Detachable unmanned aerial vehicle base based on sliding insertion connection

文档序号:1899173 发布日期:2021-11-30 浏览:12次 中文

阅读说明:本技术 基于滑插连接的可拆卸无人机底座 (Detachable unmanned aerial vehicle base based on sliding insertion connection ) 是由 郭彬檑 于 2021-09-01 设计创作,主要内容包括:本发明涉及无人机底座技术领域,具体地说,涉及基于滑插连接的可拆卸无人机底座。其包括底座,底座内至少包括支撑腿,支撑腿的上表面插接固定有支撑件,支撑件内至少包括支撑杆,支撑杆的顶部固定连接有支撑臂,支撑臂顶部固定连接有插接块,插接块左侧壁表面固定连接有上锲块,插接块右侧壁表面靠近上下两端边缘处固定连接有固定耳,支撑杆左侧壁表面位于定位块底部开设有矩形通孔,通孔内壁上表面中心处开设有缓冲槽,缓冲槽安装有缓冲件,支撑杆下表面中心处固定连接有插接耳,通过设置的插接块,支撑件通过插接块与插接槽插接固定,支撑件通过加固耳与支撑腿插接固定,通过插接固定的连接方式,便于对支撑腿进行拆卸,便于检修和收纳。(The invention relates to the technical field of unmanned aerial vehicle bases, in particular to a detachable unmanned aerial vehicle base based on sliding plug connection. The device comprises a base, wherein the base at least comprises a supporting leg, a supporting piece is fixedly inserted on the upper surface of the supporting leg, a supporting rod is at least arranged in the supporting piece, the top of the supporting rod is fixedly connected with a supporting arm, the top of the supporting arm is fixedly connected with an insertion block, the surface of the left side wall of the insertion block is fixedly connected with an upper wedge block, the surface of the right side wall of the insertion block is fixedly connected with a fixing lug close to the edges of the upper end and the lower end, the surface of the left side wall of the supporting rod is positioned at the bottom of a positioning block and is provided with a rectangular through hole, the center of the upper surface of the inner wall of the through hole is provided with a buffer groove, the buffer groove is provided with a buffer piece, the center of the lower surface of the supporting rod is fixedly connected with the insertion lug, through the arranged plugging block, the supporting piece is fixedly plugged with the plugging groove through the plugging block, the supporting piece is fixedly plugged with the supporting leg through the reinforcing lug, through the fixed connected mode of pegging graft, be convenient for dismantle the supporting leg, easy access and accomodate.)

1. Can dismantle unmanned aerial vehicle base based on slide and insert connection, its characterized in that: comprises a main body (1), and an installation clamping seat (2) and a base (3) which are arranged in the main body (1);

the mounting clamping seat (2) at least comprises a shell (201), an inserting groove (202) is formed in the position, close to the bottom, of the surface of one side of the shell (201), a fixing groove (2021) is formed in the edge of an opening of the inserting groove (202), a movable groove (2022) is formed in the top, located at one end of the fixing groove (2021), of the inner cavity of the shell (201), a through hole (204) communicated with the movable groove (2022) is formed in the lower surface of the shell (201), an inclined wedge mechanism (4) is installed in the through hole (204), at least a fixing rod (401) is arranged in the inclined wedge mechanism (4), a movable cavity (4012) communicated with the lower surface is formed in the fixing rod (401), a movable rod (402) is movably connected in the movable cavity (4012), and a limiting cover (4021) is fixedly connected to the center of the upper surface of the movable rod (402), a second spring (4013) is fixedly connected to the center of the upper surface of the limiting cover (4021), a ball (4022) is connected to the lower surface of the movable rod (402) in a nested manner, a lower wedge block (403) is fixedly connected to the center of the upper surface of the fixed rod (401), a first spring (4011) is connected to the fixed rod (401) in a nested manner, a sliding groove (203) communicated with the insertion groove (202) is formed in the lower surface of the shell (201), an installation lug (205) is fixedly connected to the surface of the shell (201) close to the edge of the side wall, and a first installation hole (2051) is formed in the surface of the installation lug (205);

the support leg structure is characterized by at least comprising a support leg (301) in the base (3), a support piece (5) is fixedly inserted into the upper surface of the support leg (301), at least a support rod (501) is arranged in the support piece (5), a support arm (5013) is fixedly connected to the top of the support arm (5013), an insertion block (502) is fixedly connected to the top of the support arm (5013), an upper wedge block (5021) is fixedly connected to the surface of the left side wall of the insertion block (502), a positioning block (503) is fixedly connected to the right side wall of the support rod (501) and is positioned under the upper wedge block (5021), a positioning hole (5031) is formed in the center of the upper surface of the positioning block (503), fixing lugs (5022) are fixedly connected to the upper end edge and the lower end edge of the surface of the right side wall of the insertion block (502), a rectangular through hole (504) is formed in the bottom of the positioning block (503) and is positioned on the surface of the left side wall of the support rod (501), rectangular through hole (504) inner wall upper surface center department has seted up dashpot (5041), bolster (6) are installed to dashpot (5041), bracing piece (501) lower surface center department fixedly connected with plug ear (5011).

2. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 1, wherein: at least including fuselage (101) in main part (1), fuselage (101) lower surface is close to left and right sides edge and has all seted up mounting groove (102), four have been seted up in mounting groove (102) two liang of settings are in fuselage (101) left and right sides edge, ear groove (1021) have been seted up in mounting groove (102) edge.

3. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 2, wherein: the installation clamping seat (2) is fixedly connected with the lug groove (1021) through the first installation hole (2051) through a bolt, the first installation hole (2051) is matched with the lug groove (1021), and the size of the insertion block (502) is matched with that of the insertion groove (202).

4. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 1, wherein: two clamping grooves (302) are formed in the upper surface of the supporting leg (301), and a first fixing hole (3021) communicated with the clamping grooves (302) is formed in the side wall of the supporting leg (301).

5. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 4, wherein: the support piece (5) passes through the insertion lug (5011) with draw-in groove (302) is pegged graft fixedly, the insertion lug (5011) lateral wall surface seted up with second fixed orifices (5012) of first fixed orifices (3021) looks adaptation, first fixed orifices (3021) with second fixed orifices (5012) pass through bolt fixed connection.

6. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 1, wherein: one end of the second spring (4013) is fixedly connected with the upper surface of the inner wall of the movable cavity (4012), and the other end of the second spring (4013) is fixedly connected with the upper surface of the limiting cover (4021).

7. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 1, wherein: the positioning block (503) is of an L-shaped structure, the upper surface of the positioning block (503) is of an arc-shaped curved surface structure, the aperture of the positioning hole (5031) is matched with that of the movable rod (402), the upper wedge block (5021) is matched with the lower wedge block (403), and the expansion amount of the movable rod (402) is matched with the vertical height of the upper surface of the positioning block (503).

8. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 1, wherein: at least, include crossbeam (601) in bolster (6), crossbeam (601) upper surface center department fixedly connected with buffering post (602), nested connection has third spring (6021) on buffering post (602), crossbeam (601) lower surface is close to the first buffering leg (603) of left end edge fixedly connected with, crossbeam (601) lower surface is close to right-hand member second buffering leg (604), first buffering leg (603) with the equal fixed mounting in second buffering leg (604) bottom has blotter (6031).

9. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 8, wherein: buffer piece (6) pass through buffer column (602) with buffer slot (5041) are pegged graft fixedly, crossbeam (601) joint is fixed in rectangle through-hole (504), third spring (6021) sets up in rectangle through-hole (504).

10. The slide-and-plug connection based detachable unmanned aerial vehicle base of claim 8, wherein: the height of the rectangular through hole (504) is matched with the height of the buffer groove (5041), the length of the buffer column (602) is matched with the height of the buffer groove (5041), the expansion amount of the third spring (6021) is matched with the length of the first buffer leg (603), and the length of the first buffer leg (603) is identical to the length of the second buffer leg (604).

Technical Field

The invention relates to the technical field of unmanned aerial vehicle bases, in particular to a detachable unmanned aerial vehicle base based on sliding plug connection.

Background

An unmanned plane, called a drone for short, is an unmanned plane operated by a radio remote control device and a self-contained program control device, or is completely or intermittently autonomously operated by an on-board computer. Drones are often more suited to tasks that are too fool, dirty, or dangerous than manned aircraft. Unmanned aerial vehicle according to the application field, can be divided into military use and civilian use, for military use, unmanned aerial vehicle divide into reconnaissance aircraft and target drone, and the application of unmanned aerial vehicle trade in civilian aspect is real just needed, at present in the application in fields such as aerial photography, agriculture, plant protection, miniature autodyne, express delivery transportation, disaster relief, observation wild animal, control infectious disease, survey and drawing, news report, electric power inspection, relief of disaster, movie & TV are shot and are made romantic, great expansion unmanned aerial vehicle's use itself, developed country is also in active expansion industry application and development unmanned aerial vehicle technique.

When the unmanned aerial vehicle is transported and stored, the base structure is complex, the transportation is inconvenient, the base is generally required to be disassembled so as to store the unmanned aerial vehicle, and the traditional unmanned aerial vehicle is complex in disassembly structure and cannot be rapidly disassembled and assembled.

Disclosure of Invention

The invention aims to provide a detachable unmanned aerial vehicle base based on sliding-plug connection, so as to solve the problems in the background technology.

In order to achieve the purpose, the invention aims to provide a detachable unmanned aerial vehicle base based on sliding insertion connection, which comprises a main body, and an installation clamping seat and a base which are installed in the main body;

the installation clamping seat at least comprises a shell, an inserting groove is arranged on the surface of one side of the shell close to the bottom, a fixed groove is arranged at the opening edge of the inserting groove on the surface of the side wall of the shell, a movable groove is arranged at the top of one end of the fixed groove in the inner cavity of the shell, a through hole communicated with the movable groove is arranged on the lower surface of the shell, an inclined wedge mechanism is arranged in the through hole, the inclined wedge mechanism at least comprises a fixed rod, a movable cavity communicated with the lower surface is arranged in the fixed rod, a movable rod is movably connected in the movable cavity, a limit cover is fixedly connected at the center of the upper surface of the movable rod, a second spring is fixedly connected at the center of the upper surface of the limit cover, a ball is connected at the lower surface of the movable rod in an embedded manner, a lower wedge block is fixedly connected at the center of the upper surface of the fixed rod, and a first spring is connected on the fixed rod in an embedded manner, the lower surface of the shell is provided with a sliding groove communicated with the inserting groove, the surface of the shell, which is close to the edge of the side wall, is fixedly connected with an installation lug, and the surface of the installation lug is provided with a first installation hole;

the installation cassette of this embodiment is when specifically using, inserts the installation cassette in the mounting groove of the fuselage left and right sides, goes into the ear inslot with the installation ear card, will install ear fixed mounting in the ear inslot through the bolt, realizes the installation and the fixed of installation cassette, and the wedge atress moves down now, and lower wedge is in compression spring, and the dead lever is synchronous to move down.

The base at least comprises a supporting leg, a supporting piece is fixedly inserted on the upper surface of the supporting leg, a supporting rod is at least arranged in the supporting piece, a supporting arm is fixedly connected to the top of the supporting arm, an inserting block is fixedly connected to the top of the supporting arm, an upper wedge block is fixedly connected to the surface of the left side wall of the inserting block, a positioning block is fixedly connected to the surface of the left side wall of the supporting rod, which is positioned right below the upper wedge block, a positioning hole is formed in the center of the upper surface of the positioning block, fixing lugs are fixedly connected to the surfaces of the right side wall of the inserting block, which are close to the edges of the upper end and the lower end of the inserting block, a rectangular through hole is formed in the surface of the left side wall of the supporting rod, a buffer groove is formed in the center of the upper surface of the inner wall of the rectangular through hole, a buffer piece is installed in the buffer groove, and an inserting lug is fixedly connected to the center of the lower surface of the supporting rod;

when the base is used specifically, the supporting element is fixedly installed in the inserting groove through the inserting block, when the inserting block moves towards the lower wedge block, the upper wedge block on the inserting block is gradually attached to the lower wedge block, the lower wedge block is stressed to move downwards, the fixed rod synchronously moves downwards, meanwhile, the ball on the lower surface of the movable rod is attached to the limiting groove on the upper surface of the positioning block, the movable rod moves towards the top of the inner cavity of the movable cavity, the second spring is stressed to compress, when the inserting block moves towards the right, the movable rod moves towards the positioning hole along the limiting groove, when the upper wedge block is completely attached to the lower wedge block, the inserting block is completely and slidably inserted into the inserting groove, the movable rod moves to be right above the positioning hole, the second spring rebounds, the movable rod moves downwards and is inserted into the positioning hole, and the limiting and fixing of the inserting block are achieved through the movable rod;

further, when the base descends, the first buffering leg and the second buffering leg firstly contact the ground, the crossbeam is driven to move upwards in the rectangular through hole, the buffering column moves upwards along the buffering groove, the third spring is compressed under the stress, the supporting leg contacts the ground after the third spring is compressed under the stress, and the supporting leg is cushioned and buffered through the buffering piece.

As a further improvement of the technical scheme, the main body at least comprises a body, mounting grooves are formed in the lower surface of the body close to the edges of the left side and the right side of the body, four mounting grooves are formed in the four mounting grooves, two mounting grooves are arranged in two pairs in the edges of the left side and the right side of the body, and ear grooves are formed in the edges of the mounting grooves.

As a further improvement of the technical scheme, the installation clamping seat is fixedly connected with the lug groove through the first installation hole by a bolt, the first installation hole is matched with the lug groove, and the size of the plug-in block is matched with that of the plug-in groove.

As a further improvement of the technical scheme, two clamping grooves are formed in the upper surface of the supporting leg, and first fixing holes communicated with the clamping grooves are formed in the side wall of the supporting leg.

As a further improvement of the technical solution, the supporting member is fixed to the clamping groove by the insertion lug in an insertion manner, a second fixing hole matched with the first fixing hole is formed in the surface of the side wall of the insertion lug, and the first fixing hole is fixedly connected with the second fixing hole through a bolt.

As a further improvement of the technical scheme, one end of the second spring is fixedly connected with the upper surface of the inner wall of the movable cavity, and the other end of the second spring is fixedly connected with the upper surface of the limiting cover.

As a further improvement of the technical scheme, the positioning block is of an L-shaped structure, the upper surface of the positioning block is of an arc-shaped curved surface structure, the aperture of the positioning hole is matched with that of the movable rod, the upper wedge block is matched with the lower wedge block, and the expansion amount of the movable rod is matched with the vertical height of the upper surface of the positioning block.

As a further improvement of the technical scheme, at least a beam is included in the buffer piece, a buffer column is fixedly connected to the center of the upper surface of the beam, a third spring is connected to the buffer column in an embedded mode, the lower surface of the beam is close to a first buffer leg fixedly connected to the edge of the left end, the lower surface of the beam is close to a second buffer leg of the right end, and a buffer pad is fixedly mounted at the bottom of the first buffer leg and the bottom of the second buffer leg.

As a further improvement of the technical scheme, the buffer piece is connected with the buffer groove in an inserting mode through the buffer column, the cross beam is connected and fixed in the rectangular through hole in a clamping mode, and the third spring is arranged in the rectangular through hole.

As a further improvement of the technical scheme, the height of the rectangular through hole is matched with the height of the buffer groove, the length of the buffer column is matched with the height of the buffer groove, the expansion amount of the third spring is matched with the length of the first buffer leg, and the length of the first buffer leg is the same as that of the second buffer leg.

Compared with the prior art, the invention has the beneficial effects that:

1. in this can dismantle unmanned aerial vehicle base based on smooth plug connection, through the grafting piece that sets up, support piece is pegged graft fixedly through grafting piece and inserting groove, and support piece is pegged graft fixedly through strengthening ear and supporting leg, through the fixed connected mode of pegging graft, is convenient for dismantle fast and assemble, easy access and accomodate the base.

2. In this can dismantle unmanned aerial vehicle base based on smooth plug-in connection, carve the mechanism to one side through setting up, carve the mechanism to one side and move down by the grafting piece promotion, realize spacing to the grafting of bracing piece through the movable rod, further ensured the stability of bracing piece in the installation block seat.

3. In this can dismantle unmanned aerial vehicle base based on connection is inserted to smooth, through the bolster that sets up, through the third spring that sets up on the bolster, absorb and cushion the impact that first buffering leg and second buffering leg received, can effectively reduce the impact force of receiving of base, play the effect of stable support to the base.

Drawings

FIG. 1 is a schematic view of the entire structure of embodiment 1;

FIG. 2 is a schematic bottom view of the overall structure of example 1;

FIG. 3 is a partial structural view of the main body of embodiment 1;

FIG. 4 is a schematic view of the structure of the fuselage of embodiment 1;

FIG. 5 is a partial schematic view of the fuselage structure of embodiment 1;

FIG. 6 is one of the schematic structural views of the case according to embodiment 1;

FIG. 7 is a second schematic structural view of the housing according to embodiment 1;

FIG. 8 is a schematic structural view of the mounting socket and the supporting member in an initial state of plugging in the embodiment 1;

FIG. 9 is a schematic view of the connection structure of the mounting socket and the supporting member in embodiment 1;

FIG. 10 is a schematic sectional view showing the structure of the cartridge according to embodiment 1;

FIG. 11 is a schematic view of a slanting wedge mechanism of embodiment 1;

FIG. 12 is a schematic plan view of the slanting wedge mechanism of embodiment 1;

FIG. 13 is a schematic view showing the overall structure of the support member according to embodiment 1;

FIG. 14 is a cross-sectional structural view of the support member of embodiment 1;

FIG. 15 is a structural view of a buffer member according to embodiment 1;

FIG. 16 is a partial schematic structural view of the support member according to embodiment 1;

FIG. 17 is a second partial structural view of the supporting member of embodiment 1;

FIG. 18 is a schematic plan view of the support member of example 1;

FIG. 19 is a schematic view showing the connection of the support leg and the support member according to embodiment 1;

fig. 20 is a schematic view of the entire structure of the base according to embodiment 1.

The various reference numbers in the figures mean:

1. a main body; 101. a body; 102. mounting grooves; 1021. an ear canal;

2. installing a card seat; 201. a housing; 202. inserting grooves; 2021. fixing grooves; 2022. a movable groove; 203. a chute; 204. a through hole; 205. mounting lugs; 2051. a first mounting hole;

3. a base; 301. supporting legs; 302. a card slot; 3021. a first fixing hole;

4. an inclined wedge mechanism; 401. fixing the rod; 4011. a first spring; 4012. a movable cavity; 4013. a second spring; 402. a movable rod; 4021. a limiting cover; 4022. a ball bearing; 403. a lower wedge block;

5. a support member; 501. a support bar; 5011. a plug-in lug; 5012. a second fixing hole; 5013. a support arm; 502. an insertion block; 5021. an upper wedge block; 5022. fixing the ear; 5023. a second mounting hole; 503. positioning blocks; 5031. positioning holes; 5032. a limiting groove; 504. a rectangular through hole; 5041. a buffer tank;

6. a buffer member; 601. a cross beam; 602. a buffer column; 6021. a third spring; 603. a first buffer leg; 6031. a cushion pad; 604. a second buffer leg.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations and positional relationships based on those shown in the drawings, and are used only for convenience of description and simplicity of description, and do not indicate or imply that the equipment or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be considered as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.

Example 1

Referring to fig. 1 to 20, the present embodiment aims to provide a detachable unmanned aerial vehicle base based on a sliding plug connection, which includes a main body 1, and an installation clamping base 2 and a base 3 installed in the main body 1;

the installation cassette 2 at least comprises a shell 201, an insertion groove 202 is arranged on the surface of one side of the shell 201 near the bottom, a fixed groove 2021 is arranged on the surface of the side wall of the shell 201 at the opening edge of the insertion groove 202, a movable groove 2022 is arranged on the top of the inner cavity of the shell 201 at one end of the fixed groove 2021, a through hole 204 communicated with the movable groove 2022 is arranged on the lower surface of the shell 201, the through hole 204 is aligned with the center of the upper surface of the movable groove 2022 up and down, an inclined wedge mechanism 4 is installed in the through hole 204, the inclined wedge mechanism 4 at least comprises a fixed rod 401, a movable cavity 4012 communicated with the lower surface is arranged in the fixed rod 401, a movable rod 402 is movably connected in the movable cavity 4012, a limit cover 4021 is fixedly connected at the center of the upper surface of the movable rod 402, a second spring 4013 is fixedly connected at the center of the upper surface of the limit cover 4021, a ball 2 is connected in a nested manner on the lower surface of the movable rod 402, and the ball 4022 plays a role in assisting sliding, the center of the upper surface of the fixing rod 401 is fixedly connected with a lower wedge 403, the fixing rod 401 is connected with a first spring 4011 in an embedded mode, one end of the first spring 4011 is fixedly connected with the lower wedge 403, the first spring 4011 enables the lower wedge 403 to automatically rebound upwards when the lower wedge 403 is not stressed, the lower surface of the shell 201 is provided with a sliding groove 203 communicated with the inserting groove 202, a supporting arm 5013 is matched with the sliding groove 203, the supporting arm 5013 can slide in the sliding groove 203, the sliding groove 203 and the through hole 204 are separated through the inner wall of the shell 201, the sliding groove 203 is not communicated with the through hole 204, the stability of the inclined wedge mechanism 4 in the through hole 204 is guaranteed, the surface of the shell 201 close to the edge of the side wall is fixedly connected with a mounting lug 205, and the surface of the mounting lug 205 is provided with a first mounting hole 2051;

when the installation clamping seat 2 of the embodiment is used specifically, the installation clamping seat 2 is inserted into the installation grooves 102 on the left and right sides of the body 101, the installation lugs 205 are clamped into the lug grooves 1021, the installation lugs 205 are fixedly installed in the lug grooves 1021 through bolts, installation and fixation of the installation clamping seat 2 are achieved, when the wedge block 403 is forced to move downwards, the lower wedge block 403 compresses the spring, and the fixing rod 401 synchronously moves downwards.

The base 3 at least comprises a supporting leg 301, a supporting piece 5 is fixedly inserted on the upper surface of the supporting leg 301, a supporting rod 501 is at least arranged in the supporting piece 5, a supporting arm 5013 is fixedly connected to the top of the supporting rod 501, an inserting block 502 is fixedly connected to the top of the supporting arm 5013, an upper wedge 5021 is fixedly connected to the surface of the left side wall of the inserting block 502, a positioning block 503 is fixedly connected to the surface of the left side wall of the supporting rod 501 under the upper wedge 5021, a positioning hole 5031 is formed in the center of the upper surface of the positioning block 503, fixing lugs 5022 are fixedly connected to the surface of the right side wall of the inserting block 502 close to the edges of the upper end and the lower end, a second mounting hole 5023 is formed in the fixing lug 5022, a rectangular through hole 504 is formed in the bottom of the positioning block 503 on the surface of the left side wall of the supporting rod 501, a buffer groove 5041 is formed in the center of the upper surface of the inner wall of the rectangular through hole 504, a buffer groove 5041 is provided with a buffer 6, and an inserting lug 5011 is fixedly connected to the center of the lower surface of the supporting rod 501;

in the specific use of the base 3 of this embodiment, the supporting member 5 is fixedly installed in the inserting slot 202 through the inserting block 502, when the inserting block 502 moves toward the lower wedge 403, the upper wedge 5021 on the inserting block 502 gradually contacts with the lower wedge 403, the lower wedge 403 is forced to move downward, the fixing rod 401 synchronously moves downward, meanwhile, the ball 4022 on the lower surface of the movable rod 402 is attached to the limit groove 5032 on the upper surface of the positioning block 503, the movable rod 402 moves to the top of the inner cavity of the movable cavity 4012, the second spring 4013 is compressed under stress, when the insertion block 502 moves to the right, the movable rod 402 moves along the limiting groove 5032 to the positioning hole 5031, when the upper wedge 5021 is completely attached to the lower wedge 403 and the socket block 502 is completely inserted into the socket 202, the movable rod 402 moves to a position right above the positioning hole 5031, the second spring 4013 rebounds, the movable rod 402 moves downwards and is inserted into the positioning hole 5031, and the movable rod 402 limits and fixes the insertion block 502;

further, when the base 3 descends, the first buffer leg 603 and the second buffer leg 604 firstly contact the ground and drive the beam 601 to move upwards in the rectangular through hole 504, the buffer column 602 moves upwards along the buffer slot 5041, the third spring 6021 is stressed and compressed, the support leg 301 contacts the ground after the third spring 6021 is stressed and compressed, and the buffer member 6 plays a role in damping and buffering for the support leg 301.

Further, including fuselage 101 in the main part 1 at least, fuselage 101 lower surface is close to left and right sides edge and has all seted up mounting groove 102, and four have been seted up to mounting groove 102, and four two liang of settings of mounting groove 102 are in fuselage 101 left and right sides edge, and ear groove 1021 has been seted up to mounting groove 102 edge, and ear groove 1021 offers the screw that is aligned with first mounting hole 2051, is convenient for go on fixing installation cassette 2.

The mounting base 2 is fixedly connected with the ear groove 1021 through a bolt through a first mounting hole 2051, the first mounting hole 2051 is matched with the ear groove 1021, the size of the plug-in block 502 is matched with the size of the plug-in groove 202, and the plug-in block 502 can slide in the plug-in groove 202.

Still further, two draw-in grooves 302 have been seted up to supporting leg 301 upper surface, and the first fixed orifices 3021 with draw-in groove 302 intercommunication is seted up to supporting leg 301 lateral wall, and further supporting leg 301 is provided with two, and the symmetry sets up in the 3 left and right sides of base respectively, through the stability of two supporting legs 301 guarantee fuselage 101.

In addition, the support piece 5 is fixedly inserted into the slot 302 through the inserting lug 5011, a second fixing hole 5012 matched with the first fixing hole 3021 is formed in the surface of the side wall of the inserting lug 5011, the first fixing hole 3021 and the second fixing hole 5012 are fixedly connected through bolts, the support piece 5 is fixedly mounted on the support leg 301, and meanwhile, the support piece is convenient to detach due to the bolt fixing mode.

In addition, second spring 4013 one end and activity chamber 4012 inner wall upper surface fixed connection, the second spring 4013 other end and spacing lid 4021 upper surface fixed connection fix the second spring 4013 in activity chamber 4012, and spacing lid 4021 size and activity chamber 4012 aperture looks adaptation, and activity chamber 4012 aperture is greater than dead lever 401 lower surface opening aperture.

Specifically, the positioning block 503 is an L-shaped structure, the upper surface of the positioning block 503 is an arc-shaped curved surface structure, a limiting groove 5032 is formed on the edge of the upper surface of the positioning block 503 close to the edge from the arc-shaped curved surface to the positioning hole 5031, the aperture of the positioning hole 5031 is matched with the aperture of the movable rod 402, the upper wedge 5021 is matched with the lower wedge 403, the expansion amount of the movable rod 402 is matched with the vertical height of the upper surface of the positioning block 503, when the upper wedge 5021 is matched with the lower wedge 403, the bottom of the movable rod 402 is matched with the limiting groove 5032, and when the lower wedge 403 moves downwards, the movable rod 402 moves towards the positioning hole 5031 along the limiting groove 5032.

Further, at least crossbeam 601 is included in bolster 6, crossbeam 601 upper surface center department fixedly connected with buffering post 602, nested connection has third spring 6021 on the buffering post 602, crossbeam 601 lower surface is close to the first buffering leg 603 of left end edge fixedly connected with, crossbeam 601 lower surface is close to right-hand member second buffering leg 604, the equal fixed mounting in first buffering leg 603 and second buffering leg 604 bottom has blotter 6031, play the effect of shock attenuation buffering to supporting leg 301 through bolster 6, and first buffering leg 603 and second buffering leg 604 are highly the same, in uncompressed state, first buffering leg 603 and second buffering leg 604 are located the below of supporting leg 301, guarantee first buffering leg 603 and second buffering leg 604 can play the cushioning effect.

The buffer member 6 is fixedly inserted into the buffer groove 5041 through the buffer column 602, the beam 601 is clamped and fixed in the rectangular through hole 504, the third spring 6021 is arranged in the rectangular through hole 504, and the damping and buffering effects are achieved through the arranged third spring 6021.

Still further, the height of the rectangular through hole 504 is matched with the height of the buffer groove 5041, the length of the buffer column 602 is matched with the height of the buffer groove 5041, the expansion amount of the third spring 6021 is matched with the length of the first buffer leg 603, the length of the first buffer leg 603 is the same as the length of the second buffer leg 604, it is guaranteed that the beam 601 can normally move in the rectangular through hole 504, and the buffer column 602 can normally move in the buffer groove 5041.

The foregoing shows and describes the general principles, essential features, and advantages of the invention. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, and the preferred embodiments of the present invention are described in the above embodiments and the description, and are not intended to limit the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

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