Aircraft cargo bridge rear end toe board tail end supporting structure

Abstract

The utility model belongs to the technical field of aircraft cargo bridge rear end toe board tail end supporting structure design, and particularly relates to an aircraft cargo bridge rear end toe board tail end supporting structure which is simple in overall structure, light in weight, capable of being located below skin at the top ends of four band plates to make contact with the ground when a cargo bridge is put down, simple in force transmission path and high in reliability. The rear end of the toe board and a cargo bridge of the toe board can be stably supported, the four band boards and the two connecting boards are arranged in a crossed mode, and the overall structure is stable.

Description

Technical Field

[0001] The present application belongs to the technical field of design of a terminal support structure for the rear end toe plate of an aircraft cargo bridge, and specifically relates to a terminal support structure for the rear end toe plate of an aircraft cargo bridge. Background Art

[0002] A cargo bridge is set in the aircraft cargo hold. The front end of the cargo bridge is hinged to the cargo hold floor, the rear end of the cargo bridge is set with a toe board, and the end of the toe board is set with a supporting structure. When the cargo bridge is lowered, the supporting structure contacts the ground, forming support for the rear end of the toe board and its cargo bridge, forming a channel for transporting cargo.

[0003] Currently, the support structure at the end of the toe plate is complex and heavy, and lacks the necessary adjustment means when the slope of the cargo bridge is large, which increases the risk of cargo transportation.

[0004] This application is proposed in view of the above-mentioned technical defects. Utility Model Content

[0005] The purpose of the present application is to provide an end support structure of the rear end toe plate of an aircraft cargo bridge to overcome or alleviate at least one of the existing technical defects.

[0006] The technical solution of this application is:

[0007] An aircraft cargo bridge rear end toe plate end support structure, comprising:

[0008] Four straps are V-shaped and arranged in a transverse direction; the bottom end of each strap is connected to the web of each longitudinal beam at the rear end of the toe plate;

[0009] Two connecting plates are connected to the four belt plates in the transverse direction and are arranged crosswise with the belt plates;

[0010] The skin is covered on the outside of the four strip plates and the two connecting plates, with the edges at both ends extending to the bottom end of the strip plates and connecting the edge strips on both sides of the longitudinal beams at the rear end of the toe plate.

[0011] Optionally, in the above-mentioned aircraft cargo bridge rear end toe plate end support structure, the bottom ends of the four strip plates have V-shaped notches.

[0012] Optionally, in the above-mentioned aircraft cargo bridge rear end toe plate end support structure, the top ends of the four strip plates have circular through holes.

[0013] Optionally, in the above-mentioned aircraft cargo bridge rear end toe plate end support structure, two pairs of double ear plates are arranged between the two outermost belt plates and the adjacent belt plates, arranged parallel to the belt plates, and arranged crosswise with the two connecting plates;

[0014] There are two notches on the skin, exposing the top ends of the two outermost strips and two pairs of double ears.

[0015] Optionally, in the above-mentioned aircraft cargo bridge rear end toe plate end support structure, there are multiple process maintenance and drainage ports under the skin, and each process maintenance and drainage port is connected to each independent space formed by the cross-intersection of four strip plates and two connecting plates.

[0016] This application has at least the following beneficial technical effects:

[0017] The support structure for the end of the toe plate at the rear end of the aircraft cargo bridge disclosed in the above embodiment has a simple overall structure and is light in weight. When the cargo bridge is lowered, it can be located below the skin at the top end of the four strip plates and in contact with the ground. The force transmission path is simple, and a stable support can be formed for the rear end of the toe plate and its cargo bridge. The four strip plates and the two connecting plates are designed to be cross-arranged, and the overall structure is stable. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 2 is a schematic structural diagram of the end support structure of the rear end toe plate of an aircraft cargo bridge provided in an embodiment of the present application;

[0019] Figure 2 This is a partial schematic diagram of the end support structure of the rear end toe plate of an aircraft cargo bridge provided in an embodiment of the present application;

[0020] in:

[0021] 1-belt plate; 2-connecting plate; 3-skin; 4-double ear piece.

[0022] In order to better illustrate this embodiment, some parts of the drawings may be omitted, enlarged or reduced, and do not represent the size of the actual product. In addition, the drawings are only used for illustrative purposes and should not be understood as limiting this application. DETAILED DESCRIPTION

[0023] To make the technical solution and its advantages of this application more clear, the technical solution of this application will be further described in detail below with reference to the accompanying drawings. It should be understood that the specific embodiments described here are only some of the embodiments of this application and are only used to explain this application, not to limit this application. It should be noted that for ease of description, only the parts relevant to this application are shown in the accompanying drawings, and other relevant parts can refer to the general design.

[0024] In addition, unless otherwise defined, the technical terms or scientific terms used in the description of this application should have the usual meanings understood by those skilled in the art in the field to which this application belongs. The words indicating orientation used in the description of this application are only used to indicate relative directions or positional relationships. When the absolute position of the described object changes, its relative positional relationship may also change accordingly. The word "include" used in the description of this application means that the elements or objects appearing before the word include the elements or objects listed after the word and their equivalents, but does not exclude other elements or objects.

[0025] In addition, it should be noted that, unless otherwise clearly stipulated and limited, the words "installation", "connection" and similar terms used in the description of this application should be understood in a broad sense. For example, the connection can be a fixed connection or a detachable connection; it can be a mechanical connection or an electrical connection; it can be a direct connection or an indirect connection through an intermediate medium. Technical personnel in the field can understand its specific meaning in this application according to the specific circumstances.

[0026] Currently, the front end of the aircraft toe plate is connected to the rear end of the cargo bridge through two single and double ear joints, and the upper wall plate and the lower wall plate are connected to the upper wall surface and the lower wall surface of the rear end of the cargo bridge. A plurality of longitudinal beams are set at the rear end of the toe plate. Based on this, this application provides an aircraft cargo bridge rear end toe plate end support structure, such as Figure 1-Figure 2 Shown, including:

[0027] Four strip plates 1 are V-shaped and arranged in a transverse direction; the bottom end of each strip plate 1 is connected to the web of each longitudinal beam at the rear end of the toe plate, and can be connected by bolts;

[0028] Two connecting plates 2 are connected to the four strip plates 1 in the transverse direction and are arranged crosswise with the strip plates 1. They can be welded or integrally formed.

[0029] The skin 3 is covered on the outside of the four strip plates 1 and the two connecting plates 2, and can be connected to the edges of the four strip plates 1 and the two connecting plates 2 by screws or welding;

[0030] The edges of both ends of the skin 3 extend toward the bottom end of the belt plate 1 and are connected to the edge strips on both sides of the longitudinal beams at the rear end of the toe plate, and can be connected specifically by bolts.

[0031] The support structure for the end of the toe plate at the rear end of the aircraft cargo bridge disclosed in the above embodiment has a simple overall structure and is light in weight. When the cargo bridge is lowered, it can be located below the skin 3 at the top end of the four strip plates 1 and in contact with the ground. The force transmission path is simple, and a stable support can be formed for the rear end of the toe plate and its cargo bridge. The four strip plates 1 and the two connecting plates 2 are designed to be cross-arranged, and the overall structure is stable.

[0032] Furthermore, in the above-mentioned aircraft cargo bridge rear end toe plate end support structure, the bottom ends of the four strip plates 1 have V-shaped notches to reduce the overall mass of the structure.

[0033] Furthermore, in the above-mentioned aircraft cargo bridge rear end toe plate end support structure, the top ends of the four strip plates 1 have circular through holes to reduce the overall mass of the structure.

[0034] Furthermore, in the above-mentioned aircraft cargo bridge rear end toe plate end support structure, two pairs of double ear plates 4 are arranged between the two outermost belt plates 1 and the adjacent belt plates 4, are arranged parallel to the belt plates 4, and are arranged crosswise with the two connecting plates 2;

[0035] There are two notches on the skin 3, exposing the top ends of the two outermost strips 1 and the two pairs of double-ear pieces 4. When the cargo bridge is lowered at a large slope, the two joints at the front end of another separate toe plate can be connected to the top ends of the two pairs of double-ear pieces 4, and the upper and lower wall panels at the front end of the separate toe plate can be placed above and below the skin 3, so as to extend the length of the cargo bridge, reduce the slope when the cargo bridge is lowered, and reduce the risk of cargo transportation.

[0036] Furthermore, in the above-mentioned aircraft cargo bridge rear end toe plate end support structure, a plurality of process maintenance and drainage ports can be designed under the skin 3, and each process maintenance and drainage port is connected to each independent space formed by the cross-intersection of four strip plates 1 and two connecting plates 2, so as to facilitate the maintenance of the structure and drainage, and have a weight reduction effect.

[0037] The various embodiments in the specification are described in a progressive manner, and each embodiment focuses on the differences from other embodiments. The same or similar parts between the various embodiments can be referenced to each other. In the absence of conflict, the embodiments in this application and the technical features in the embodiments can be combined with each other to obtain new embodiments.

[0038] So far, the technical solution of the present application has been described in conjunction with the preferred embodiments shown in the accompanying drawings. Those skilled in the art should understand that the scope of protection of the present application is obviously not limited to these specific embodiments. Without departing from the principles of the present application, those skilled in the art can make equivalent changes or replacements to the relevant technical features, and the technical solutions after these changes or replacements will fall within the scope of protection of the present application.

Claims

1. An aircraft cargo bridge rear end toe plate end support structure, characterized in that: include: Four strip plates (1) are V-shaped and arranged in a transverse direction; the bottom end of each strip plate (1) is connected to the web of each longitudinal beam at the rear end of the toe plate; Two connecting plates (2) are connected to the four belt plates (1) in the transverse direction and are arranged in a cross pattern with the belt plates (1); The skin (3) is covered on the outside of the four strip plates (1) and the two connecting plates (2), and the edges at both ends extend toward the bottom end of the strip plates (1) to connect the edge strips on both sides of the longitudinal beams at the rear end of the toe plate.

2. The aircraft cargo bridge rear end toe plate end support structure according to claim 1, characterized in that: The bottom ends of the four strip plates (1) have V-shaped notches.

3. The aircraft cargo bridge rear end toe plate end support structure according to claim 2, characterized in that: The top ends of the four strip plates (1) are provided with circular through holes.

4. The aircraft cargo bridge rear end toe plate end support structure according to claim 3, characterized in that: Two pairs of double-ear pieces (4) are arranged between the two outermost strips (1) and the adjacent strips (4), are arranged parallel to the strips (4), and are arranged crosswise with the two connecting plates (2); There are two notches on the skin (3), exposing the top ends of the two outermost strips (1) and the two pairs of double ear pieces (4).

5. The aircraft cargo bridge rear end toe plate end support structure according to claim 4, characterized in that: There are multiple process maintenance and drainage openings below the skin (3), and each process maintenance and drainage opening is connected to each independent space formed by the cross-intersection of the four strip plates (1) and the two connecting plates (2).

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