CN210474702U - Thrust plate testing device - Google Patents
Thrust plate testing device Download PDFInfo
- Publication number
- CN210474702U CN210474702U CN201921203545.7U CN201921203545U CN210474702U CN 210474702 U CN210474702 U CN 210474702U CN 201921203545 U CN201921203545 U CN 201921203545U CN 210474702 U CN210474702 U CN 210474702U
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- gauge
- diameter
- inner diameter
- measuring hole
- thrust plate
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Abstract
The utility model provides a thrust plate verifying attachment, include: the outer diameter go gauge is provided with a first measuring hole along the axial direction; the outer diameter no-go gauge is coaxially arranged in the first measuring hole, a second measuring hole coaxial with the first measuring hole is formed in the outer diameter no-go gauge, and the diameter of the first measuring hole is larger than that of the second measuring hole; the inner diameter gauge is cylindrical; the inner diameter no-go gauge is a cylinder, is connected with the end part of the inner diameter go gauge and is coaxially arranged with the inner diameter go gauge, and the outer diameter of the inner diameter no-go gauge is larger than that of the inner diameter go gauge. The utility model discloses an useful part lies in, simple structure, and the external diameter through accurate processing only leads to rule and the internal diameter only leads to rule and cooperatees, can carry out accurate inspection to the inside and outside diameter of thrust plate, and application method is simple, has improved inspection and production efficiency greatly.
Description
Technical Field
The utility model relates to an inside and outside diameter inspection technical field of part especially relates to a thrust plate's verifying attachment.
Background
The thrust plate is installed between the thrust end face of crankshaft and cylinder plane of engine, and can bear the axial thrust force resulted from clutch, etc. and can be used for axially positioning crankshaft, at the same time can ensure a certain axial gap. Because the thrust plate has an important function, the requirement on the dimensional accuracy of the inner diameter and the outer diameter of the thrust plate is extremely high during processing, equipment with higher precision is required for measurement, the time spent in the measurement process is longer, and the inspection and production efficiency is reduced.
SUMMERY OF THE UTILITY MODEL
To the above defect, the to-be-solved technical problem of the utility model is to provide a simple structure, convenient to use's thrust plane verifying attachment promotes detection efficiency.
The utility model provides a thrust plate verifying attachment, include: the outer diameter go gauge is provided with a first measuring hole along the axial direction; the outer diameter no-go gauge is coaxially arranged in the first measuring hole, a second measuring hole coaxial with the first measuring hole is formed in the outer diameter no-go gauge, and the diameter of the first measuring hole is larger than that of the second measuring hole; the inner diameter gauge is cylindrical; the inner diameter no-go gauge is a cylinder, is connected with the end part of the inner diameter go gauge and is coaxially arranged with the inner diameter go gauge, and the outer diameter of the inner diameter no-go gauge is larger than that of the inner diameter go gauge.
Preferably, the first measuring hole is a through hole.
Preferably, the second measuring hole is provided at a middle portion of the first measuring hole.
Preferably, one end of the inner diameter no-go gauge is connected with the inner diameter go-gauge, and the other end of the inner diameter no-go gauge is provided with a handle.
The utility model discloses an useful part lies in, simple structure, and the external diameter through accurate processing only leads to rule and the internal diameter only leads to rule and cooperatees, can carry out accurate inspection to the inside and outside diameter of thrust plate, and application method is simple, has improved inspection and production efficiency greatly.
Drawings
FIG. 1 is a schematic structural view of a thrust plate;
FIG. 2 is a schematic view of the inspection device of the present invention in use;
FIG. 3 is a schematic structural view of an outer diameter no-go gauge;
FIG. 4 is a schematic structural view of an inner diameter no-go gauge;
element number description:
1 outside diameter no go gauge
11 outside diameter go gauge
111 first measuring hole
12 outer diameter no-go gauge
121 second measuring hole
2 inside diameter no-go gauge
21 bore go gauge
22 bore no-go gage
23 handle
3 thrust plate
31 extrados surface
32 intrados
Detailed Description
The following describes the present invention in further detail with reference to the accompanying drawings. These embodiments are provided only for illustrating the present invention and are not intended to limit the present invention.
In the description of the present invention, it should be noted that the terms "middle part", "inside", "outside", and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, which is only for convenience of description and simplification of the description, and do not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the term "connected" is to be interpreted broadly, for example, as a fixed connection, a detachable connection, or an integral connection; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
As shown in FIG. 1 and FIG. 2, the utility model provides an inspection device for examining the internal and external diameters of thrust plate 3, including the external diameter no-go gage 1 that is used for examining the external diameter of thrust plate 3 and the internal diameter no-go gage 2 that is used for examining the internal diameter of thrust plate 3, external diameter no-go gage 1 is as shown in FIG. 3, including external diameter no-go gage 11 and external diameter no-go gage 12. The outer diameter gauge 11 is a cylinder, in which a first measuring hole 111 is formed along the axial direction. The outer diameter no-go gauge 12 is an annular baffle plate, is coaxially arranged in the first measuring hole 111, and is internally provided with a second measuring hole 121 which is coaxial with the first measuring hole 111, and the second measuring hole 121 is communicated with the first measuring hole 111. The diameter of the first measurement hole 111 is greater than the diameter of the second measurement hole 121 because the diameter of the first measurement hole 111 is the upper limit value of the tolerance of the outer diameter of the push piece 3 and the diameter of the second measurement hole 121 is the lower limit value of the tolerance of the outer diameter of the push piece 3.
When the thrust plate 3 is used, the thrust plate 3 is pushed to the outer diameter stop gauge 1, and if the outer arc surface 31 of the thrust plate 3 can penetrate into the first measuring hole 111 but cannot penetrate into the second measuring hole 121, the outer diameter of the thrust plate 3 is judged to be qualified; if the extrados surface 31 of the thrust plate 3 cannot penetrate into the first measurement hole 111, or can penetrate into both the first measurement hole 111 and the second measurement hole 121, the outer diameter of the thrust plate 3 is determined to be unqualified. Preferably, the first measuring hole 111 is a through hole, and the second measuring hole 121 is disposed in the middle of the first measuring hole 111, so that after the arrangement, the two thrust plates 3 can be pushed into the first measuring hole 111 at the same time, and the detection efficiency is improved.
As shown in fig. 1, 2 and 4, the inner diameter no-go gauge 2 includes an inner diameter no-go gauge 21 and an inner diameter no-go gauge 22 both having a cylindrical shape, and the inner diameter no-go gauge 22 is connected to an end portion of the inner diameter no-go gauge 21 and is disposed coaxially with the inner diameter no-go gauge 21. Since the outer diameter of the inner diameter gauge 21 is the lower limit of the tolerance of the inner diameter of the push piece 3 and the outer diameter of the inner diameter gauge 22 is the upper limit of the tolerance of the inner diameter of the push piece 3, the outer diameter of the inner diameter gauge 22 is larger than the outer diameter of the inner diameter gauge 21.
When the thrust plate is used, the thrust plate 3 with qualified outer diameter is placed in the first measuring hole 111, then the inner diameter go gauge 21 of the inner diameter go gauge 2 is pushed to the thrust plate 3, and if the inner diameter go gauge 21 can pass through the intrados 32 of the thrust plate 3 but the inner diameter no gauge 22 cannot pass through, the inner diameter of the thrust plate 3 is judged to be qualified; if the internal diameter gauge 21 cannot pass through the intrados 32 of the thrust plate 3 or the internal diameter gauge 22 can pass through the intrados 32 of the thrust plate 3, the internal diameter of the thrust plate 3 is judged to be unqualified. Preferably, one end of the inner diameter no-go gauge 22 is connected with the inner diameter go gauge 21, and the other end is provided with a handle 23, so that an operator can conveniently hold the inner diameter no-go gauge by hand during inspection.
To sum up, the utility model discloses an useful part lies in, simple structure, and the external diameter through accurate processing ends to lead to rule and internal diameter end to lead to rule and cooperate, can carry out accurate inspection to the inside and outside diameter of thrust piece, and application method is simple, has improved inspection and production efficiency greatly.
The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and replacements can be made without departing from the technical principle of the present invention, and these modifications and replacements should also be regarded as the protection scope of the present invention.
Claims (4)
1. A thrust plate testing apparatus, comprising:
the outer diameter go gauge (11) is provided with a first measuring hole (111) along the axial direction;
the outer diameter no-go gauge (12) is coaxially arranged in the first measuring hole (111), a second measuring hole (121) coaxial with the first measuring hole (111) is formed in the inner portion of the outer diameter no-go gauge, and the diameter of the first measuring hole (111) is larger than that of the second measuring hole (121);
an inner diameter gauge (21) which is a cylinder;
the inner diameter no-go gauge (22) is cylindrical, is connected with the end part of the inner diameter go gauge (21), is coaxially arranged with the inner diameter go gauge (21), and has an outer diameter larger than that of the inner diameter go gauge (21).
2. The thrust plate inspection device of claim 1, wherein the first measuring hole (111) is a through hole.
3. The thrust plate inspection device of claim 2, wherein the second measurement hole (121) is provided in a middle portion of the first measurement hole (111).
4. The thrust plate testing device according to claim 1, wherein one end of the inner diameter no-go gauge (22) is connected to the inner diameter no-go gauge (21), and the other end is provided with a handle (23).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921203545.7U CN210474702U (en) | 2019-07-29 | 2019-07-29 | Thrust plate testing device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201921203545.7U CN210474702U (en) | 2019-07-29 | 2019-07-29 | Thrust plate testing device |
Publications (1)
Publication Number | Publication Date |
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CN210474702U true CN210474702U (en) | 2020-05-08 |
Family
ID=70533614
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201921203545.7U Active CN210474702U (en) | 2019-07-29 | 2019-07-29 | Thrust plate testing device |
Country Status (1)
Country | Link |
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CN (1) | CN210474702U (en) |
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2019
- 2019-07-29 CN CN201921203545.7U patent/CN210474702U/en active Active
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