CN218536338U - Body reinforcing plate structure - Google Patents
Body reinforcing plate structure Download PDFInfo
- Publication number
- CN218536338U CN218536338U CN202223003497.1U CN202223003497U CN218536338U CN 218536338 U CN218536338 U CN 218536338U CN 202223003497 U CN202223003497 U CN 202223003497U CN 218536338 U CN218536338 U CN 218536338U
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- Prior art keywords
- reinforcing plate
- organism
- threaded hole
- machine body
- internal thread
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- 230000003014 reinforcing effect Effects 0.000 title claims abstract description 55
- 239000003351 stiffener Substances 0.000 claims 2
- 238000005728 strengthening Methods 0.000 abstract description 2
- 238000005452 bending Methods 0.000 description 4
- 230000005484 gravity Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000000725 suspension Substances 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Abstract
The utility model discloses a machine body reinforcing plate structure, which comprises a machine body and reinforcing plates, wherein two sides of the bottom of each cylinder of the machine body are respectively provided with a group of mounting holes, each group of mounting holes consists of an upper threaded hole and a lower threaded hole, each reinforcing plate is square, four corners of each reinforcing plate are respectively provided with an internal thread column, and the middle part of each reinforcing plate is provided with an oval through hole; the reinforcing plate is installed at the bottom of the machine body through the matching of the bolt, the internal thread column and the threaded hole. The utility model discloses install the reinforcing plate on the mounting hole, make the organism form stable triangular structure, the bottom of reinforcing plate is equipped with the strengthening rib simultaneously, installs the reinforcing plate in the multiplicable organism tensile compressive capacity of bottom of the body, prevents the organism fracture. Has the advantages of tensile and compressive capacity and body strength improvement.
Description
Technical Field
The utility model relates to an engine field especially relates to a fuselage reinforcing plate structure.
Background
At present, when an engine is subjected to external load transmitted by a finished automobile frame through a suspension in the use process of the vehicle, the gravity of the engine and the support of the finished automobile frame form an upper bending moment and a lower bending moment, the inner side of the engine body forms an outward bending moment, and the outer side of the engine body forms an inward bending moment, so that the engine body is easy to crack, the engine fault is caused, and the use safety of the vehicle is influenced.
The above background disclosure is only provided to aid understanding of the inventive concepts and solutions of the present invention, and it does not necessarily pertain to the prior art of this patent application, and it should not be used to assess the novelty and inventive aspects of this application without explicit evidence that such contents are disclosed at the filing date of this patent application.
SUMMERY OF THE UTILITY MODEL
The utility model discloses to above problem, provide a body reinforcing plate structure and solve and receive whole car frame because of the engine at present when the external load that the suspension was transmitted and was come, moment of flexure about engine gravity supported the formation with whole car frame, and the inboard outside moment of flexure that forms of organism forms, and the outside forms inside moment of flexure, leads to the organism fracture easily, causes engine failure, influences the problem of vehicle safety in utilization.
In order to realize the above purpose, the utility model discloses a technical scheme as follows:
the utility model provides a fuselage reinforcing plate structure which characterized in that: the cylinder bottom of the engine body is provided with a group of mounting holes on two sides, each group of mounting holes consists of an upper threaded hole and a lower threaded hole, the reinforcing plate is square, four corners of the reinforcing plate are provided with an internal threaded column, and the middle part of the reinforcing plate is provided with an oval through hole; the reinforcing plate is installed at the bottom of the machine body through the matching of the bolt, the internal thread column and the threaded hole.
Further, two adjacent cylinder bottoms of the machine body share one group of mounting holes.
Furthermore, reinforcing ribs are respectively arranged between every two internal thread columns at the four corners of the reinforcing plate, and the reinforcing ribs are also connected with the bottom of the reinforcing plate.
Furthermore, the internal thread columns at the four corners of the reinforcing plate are on the same plane.
Further, the engine body is an in-line four-cylinder engine body or an in-line six-cylinder engine body.
Compared with the prior art, the utility model discloses an advantage and beneficial effect do:
1. the utility model discloses mainly constitute by organism and reinforcing plate, be equipped with a set of mounting hole through every cylinder bottom both sides at the organism, install the reinforcing plate on the mounting hole, make the organism form stable triangular structure, the bottom of reinforcing plate is equipped with the strengthening rib simultaneously, installs the reinforcing plate at the multiplicable organism tensile compressive capacity of organism bottom, prevents the organism fracture. Has the advantages of tensile and compressive capacity and body strength improvement.
2. The utility model discloses a reinforcing plate can install in organism atress department according to CAE analysis result, is equipped with the mounting hole between each jar and can installs in a flexible way, can also realize the part universalization installation simultaneously on four, six jar engines with the platform, saves part mould and administrative expense.
Drawings
FIG. 1 is a front view of the present invention;
fig. 2 is a bottom view of the present invention;
FIG. 3 is a schematic structural view of an in-line four-cylinder engine of the present invention;
FIG. 4 is a schematic structural view of the reinforcing plate of the present invention;
FIG. 5 is a schematic structural view of the bottom of the reinforcing plate of the present invention;
fig. 6 is a cross-sectional view of the reinforcing plate of the present invention;
fig. 7 is a schematic structural diagram of the present invention.
Detailed Description
The present invention will be described in further detail with reference to the following embodiments. It should be emphasized that the following description is merely exemplary in nature and is in no way intended to limit the scope of the invention or its applications.
As shown in fig. 1 to 7, the reinforcing plate structure of the machine body is characterized in that: the engine comprises an engine body 1 and a reinforcing plate 2, wherein the engine body 1 is an in-line four-cylinder engine body or an in-line six-cylinder engine body, a group of mounting holes 3 is formed in two sides of the bottom of each cylinder of the engine body 1, each group of mounting holes 3 consists of an upper threaded hole and a lower threaded hole 4, and two adjacent cylinder bottoms of the engine body 1 share one group of mounting holes 3 and are used for mounting the reinforcing plate 2; the reinforcing plate 2 is square, the four corners of the reinforcing plate 2 are respectively provided with an internal thread column 5 for being connected with the mounting hole 3 at the bottom of the machine body 1, the internal thread columns 5 at the four corners of the reinforcing plate 2 are on the same plane, reinforcing ribs 6 are respectively arranged between every two internal thread columns 5 at the four corners of the reinforcing plate 2, the reinforcing ribs 6 are also connected with the bottom of the reinforcing plate 2, the tensile and compressive capacities of the reinforcing plate 2 can be improved, the middle part of the reinforcing plate 2 is provided with an oval through hole 7, the lightweight design is realized, and meanwhile, the lubricating oil in the machine body 1 can be prevented from being deposited on the reinforcing plate 2; reinforcing plate 2 passes through the bolt and installs in 1 bottom of organism with the cooperation of internal thread post 5 and screw hole 4, makes organism 1 form stable triangular structure, and multiplicable 1 tensile compressive capacity of organism prevents the fracture of organism 1. Reinforcing plate 2 can be installed at 1 atress department of organism according to CAE analysis result, is equipped with mounting hole 3 between each jar and can installs in a flexible way, can also realize the part universalization installation simultaneously on four, six jar engines with the platform.
The foregoing is a further detailed description of the present invention in connection with specific/preferred embodiments and it is not to be construed as limiting the invention to the specific embodiments set forth herein. For those skilled in the art to which the present invention pertains, a plurality of alternatives or modifications can be made to the described embodiments without departing from the concept of the present invention, and all such alternatives or modifications should be considered as falling within the protection scope of the present invention.
Claims (5)
1. The utility model provides a fuselage reinforcing plate structure which characterized in that: the cylinder bottom of the engine body is provided with a group of mounting holes on two sides, each group of mounting holes consists of an upper threaded hole and a lower threaded hole, the reinforcing plate is square, four corners of the reinforcing plate are provided with an internal threaded column, and the middle part of the reinforcing plate is provided with an oval through hole; the reinforcing plate is installed at the bottom of the machine body through the matching of the bolt, the internal thread column and the threaded hole.
2. The body gusset structure of claim 1, wherein: two adjacent cylinder bottoms of the machine body share one group of mounting holes.
3. The body stiffener structure of claim 1, wherein: and reinforcing ribs are arranged between every two internal thread columns at four corners of the reinforcing plate respectively and are also connected with the bottom of the reinforcing plate.
4. The body stiffener structure of claim 1, wherein: the internal thread columns at the four corners of the reinforcing plate are on the same plane.
5. The body gusset structure of claim 1, wherein: the engine body is an in-line four-cylinder engine body or an in-line six-cylinder engine body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223003497.1U CN218536338U (en) | 2022-11-11 | 2022-11-11 | Body reinforcing plate structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202223003497.1U CN218536338U (en) | 2022-11-11 | 2022-11-11 | Body reinforcing plate structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218536338U true CN218536338U (en) | 2023-02-28 |
Family
ID=85261271
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202223003497.1U Active CN218536338U (en) | 2022-11-11 | 2022-11-11 | Body reinforcing plate structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218536338U (en) |
-
2022
- 2022-11-11 CN CN202223003497.1U patent/CN218536338U/en active Active
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