CN218713478U

CN218713478U - Electric loader

Info

Publication number: CN218713478U
Application number: CN202222666212.6U
Authority: CN
Inventors: 陆其东; 黄胤真; 唐柏玉; 韦建明; 王慧春; 程顺; 程范清; 尹向瑜; 黄浩; 黄桂华
Original assignee: Guangxi Liugong Machinery Co Ltd
Current assignee: Guangxi Liugong Machinery Co Ltd
Priority date: 2022-10-11
Filing date: 2022-10-11
Publication date: 2023-03-24
Anticipated expiration: 2032-10-11

Abstract

The utility model relates to an electric loader leads to the problem that the aircraft bonnet curb plate rocked easily for solving the inside nothing of aircraft bonnet of current loader, the utility model discloses construct an electric loader, hold the aircraft bonnet at its inner chamber including installing the battery support that is used for installing power battery on the frame, when closing with battery support, its characterized in that first stop gear is all installed to the left and right sides face of battery support, the aircraft bonnet inboard is provided with second stop gear, the last spacing face towards the aircraft bonnet medial surface that has of first stop gear, second stop gear on have with the spacing contact surface of the laminating of spacing face contact. The utility model discloses in, a stop gear is all installed to battery holder's the left and right sides face, forms the support to curb plate about the aircraft bonnet to less cost is avoided the aircraft bonnet to rock effectively.

Description

Electric loader

Technical Field

The utility model relates to a loader, more specifically say, relate to an electric loader.

Background

In the nacelle of the electric loader, an electric motor, a power battery, and the like are mounted. The engine room is covered by a hood, and the front end of the hood at the top of the hood is connected with a frame structural member through a hinge structure and is seated on the frame by means of gravity or is supported by the bottom of the hood in contact with the frame structural member.

The existing hood is not supported inside, and the installation stability of the existing hood is completely determined by the strength of the existing hood. The front part and the bottom part of the hood are open, and the bottom part of the front part of the hood is in a cantilever state and is easy to shake along with the vibration of the whole machine. In order to prevent the lower portions of the two side plates of the hood from shaking during the operation of the loader, a high requirement is imposed on the strength of the framework of the hood, which also leads to an increase in the weight and manufacturing cost of the hood.

SUMMERY OF THE UTILITY MODEL

The to-be-solved technical problem of the utility model is that the inside no support of aircraft bonnet of current loader leads to the problem that the aircraft bonnet curb plate rocked easily, and provides an electronic loader to less cost avoids the aircraft bonnet to rock.

The utility model discloses a realize that the technical scheme of its purpose is like: the structure of the electric loader comprises a battery support arranged on a frame and used for mounting a power battery, and a hood accommodated in an inner cavity of the battery support when the battery support is closed, and is characterized in that first limiting mechanisms are mounted on the left side surface and the right side surface of the battery support, a second limiting mechanism is arranged on the inner side of the hood, a limiting surface facing the inner side surface of the hood is arranged on the first limiting mechanism, and a limiting contact surface contacted with the limiting surface is arranged on the second limiting mechanism. The utility model discloses in, first stop gear is all installed to battery holder's the left and right sides face, forms the support to curb plate about the aircraft bonnet to less cost avoids the aircraft bonnet to rock effectively.

In the electric loader, the limiting surface is an inclined slope, and the upper end of the limiting surface is inclined towards the battery support. Or the limiting surfaces are vertical surfaces, and the limiting surfaces of the first limiting mechanisms on the left side and the right side are parallel to each other.

In the electric loader, the first limiting mechanism is further provided with a guide surface, the guide surface is an inclined plane, the lower end of the guide surface is connected with the limiting surface, and the upper end of the guide surface is inclined towards the battery support.

In the above electric loader, the first limiting mechanism comprises a first mounting frame fixedly connected with the battery support and a limiting block fixedly mounted on the first mounting frame, and the limiting face is arranged on the limiting block.

In the electric loader, the first limiting mechanism is provided with a supporting surface which is used for contacting with the lower end of the second limiting mechanism and supporting the second limiting mechanism.

In the electric loader, the first limiting mechanism further comprises a supporting block fixedly mounted on the first mounting frame, and the supporting surface is located on the supporting block.

In the above-mentioned electric loader, second stop gear includes the second mounting bracket and fixes the limiting plate that sets up on the second mounting bracket, the limiting plate has vertical portion and the horizontal part that is L shape and arranges, and spacing contact surface is located the vertical portion of limiting plate, the bottom surface of horizontal part be used for with the holding surface laminating of supporting shoe.

In the electric loader, the second limiting mechanism is arranged in the middle of the hood side plate in the up-down direction. Further, the second limiting mechanism is arranged at the front part of the side plate of the hood.

Compared with the prior art, the utility model discloses set up stop gear on battery holder, support the aircraft bonnet side to less cost is avoided the aircraft bonnet effectively to rock

Drawings

Fig. 1 is a schematic diagram of the battery support arrangement of the electric loader of the present invention.

Fig. 2 is a schematic view of the arrangement of the first limit mechanism on the battery holder.

Fig. 3 is a schematic view of the arrangement of the first and second limit mechanisms on the electric loader.

Fig. 4 is a schematic diagram of the first and second limiting mechanisms in cooperation.

Fig. 5 is a schematic structural view of the first stopper mechanism.

Fig. 6 is a schematic structural view of the second limiting mechanism.

Part names and serial numbers in the figure:

battery support 100, bonnet 200, rear frame 300.

The first limiting mechanism 10, the first mounting frame 11, the limiting block 12, the limiting surface 121, the guide surface 122, the supporting block 13 and the supporting surface 131.

The second limiting mechanism 20, the second mounting frame 21, the limiting plate 22, the vertical part 221, the horizontal part 222 and the limiting contact surface 223.

Detailed Description

The following description of the embodiments refers to the accompanying drawings.

As shown in fig. 1 to 3, in the loader according to the present embodiment, a battery bracket 100 is mounted on the rear frame for mounting a power battery. A hood 200 is disposed on the rear frame 300, and the top of the front end of the hood 200 is hinged to the frame structure by a hinge mechanism so that the rear end of the hood 200 can be flipped open upward around the front end. When the hood 200 is closed, the battery holder 100 is located in the inner cavity of the hood.

The first limiting mechanisms 10 are respectively arranged at the left side and the right side of the battery bracket 100, the second limiting mechanisms 20 are respectively arranged at the inner sides of the side plates at the left side and the right side of the hood 200, when the hood is in a closed state, the first limiting mechanisms 10 at the same side are matched with the second limiting mechanisms 20, the first limiting mechanisms 10 support and limit the second limiting mechanisms 20,

the front end and the bottom of the hood 200 are open, and the second limiting mechanism 10 is installed in the middle of the side plate of the hood 200 in the up-down direction and in the front of the hood in the front-back direction. The front end of the hood is adjacent to the cab.

As shown in fig. 4 to 6, the first limiting mechanism 10 includes a first mounting bracket 11, and the first mounting bracket 11 is fixedly connected to the battery support 100. A supporting block 13 and a limiting block 12 are fixedly mounted on the first mounting bracket 11. The vertical surface of the side plate of the limiting block 12 facing the hood 200 is a limiting surface 121, a guide surface 122 is arranged in the direction of the limiting surface 121, the guide surface 122 is an inclined surface, the lower end of the guide surface is connected with the limiting surface, and the upper end of the guide surface inclines towards the battery support. The upward horizontal plane of the supporting block 13 is a supporting surface 131, and is used for contacting the second limiting mechanism 20 and supporting the second limiting mechanism 20 in the up-down direction.

The second limiting mechanism 20 comprises a second mounting frame 21, and the second mounting frame 21 is fixedly mounted on a side plate of the hood. A limiting plate 22 is arranged on the second mounting frame 21, the limiting plate 22 is provided with a vertical part 221 and a horizontal part 222 which are arranged in an L shape, a limiting contact surface 223 is positioned on the vertical part of the limiting plate, and the bottom surface of the horizontal part 222 is used for being attached to the supporting surface of the supporting block.

The embodiment of the utility model provides an in, when the aircraft bonnet 200 overturns downwards and closes, if when the aircraft bonnet 200 incline appears, limiting plate 22 earlier with the spigot surface 122 contact, slide down along spigot surface 122, the limiting plate is located on the supporting shoe at last, and spacing contact surface on the limiting plate and the spacing face 121 laminating on the first stop gear 100 for aircraft bonnet 200 can not rock in the left and right directions.

In this embodiment, the first limit mechanism is mounted on the battery holder to form a supporting point for the hood, so that the stability of the hood after closing is enhanced.

In this embodiment, the limiting surface may be an inclined surface, the upper end of which is inclined toward the battery holder, and when the hood is closed, the inclined limiting surface not only limits the hood in the left-right direction, but also supports the hood.

Claims

1. The utility model provides an electric loader, is including installing the aircraft bonnet that is used for installing power battery's battery support on the frame, holds at its inner chamber when closing, its characterized in that first stop gear is all installed to the left and right sides face of battery support, the aircraft bonnet inboard is provided with second stop gear, the last spacing face towards the aircraft bonnet medial surface that has of first stop gear, second stop gear on have with spacing contact surface of spacing face contact laminating.

2. The electric loader of claim 1, wherein said stopper surface is an inclined surface, and an upper end thereof is inclined toward the battery holder.

3. The electric loader of claim 1, wherein said stop surface is a vertical surface.

4. The electric loader of claim 3, wherein the first position-limiting mechanism further comprises a guide surface, the guide surface is an inclined surface, the lower end of the guide surface is connected to the position-limiting surface, and the upper end of the guide surface is inclined toward the battery holder.

5. The electric loader of any one of claims 1 to 4, wherein the first limiting mechanism comprises a first mounting bracket fixedly connected with the battery bracket, and a limiting block fixedly mounted on the first mounting bracket, and the limiting surface is disposed on the limiting block.

6. The electric loader of claim 5, wherein the first position limiting mechanism has a support surface thereon for contacting and supporting a lower end of the second position limiting mechanism.

7. The power loader of claim 6 wherein said first stop mechanism further comprises a support block fixedly mounted to said first mounting bracket, said support surface being located on said support block.

8. The electric loader of claim 7, wherein the second limiting mechanism comprises a second mounting frame and a limiting plate fixedly arranged on the second mounting frame, the limiting plate has a vertical part and a horizontal part arranged in an L shape, a limiting contact surface is located on the vertical part of the limiting plate, and the bottom surface of the horizontal part is used for being attached to the supporting surface of the supporting block.

9. The electric loader of claim 7, wherein said second stopper mechanism is arranged in the middle of the hood side plate in the up-down direction.

10. The electric loader of claim 7, wherein said second stop mechanism is disposed at a front portion of the hood side plate.