CN219325212U - Tool for disassembling aircraft landing gear bolt - Google Patents

Abstract

The utility model discloses a tool for disassembling an aircraft landing gear bolt, which belongs to the technical field of manual tools and comprises the following components: the bolt attaching part is a cylinder, a wide groove is formed in the bolt attaching part, and the width of the groove is the same as the hexagonal opposite side width of the aircraft landing gear bolt; the hexagonal part is a hexagonal prism, and the opposite side width is consistent with the opening width of the common universal wrench; the tool is fully attached to the bolt of the aircraft landing gear, and does not slip when in use, and the tool can be placed on the bolt from different directions, so that a user can conveniently use the tool in a narrow space.

Description

Tool for disassembling aircraft landing gear bolt

Technical Field

The utility model relates to the technical field of manual tools, in particular to a tool for disassembling an aircraft landing gear bolt.

Background

The bolt disassembly process on the aircraft landing gear is time-consuming and labor-consuming, the bolt is a non-standard component, a tool commonly used in the market cannot be fully attached to the bolt, slipping or skewing is caused between the tool and the bolt during disassembly, and the bolt is damaged when serious, so that the bolt is more difficult to disassemble. The present utility model therefore proposes a tool for the bolt removal of an aircraft landing gear.

Disclosure of Invention

The utility model aims to provide a tool for disassembling an aircraft landing gear bolt, which solves the technical problem.

In order to achieve the above purpose, the present utility model provides the following technical solutions:

a tool for aircraft landing gear bolt removal, comprising:

the bolt attaching part is a cylinder, a wide groove is formed in the bolt attaching part, and the width of the groove is the same as the hexagonal opposite side width of the aircraft landing gear bolt;

and the hexagonal part is a hexagonal prism, and the opposite side width is consistent with the opening width of a common universal wrench.

As a further technical scheme of the utility model, through holes are arranged at the centers of the bolt attaching part and the hexagonal part.

Compared with the prior art, the utility model has the beneficial effects that: the tool is fully attached to the bolt of the aircraft landing gear, and does not slip when in use, and the tool can be placed on the bolt from different directions, so that a user can conveniently use the tool in a narrow space.

Drawings

FIG. 1 is a schematic structural view of a tool for aircraft landing gear bolt removal.

Fig. 2 is a schematic view of the structure of a tool for aircraft landing gear bolt removal in use.

Reference numerals annotate: 1-bolt laminating part, 2-hexagon part, 3-wide groove.

Detailed Description

In the description of the present utility model, it should 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", "axial", "radial", "circumferential", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings are merely for convenience in describing the present utility model and simplifying the description, and do not indicate or imply that the device or element being referred to must have a specific orientation, be configured and operated in a specific orientation, and therefore should not be construed as limiting the present utility model.

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

In the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the present utility model can be understood by those of ordinary skill in the art according to the specific circumstances.

The technical scheme of the patent is further described in detail below with reference to the specific embodiments.

Referring to fig. 1-2 as one embodiment of the present utility model, a tool for aircraft landing gear bolt removal includes:

the bolt attaching part 1 is a cylinder, a wide groove 3 is formed in the bolt attaching part 1, and the groove width is the same as the hexagonal opposite side width of the aircraft landing gear bolt;

and the hexagonal part 2 is a hexagonal prism, and the opposite side width is consistent with the opening width of a common universal wrench.

In the embodiment of the utility model, through holes are arranged at the centers of the bolt attaching part 1 and the hexagonal part 2, so that the bolt attaching part is conveniently sleeved on a tool hook.

In use, the wide slot 3 in the bolt engaging portion 1 of the tool is aligned with the hexagon of the aircraft landing gear bolt head, and the tool is engaged with the aircraft landing gear bolt. The opening of the universal open spanner is matched with the parallel edge of the hexagonal part 2 of the tool, the spanner is rotated anticlockwise, the bolt is unscrewed, the open spanner is taken away after the bolt is disassembled, and the tool is taken down from the bolt.

It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model 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.

Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art.

Claims (2)

1. A tool for aircraft landing gear bolt removal, comprising:

the bolt attaching part is a cylinder, a wide groove is formed in the bolt attaching part, and the width of the groove is the same as the hexagonal opposite side width of the aircraft landing gear bolt;

and the hexagonal part is a hexagonal prism, and the opposite side width is consistent with the opening width of a common universal wrench.

2. A tool for aircraft landing gear bolt removal according to claim 1, wherein the bolt engaging portion and hexagonal portion are provided with a through hole at the centre thereof.

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