CN205300474U - Utensil is examined to taper sleeve pipe external dimension - Google Patents

Utensil is examined to taper sleeve pipe external dimension Download PDF

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Publication number
CN205300474U
CN205300474U CN201521110736.0U CN201521110736U CN205300474U CN 205300474 U CN205300474 U CN 205300474U CN 201521110736 U CN201521110736 U CN 201521110736U CN 205300474 U CN205300474 U CN 205300474U
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CN
China
Prior art keywords
gage
rule
axis radius
drift
utility
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201521110736.0U
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Chinese (zh)
Inventor
蔡灏
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Wuxi Qingshan Railway Equipment Co Ltd
Original Assignee
Wuxi Qingshan Railway Equipment Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Wuxi Qingshan Railway Equipment Co Ltd filed Critical Wuxi Qingshan Railway Equipment Co Ltd
Priority to CN201521110736.0U priority Critical patent/CN205300474U/en
Application granted granted Critical
Publication of CN205300474U publication Critical patent/CN205300474U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides an utensil is examined to taper sleeve pipe external dimension, including: no -go gage, logical rule, base plate, seted up the no -go gage on the base plate, led to two back taper through -holes on the rule, the major axis radius I of leading to the rule top is not less than the top major axis radius II of no -go gage, the top minor axis radius I of leading to rule is not less than the top minor axis radius II of no -go gage, the utility model discloses setting up on a block base board and leading to rule, no -go gage, the size of these expert's rule, no -go gage accords with awl sheathed tube appearance, corresponding with awl sheathed tube overall dimension, can realize improving test efficiency to the short -term test of awl sheathed tube size.

Description

A kind of taper bushing overall dimensions cubing
Technical field
This utility model relates generally to product cubing detection field, particularly relates to a kind of taper bushing overall dimensions cubing.
Background technology
High owing to adjusting taper bushing length and width dimensional requirement, tolerance is little, standard: 59.1 �� 0.2, and 41.1 �� 0.2, when detecting with slide gauge, workload is big, and efficiency is low.
Utility model content
This utility model provides a kind of taper bushing overall dimensions cubing, whether the gradient simply measuring track gauge block inclined-plane is qualified, in order to achieve the above object, this utility model is by the following technical solutions: this utility model includes: no-go gage, drift, substrate, described substrate offers no-go gage, two inverted cone through holes of drift, the major axis radius I at described drift top is not less than the top major axis radius II of described no-go gage, and the top minor axis radius I of described drift is not less than the top minor axis radius II of described no-go gage.
Preferably, breach I is offered bottom described no-go gage.
Preferably, breach II is offered bottom described drift.
Preferably, described substrate adopts metal material.
The beneficial effects of the utility model: this utility model arranges drift, no-go gage on one piece of substrate, this drift, no-go gage size to meet the profile of taper bushing corresponding with the overall dimensions of taper bushing, it is capable of the quick detection of the size to taper bushing, improves checkability.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is about the A-A sectional view of no-go gage in Fig. 1 in this utility model;
Fig. 3 is about the B-B sectional view of no-go gage in Fig. 1 in this utility model;
Fig. 4 is about the C-C sectional view of drift in Fig. 1 in this utility model;
Fig. 5 is about the D-D sectional view of drift in Fig. 1 in this utility model;
In figure, 1, substrate; 2, no-go gage; 3, drift.
Detailed description of the invention
Known as shown in Figure 1, this utility model includes: substrate 1, no-go gage 2, drift 3, described substrate 1 adopts metal material, described substrate 1 offers no-go gage 2,3 two inverted cone through holes of drift, known as Figure 2-Figure 5, preferably, the inclined plane number of degrees value of described inverted cone through-hole wall is 2 ��;
The major axis radius I at described drift 3 top is not less than the top major axis radius II of described no-go gage 2, the top minor axis radius I of described drift 3 is not less than the top minor axis radius II of described no-go gage 2, preferably, the major diameter at described drift 3 top is 59.1+0.2, and the minor axis diameter at described drift 3 top is 41.1+0.2;The major diameter at described no-go gage 2 top is 59.1-0.2, and the minor axis diameter at described no-go gage 2 top is 41.1-0.2.
As it is shown on figure 3, offer breach I bottom described no-go gage 2.
As it is shown in figure 5, also offer breach II bottom described drift 3.
The principle of above-described embodiment only illustrative present patent application and effect thereof, not for restriction present patent application. Above-described embodiment all under the spirit and category of present patent application, can be modified or change by any those skilled in the art. Therefore, such as having all equivalence modification or changes that usually intellectual completes under the spirit disclosed without departing from present patent application with technological thought in art, the claim must asked by this patent is contained.

Claims (4)

1. a taper bushing overall dimensions cubing, include: no-go gage, drift, substrate, it is characterized in that: described substrate offers no-go gage, two inverted cone through holes of drift, the major axis radius I at described drift top is not less than the top major axis radius II of described no-go gage, and the top minor axis radius I of described drift is not less than the top minor axis radius II of described no-go gage.
2. a kind of taper bushing overall dimensions cubing according to claim 1, it is characterised in that: offer breach I bottom described no-go gage.
3. a kind of taper bushing overall dimensions cubing according to claim 1, it is characterised in that: offer breach II bottom described drift.
4. a kind of taper bushing overall dimensions cubing according to claim 1, it is characterised in that: described substrate adopts metal material.
CN201521110736.0U 2015-12-29 2015-12-29 Utensil is examined to taper sleeve pipe external dimension Expired - Fee Related CN205300474U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201521110736.0U CN205300474U (en) 2015-12-29 2015-12-29 Utensil is examined to taper sleeve pipe external dimension

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201521110736.0U CN205300474U (en) 2015-12-29 2015-12-29 Utensil is examined to taper sleeve pipe external dimension

Publications (1)

Publication Number Publication Date
CN205300474U true CN205300474U (en) 2016-06-08

Family

ID=56474106

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201521110736.0U Expired - Fee Related CN205300474U (en) 2015-12-29 2015-12-29 Utensil is examined to taper sleeve pipe external dimension

Country Status (1)

Country Link
CN (1) CN205300474U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109916275A (en) * 2019-04-03 2019-06-21 西安飞机工业(集团)有限责任公司 A kind of straight-neck rivet chamfering detection method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109916275A (en) * 2019-04-03 2019-06-21 西安飞机工业(集团)有限责任公司 A kind of straight-neck rivet chamfering detection method

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160608

Termination date: 20211229