CN211009398U - Machine body connecting sheet - Google Patents
Machine body connecting sheet Download PDFInfo
- Publication number
- CN211009398U CN211009398U CN201921582675.6U CN201921582675U CN211009398U CN 211009398 U CN211009398 U CN 211009398U CN 201921582675 U CN201921582675 U CN 201921582675U CN 211009398 U CN211009398 U CN 211009398U
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- China
- Prior art keywords
- horizontal fixing
- connection piece
- fixing plate
- mounting holes
- plate
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Abstract
The utility model discloses a fuselage connection piece, it includes: a horizontal fixing plate (10) provided with a plurality of first mounting holes (100); and a trapezoidal plate (11) vertically mounted on the horizontal fixing plate and provided with a plurality of second mounting holes (110). The utility model discloses following beneficial effect has: this fuselage connection piece structural strength is high.
Description
Technical Field
The utility model belongs to the technical field of logistics equipment and specifically relates to a fuselage connection piece is related to.
Background
The frames of the conveying equipment need to be connected by using connecting sheets, the connecting sheet structure is shown in figures 1-2, the connecting sheet comprises a rectangular plate 1, mounting holes 2 are arranged at four corners of the rectangular plate, and the strength of the connecting sheet mechanism is insufficient.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a fuselage connection piece, its structural strength is high.
In order to solve the above technical problem, an embodiment of the utility model provides a fuselage connection piece, it includes: a horizontal fixing plate (10) provided with a plurality of first mounting holes (100); and a trapezoidal plate (11) vertically mounted on the horizontal fixing plate and provided with a plurality of second mounting holes (110).
Furthermore, the included angle between the inclined edge of the trapezoidal plate and the horizontal fixing plate is 60 degrees.
Further, two first mounting holes are arranged.
Further, four second mounting holes are arranged.
Further, the horizontal fixing plate and the trapezoidal plate are integrally formed.
The utility model discloses following beneficial effect has: this fuselage connection piece structural strength is high.
The principle of the structural strength increase of the connecting sheet is that the connecting sheet is made into L type, the external dimension is enlarged, the fixing hole position is increased, the long side is attached to the machine frame, and the short side is vertical to the machine frame, so the structural strength is increased.
Drawings
Fig. 1 is a front view of a connecting piece according to the background art.
Fig. 2 is a top view of fig. 1.
Fig. 3 is a front view of the connecting piece of the machine body in the embodiment of the present invention.
Fig. 4 is a top view of the connecting piece of the fuselage according to an embodiment of the present invention.
Fig. 5 is a side view of the connecting piece of the fuselage in the embodiment of the present invention.
Fig. 6 is an installation effect diagram of the machine body connecting piece in the embodiment of the present invention.
Detailed Description
In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention will be further described with reference to the following embodiments.
An embodiment of the present invention provides a fuselage connection piece, see fig. 3-5, which includes: the horizontal fixing plate 10 is provided with 2 first mounting holes 100, which are elongated square holes (end portions are in a semicircular structure).
And a trapezoidal plate 11 vertically installed on the horizontal fixing plate, wherein a circular arc-shaped chamfer structure is arranged between the trapezoidal plate and the horizontal fixing plate, and 4 second installation holes 110 are formed in the circular arc-shaped chamfer structure.
Referring to fig. 4, the inclined edge of the trapezoidal plate forms an angle of 60 degrees with the horizontal fixing plate.
The horizontal fixing plate and the trapezoidal plate are integrally formed, and the whole machine body connecting piece can be a metal piece.
Referring to fig. 6, the installation effect of the body attachment piece includes a frame a200, a frame B300, and a body attachment piece 400 connecting the frame a200 and the frame B300. The mounting mode of the machine body connecting piece is as follows: the fuselage connection tabs 400 are first bolted to the frame a200, and then the frame B300 is aligned with the frame a200 and bolted.
As right the utility model discloses a further improvement lies in, fuselage connection piece 400 is provided with rectangle location boss towards the surface of frame one side, and the frame be provided with rectangle location boss complex rectangle recess, when the frame that is provided with the rectangle recess is connected with the fuselage connection piece, can install fuselage connection piece quick location in the frame to avoid the bolt butt joint not in place and reduce the installation effectiveness, here the rectangle location boss sets up in fuselage connection piece left surface, it is that frame A200 sets up a rectangle recess that corresponds with it can to correspond.
It will be understood by those skilled in the art that the foregoing embodiments are specific examples of the invention, and that various changes in form and details may be made therein without departing from the spirit and scope of the invention in its practical application.
Claims (4)
1. A fuselage connection piece, comprising:
a horizontal fixing plate (10) provided with a plurality of first mounting holes (100);
a trapezoidal plate (11) vertically mounted on the horizontal fixing plate and provided with a plurality of second mounting holes (110);
the included angle between the inclined edge of the trapezoidal plate and the horizontal fixing plate is 60 degrees;
the surface of one side, facing the rack, of the machine body connecting sheet is provided with a rectangular positioning boss, and the rack is provided with a rectangular groove matched with the rectangular positioning boss;
the first mounting hole is a strip-shaped square hole;
and an arc-shaped chamfer structure is arranged between the trapezoidal plate and the horizontal fixing plate.
2. The fuselage connection piece of claim 1, wherein there are two of the first mounting holes.
3. The fuselage connection piece of claim 1, wherein four of the second mounting holes are arranged.
4. The fuselage connection piece of claim 1, wherein the horizontal securing plate is integrally formed with the trapezoidal plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921582675.6U CN211009398U (en) | 2019-09-23 | 2019-09-23 | Machine body connecting sheet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921582675.6U CN211009398U (en) | 2019-09-23 | 2019-09-23 | Machine body connecting sheet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211009398U true CN211009398U (en) | 2020-07-14 |
Family
ID=71478553
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921582675.6U Active CN211009398U (en) | 2019-09-23 | 2019-09-23 | Machine body connecting sheet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211009398U (en) |
-
2019
- 2019-09-23 CN CN201921582675.6U patent/CN211009398U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |