CN216076675U

CN216076675U - Convenient-to-position hood lock assembly tool

Info

Publication number: CN216076675U
Application number: CN202122125835.8U
Authority: CN
Inventors: 杜兢
Original assignee: Suzhou Lake Precision Machinery Co ltd
Current assignee: Suzhou Lake Precision Machinery Co ltd
Priority date: 2021-09-05
Filing date: 2021-09-05
Publication date: 2022-03-18
Anticipated expiration: 2031-09-05

Abstract

The utility model discloses a conveniently-positioned hood lock assembling tool, and particularly relates to the technical field of hood locks. The protective cover can better cover and protect the lock hole when the lock hole is not used, the lock hole is prevented from being exposed, the damage to the lock hole is reduced, the service life of the hood lock body is prolonged, the hood lock body is conveniently installed on related equipment through the connecting piece, and the adaptability and the flexibility of the hood lock during installation are enhanced.

Description

Convenient-to-position hood lock assembly tool

Technical Field

The utility model relates to the technical field of hood locks, in particular to a hood lock assembling tool convenient to position.

Background

The aircraft bonnet is part mechanical equipment's important component part, when fixing the aircraft bonnet, need use the aircraft bonnet lock, the aircraft bonnet lock is generally through screw and bolt-up on relevant equipment, its installation location is comparatively convenient, but the keyhole on most aircraft bonnet locks on the market is direct often exposed outside, do not cover the protection well to it, external factors causes damage etc. to the keyhole easily, influence the use and the life of aircraft bonnet lock, and the aircraft bonnet lock is suitable for seting up more screw, its adaptability is general.

SUMMERY OF THE UTILITY MODEL

In order to overcome the above-mentioned drawbacks of the prior art, embodiments of the present invention provide a hood lock assembly fixture with convenient positioning, so as to solve the problems mentioned in the above background art.

In order to achieve the purpose, the utility model provides the following technical scheme: the utility model provides a location convenient aircraft bonnet lock assembly fixture, includes aircraft bonnet lock body and locates the keyhole on the aircraft bonnet lock body, recess and fixed orifices are seted up in the front of aircraft bonnet lock body, just keyhole and fixed orifices all are located the recess, the inside rotation of recess is connected with the bull stick, the surface of bull stick is equipped with the protection casing, just one side that the protection casing is close to the aircraft bonnet lock body closely contradicts at the surface of keyhole, the back of aircraft bonnet lock body is equipped with the connecting piece, a plurality of threaded connection hole has been seted up to the inside of connecting piece, the surface of connecting piece is equipped with a plurality of spacer, and a plurality of even hole has all been seted up to the inside of spacer.

Preferably, the interior capping of protection casing is equipped with flexible inserted bar, the one end of flexible inserted bar is equipped with magnet one, the inside of fixed orifices is equipped with magnet two, just the surface of flexible inserted bar and magnet one all contradicts at the internal surface of fixed orifices, just the surface of magnet one and magnet two passes through magnetic force and adsorbs.

Preferably, the front face of the protective cover is provided with a pulling convex piece.

Preferably, the front surface of the connecting piece is provided with an indicating line.

Preferably, the keyhole is located between the rotating rod and the fixing hole.

Preferably, a plurality of the threaded connecting holes are distributed in a straight line at equal intervals.

Preferably, the hood lock body is located between a plurality of the positioning pieces.

The utility model has the technical effects and advantages that:

1. compared with the prior art, through setting up the protection casing etc. can drive the protection casing and expose or block the keyhole, cover the protection when the keyhole does not use better, avoid the keyhole to expose, reduce the damage to the keyhole, prolonged the life of aircraft bonnet lock body.

2. Compared with the prior art, through setting up the connecting piece, can select and install the aircraft bonnet lock body on relevant equipment through the bolt according to required a plurality of threaded connection holes on the connecting piece, adaptability and flexibility when reinforcing aircraft bonnet lock installation, the installation of being convenient for is used, and spacer and instruction line can indicate better and fix a position when aircraft bonnet lock body installs, the use of the aircraft bonnet lock main part of being convenient for.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention.

Fig. 2 is a schematic view of a specific structure of the keyhole of the present invention.

Fig. 3 is a schematic view of a specific structure of the connector of the present invention.

FIG. 4 is a schematic view of the enlarged structure of part A of the present invention.

FIG. 5 is a side sectional partial view of the hood lock body of the present invention.

The reference signs are: 1. a hood lock body; 2. a keyhole; 3. a groove; 4. a fixing hole; 5. a rotating rod; 6. a protective cover; 7. a connecting member; 8. connecting a threaded hole; 9. positioning plates; 10. connecting holes; 11. a flexible insertion rod; 12. a magnet I; 13. a second magnet; 14. pulling the convex piece; 15. lines are indicated.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is described in further detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the utility model and are not intended to limit the utility model.

The hood lock assembling tool convenient to position as shown in the attached figures 1-5 comprises a hood lock body 1 and a lock hole 2 arranged on the hood lock body 1, wherein a groove 3 and a fixing hole 4 are formed in the front surface of the hood lock body 1, the lock hole 2 and the fixing hole 4 are both positioned in the groove 3, a rotating rod 5 is rotatably connected inside the groove 3, a protective cover 6 is arranged on the outer surface of the rotating rod 5, and one side, close to the hood lock body 1, of the protective cover 6 tightly abuts against the outer surface of the lock hole 2;

the protective cover 6 can be pulled open, the rotating rod 5 is stressed to rotate in the groove 3, so that the keyhole 2 on the hood lock body 1 is exposed for related use such as key insertion, when the keyhole 2 is not required to be exposed, the protective cover 6 can be retracted into the groove 3, so that the keyhole 2 is better covered and protected by the protective cover 6, the keyhole 2 is prevented from being exposed when not used, the damage to the keyhole 2 is reduced, and the service life of the hood lock body 1 is prolonged;

the back of the hood lock body 1 is provided with a connecting piece 7, a plurality of threaded connecting holes 8 are formed in the connecting piece 7, a plurality of positioning pieces 9 are arranged on the outer surface of the connecting piece 7, and connecting holes 10 are formed in the plurality of positioning pieces 9; wherein, can select and install aircraft bonnet lock body 1 on relevant equipment through the bolt according to required threaded connection hole 8 on to connecting piece 7, adaptability and flexibility when reinforcing aircraft bonnet lock installation, and need not to lock at the aircraft bonnet and trompil makes it be connected with relevant equipment, and the spacer 9 on the connecting piece 7 can instruct the location better when aircraft bonnet lock body 1 installs, the use of the location and the aircraft bonnet lock cover of being convenient for.

In a preferred embodiment, as shown in fig. 5, the inner cover surface of the protective cover 6 is provided with a flexible insertion rod 11, one end of the flexible insertion rod 11 is provided with a first magnet 12, the inside of the fixing hole 4 is provided with a second magnet 13, the outer surfaces of the flexible insertion rod 11 and the first magnet 12 are abutted against the inner surface of the fixing hole 4, and the outer surfaces of the first magnet 12 and the second magnet 13 are attracted by magnetic force, so that when the protective cover 6 covers the keyhole 2, the flexible insertion rod 11 and the first magnet 12 on the protective cover 6 are forced to be inserted into the fixing hole 4 and mutually attracted with the second magnet 13 for fixing, and when the protective cover 6 is opened, the flexible insertion rod 11 and the first magnet 12 are forced to be removed from the fixing hole 4, and the first magnet 12 is separated from the second magnet 13, thereby enhancing flexibility and stability of the protective cover 6.

In a preferred embodiment, as shown in fig. 1 and 5, the front surface of the hood 6 is provided with a pull tab 14 to facilitate grasping, forcing, etc., and to facilitate opening or closing of the hood 6.

In a preferred embodiment, as shown in fig. 1, 2 and 3, the front surface of the connecting member 7 is provided with an indicating line 15 to facilitate the positioning indication of the installation and use of the hood lock body 1, which is more intuitive.

In a preferred embodiment, as shown in fig. 1 and 2, the keyhole 2 is located between the rotating rod 5 and the fixing hole 4, so as to avoid the contact between the keyhole 2 and the rotating rod 5 and other related devices, so that the opening or closing of the protective cover 6 is facilitated, thereby facilitating the use and protective protection of the hood lock and reducing the external influence.

In a preferred embodiment, as shown in fig. 1, fig. 2 and fig. 3, a plurality of threaded connection holes 8 are distributed in a straight line at equal intervals, so that the plurality of threaded connection holes 8 increase the adaptability during installation, can be appropriately selected according to needs, and is convenient.

In a preferred embodiment, as shown in fig. 1 and 2, the hood lock body 1 is located between a plurality of positioning pieces 9 to facilitate better indexing of the periphery of the hood lock body 1.

The working principle of the utility model is as follows: when in use, the protective cover 6 can be pulled open by pulling the convex piece 14, the rotating rod 5 is forced to rotate in the groove 3, thereby exposing the keyhole 2 on the hood lock body 1 for related use such as key insertion, when the keyhole 2 is not required to be exposed, the protective cover 6 can be retracted into the groove 3, at the moment, the flexible inserted rod 11 and the first magnet 12 on the protective cover 6 are inserted into the fixing hole 4 under force and mutually attract and fix with the second magnet 13, thereby leading the protective cover 6 to better cover and protect the keyhole 2, avoiding the keyhole 2 from being exposed when not in use, reducing the damage to the keyhole 2, prolonging the service life of the hood lock body 1, and the threaded connection hole 8 on the connecting piece 7 can be selected according to the requirement and the hood lock body 1 is installed on the related equipment through the bolt, thus enhancing the adaptability and flexibility of the hood lock, facilitating the operation, and the positioning piece 9 and the indicating line 15 can be better indicated and positioned when the hood lock body 1 is installed.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a convenient aircraft bonnet lock assembly fixture fixes a position, includes aircraft bonnet lock body (1) and locates keyhole (2) on aircraft bonnet lock body (1), its characterized in that: the front of aircraft bonnet lock body (1) is seted up flutedly (3) and fixed orifices (4), just keyhole (2) and fixed orifices (4) all are located flutedly (3), the inside rotation of recess (3) is connected with bull stick (5), the surface of bull stick (5) is equipped with protection casing (6), just protection casing (6) are close to the surface of closely conflicting at keyhole (2) in one side of aircraft bonnet lock body (1), the back of aircraft bonnet lock body (1) is equipped with connecting piece (7), a plurality of threaded connection hole (8) have been seted up to the inside of connecting piece (7), the surface of connecting piece (7) is equipped with a plurality of spacer (9), and a plurality of even hole (10) have all been seted up to the inside of spacer (9).

2. The convenient-to-position hood lock assembling tool of claim 1, characterized in that: the interior capping of protection casing (6) is equipped with flexible inserted bar (11), the one end of flexible inserted bar (11) is equipped with magnet (12), the inside of fixed orifices (4) is equipped with magnet two (13), just the surface of flexible inserted bar (11) and magnet one (12) all contradicts at the internal surface of fixed orifices (4), just the surface of magnet one (12) and magnet two (13) passes through magnetic force and adsorbs.

3. The convenient-to-position hood lock assembling tool of claim 1, characterized in that: the front surface of the protective cover (6) is provided with a pulling convex part (14).

4. The convenient-to-position hood lock assembling tool of claim 1, characterized in that: the front surface of the connecting piece (7) is provided with an indicating line (15).

5. The convenient-to-position hood lock assembling tool of claim 1, characterized in that: the keyhole (2) is positioned between the rotating rod (5) and the fixing hole (4).

6. The convenient-to-position hood lock assembling tool of claim 1, characterized in that: the plurality of the threaded connecting holes (8) are distributed in a straight line at equal intervals.

7. The convenient-to-position hood lock assembling tool of claim 1, characterized in that: the hood lock body (1) is positioned among the positioning pieces (9).