under the action of inertia, the overall operation cost is greatly improved, meanwhile, the unmanned aerial vehicle distribution efficiency is greatly reduced, and the practicality of unmanned aerial vehicle distribution is greatly reduced.
In order to achieve the above object, the present invention provides an unmanned aerial vehicle loading platform vibration-proof device, which comprises a loading platform, a vibration-proof mechanism and a plurality of cross plates, wherein the cross plates are respectively hinged on the loading platform to realize the connection of the gap between the loading platform and the vibration-proof mechanism,
the vibration prevention mechanism comprises a buffer assembly, a transverse plate adjusting assembly, an elastic supporting assembly and a limiting clamping assembly, wherein the buffer assembly capable of buffering an unmanned aerial vehicle filled with articles is arranged on the inner side of the loading platform, the limiting clamping assembly capable of clamping the articles on the buffer assembly is arranged on the inner side of the buffer assembly, a plurality of elastic supporting assemblies which are circumferentially distributed along the buffer assembly and used for buffering and resetting when the buffer assembly swings are arranged on the outer side of the buffer assembly, and the elastic supporting assemblies are provided with the transverse plate adjusting assembly capable of adjusting the transverse plate to avoid obstruction caused when the buffer assembly swings.
Preferably, the hemisphere support of buffering subassembly, the hemisphere support is set up the inboard lower terminal surface of loading platform, the mount pad that the level set up is installed to hemisphere support up end, the concave buffer tank that is equipped with of mount pad up end, the buffer spring that vertical setting and descend to the buffering at unmanned aerial vehicle is installed to the buffer tank inboard, the buffer spring top is installed and is convenient for unmanned aerial vehicle to descend to drive the buffer board.
Preferably, the spacing clamping assembly is two at least pivots, the mount pad is located the buffer tank both sides are all concave respectively to be equipped with the mounting groove, every pivot all level respectively and rotationally assemble the mounting groove is inboard, pivot surface fixed cover is equipped with cylindrical cam, cylindrical cam establishes at its surperficial assembly groove slidable ground through the concave guide arm that is equipped with along its length direction, the push pedal is installed to guide arm one end, the second elastic telescopic link that the level set up is installed to push pedal one end, the splint that can run through the concave through-hole of establishing the mounting groove inner wall and carry out the centre gripping to the article on the unmanned aerial vehicle are installed to the telescopic link of second elastic telescopic link.
Preferably, the limiting clamping assembly further comprises at least two limiting seats, each limiting seat is horizontally assembled on the inner sides of the two mounting grooves, and the limiting seats are matched with the guide rod in a sliding manner through sliding grooves formed in the length direction of the limiting seats.
Preferably, the limiting clamping assembly further comprises at least two racks and transmission gears corresponding to the racks one by one, the two racks are vertically and intermittently assembled on the lower end face of the buffer plate, and one end part of each rotating shaft penetrates through the inner side of the mounting groove in a rotatable mode and is fixedly sleeved with the transmission gear which can be meshed with the racks.
Preferably, each elastic supporting component comprises a first fixed sleeve and a second fixed sleeve, the first fixed sleeve is mounted on the lower end face of the inner side of the loading platform, a first universal ball is movably mounted on the inner side of the first fixed sleeve, the second fixed sleeve is mounted on the lower end face of the mounting seat, a second universal ball is movably mounted on the inner side of the second fixed sleeve, a telescopic first elastic telescopic rod is hinged to the top end of the first universal ball, and the top end of the first elastic telescopic rod is hinged to the bottom end of the second universal ball.
Preferably, the diaphragm adjusting part comprises a sliding rail and a sliding seat, the sliding rail is vertically arranged on the inner side wall of the loading platform, the sliding seat is slidably assembled on the outer surface of the sliding rail, one end part of the sliding seat is sequentially hinged with a second connecting rod and a first connecting rod from top to bottom, the top end of the second connecting rod is mutually hinged with the lower end surface of the diaphragm, the bottom end of the first connecting rod is hinged with a fixing seat, and the fixing seat is fixedly sleeved on the outer surface of the fixing end of the first elastic telescopic rod.
Preferably, the first elastic telescopic rod and the second elastic telescopic rod are both elastically connected with each other through a return spring.
According to the technical scheme, the unmanned aerial vehicle loading platform shockproof device provided by the invention has the following beneficial effects:
1. through setting up the mutually supporting between buffer assembly, elastic support subassembly and the spacing centre gripping subassembly, can be better to avoiding taking place to turn on one's side when article falls onto loading platform to better protect article and unmanned aerial vehicle, avoided article and unmanned aerial vehicle's damage, thereby very big reduction holistic operation cost.
2. Through setting up the diaphragm, elastic support subassembly and diaphragm adjusting part between mutually supporting, can be better adjust the diaphragm position in the buffering to avoided the diaphragm to hinder to buffer unit, thereby very big improvement work efficiency, also very big improvement the practicality simultaneously.
Additional features and advantages of the invention will be set forth in the detailed description which follows; and none of the inventions are related to the same or are capable of being practiced in the prior art.
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 the invention and together with the description serve to explain, without limitation, the invention. In the drawings:
FIG. 1 is a schematic view of the overall structure of a unmanned aerial vehicle loading dock vibration isolation device provided in a preferred embodiment of the present invention;
FIG. 2 is a schematic overall cross-sectional view of an unmanned aerial vehicle loading dock vibration isolation device provided in a preferred embodiment of the present invention;
FIG. 3 is a schematic view of the internal top view of a dock section of a unmanned dock vibration isolation device according to a preferred embodiment of the present invention;
FIG. 4 is a schematic view of the internal side view of a dock section of a unmanned dock vibration isolation device according to a preferred embodiment of the present invention;
FIG. 5 is a schematic view of the internal connection structure of the mounting base of the unmanned aerial vehicle loading dock vibration isolation device according to a preferred embodiment of the present invention;
fig. 6 is a schematic view showing a connection structure between an elastic support assembly and a cross plate adjusting assembly of a shock absorbing device for a loading platform of an unmanned aerial vehicle according to a preferred embodiment of the present invention.
Description of the reference numerals
In the figure: 1. loading platform, 2, cross plate, 3, buffer assembly, 301, mount pad, 3011, buffer slot, 3012, mount slot, 302, buffer plate, 303, buffer spring, 304, hemisphere support, 4, cross plate adjusting assembly, 401, first connecting rod, 402, fixing base, 403, slide, 404, slide rail, 405, second connecting rod, 5, elastic supporting assembly, 501, first fixed sleeve, 502, first universal ball, 503, first elastic telescopic rod, 504, second universal ball, 505, second fixed sleeve, 6, limit clamping assembly, 601, rotation shaft, 602, cylindrical cam, 603, limit seat, 604, guide rod, 605, push plate, 606, second elastic telescopic rod, 607, clamping plate, 608, rack, 609, and transmission gear.
Detailed Description
The following describes specific embodiments of the present invention in detail with reference to the drawings. It should be understood that the detailed description and specific examples, while indicating and illustrating the invention, are not intended to limit the invention.
In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the present invention.
As shown in fig. 1-6, an unmanned aerial vehicle loading platform vibration-proof device comprises a loading platform 1, a vibration-proof mechanism and a plurality of transverse plates 2, wherein the transverse plates 2 are respectively hinged on the loading platform 1 to realize the connection of gaps between the loading platform 1 and the vibration-proof mechanism,
the vibration prevention mechanism comprises a buffer assembly 3, a diaphragm adjusting assembly 4, an elastic supporting assembly 5 and a limiting clamping assembly 6, wherein the buffer assembly 3 which can buffer an unmanned aerial vehicle filled with articles is arranged on the inner side of the loading platform 1, the limiting clamping assembly 6 which can clamp the articles on the buffer assembly 3 for limiting is arranged on the inner side of the buffer assembly 3, a plurality of elastic supporting assemblies 5 which are distributed circumferentially along the buffer assembly 3 and used for buffering and resetting when the buffer assembly 3 swings are arranged on the outer side of the buffer assembly 3, and the elastic supporting assemblies 5 are provided with diaphragm adjusting assemblies 4 which can adjust the diaphragm 2 to prevent the buffer assembly 3 from being blocked when swinging.
Specifically, when unmanned aerial vehicle transportation article removes to buffer assembly 3, make buffer assembly 3 downwardly moving under the effect of article gravity, make buffer assembly 3 slowly slide under the effect of elastic support assembly 5 simultaneously, make elastic support assembly 5 drive diaphragm adjusting part 4 and remove when removing, make diaphragm adjusting part 4 drive diaphragm 2 and rotate, thereby avoid diaphragm 2 to make the fender to buffer assembly 3, make buffer assembly 3 drive spacing clamping assembly 6 in downwardly moving simultaneously, make spacing clamping assembly 6 carry out the centre gripping protection to the article, thereby realize taking precautions against earthquakes to unmanned aerial vehicle transportation article, so can be better avoid taking place to turn on one's side when article falls to loading platform 1, thereby better protect article and unmanned aerial vehicle, article and unmanned aerial vehicle's damage has been avoided, thereby very big reduction holistic running cost, simultaneously also very big improvement unmanned aerial vehicle's delivery efficiency.
In this embodiment, buffer module 3 hemisphere support 304, hemisphere support 304 is set up the inboard lower terminal surface of loading platform 1, mount pad 301 that the level set up is installed to hemisphere support 304 up end, mount pad 301 up end is concave to be equipped with buffer tank 3011, buffer spring 303 that vertical setting just descends to the buffering at unmanned aerial vehicle is installed to buffer tank 3011 inboard, buffer spring 303 top is installed and is convenient for unmanned aerial vehicle to descend and drive buffer board 302.
Specifically, when the unmanned aerial vehicle transporting object moves onto the buffer plate 302, the buffer plate 302 is moved downward by the weight of the unmanned aerial vehicle transporting object and the object, and the buffer spring 303 is buffered as the buffer plate 302 moves downward.
In this embodiment, the spacing clamping assembly 6 is at least two pivots 601, the mount pad 301 is located buffer 3011 both sides all concave mounting groove 3012 that is equipped with respectively, every pivot 601 respectively horizontal and rotationally assemble the mounting groove 3012 inboard, pivot 601 surface mounting cover is equipped with cylindrical cam 602, cylindrical cam 602 is equipped with the gliding guide arm 604 along its length direction through the mounting groove of concave setting on its surface in a slidable manner, push pedal 605 is installed to guide arm 604 one end, the second elastic expansion link 606 of level setting is installed to push pedal 605 one end, the telescopic link of second elastic expansion link 606 is installed and can be run through the concave splint 607 of establishing the through-hole of mounting groove 3012 inner wall and carrying out the centre gripping to the article on the unmanned aerial vehicle.
In this embodiment, the limiting clamping assembly 6 further includes at least two limiting seats 603, each of the limiting seats 603 is horizontally assembled inside two of the mounting grooves 3012, and the limiting seats 603 are slidably matched with the guide rods 604 through sliding grooves along the length direction of the limiting seats 603.
In this embodiment, the limiting clamping assembly 6 further includes at least two racks 608 and transmission gears 609 corresponding to the racks 608 one to one, the two racks 608 are vertically and separately assembled on the lower end surface of the buffer plate 302, and one end of each rotating shaft 601 rotatably penetrates through the inner side of the mounting groove 3012 and is fixedly sleeved with a transmission gear 609 capable of being meshed with the racks 608.
Specifically, when the buffer plate 302 moves downwards, the buffer plate 302 drives the rack 608 to move downwards, the rack 608 drives the transmission gear 609 to rotate, the transmission gear 609 drives the rotating shaft 601 to rotate, the rotating shaft 601 drives the cylindrical cam 602 to rotate, the cylindrical cam 602 drives the guide rod 604 to drive the push plate 605 to move, the push plate 605 drives the clamping plate 607 to move towards the buffer plate 302 through the second elastic telescopic rod 606, the clamping plate 607 is driven to extrude the side wall of the buffer plate 302, and when the buffer plate 302 moves to the lower part of the clamping plate 607, the clamping plate 607 clamps and fixes articles transported by the unmanned aerial vehicle under the action of the second elastic telescopic rod 606, so that the articles transported by the unmanned aerial vehicle are clamped.
In this embodiment, each elastic supporting component 5 includes a first fixing sleeve 501 and a second fixing sleeve 505, the first fixing sleeve 501 is mounted on the lower end surface of the inner side of the loading platform 1, a first universal ball 502 is movably mounted on the inner side of the first fixing sleeve 501, the second fixing sleeve 505 is mounted on the lower end surface of the mounting seat 301, a second universal ball 504 is movably mounted on the inner side of the second fixing sleeve 505, a telescopic first elastic telescopic rod 503 is hinged to the top end of the first universal ball 502, and the top end of the first elastic telescopic rod 503 is hinged to the bottom end of the second universal ball 504.
Specifically, when the articles transported by the unmanned aerial vehicle fall onto the buffer plate 302, the mount base 301 is offset under the action of the inertia of the unmanned aerial vehicle, so that the mount base 301 is offset under the action of the first elastic telescopic rod 503 and simultaneously provides elastic force for the mount base 301, thereby realizing buffering and vibration prevention of the mount base 301.
In this embodiment, the diaphragm adjusting assembly 4 includes slide rail 404 and slide 403, the slide rail 404 is vertical to be installed on the loading platform 1 inside wall, slide 403 slidable assembly is in slide rail 404 surface, slide 403 tip from the top down has articulated second connecting rod 405 and first connecting rod 401 in proper order, second connecting rod 405 top with terminal surface is articulated each other under the diaphragm 2, first connecting rod 401 bottom articulates there is fixing base 402, fixing base 402 fixed cover is established the surface of first elastic expansion link 503 stiff end.
Specifically, when the first elastic telescopic rod 503 is deviated, the first elastic telescopic rod 503 drives the fixing seat 402 to move, the fixing seat 402 drives the sliding seat 403 to move through the first connecting rod 401, and the sliding seat 403 drives the transverse plate 2 to rotate through the second connecting rod 405, so that the transverse plate 2 is adjusted.
In this embodiment, the first elastic telescopic rod 503 and the second elastic telescopic rod 606 are elastically connected to each other by two sleeves through a return spring.
In particular, the first elastic expansion link 503 and the second elastic expansion link 606 are facilitated to be elastic.
The preferred embodiments of the present invention have been described in detail above with reference to the accompanying drawings, but the present invention is not limited to the specific details of the above embodiments, and various simple modifications can be made to the technical solution of the present invention within the scope of the technical concept of the present invention, and all the simple modifications belong to the protection scope of the present invention.
In addition, the specific features described in the above embodiments may be combined in any suitable manner, and in order to avoid unnecessary repetition, various possible combinations are not described further.
Moreover, any combination of the various embodiments of the invention can be made without departing from the spirit of the invention, which should also be considered as disclosed herein.

Claims (8)

1. An unmanned aerial vehicle loading platform shock mounting, its characterized in that: the shockproof device comprises a loading platform (1), a shockproof mechanism and a plurality of transverse plates (2), wherein the transverse plates (2) are respectively hinged on the loading platform (1) to realize the connection of gaps between the loading platform (1) and the shockproof mechanism,
the anti-vibration mechanism comprises a buffer assembly (3), a diaphragm adjusting assembly (4), an elastic supporting assembly (5) and a limiting clamping assembly (6), wherein the buffer assembly (3) capable of buffering an unmanned aerial vehicle filled with articles is arranged on the inner side of the loading platform (1), the limiting clamping assembly (6) capable of clamping the articles on the buffer assembly (3) is arranged on the inner side of the buffer assembly (3), a plurality of elastic supporting assemblies (5) which are distributed circumferentially along the buffer assembly and used for buffering and resetting when the buffer assembly (3) swings are arranged on the outer side of the buffer assembly (3), and the elastic supporting assembly (5) is provided with the diaphragm adjusting assembly (4) capable of adjusting the diaphragm (2) to prevent the buffer assembly (3) from being blocked when the buffer assembly (3) swings.
2. The unmanned aerial vehicle loading platform shock-proof device according to claim 1, wherein the buffer assembly (3) is a hemispherical support (304), the hemispherical support (304) is erected on the inner lower end face of the loading platform (1), a horizontally arranged mounting seat (301) is mounted on the upper end face of the hemispherical support (304), a buffer groove (3011) is concavely formed in the upper end face of the mounting seat (301), a buffer spring (303) which is vertically arranged on the inner side of the buffer groove (3011) and used for buffering is arranged on the unmanned aerial vehicle, and a buffer plate (302) is mounted on the top end of the buffer spring (303) and is convenient for the unmanned aerial vehicle to fall to drive.
3. The unmanned aerial vehicle loading platform shock-proof device according to claim 2, wherein the limit clamping assembly (6) comprises at least two rotating shafts (601), the mounting seats (301) are respectively and concavely provided with mounting grooves (3012) on two sides of the buffer groove (3011), each rotating shaft (601) is respectively and horizontally and rotatably assembled on the inner side of the mounting groove (3012), a cylindrical cam (602) is fixedly sleeved on the outer surface of the rotating shaft (601), a guide rod (604) sliding along the length direction of the guide rod is slidably assembled on the cylindrical cam (602) through an assembling groove concavely arranged on the surface of the cylindrical cam, a push plate (605) is arranged at one end of the guide rod (604), a second elastic telescopic rod (606) horizontally arranged is arranged at one end of the push plate (605), and a clamping plate (607) capable of penetrating through a through hole concavely arranged on the inner wall of the mounting groove (3012) and clamping an article on the unmanned aerial vehicle is arranged on the telescopic rod.
4. A vibration-proof device for a loading platform of an unmanned aerial vehicle according to claim 3, wherein the limit clamping assembly (6) further comprises at least two limit seats (603), each limit seat (603) is horizontally assembled inside two mounting grooves (3012), and the limit seats (603) are slidably matched with the guide rods (604) through sliding grooves arranged along the length direction of the limit seats.
5. The vibration damper for the loading platform of the unmanned aerial vehicle according to claim 4, wherein the limiting clamping assembly (6) further comprises at least two racks (608) and transmission gears (609) corresponding to the racks (608) one by one, the two racks (608) are vertically and alternately assembled on the lower end face of the buffer plate (302), and one end part of each rotating shaft (601) rotatably penetrates through the inner side of the mounting groove (3012) and is fixedly sleeved with the transmission gear (609) capable of being meshed with the racks (608).
6. The unmanned aerial vehicle loading dock shock-absorbing device according to claim 5, wherein each elastic supporting component (5) comprises a first fixing sleeve (501) and a second fixing sleeve (505), the first fixing sleeve (501) is installed on the lower end face of the inner side of the loading dock (1), a first universal ball (502) is movably installed on the inner side of the first fixing sleeve (501), a second fixing sleeve (505) is installed on the lower end face of the installation seat (301), a second universal ball (504) is movably installed on the inner side of the second fixing sleeve (505), a telescopic first elastic telescopic rod (503) is hinged to the top end of the first universal ball (502), and the top end of the first elastic telescopic rod (503) is hinged to the bottom end of the second universal ball (504).
7. The unmanned aerial vehicle loading dock shock-proof device of claim 6, wherein the diaphragm adjusting assembly (4) comprises a sliding rail (404) and a sliding seat (403), the sliding rail (404) is vertically installed on the inner side wall of the loading dock (1), the sliding seat (403) is slidably assembled on the outer surface of the sliding rail (404), a second connecting rod (405) and a first connecting rod (401) are sequentially hinged to one end of the sliding seat (403) from top to bottom, the top end of the second connecting rod (405) is hinged to the lower end face of the diaphragm (2), a fixing seat (402) is hinged to the bottom end of the first connecting rod (401), and the fixing seat (402) is fixedly sleeved on the outer surface of the fixing end of the first elastic telescopic rod (503).
8. The unmanned aerial vehicle loading dock vibration damping device of claim 6, wherein the first elastic telescoping rod (503) and the second elastic telescoping rod (606) are each resiliently connected to each other by a return spring.
CN202311727126.4A 2023-12-14 2023-12-14 Unmanned aerial vehicle loading platform shock mounting Pending CN117566113A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202311727126.4A CN117566113A (en) 2023-12-14 2023-12-14 Unmanned aerial vehicle loading platform shock mounting

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202311727126.4A CN117566113A (en) 2023-12-14 2023-12-14 Unmanned aerial vehicle loading platform shock mounting

Publications (1)

Publication Number Publication Date
CN117566113A true CN117566113A (en) 2024-02-20

Family

ID=89862404

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202311727126.4A Pending CN117566113A (en) 2023-12-14 2023-12-14 Unmanned aerial vehicle loading platform shock mounting

Country Status (1)

Country Link
CN (1) CN117566113A (en)

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