CN212395856U - Airplane model airplane with anti-collision device - Google Patents

Abstract

The utility model discloses a take buffer stop's aircraft model aeroplane and model ship, including the model aeroplane and model ship body, the lower extreme of model aeroplane and model ship body is equipped with the layer board, the layer board is the camber structure, be equipped with the base under the layer board, the upper end of base is equipped with supports the cover, support the one end and the base fixed connection of cover, the other end of supporting the cover is equipped with well dead slot, well dead slot is equipped with the bracing piece, sliding connection between bracing piece and the well dead slot inside wall, the upper end of bracing piece extend support the cover and with layer board fixed connection, two wing edges of model aeroplane and model ship body all are equipped with the mounting panel, threaded connection has the staple on the lateral wall of mounting panel, threaded connection between staple and the model aerop. The anti-collision device arranged at the wing of the aircraft model airplane with the anti-collision device can effectively buffer and avoid the damage of the aircraft model airplane after the collision of the aircraft model airplane, and the aircraft model airplane is placed stably on the supporting plate and is not easy to collide and damage when not flying.

Description

Airplane model airplane with anti-collision device

Technical Field

The utility model relates to an aircraft model aeroplane and model ship correlation technique field specifically is a take buffer stop's aircraft model aeroplane and model ship.

Background

The model airplane is a generic term for various aircraft models. It includes model airplanes and other model airplanes. The aviation model activity arouses people's intense interest from the beginning, and the activity is prosperous for hundreds of years, and the main reason is that the aviation model has very important functions in the aspects of development of aviation industry and cultivation of scientific and technical talents, and the aviation model airplane can be used for carrying pesticide and killing insects, such as a plant protection machine, and the aviation model airplane is used for dragging a nylon wire from one mountain head to another mountain head, and then the steel wire is changed into a steel wire rope for high mountain stringing. And the model airplane can fly into the cloud layer, release the catalyst, perform artificial rainfall and the like.

The wings of the existing aircraft model are easy to collide when flying, so that the aircraft model is damaged, and the stability of the existing aircraft model placed on the aircraft model placing rack is not high when the existing aircraft model does not fly, so that the existing aircraft model is easy to collide and damage.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a take buffer stop's aircraft model aeroplane and model ship to the wing easily receives the collision when solving above-mentioned background art and proposing aircraft model aeroplane and model ship in flight, leads to the aircraft model aeroplane and model ship to destroy, and aircraft model aeroplane and model ship when not flying, places on aircraft model aeroplane and model ship rack stability not high, the problem of easy collision damage.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a take buffer stop's aircraft model aeroplane and model ship, includes the model aeroplane and model ship body, the lower extreme of model aeroplane and model ship body is equipped with the layer board, the layer board is the camber structure, be equipped with the base under the layer board, the upper end of base is equipped with supports the cover, the one end and the base fixed connection who supports the cover, the other end that supports the cover is equipped with well chute, well chute in is equipped with the bracing piece, sliding connection between bracing piece and the well chute inside wall, the upper end of bracing piece extend support cover and with layer board fixed connection, two wing edges of model aeroplane and model ship body all are equipped with the mounting panel, threaded connection has the staple on the lateral wall of mounting panel, threaded connection between staple and the model aeroplane and model aeroplane body, be equipped with the cushion chamber on the lateral wall of mounting panel, be equipped with.

Preferably, buffer gear includes first branch and second branch, first branch is fixed on the inside wall of cushion chamber, first branch is hollow structure, second branch slip cover is established in first branch, second branch extends the one end and the crashproof board fixed connection of first branch, the cover is equipped with the second spring on the second branch, the both ends of second spring respectively with crashproof board, first branch fixed connection.

Preferably, all be equipped with the recess on the relative lateral wall in the layer board, be equipped with first spring in the recess, the one end and the recess inside wall fixed connection of first spring, the other end fixedly connected with of first spring presss from both sides tight piece, it offsets with the model aeroplane and model ship body to press from both sides tight piece.

Preferably, the outer side wall of the support sleeve is provided with a locking screw for fixing the support rod inside.

Preferably, the lower end of the base is fixedly connected with a bottom cushion.

Preferably, the inner side wall of the supporting plate is fixedly connected with a bottom plate, and the bottom plate is abutted to the model airplane body.

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

1. when the model airplane does not fly, the model airplane body is placed on the supporting plate, the model airplane body is supported through the bottom plate, in the process of placing the model airplane body, the clamping block is stressed to compress the first spring, the first spring elastically returns to enable the clamping block to clamp the model airplane body, the stable placement of the model airplane body is guaranteed, the supporting plate is supported through the supporting rod in the supporting sleeve on the base, the supporting rod moves in the supporting sleeve, the height of the model airplane body is adjusted, the model airplane is convenient to view and rub, the model airplane body moves to a proper viewing height, the supporting rod is fixed in the supporting sleeve by rotating the locking screw, and the bottom pad at the lower end of the base is integrally stable;

2. when needs fly, place model aeroplane and model ship body flight in-process collision through the crashproof board on the mounting panel of model aeroplane and model ship body wing both sides, when encountering the collision, crashproof board atress makes second branch remove in first branch, the compression second spring, realize the atress buffering, avoid model aeroplane and model ship body damage, this take buffer of buffer's aircraft model aeroplane and model ship wing department's buffer stop that sets up on the aircraft model aeroplane and model ship, can effectively cushion after making the aircraft model aeroplane and model ship collision and avoid the aircraft model aeroplane and model ship impaired, and when the aircraft model aeroplane and model ship does not fly, place stably on the layer board, difficult collision is impaired.

Drawings

Fig. 1 is a schematic structural view of an aircraft model with an anti-collision device according to the present invention;

FIG. 2 is a schematic view of the internal structure of a supporting plate of an aircraft model with an anti-collision device according to the present invention;

fig. 3 is a schematic top view of an aircraft model with an anti-collision device according to the present invention;

fig. 4 is a schematic structural view of a portion a of fig. 3.

In the figure: the anti-collision device comprises a base pad 1, a support sleeve 2, a base 3, a locking screw 4, a support rod 5, a support plate 6, a model airplane body 7, a bottom plate 8, a first spring 9, a clamping block 10, a mounting plate 11, a fixing nail 12, a buffer mechanism 13, a buffer cavity 14 and an anti-collision plate 15.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.

Referring to fig. 1-4, the present invention provides an embodiment: the utility model provides a take buffer stop's aircraft model aeroplane and model ship, including model aeroplane and model ship body 7, the lower extreme of model aeroplane and model ship body 7 is equipped with layer board 6, layer board 6 is the camber structure, be equipped with base 3 under layer board 6, the upper end of base 3 is equipped with supports cover 2, the one end and the base 3 fixed connection of supporting cover 2, the other end of supporting cover 2 is equipped with the cavity groove, be equipped with bracing piece 5 in the cavity groove, sliding connection between bracing piece 5 and the cavity inslot lateral wall, the upper end of bracing piece 5 extends to support cover 2 and with layer board 6 fixed connection, two wing edges of model aeroplane and model ship body 7 all are equipped with mounting panel 11, threaded connection has staple 12 on the lateral wall of mounting panel 11, threaded connection between staple 12 and the model aeroplane and model aeroplane body 7, be equipped with buffer cavity 14 on the lateral wall of mounting panel 11, be.

The utility model discloses in: the buffer mechanism 13 comprises a first supporting rod and a second supporting rod, the first supporting rod is fixed on the inner side wall of the buffer cavity 14, the first supporting rod is of a hollow structure, the second supporting rod is slidably sleeved in the first supporting rod, one end, extending out of the first supporting rod, of the second supporting rod is fixedly connected with the anti-collision plate 15, the second supporting rod is sleeved with a second spring, two ends of the second spring are respectively and fixedly connected with the anti-collision plate and the first supporting rod, when the airplane needs to fly, the airplane model body 7 is placed through the anti-collision plates 15 on the mounting plates 11 on two sides of the wing of the airplane model body 7 to collide in the flying process, when the airplane encounters collision, the anti-collision plate 15 is stressed, the second supporting rod moves in the first supporting rod, the second spring is compressed, stress buffering is realized, and the; the opposite side walls in the supporting plate 6 are provided with grooves, a first spring 9 is arranged in each groove, one end of each first spring 9 is fixedly connected with the inner side wall of each groove, the other end of each first spring 9 is fixedly connected with a clamping block 10, each clamping block 10 abuts against the model airplane body 7, and in the placing process of the model airplane body 7, the clamping blocks 10 are stressed to compress the first springs 9, the first springs 9 are elastically restored, so that the clamping blocks 10 clamp the model airplane body 7, and the stable placing of the model airplane body 7 is ensured; the outer side wall of the supporting sleeve 2 is provided with a locking screw 4 for fixing the supporting rod 5 inside the supporting sleeve 2, the supporting rod 5 in the supporting sleeve 2 on the base 3 realizes the support of the supporting plate 6, the supporting rod 5 moves in the supporting sleeve 2, so that the height of the model airplane body 7 is adjusted, the model airplane is convenient to watch and rub, the supporting rod 5 is moved to a proper watching height, and the locking screw 4 is rotated to realize the fixation of the supporting rod 5 in the supporting sleeve 2; the lower end of the base 3 is fixedly connected with a bottom pad 1, and the bottom pad 1 at the lower end of the base 3 realizes the integral stability; fixedly connected with bottom plate 8 on the inside wall of layer board 6, bottom plate 8 offsets with model aeroplane and model ship body 7, places model aeroplane and model ship body 7 on layer board 6, realizes the support to model aeroplane and model ship body 7 through bottom plate 8.

The working principle is as follows: when the model airplane is not in flight, the model airplane body 7 is placed on the supporting plate 6, the supporting of the model airplane body 7 is realized through the bottom plate 8, in the process of placing the model airplane body 7, the clamping block 10 is stressed to compress the first spring 9, the first spring 9 elastically returns to enable the clamping block 10 to clamp the model airplane body 7, the stable placement of the model airplane body 7 is ensured, the supporting of the supporting plate 6 is realized through the supporting rod 5 in the supporting sleeve 2 on the base 3, the supporting rod 5 moves in the supporting sleeve 2 to enable the height of the model airplane body 7 to be adjusted to be convenient to observe and massage, the model airplane body 7 is moved to a proper observation height, the locking screw 4 is rotated to realize the fixation of the supporting rod 5 in the supporting sleeve 2, the bottom cushion 1 at the lower end of the base 3 realizes the integral stability, when the model airplane needs to fly, the collision is caused in the flight process of placing the model airplane body 7 through the collision-proof plates 15 on the mounting plates, the second supporting rod moves in the first supporting rod, the second spring is compressed, stress buffering is achieved, and damage to the model airplane body 7 is avoided.

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

Claims (6)

1. The utility model provides a take buffer stop's aircraft model aeroplane and model ship, includes model aeroplane and model ship body (7), its characterized in that: the lower extreme of model aeroplane and model ship body (7) is equipped with layer board (6), layer board (6) are the camber structure, be equipped with base (3) under layer board (6), the upper end of base (3) is equipped with supports cover (2), the one end and base (3) fixed connection of supporting cover (2), the other end of supporting cover (2) is equipped with well chute, well chute in is equipped with bracing piece (5), sliding connection between bracing piece (5) and the well chute inside wall, the upper end of bracing piece (5) extends to support cover (2) and with layer board (6) fixed connection, two edges of model aeroplane and model ship body (7) all are equipped with mounting panel (11), threaded connection has staple (12) on the lateral wall of mounting panel (11), threaded connection between staple (12) and model aeroplane body (7), be equipped with cushion chamber (14) on the lateral wall of mounting panel (11), an anti-collision plate (15) is arranged in the buffer cavity (14), and a buffer mechanism (13) is arranged between the anti-collision plate (15) and the mounting plate (11).

2. An aircraft model with an anti-collision device according to claim 1, characterized in that: buffer gear (13) include first branch and second branch, first branch is fixed on the inside wall of cushion chamber (14), first branch is hollow structure, the slip cover of second branch is established in first branch, second branch extends the one end and crashproof board (15) fixed connection of first branch, the cover is equipped with the second spring on the second branch, the both ends of second spring respectively with crashproof board, first branch fixed connection.

3. An aircraft model with an anti-collision device according to claim 1, characterized in that: all be equipped with the recess on the relative lateral wall in layer board (6), be equipped with first spring (9) in the recess, the one end and the recess inside wall fixed connection of first spring (9), the other end fixedly connected with of first spring (9) presss from both sides tight piece (10), it offsets with model aeroplane and model ship body (7) to press from both sides tight piece (10).

4. An aircraft model with an anti-collision device according to claim 1, characterized in that: and the outer side wall of the support sleeve (2) is provided with a locking screw (4) for fixing the support rod (5) inside.

5. An aircraft model with an anti-collision device according to claim 1, characterized in that: the lower end of the base (3) is fixedly connected with a bottom cushion (1).

6. An aircraft model with an anti-collision device according to claim 1, characterized in that: and a bottom plate (8) is fixedly connected to the inner side wall of the supporting plate (6), and the bottom plate (8) is abutted to the model airplane body (7).

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