Amphibious vehicle cockpit assembly device

Abstract

The present invention provides an amphibious vehicle cockpit assembly device, comprising a taillight support plate for assembling taillights, the taillight support plate being vertically mounted on a heat radiating hood bracket, the heat radiating hood bracket being fixed on the top of the heat radiating hood plate, the heat radiating hood bracket being also fitted and fixed on the cockpit support plate, and the cockpit support plate being fixedly connected to the engine cover plate of the engine. The present invention has the beneficial effect that the taillight support plate for assembling the taillight is connected to the cockpit support plate on the engine cover plate on the basis of installing the heat radiating hood bracket, because the heat radiating hood bracket is connected in the vertical direction and the cockpit support plate is supported in the horizontal direction, the stability of the taillight support plate can be greatly improved, thereby improving the installation stability of the taillight of the following vehicle.

Description

Technical Field

[0001] The present invention relates to the technical field of amphibious vehicle intelligent equipment, and in particular to an amphibious vehicle cockpit assembly device. Background Art

[0002] The rear taillight of the amphibious vehicle is mounted on the radiator bracket above the radiator. The existing taillight is only supported by the radiator bracket. The amphibious vehicle vibrates violently during operation and the working environment is relatively harsh. The existing taillight support is not stable enough and the lampshade is often loose. Therefore, the existing technology has defects and needs to be further improved and perfected. Summary of the invention

[0003] The present invention aims to provide an amphibious vehicle cockpit assembly device to alleviate the technical problem of insufficient taillight assembly stability.

[0004] To achieve the above object, the technical solution of the present invention is achieved as follows:

[0005] A cockpit assembly device for an amphibious vehicle comprises a taillight support plate for assembling taillights, wherein the taillight support plate is vertically mounted on a heat dissipation cover bracket, the heat dissipation cover bracket is fixed on the top of the heat dissipation cover plate, the heat dissipation cover bracket is also fitted and fixed on the cockpit support plate, and the cockpit support plate is fixedly connected to a hood cover plate of an engine.

[0006] Furthermore, the cockpit support plate and the heat dissipation cover bracket are arranged in parallel and in close contact with each other, and the heat dissipation cover bracket is assembled on the cockpit support plate by fixing bolts.

[0007] Furthermore, a cockpit bracket is also provided on the cockpit support plate, and the cockpit bracket includes a second flange, and the second flange forms a bent positioning groove, and the positioning groove matches the first flange of the heat dissipation cover bracket.

[0008] Furthermore, a shoulder frame for avoiding the heat dissipation cover frame is provided between the cockpit frame and the second flange.

[0009] Furthermore, the cockpit bracket covers both sides of the cockpit support plate.

[0010] Furthermore, the outer edge of the second flange is also provided with a folded edge for increasing the clamping force.

[0011] Furthermore, the cockpit bracket, the second flange and the folded edge are integrally formed.

[0012] Furthermore, a guide groove is arranged in the positioning groove of the second flange, and the guide groove is arranged along the insertion direction of the first flange.

[0013] Furthermore, the heat dissipation cover bracket and the cabin support plate are aluminum plates that are easy to dissipate heat.

[0014] Compared with the prior art, the amphibious vehicle cockpit assembly device described in the present invention has the following advantages: the taillight support plate for assembling the taillight is connected to the cockpit support plate on the hood cover plate on the basis of installing the heat dissipation cover bracket. Since the heat dissipation cover bracket is connected in the vertical direction and the cockpit support plate is supported in the horizontal direction, the temperature resistance of the taillight support plate can be greatly improved, thereby improving the installation stability of the taillight of the following vehicle. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] The drawings constituting part of the present invention are used to provide a further understanding of the present invention. The exemplary embodiments and descriptions of the present invention are used to explain the present invention and do not constitute an improper limitation on the present invention. In the drawings:

[0016] Figure 1 It is a structural schematic diagram of an amphibious vehicle cockpit assembly device according to an embodiment of the present invention;

[0017] Figure 2 It is a schematic assembly diagram of the amphibious vehicle cockpit assembly device according to an embodiment of the present invention.

[0018] Description of reference numerals:

[0019] 10-heat dissipation cover plate; 11-heat dissipation cover bracket; 12-tail light support plate; 13-hood cover plate; 14-cockpit support plate; 15-positioning groove; 16-cockpit bracket; 17-shoulder frame; 18-fixing bolt; 19-first flange; 20-second flange. DETAILED DESCRIPTION

[0020] The technical solution of the present invention will be described clearly and completely in conjunction with the embodiments below. Obviously, the described embodiments are part of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0021] Example

[0022] The technical problem to be solved by this embodiment is that the rear taillight of the amphibious vehicle is assembled on the heat dissipation cover bracket 11 above the heat dissipation cover. The existing taillight only passes through the heat dissipation cover bracket 11. The amphibious vehicle vibrates relatively violently during operation and the working environment is relatively harsh. The existing taillight support stability is insufficient and the lampshade is often loose.

[0023] In order to solve the above technical problems, this embodiment provides an amphibious vehicle cockpit assembly device, such as Figure 1-2As shown, it includes a taillight support plate 12 for assembling the taillight, the taillight support plate 12 is vertically mounted on a heat dissipation cover bracket 11, the heat dissipation cover bracket 11 is fixed on the top of the heat dissipation cover plate 10, the heat dissipation cover bracket 11 is also fitted and fixed on a cabin support plate 14, and the cabin support plate 14 is fixedly connected to the engine cover cover plate 13.

[0024] Specifically, the cockpit support plate 14 is arranged in parallel with the heat dissipation cover bracket 11 , and the heat dissipation cover bracket 11 is assembled on the cockpit support plate 14 by fixing bolts 18 .

[0025] The cockpit support plate 14 is also provided with a cockpit bracket 16, and the cockpit bracket 16 includes a second flange 20, and the second flange 20 forms a bent positioning groove 15, and the positioning groove 15 matches the first flange 19 of the heat dissipation cover bracket 11. A shoulder frame 17 is provided between the cockpit bracket 16 and the second flange 20 to avoid the heat dissipation cover bracket 11. The cockpit bracket 16 covers both sides of the cockpit support plate 14. The outer edge of the second flange 20 is also provided with a return folding edge to increase the clamping force. The cockpit bracket 16, the second flange 20 and the return folding edge are integrally formed. A guide slide is provided in the positioning groove 15 of the second flange 20, and the guide slide is provided along the direction in which the first flange 19 is inserted. The heat dissipation cover bracket 11 and the cockpit support plate 14 are aluminum plates that are easy to dissipate heat.

[0026] The taillight support plate 12 for assembling the taillight is connected to the cockpit support plate 14 on the hood cover plate 13 on the basis of installing the heat dissipation cover bracket 11. Since the heat dissipation cover bracket 11 is connected in the vertical direction and the cockpit support plate 14 is supported in the horizontal direction, the stability of the taillight support plate 12 can be greatly improved, thereby improving the installation stability of the taillight of the following vehicle.

[0027] In the description of the present invention, it should be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present invention. In addition, the terms "first", "second", etc. are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, features defined as "first", "second", etc. may explicitly or implicitly include one or more of the features. In the description of the present invention, unless otherwise specified, "multiple" means two or more.

[0028] In the description of the invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be indirectly connected through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the invention can be understood according to specific circumstances.

[0029] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. An amphibious vehicle cockpit assembly device, comprising a taillight support plate for assembling a taillight, wherein the taillight support plate is vertically mounted on a heat dissipation cover bracket, and the heat dissipation cover bracket is fixed on the top of the heat dissipation cover plate, characterized in that: The heat dissipation cover bracket is also fitted and fixed on the cockpit support plate, and the cockpit support plate is fixedly connected to the engine cover sealing plate; The cockpit support plate is arranged parallel to the heat dissipation cover bracket, and the heat dissipation cover bracket is assembled on the cockpit support plate by fixing bolts; The cockpit support plate is also provided with a cockpit bracket, the cockpit bracket includes a second flange, the second flange forms a bent positioning groove, and the positioning groove matches the first flange of the heat dissipation cover bracket; A shoulder frame for avoiding the heat dissipation cover frame is arranged between the cockpit frame and the second flange; The cockpit bracket covers both sides of the cockpit support plate; The outer edge of the second flange is also provided with a folded edge to increase the clamping force; The cockpit bracket, the second flange and the return fold are integrally formed; A guide slot is arranged in the positioning slot of the second flange, and the guide slot is arranged along the direction in which the first flange is inserted.

2. The amphibious vehicle cockpit assembly device according to claim 1, characterized in that: The heat dissipation cover bracket and the cabin support plate are aluminum plates that are easy to dissipate heat.

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