CN212202728U - Quick mounting and dismounting clip for airplane - Google Patents

Abstract

The utility model discloses a checkpost is dismantled in quick installation of aircraft, the on-line screen storage device comprises a base, the base the upper portion position fixed mounting placed in the middle of the base has the support column, the top fixed mounting of support column has the card ball, the outside cover of support column is equipped with the fixed plate, upper portion one side position fixed mounting of fixed plate has first checkpost seat, the upper portion opposite side position fixed mounting of fixed plate has second checkpost seat, be equipped with the spliced pole between first checkpost seat and the second checkpost seat, upper surface position placed in the middle between first checkpost seat and the second checkpost seat has seted up logical groove, the fixed orifices has been seted up to the upper surface turning position of first checkpost seat and second checkpost seat. A checkpost is dismantled in quick installation of aircraft, the resilience ability after can increasing the elasticity performance and the deformation of checkpost improves the stability of checkpost, secondly has regulatory function, can be suitable for the not card ball of equidimension.

Description

Quick mounting and dismounting clip for airplane

Technical Field

The utility model relates to a checkpost field, in particular to checkpost is dismantled in quick installation of aircraft.

Background

The airplane clamp is a connecting tool used on an airplane, is mainly connected in a clamping mode, can be used for connecting two plates, sheets and blocky objects, and belongs to a clamping structure; but current aircraft checkpost has the phenomenon that elasticity reduces after the frequent use for the life of checkpost reduces, and the phenomenon that drops also appears easily in checkpost elasticity reduction, is unfavorable for the use, secondly does not possess regulatory function, and the inconvenient block interval to the condition regulation checkpost has reduced application scope, and the result of use is relatively poor.

SUMMERY OF THE UTILITY MODEL

The utility model discloses a main aim at provides a checkpost is dismantled in quick installation of aircraft, can effectively solve the problem in the background art.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

the utility model provides a checkpost is dismantled in quick installation of aircraft, the on-line screen storage device comprises a base, the base the upper portion position fixed mounting placed in the middle of the base has the support column, the top fixed mounting of support column has the card ball, the outside cover of support column is equipped with the fixed plate, upper portion one side position fixed mounting of fixed plate has first checkpost seat, the upper portion opposite side position fixed mounting of fixed plate has second checkpost seat, be equipped with the spliced pole between first checkpost seat and the second checkpost seat, upper surface position placed in the middle between first checkpost seat and the second checkpost seat has seted up logical groove, the fixed orifices has been seted up to the upper surface turning position of first checkpost seat and second checkpost seat.

Preferably, the upper portion fixed mounting of first checkpost seat has the checkpost, the top an organic whole of checkpost is connected with spacing piece, be the V font between checkpost and the spacing piece.

Preferably, a second reinforcing elastic rib is fixedly connected between the clip and the first clip seat, and a first reinforcing elastic rib is fixedly connected between the clip and the limiting piece.

Preferably, the number of spliced pole is two, spliced pole and first checkpost seat fixed connection, spliced pole and second checkpost seat swing joint.

Preferably, the number of the second reinforcing elastic ribs is two, and the first reinforcing elastic ribs and the second reinforcing elastic ribs are arranged in a V shape.

Compared with the prior art, the utility model discloses following beneficial effect has: the utility model discloses in, consolidate through the first reinforcement that sets up and play the muscle and the second and play the muscle, first reinforcement plays muscle fixed connection between spacing piece and checkpost, the second consolidates and plays muscle fixed connection between checkpost and first checkpost, can increase elasticity and the ability of resetting after the deformation between spacing piece and checkpost and the first checkpost respectively, great improvement the life of aircraft checkpost, the practicality is higher, and elasticity reinforcing, be difficult to appear the problem that drops, through the spliced pole that sets up, divide into two parts with the checkpost, be first checkpost seat and second checkpost seat respectively, then connect through the spliced pole, in the installation, can adjust the interval between first checkpost seat and the second checkpost seat to needs, make and be applicable to the card ball of equidimension not, the application scope is improved.

Drawings

FIG. 1 is a schematic view of the overall structure of a quick mounting and dismounting clip for an aircraft according to the present invention;

FIG. 2 is a view showing the base and the fixing plate of the quick mounting and dismounting clip of the aircraft of the present invention;

fig. 3 is the utility model relates to a local structure plan view of checkpost is dismantled in quick installation of aircraft.

In the figure: 1. a base; 2. a support pillar; 3. blocking the ball; 4. a fixing plate; 5. a first card base; 6. a second card base; 7. a clip; 8. a limiting sheet; 9. a first reinforcing elastic rib; 10. a second reinforcing elastic rib; 11. connecting columns; 12. a through groove; 13. and (7) fixing holes.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element to which the reference is made must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

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

As shown in fig. 1-3, a clip for quickly mounting and dismounting an airplane comprises a base 1, wherein a support column 2 is fixedly mounted at the middle position of the upper part of the base 1, a clip ball 3 is fixedly mounted at the top end of the support column 2, a fixing plate 4 is sleeved outside the support column 2, a first clip seat 5 is fixedly mounted at one side position of the upper part of the fixing plate 4, a second clip seat 6 is fixedly mounted at the other side position of the upper part of the fixing plate 4, a connecting column 11 is arranged between the first clip seat 5 and the second clip seat 6, a through groove 12 is formed at the middle position of the upper surface between the first clip seat 5 and the second clip seat 6, and fixing holes 13 are formed at the corner positions of the upper surfaces of the first clip seat 5 and the second clip seat 6;

a clip 7 is fixedly installed on the upper part of the first clip seat 5, a limiting piece 8 is integrally connected to the top end of the clip 7, and the clip 7 and the limiting piece 8 are in a V shape; the second reinforcing elastic rib 10 is fixedly connected between the clip 7 and the first clip seat 5, the first reinforcing elastic rib 9 is fixedly connected between the clip 7 and the limiting piece 8, and the elasticity and the resetting capability after deformation between the limiting piece 8 and the clip 7 and between the clip 7 and the first clip seat 5 can be respectively increased through the arrangement of the first reinforcing elastic rib 9 and the second reinforcing elastic rib 10, so that the service life of the aircraft clip is greatly prolonged, the practicability is higher, the elasticity is enhanced, and the problem of falling off is not easy to occur; the aircraft clip is divided into two parts, namely a first clip seat 5 and a second clip seat 6 through the arrangement of the connecting columns 11, and then the two parts are connected through the connecting columns 11, so that the space between the first clip seat 5 and the second clip seat 6 can be adjusted according to the requirement during installation, the aircraft clip is suitable for the clip balls 3 with different sizes, and the application range is improved; the number of the second reinforcing elastic ribs 10 is two, and the first reinforcing elastic ribs 9 and the second reinforcing elastic ribs 10 are arranged in a V shape.

What need explain, the utility model relates to a checkpost is dismantled in quick installation of aircraft, when using, at first adjust the interval between first checkpost seat 5 and the second checkpost seat 6 to the in service behavior, during the operation, directly with first checkpost seat 5 and second checkpost seat 6 with opposite direction pulling can, first checkpost seat 5 drives the inside activity of spliced pole 11 at second checkpost seat 6, thereby adjust the space, then can push into logical groove 12 with calorie ball 3, the application of force extrusion, pressure leads to two spacing pieces 8 and two checkposts 7 to produce the deformation phenomenon, thereby calorie ball 3 crosses two spacing pieces 8, can accomplish the joint work, be equipped with first reinforcement bullet muscle 9 between checkpost 7 and the spacing piece 8, be equipped with second reinforcement bullet muscle 10 between checkpost 7 and the first checkpost seat 5, first reinforcement bullet muscle 9 and second reinforcement muscle 10 can increase spacing piece 8 and 7 respectively and the checkpost 7 and the elasticity between checkpost seat 5 and the ability of restoreing after the deformation can Power, great improvement the life of aircraft checkpost, the practicality is higher, and the elasticity reinforcing is difficult to the problem that drops to appear moreover.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims (5)

1. The utility model provides an aircraft is quick to be installed and is dismantled checkpost which characterized in that: including base (1), base (1) the upper portion position fixed mounting placed in the middle of base (1) has support column (2), the top fixed mounting of support column (2) has calorie ball (3), the outside cover of support column (2) is equipped with fixed plate (4), upper portion one side position fixed mounting of fixed plate (4) has first card seat (5), the upper portion opposite side position fixed mounting of fixed plate (4) has second card seat (6), be equipped with spliced pole (11) between first card seat (5) and second card seat (6), logical groove (12) have been seted up to the upper surface position placed in the middle between first card seat (5) and second card seat (6), fixed orifices (13) have been seted up to the upper surface corner position of first card seat (5) and second card seat (6).

2. An aircraft quick-attach and detach clip according to claim 1, wherein: the upper portion fixed mounting of first checkpost seat (5) has checkpost (7), the top an organic whole of checkpost (7) is connected with spacing piece (8), be the V font between checkpost (7) and spacing piece (8).

3. An aircraft quick-attach and detach clip according to claim 1, wherein: fixedly connected with second reinforcement bullet muscle (10) between checkpost (7) and first checkpost seat (5), fixedly connected with first reinforcement bullet muscle (9) between checkpost (7) and spacing piece (8).

4. An aircraft quick-attach and detach clip according to claim 1, wherein: the number of the connecting columns (11) is two, the connecting columns (11) are fixedly connected with the first clamping seats (5), and the connecting columns (11) are movably connected with the second clamping seats (6).

5. An aircraft quick-attach and detach clip according to claim 3, wherein: the number of the second reinforcing elastic ribs (10) is two, and the first reinforcing elastic ribs (9) and the second reinforcing elastic ribs (10) are arranged in a V shape.

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