CN205166466U - Radial coaxial irregularly -shaped hole of multilayer part processing frock - Google Patents

Radial coaxial irregularly -shaped hole of multilayer part processing frock Download PDF

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Publication number
CN205166466U
CN205166466U CN201521017988.9U CN201521017988U CN205166466U CN 205166466 U CN205166466 U CN 205166466U CN 201521017988 U CN201521017988 U CN 201521017988U CN 205166466 U CN205166466 U CN 205166466U
Authority
CN
China
Prior art keywords
floor
mount pad
cover plate
apron
shaped hole
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
CN201521017988.9U
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Chinese (zh)
Inventor
陈继宁
黄斌
聂光万
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.)
Guizhou Aerospace Fenghua Precision Equipment Co Ltd
Original Assignee
Guizhou Aerospace Fenghua Precision 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 Guizhou Aerospace Fenghua Precision Equipment Co Ltd filed Critical Guizhou Aerospace Fenghua Precision Equipment Co Ltd
Priority to CN201521017988.9U priority Critical patent/CN205166466U/en
Application granted granted Critical
Publication of CN205166466U publication Critical patent/CN205166466U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model provides a radial coaxial irregularly -shaped hole of multilayer part processing frock, including base, floor, mount pad, outer apron, interior apron, well apron, be provided with the floor on the base, a side of floor is the inclined plane, is provided with the mount pad on the inclined plane of floor, treat processing the part place in on the mount pad to approximately be equipped with well apron, interior apron from inside to outside in proper order on the part, lap outward in the relative one side of mount pad place one side, outer apron, interior apron, the well apron compress tightly the cover in the three -layer part successive layer of treating processing. The utility model discloses time that axial between each part of assurance that can be stable, circumference, concentricity requirement, the process of the pincers worker that can simplify simultaneously repair irregularly -shaped hole consume, and once only process 3 parts, great improvement the machining efficiency of part.

Description

The radial coaxial special-shaped hole machined frock of a kind of multilayer part
Technical field
The utility model relates to the radial coaxial special-shaped hole machined frock of a kind of multilayer part.
Background technology
The structure of multilayer part concentric arrangement is there is in aero-engine structure as shown in Figure 1; the object that multilayer part and pipeline pass through multiple part is supported for playing; the structural design of radial hollow rectification support plate can be increased in structural design of fittings; simultaneously for ensureing the aerodynamic arrangement of engine runner, the cross section of hollow rectification support plate can be designed to polymorphic structure usually.
In tradition processing, it is independent processing that plate hole is propped up in different part rectification, independently add the error accumulation of trade union due to the frock of work in-process, lathe, location, centering, cause part to coordinate not mate carrying out in assembling process size, size is not mated and is comprised axial length dimension, circumferential angular position relative and each part rectification and prop up the unmatched situation of plate hole hole shape and occur.When after the unmatched situation of generation size, often adopt the mode of pincers worker repair to reprocess, owing to cannot find the place place of problem timely and effectively, pincers worker repair part process will expend the too much time.
Utility model content
For solving the problems of the technologies described above, the utility model provides the radial coaxial special-shaped hole machined frock of a kind of multilayer part, the radial coaxial special-shaped hole machined frock of this multilayer part can be stable each part of guarantee between axial, circumferential, concentricity requirement, the time of the process consumes of the pincers worker repair irregularly-shaped hole that simultaneously can simplify, and disposable processing 3 parts, improve the working (machining) efficiency of part greatly.
The utility model is achieved by the following technical programs.
The radial coaxial special-shaped hole machined frock of a kind of multilayer part that the utility model provides, comprises base, floor, mount pad, outer cover plate, inner cover plate, cover plate; Described base is provided with floor, and a side of floor is inclined-plane, and the inclined-plane of floor is provided with mount pad; Part to be processed is positioned on described mount pad, and in the one side that mount pad place one side is relative, has mounted cover cover plate, inner cover plate, outer cover plate successively from inside to outside on part; Described outer cover plate, inner cover plate, cover plate successively compress covering in be processed three layers of part.
Also be fixed with fixed axis between described floor and mount pad, fixed axis and part to be processed are coaxially arranged.
Described fixed axis is fixed by alignment pin and floor.
The beneficial effects of the utility model are: axial, circumferential, the concentricity requirement between each part of guarantee that can be stable, the time of the process consumes of the pincers worker repair irregularly-shaped hole that simultaneously can simplify, and disposable processing 3 parts, improve the working (machining) efficiency of part greatly.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of part to be processed.
In figure: 1-base, 2-floor, 3-fixed axis, 4-mount pad, 5-outer cover plate, 6-inner cover plate, 7-cover plate, 8-alignment pin.
Detailed description of the invention
Further describe the technical solution of the utility model below, but described in claimed scope is not limited to.
The radial coaxial special-shaped hole machined frock of a kind of multilayer part as shown in Figure 1, comprises base 1, floor 2, mount pad 4, outer cover plate 5, inner cover plate 6, cover plate 7; Described base 1 is provided with floor 2, and a side of floor 2 is inclined-plane, the inclined-plane of floor 2 is provided with mount pad 4; Part to be processed is positioned on described mount pad 4, and in the one side that mount pad 4 place one side is relative, has mounted cover cover plate 7, inner cover plate 6, outer cover plate 5 from inside to outside successively on part; Described outer cover plate 5, inner cover plate 6, cover plate 7 successively compress covering in be processed three layers of part.
Also be fixed with fixed axis 3 between described floor 2 and mount pad 4, fixed axis 3 and part to be processed are coaxially arranged.
Described fixed axis 3 is fixed by alignment pin 8 and floor 2.
Adopt above-mentioned setting, mount pad 4 carries out axis, circumference and concentricity to 3 parts and controls, base 1 for lathe table top location and installation, floor 2 connects for being fixed and ensureing the angle of part irregularly-shaped hole, fixed axis 3 is for ensureing that mount pad 4 pivot immobilizes, mount pad 4 carries out Set and Positioning for part and special-shaped circumferential angle positions, and alignment pin 8 is located for the calibration of part, and cover plate 7, inner cover plate 6, outer cover plate 5 are for compressing component.
The utility model in use, first part is installed on mount pad 4, compress with cover plate 5,6, then mount pad 4 is installed on fixed axis 3, circumferential dowel hole on alignment fixed axis 3 and on mount pad 4, by alignment pin 8 patchhole, be fixed with cover plate 7 pairs of parts, can to irregularly-shaped hole processing on part; After machining place's irregularly-shaped hole, unclamp cover plate 7 screwing, rotary mounting seat 4 screwing, rotary mounting seat 4 certain angle, again the circumferential dowel hole on alignment fixed axis 3 and on mount pad 4, again be fixed with cover plate 7 pairs of parts, can, to next place's irregularly-shaped hole processing on part, repeat to process irregularly-shaped holes all on part with this.

Claims (3)

1. the radial coaxial special-shaped hole machined frock of multilayer part, comprise base (1), floor (2), mount pad (4), outer cover plate (5), inner cover plate (6), cover plate (7), it is characterized in that: described base (1) is provided with floor (2), one side of floor (2) is inclined-plane, the inclined-plane of floor (2) is provided with mount pad (4); Part to be processed is positioned on described mount pad (4), and in the one side that mount pad (4) place one side is relative, has mounted cover cover plate (7), inner cover plate (6), outer cover plate (5) from inside to outside successively on part; Described outer cover plate (5), inner cover plate (6), cover plate (7) successively compress covering in be processed three layers of part.
2. the radial coaxial special-shaped hole machined frock of multilayer part as claimed in claim 1, it is characterized in that: be also fixed with fixed axis (3) between described floor (2) and mount pad (4), fixed axis (3) and part to be processed are coaxially arranged.
3. the radial coaxial special-shaped hole machined frock of multilayer part as claimed in claim 1, is characterized in that: described fixed axis (3) is fixed by alignment pin (8) and floor (2).
CN201521017988.9U 2015-12-09 2015-12-09 Radial coaxial irregularly -shaped hole of multilayer part processing frock Expired - Fee Related CN205166466U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201521017988.9U CN205166466U (en) 2015-12-09 2015-12-09 Radial coaxial irregularly -shaped hole of multilayer part processing frock

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201521017988.9U CN205166466U (en) 2015-12-09 2015-12-09 Radial coaxial irregularly -shaped hole of multilayer part processing frock

Publications (1)

Publication Number Publication Date
CN205166466U true CN205166466U (en) 2016-04-20

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201521017988.9U Expired - Fee Related CN205166466U (en) 2015-12-09 2015-12-09 Radial coaxial irregularly -shaped hole of multilayer part processing frock

Country Status (1)

Country Link
CN (1) CN205166466U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106670849A (en) * 2016-12-02 2017-05-17 中国兵器科学研究院宁波分院 Machining device and method for seat ring and guide pipe hole in engine cylinder cover
CN107877210A (en) * 2017-12-16 2018-04-06 贵州航天风华精密设备有限公司 A kind of fixture for the coaxial special-shaped hole machined of multilayer part

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106670849A (en) * 2016-12-02 2017-05-17 中国兵器科学研究院宁波分院 Machining device and method for seat ring and guide pipe hole in engine cylinder cover
CN106670849B (en) * 2016-12-02 2019-07-16 中国兵器科学研究院宁波分院 The process equipment and processing method of engine cylinder cover top race and guide hole
CN107877210A (en) * 2017-12-16 2018-04-06 贵州航天风华精密设备有限公司 A kind of fixture for the coaxial special-shaped hole machined of multilayer part

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20160420