CN208451440U - A kind of auxiliary eccentric bush graduating device - Google Patents

A kind of auxiliary eccentric bush graduating device Download PDF

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Publication number
CN208451440U
CN208451440U CN201821004684.2U CN201821004684U CN208451440U CN 208451440 U CN208451440 U CN 208451440U CN 201821004684 U CN201821004684 U CN 201821004684U CN 208451440 U CN208451440 U CN 208451440U
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CN
China
Prior art keywords
eccentric
positioning base
positioning
eccentric bush
bush
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Active
Application number
CN201821004684.2U
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Chinese (zh)
Inventor
王建
闫佳康
艾红云
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Xian Aircraft Industry Group Co Ltd
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Xian Aircraft Industry Group Co Ltd
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Priority to CN201821004684.2U priority Critical patent/CN208451440U/en
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Publication of CN208451440U publication Critical patent/CN208451440U/en
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Abstract

This application discloses a kind of auxiliary eccentric bush graduating devices, it is made of positioning base, positioning pin, positioning base and detent fit use, and positioning base is identified with eccentric orfice, positioning shaft shoulder, angle groove, and the excircle eccentricity amount of eccentric orfice and positioning base is identical as the eccentricity of eccentric bush;Groove slot carries out 6 equal parts by 0-180 degree;Positioning pin section and end with form, end has non-slip texture, cooperation section and part, positioning base eccentric through-hole are small―gap suture cooperation, positioning pin passes through the eccentric orfice of positioning base and eccentric bush from the bottom to top, keep the eccentric axis of eccentric bush consistent with the axis of positioning base eccentric orfice, carries out groove according to the graduation mark on positioning base end face.

Description

A kind of auxiliary eccentric bush graduating device
Technical field
This application involves the manufacturing technology field of lining cover parts, especially a kind of graduating device for assisting eccentric bush.
Background technique
It is arranged with leading edge slat in the fixation leading edge of large aircraft at present, is risen by the airplane critical angle of attack is increased Power.Slat is connect with sliding rail, and is moved under the constraint of the fixed leading edge partition idler wheel of wing along the sliding rail face of leading, realizes slat Folding and unfolding.For convenience of adjustment slat and fixed leading edge relative position, a kind of eccentric lining is used in the connecting portion of slat and sliding rail Set adjusts slat and fixed up-front relative position by rotating eccentricity bushing.But due to lining during practical set adjustment End face non-angular groove mark is covered, can not determine adjusting angle, can only be groped by the experience of manual operator, Wu Faji Tired data, regulated efficiency are lower.
Since bushing is thermally treated steel part, surface hardness is higher, and liner size is small, and specification is more, uses ruler by hand Rule method correct error is larger, low efficiency, it is difficult to obtain eccentric axis accurate location.Although using digital control laser groove precision Height, but equipment manufacturing cost is expensive, the development cycle is long.Therefore need a kind of auxiliary positioning for eccentric bush end face groove and point Degree, graduating device, both can quickly carry out manual centering, find bushing eccentric axis, while can provide groove indexing reference, auxiliary It helps scribing cutter to cross, realizes the quick groove of eccentric bush class part.
Innovation and creation content
The application solves its technical problem the technical scheme adopted is that a kind of auxiliary eccentric bush graduating device, by fixed Position pedestal, positioning pin composition, positioning base and detent fit use, and positioning base is carved with eccentric orfice, positioning shaft shoulder, angle The excircle eccentricity amount of line mark, eccentric orfice and positioning base is identical as the eccentricity of eccentric bush;Groove slot by 0-180 degree into 6 equal part of row;Positioning pin section and end with form, and end has non-slip texture, and cooperation section and part, positioning base bias are logical Hole is small―gap suture cooperation, and positioning pin passes through the eccentric orfice of positioning base and eccentric bush from the bottom to top, makes the inclined of eccentric bush Mandrel line is consistent with the axis of positioning base eccentric orfice, carries out groove according to the graduation mark on positioning base end face.
The application's has the beneficial effect that positioning mechanism structure is simple, easy to use, can be realized by simple manual action The quick positioning of bushing and according to the direct groove in positioning base end face, and device manufacturing difficulty is low, precision is high, and can meet scene makes With requiring.With expansibility, different positioning tools can be designed according to the eccentricity of other specification bushings, diameter feature.
Detailed description of the invention
Fig. 1 graduating device operation principle schematic diagram.
Fig. 2 positioning base structural schematic diagram.
Fig. 3 positioning pin stick structural schematic diagram.
Explanation: 1. eccentric bush is numbered in figure;2. positioning base;3. positioning pin;.
Specific embodiment
In order to which the technical features, objects and effects to the application have clearer understanding, Detailed description of the invention the application is now compareed Specific embodiment.As shown in Figure 1 to Figure 3, the application proposes a kind of auxiliary eccentric bush graduating device, eccentric for aircraft The device of bushing groove, the device are mainly made of positioning base, positioning pin.
It referring to fig. 2, is the top view of the positioning base 2, the generally revolving body of positioning base 2 makes with the cooperation of positioning pin 3 With, positioning base 2 with eccentric orfice, positioning shaft shoulder, angle groove mark, the excircle eccentricity amount of eccentric orfice and positioning base 2 with The eccentricity of eccentric bush is identical;Groove slot carries out 6 etc. by 0-180 degree and divides
Referring to Fig. 3 positioning pin 3, section and end are formed with, end have non-slip texture, cooperation section and eccentric bush 1, 2 eccentric through-hole of positioning base is small―gap suture cooperation, and positioning pin 3 passes through the bias of positioning base 2 and eccentric bush 1 from the bottom to top Hole keeps the eccentric axis of eccentric bush 1 consistent with the axis of 2 eccentric orfice of positioning base, according to the scale on 2 end face of positioning base Line carries out groove.
In an inactive state, positioning base 2 and positioning pin 3, eccentric bush 1 are all in discrete state.In use process In, eccentric bush 1 is put into from 2 top of positioning base, and adjustment 1 end cap of eccentric bush makes positioning pin 3 be just passed through positioning base 2 1 eccentric orfice of eccentric orfice and eccentric bush, the at this time positioning of eccentric bush 1 are completed, i.e. the eccentric axis of eccentric bush 1 and positioning bottom The eccentric axis of seat 2 is overlapped, and carries out groove using the groove mark having on positioning base 2.

Claims (1)

1. a kind of auxiliary eccentric bush graduating device, is made of, positioning base makes with detent fit positioning base, positioning pin With, it is characterised in that the positioning base is with eccentric orfice, positioning shaft shoulder, angle groove mark, eccentric orfice and positioning base Excircle eccentricity amount it is identical as the eccentricity of eccentric bush;Groove slot carries out 6 equal parts by 0-180 degree;The positioning pin is by matching Section and end composition are closed, end has non-slip texture, and cooperation section and part, positioning base eccentric through-hole are small―gap suture cooperation, Positioning pin passes through the eccentric orfice of positioning base and eccentric bush from the bottom to top, keeps the eccentric axis of eccentric bush and positioning base inclined The axis in heart hole is consistent, carries out groove according to the graduation mark on positioning base end face.
CN201821004684.2U 2018-06-27 2018-06-27 A kind of auxiliary eccentric bush graduating device Active CN208451440U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821004684.2U CN208451440U (en) 2018-06-27 2018-06-27 A kind of auxiliary eccentric bush graduating device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821004684.2U CN208451440U (en) 2018-06-27 2018-06-27 A kind of auxiliary eccentric bush graduating device

Publications (1)

Publication Number Publication Date
CN208451440U true CN208451440U (en) 2019-02-01

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821004684.2U Active CN208451440U (en) 2018-06-27 2018-06-27 A kind of auxiliary eccentric bush graduating device

Country Status (1)

Country Link
CN (1) CN208451440U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112809644A (en) * 2021-01-15 2021-05-18 陕西科技大学 Circular part cylindrical surface scribing device and scribing method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112809644A (en) * 2021-01-15 2021-05-18 陕西科技大学 Circular part cylindrical surface scribing device and scribing method

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