CN211048959U

CN211048959U - Multi-angle rotating's aircraft model support and aircraft model fight exercise device

Info

Publication number: CN211048959U
Application number: CN201920987929.6U
Authority: CN
Inventors: 邓干恒
Original assignee: Zhongshan Wandexing Toy Technology Co ltd; Hengchang Industry Co ltd
Current assignee: Zhongshan Wandexing Toy Technology Co ltd; Hengchang Industry Co ltd
Priority date: 2019-06-27
Filing date: 2019-06-27
Publication date: 2020-07-21
Anticipated expiration: 2029-06-27

Abstract

The utility model provides a multi-angle rotating's aircraft model support, the on-line screen storage device comprises a base, the rotary disk that has rectangular hole, the arc connecting plate, bracing piece and be used for placing the supporting seat of aircraft, the base middle part is equipped with the through-hole, the base that is close to the through-hole top is equipped with the heavy limit of annular, the rotary disk includes the dish body and radially stretches out two mount pads along a dish body bottom, the dish body sinks limit normal running fit with annular, two mount pads set up in the both sides in rectangular hole symmetrically respectively, the lateral wall of bracing piece bottom stretches out the first extension rod that has two symmetries along the axial, every first extension rod is equallyd divide and is do not through arc connecting plate pin joint on corresponding mount pad, the bracing piece top has stretched out the second extension rod along the axial, the support base bottom. The method and the device realize multi-angle arrangement of the airplane model, and find out a better display angle for people to view; meanwhile, the operation is simple and the use is convenient as long as the adjustment is carried out by hand. The application also provides an airplane model battle exercise device.

Description

Multi-angle rotating's aircraft model support and aircraft model fight exercise device

Technical Field

The utility model belongs to the technical field of the supporting equipment, a multi-angle rotating's aircraft model support and aircraft model fight exercise device is related to.

Background

At present, an airplane is one of the most important utility models for human beings. Nowadays, with the improvement of living conditions, a large number of model airplane enthusiasts appear. Therefore, various airplane models need to be designed according to different requirements. The airplane model is generally displayed and exhibited through the support, and the general airplane model support comprises a base and a vertical support rod arranged on the base, and the airplane model is fixed on the support rod and used for exhibiting the airplane model. It has the problems that: the support cannot be adjusted at multiple angles, and the airplane model cannot be displayed at a better angle for people to watch.

Therefore, the utility model provides a multi-angle rotating's aircraft model support.

Furthermore, the utility model also provides an airplane model battle exercise device.

SUMMERY OF THE UTILITY MODEL

In view of the above problems in the prior art, the present invention is directed to provide a multi-angle rotating airplane model support, which can adjust a multi-angle set airplane model after the airplane model is placed on a supporting seat, so as to find a better display angle for people to view; meanwhile, the operation is very simple and the use is convenient only by hand adjustment.

The purpose of the utility model can be realized by the following technical proposal:

the utility model provides a multi-angle rotating's aircraft model support, includes the base, has the rotary disk in rectangular hole, arc connecting plate, bracing piece and is used for placing the supporting seat of aircraft, and the base middle part is equipped with the through-hole, and the base that is close to the through-hole top is equipped with the heavy limit of annular, and the rotary disk includes the dish body and radially stretches out two mount pads along a dish body bottom, dish body and the heavy limit normal running fit of annular, two the mount pad sets up in the both sides in rectangular hole symmetrically respectively, and the lateral wall of bracing piece bottom stretches out the first extension rod that has two symmetries along the axial, and every first extension rod divide equally do not through arc connecting plate pin joint in on the corresponding mount pad, the bracing piece top stretches out along the axial has the second extension rod, and the support seat bottom is equipped with the mounting hole.

As a preferred technical scheme, the support rod further comprises a lock catch ring, the support rod comprises a hollow first rod body and a second rod body which is slidably sleeved on the first rod body, a plurality of notches are arranged on the side wall of the second rod body along the radial direction, each notch is arranged at intervals, and the lock catch ring is clamped in one of the notches.

As a preferred technical scheme, the lock catch ring is provided with an arc ring body and an insertion body extending out of the middle of the inner side wall of the arc ring body, the inner side wall of the arc ring body is attached to the outer side wall of the second rod body, and the insertion body is clamped in the notch.

Preferably, the number of the notches is five, and each notch is arranged on the side wall of the second rod body along a radial straight line.

Preferably, the top of the support rod extends to form an arc-shaped plate body, the arc-shaped plate body is provided with a flat plate part and a triangular reinforcing plate part extending out along one surface of the flat plate part, and the second extending rod is axially arranged on the other surface of the flat plate part.

As a preferred technical scheme, a plurality of hook parts are arranged at the outer edge of the bottom of the plate body, and each hook part is in sliding fit with the bottom of the annular sunk edge.

As a preferred technical scheme, the number of the hook parts is three, and each hook part is uniformly distributed at the bottom of the disc body along the circumferential direction.

As the preferred technical scheme, the supporting seat comprises a seat body with an upper opening and a hollow hexagonal prism which is used for being connected with an airplane, the hexagonal prism is arranged in the accommodating cavity, and two side walls of the seat body close to the hexagonal prism respectively extend to form a U-shaped body.

As a preferred technical scheme, the base comprises a base plate and a base support plate extending out of the peripheral edge of the base plate, two first partition plates are arranged between the lower surface of the base plate and the base support plate adjacent to the base plate, and second partition plates are arranged between every two adjacent first partition plates and between the first partition plates and the base support plate.

The utility model also provides an aircraft model battle exercise device, as above including the several the multi-angle rotating's aircraft model support, every adjacent two can dismantle the connection between the base.

As above, the utility model relates to an aircraft model support of multi-angle rotating has following beneficial effect:

after the multi-angle rotating airplane model support is utilized, compared with the prior art, due to the adoption of the structure, the rotary disc is rotated for 360 degrees relative to the base by rotating and matching the disc body of the rotary disc with the annular sunk edge, so that different flight directions of the airplane model can be adjusted; each first extension rod of the support rod is pivoted to the corresponding mounting seat through an arc-shaped connecting plate, so that the support rod can rotate and swing back and forth relative to the rotating disc, and different diving postures of the airplane model can be realized; the second extension rod of the support rod is pivoted in the mounting hole at the bottom of the support seat, so that the support seat can horizontally incline at different angles relative to the support rod, and different side flight states of the airplane model can be realized; after the airplane model is placed on the supporting seat, the airplane model can be arranged at multiple angles, and a better display angle can be found conveniently for people to watch; meanwhile, the operation is very simple and the use is convenient only by hand adjustment.

The present invention will be further described with reference to the following embodiments.

Drawings

FIG. 1 is a perspective view of a multi-angle rotating airplane model support;

FIG. 2 is a schematic structural diagram of an aircraft model support with multi-angle rotation, which only comprises a base, a rotating disk and an arc-shaped connecting plate at another view angle;

FIG. 3 is a front view of a multi-angle rotating airplane model support;

FIG. 4 is a cross-sectional view taken along line A-A of FIG. 3;

FIG. 5 is an enlarged view of a portion of the structure of a multi-angle rotating model airplane support on the upper portion of a base;

fig. 6 is an enlarged view of a structure of a latch body of a multi-angle rotary model airplane stand.

Detailed Description

The following description is provided for illustrative purposes, and other advantages and features of the present invention will become apparent to those skilled in the art from the following detailed description.

It should be understood that the structures, ratios, sizes, etc. shown in the drawings of the present application are only used for matching with the contents disclosed in the specification, so as to be known and read by those skilled in the art, and are not used for limiting the limit conditions that the present invention can be implemented, so that the present invention has no technical essential meaning, and any modification of the structures, change of the ratio relationship or adjustment of the sizes should still fall within the scope of the present invention without affecting the functions and the achievable purposes of the present invention. Meanwhile, the terms such as "upper", "lower", "left", "right", "middle" and "one" used in the present specification are for convenience of description only, and are not intended to limit the scope of the present invention, and changes or adjustments of the relative relationship thereof are considered as the scope of the present invention without substantial changes in the technical content. The specific structure can be explained with reference to the drawings of the patent application.

In the following embodiments, the direction is defined by the arrow in fig. 1, the left side of the paper is the left direction, the right side of the paper is the right direction, the upper side of the paper is the up direction, the lower side of the paper is the down direction, the front side perpendicular to the paper is the front direction, the rear side perpendicular to the paper is the rear direction, the inner cavity of the first rod is the inside, and the outer wall of the first rod is the outside.

Referring to fig. 1, 2, 3 and 4, a multi-angle rotating airplane model support comprises a base 1, a rotating disk 2 with a strip hole 200, an arc-shaped connecting plate 3, a supporting rod 4 and a supporting seat 5 for placing an airplane, wherein a through hole 10 is formed in the middle of the base 1, an annular sunken edge 11 is formed on the base 1 close to the top of the through hole 10, the rotating disk 2 comprises a disk body 20 and two mounting seats 21 extending radially from the bottom of the disk body 20, the disk body 20 is rotationally matched with the annular sunken edge 11, the two mounting seats 21 are respectively and symmetrically arranged on two sides of the strip hole 200, two symmetrical first extending rods 40 axially extend from the side wall of the bottom of the supporting rod 4, each first extending rod 40 is respectively pivoted to the corresponding mounting seat 21 through the arc-shaped connecting plate 3, a second extending rod 41 axially extends from the top of the supporting rod 4, a mounting hole 50 is formed in the bottom of the supporting seat 5, the second extension rod 41 is pivoted in the mounting hole 50. Compared with the prior art, the rotary disc 2 rotates 360 degrees relative to the base 1 by matching the disc body 20 of the rotary disc 2 with the annular sunk edge 11 in a rotating way, so as to adjust different flight directions of the airplane model; each first extension rod 40 of the support rod 4 is pivoted to the corresponding mounting seat 21 through the arc-shaped connecting plate 3, so that the support rod 4 can rotate and swing back and forth relative to the rotating disc 2, and different diving postures of the airplane model can be realized; the second extension rod 41 of the support rod 4 is pivoted in the mounting hole 50 at the bottom of the support seat 5, so that the support seat 5 can horizontally incline at different angles relative to the support rod 4, and different side flight states of the airplane model can be realized; after the airplane model is placed on the supporting seat, the airplane model can be arranged at multiple angles, and a better display angle can be found conveniently for people to watch; meanwhile, the operation is very simple and the use is convenient only by hand adjustment.

It should be noted that: referring to fig. 1, for the above-mentioned supporting seat 5 to achieve different angles of horizontal tilting relative to the supporting rod 4, a positioning gear (not shown in the figure) may be provided on the supporting seat 5, specifically, it can rotate by 36 ° to form one gear, so that 10 different angles of horizontal tilting can be achieved within the circumference, thereby achieving different flying states of the airplane model; meanwhile, as the rotating disc 2 is provided with the elongated hole 200, when the angle between the support rod 4 and the rotating disc 2 is adjusted, the support rod 4 can rotate and swing in the front-back direction in the elongated hole 200; preferably, the range of the fore-and-aft swing of the support rod 4 is 50 to-50 degrees, and the stepless angle adjustment of 50 degrees of the fore-and-aft can be realized, so that different angle diving postures of the airplane model ascending or descending can be realized.

Referring to fig. 1 and 5, in order to achieve the height adjustment of the supporting rod 4 in the radial direction, the supporting rod 4 further includes a locking ring 6, the supporting rod 4 includes a hollow first rod 42 and a second rod 43 slidably sleeved on the first rod 42, a plurality of notches 430 are radially disposed on a side wall of the second rod 43, each notch 430 is alternately disposed, and the locking ring 6 is engaged in one of the notches 430. Through setting up like this the structure, position between manually operation snap close ring 6 and corresponding notch 430 is adjusted the second body of rod 43 realizes setting up in the adjustability of the aircraft model altitude mixture control at bracing piece 4 top for the position of the first body of rod 42, thereby not only makes the utility model discloses have multi-angle rotating's function, have height lift adjustable function moreover, further be convenient for find the show angle, the height of preferred, the user of being convenient for uses. Generally, the second rod 43 can be lifted and lowered in a range of 6cm to 15cm relative to the first rod 42, so that all states of displaying the airplane model can be realized.

Referring to fig. 5 and 6, the latch ring 6 has an arc ring body 60 and an insertion body 61 extending along the middle of the inner side wall of the arc ring body 60, the inner side wall of the arc ring body 60 is attached to the outer side wall of the second rod 43, and the insertion body 61 is engaged with the notch 430. The latch ring 6 is provided, and the insertion body 61 of the latch ring 6 is clamped with the notch 430, so that the structure is simple, the operation is simple, and the use is convenient.

As shown in fig. 5, the number of the notches 430 is five, and each of the notches 430 is disposed on the sidewall of the second rod 43 along a radial line. It should be noted that: the number of the notches 430 is not limited thereto, and other suitable numbers of notches 430 may be designed, and will not be described herein. By providing the five notches 430, the free height adjustment of five gears can be realized, so that the flying states of the airplane with different space heights can be realized, and the distance between the bases can be 11cm, 13cm, 15cm, 17cm and 19cm, but the invention is not limited to this, and other distances can also be set.

Referring to fig. 3 and 5, an arc-shaped plate 44 extends from the top of the supporting rod 4, the arc-shaped plate 44 has a flat plate portion 440 and a triangular reinforcing plate portion 441 extending along one surface of the flat plate portion 440, and the second extending rod 41 is axially disposed on the other surface of the flat plate portion 440.

Referring to fig. 2, 3 and 4, when the rotary disc 2 is rotated, in order to prevent the rotary disc 2 from falling off from the base 1, a plurality of hooks 22 are disposed at an outer edge of the bottom of the disc body 20, and each hook 22 is slidably engaged with the bottom of the annular countersink 11. Set up several and collude portion 22, can form certain direction spacing between rotary disk 2 and base 1, avoid rotary disk 2 to drop out from base 1, ensure the stability between rotary disk 2 and the base 1 to promote the user experience at angle of adjustment's process.

As shown in fig. 2, the number of the hook portions 22 is three, and each hook portion 22 is uniformly arranged at the bottom of the tray body 20 along the circumferential direction.

Referring to fig. 4 and 5, in order to facilitate the placement of the airplane model, the support base 5 includes a base body 51 having an accommodating cavity 510 with an upper opening and a hexagonal prism 52 for connecting the airplane, the hexagonal prism 52 is disposed in the accommodating cavity 510, and U-shaped bodies 53 extend from two side walls of the base body 51 near the hexagonal prism 52. Set up above-mentioned structure, can increase the area of contact between aircraft model and the supporting seat 5, be convenient for drag aircraft model, avoid it to drop to improve the connection steadiness between aircraft model and the supporting seat 5.

Referring to fig. 1 and 2, the base 1 includes a seat plate 12, a base support plate 13 extending along a peripheral edge of the seat plate 12, two first partition plates 14 are disposed between a lower surface of the base plate 12 and the base support plate 13 adjacent to the base plate 12, and a second partition plate 15 is disposed between each two adjacent first partition plates 14 and between each first partition plate 14 and the base support plate 13.

It should be noted that: the user can mount a steering wheel on the base 1 to rotate clockwise or counterclockwise, which helps to distinguish the direction for easy use.

The utility model also provides an aircraft model battle exercise device, as above including the several the multi-angle rotating's aircraft model support, every adjacent two can dismantle the connection between the base 1. Two adjacent bases 1 of different multi-angle rotating's aircraft model support are through dismantling the connection, for example through the form of buckle each other's fastening to realize aircraft model battle team formation or fight exercise, so the house can purchase the aircraft model support of several multi-angle rotating, then piece together them and build the visual effect of a blue sky of a quota.

To sum up, the utility model discloses various shortcomings in the prior art have effectively been overcome and high industry value has.

The above embodiments are merely illustrative of the principles and effects of the present invention, and are not to be construed as limiting the invention. Modifications and variations can be made to the above-described embodiments by those skilled in the art without departing from the spirit and scope of the present invention. Accordingly, it is intended that all equivalent modifications or changes which may be made by those skilled in the art without departing from the spirit and technical spirit of the present invention be covered by the claims of the present invention.

Claims

1. The utility model provides a multi-angle rotating's aircraft model support which characterized in that: including the base, have the rotary disk in rectangular hole, arc connecting plate, bracing piece and be used for placing the supporting seat of aircraft, the base middle part is equipped with the through-hole, and the base that is close to the through-hole top is equipped with annular heavy limit, and the rotary disk includes set body and along set body bottom two mount pads that radially stretch out, set body and annular heavy limit normal running fit, two the mount pad sets up in the both sides in rectangular hole symmetrically respectively, and the lateral wall of bracing piece bottom stretches out the first extension rod that has two symmetries along the axial, and every first extension rod equally divide do not through arc connecting plate pin joint in on the corresponding mount pad, the bracing piece top stretches out along the axial has the second extension rod, and the supporting seat bottom is equipped with the mounting hole, the second extension rod pin joint is in the mounting hole.

2. An aircraft model support of multi-angle rotation as claimed in claim 1, wherein: the support rod comprises a hollow first rod body and a second rod body which is sleeved on the first rod body in a sliding mode, a plurality of notches are formed in the side wall of the second rod body along the radial direction, each notch is arranged at intervals, and the lock catch ring is clamped in one of the notches.

3. An aircraft model support of multi-angle rotation as claimed in claim 2, wherein: the lock catch ring is provided with an arc ring body and an inserting body extending out of the middle of the inner side wall of the arc ring body, the inner side wall of the arc ring body is attached to the outer side wall of the second rod body, and the inserting body is clamped in the notch.

4. An aircraft model support of multi-angle rotation as claimed in claim 2, wherein: the number of the notches is three, and each notch is arranged on the side wall of the second rod body along a radial straight line.

5. An aircraft model support of multi-angle rotation as claimed in claim 1, wherein: the bracing piece top extends there is the arc plate body, the arc plate body has the flat board portion and follows the triangle reinforcing plate portion that a flat board portion surface stretches out, and the second extension rod sets up on another surface of flat board portion along the axial.

6. An aircraft model support of multi-angle rotation as claimed in claim 1, wherein: the outer edge of the bottom of the disc body is provided with a plurality of hook parts, and each hook part is in sliding fit with the bottom of the annular sunk edge.

7. An aircraft model support frame of multi-angle rotation as claimed in claim 6, wherein: the hook parts are five, and each hook part is uniformly distributed at the bottom of the plate body along the circumferential direction.

8. An aircraft model support frame of multi-angle rotation as claimed in any one of claims 1 to 7, wherein: the supporting seat comprises a seat body with an upper opening and a containing cavity and a hexagonal prism which is used for connecting the aircraft and is hollow, the hexagonal prism is arranged in the containing cavity, and two side walls of the seat body close to the hexagonal prism respectively extend to form a U-shaped body.

9. An aircraft model support frame of multi-angle rotation as claimed in any one of claims 1 to 7, wherein: the base comprises a base plate and a base support plate extending out of the peripheral edge of the base plate, two first partition plates are arranged between the lower surface of the base plate and the base support plate adjacent to the base plate, and second partition plates are arranged between every two adjacent first partition plates and between the first partition plates and the base support plate.

10. The utility model provides an aircraft model battle exercise device which characterized in that: an airplane model support frame with multiple rotation angles as claimed in any one of claims 1 to 9, wherein each two adjacent bases are detachably connected.