CN206717785U - A kind of airplane parts composite processing support meanss - Google Patents

A kind of airplane parts composite processing support meanss Download PDF

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Publication number
CN206717785U
CN206717785U CN201720608888.6U CN201720608888U CN206717785U CN 206717785 U CN206717785 U CN 206717785U CN 201720608888 U CN201720608888 U CN 201720608888U CN 206717785 U CN206717785 U CN 206717785U
Authority
CN
China
Prior art keywords
sleeve
platen
support meanss
composite processing
threaded rod
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
CN201720608888.6U
Other languages
Chinese (zh)
Inventor
李彦斌
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.)
Harbin Shili Auto Parts Co Ltd
Original Assignee
Harbin Shili Auto Parts 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 Harbin Shili Auto Parts Co Ltd filed Critical Harbin Shili Auto Parts Co Ltd
Priority to CN201720608888.6U priority Critical patent/CN206717785U/en
Application granted granted Critical
Publication of CN206717785U publication Critical patent/CN206717785U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A kind of airplane parts composite processing support meanss, belong to airplane parts technical field of processing equipment.It provides a kind of airplane parts composite processing support meanss that can be adjusted height, be capable of retaining element or fixture.Four upper surfaces of threaded rod one are fixedly connected with platen bottom surface, each lower end of threaded rod one respectively sets female sleeve one with one and is threadedly coupled, four bases are arranged on four lower sections of sleeve one, it is rotatablely connected between four bases and corresponding sleeve one, hanging plate bottom surface on rear side of platen upper surface with being fixedly connected, hanging plate leading flank lower end opens up fluted, groove upper and lower ends face offers slide rail, two sliding block upper and lower ends are slided and are rotatablely connected with two slide rails of groove, each sliding block lateral surface is respectively fixedly connected with a fix bar one end, two fix bars are expansion link, connected between two fix bars by fixing device.The utility model is applied to airplane parts composite processing operation.

Description

A kind of airplane parts composite processing support meanss
Technical field
The utility model belongs to airplane parts technical field of processing equipment, is processed more particularly to a kind of part with support dress Put.
Background technology
Composite, it is by two or more material of different nature, by method physically or chemically, in macroscopic view (It is microcosmic)Upper material of the composition with new capability.Various materials make up for each other's deficiencies and learn from each other in performance, produce cooperative effect, make compound The combination property of material meets a variety of requirements better than former composition material.
Because composite heat endurance is good, specific strength, specific stiffness are high, available for manufacture airplane parts etc., fly making During machine part, typically using workbench as support meanss, and existing workbench function is single, it is impossible to is processed needed for fixed Part or fixture, certain inconvenience caused to part processing, while support meanss can not adjust height, to too high or too short People all cause certain inconvenience.
The content of the invention
In view of the above-mentioned problems of the prior art, the utility model provide one kind can adjust height, being capable of constant zero The airplane parts composite processing support meanss of part or fixture.
Technical solution adopted in the utility model is:A kind of airplane parts composite processing support meanss, including Platen, hanging plate, fixing device, two sliding blocks, two fix bars, four threaded rods, one, four sleeve one and four bases;It is described Platen is horizontally disposed with, and described four upper surfaces of threaded rod one being vertically arranged are fixedly connected with platen bottom surface, four threaded rods one Rectangular arrangement, each lower end of threaded rod one respectively set female sleeve one with one and are threadedly coupled, and four bases are set Put below four sleeves one, be rotatablely connected between four bases and corresponding sleeve one, the hanging plate bottom surface being vertically arranged With being fixedly connected on rear side of platen upper surface, hanging plate leading flank lower end offers groove, the groove upper and lower ends in the horizontal direction Face offers slide rail in the horizontal direction, and described two sliding block upper and lower ends are slided and are rotatablely connected with two slide rails of groove, Each sliding block lateral surface is respectively fixedly connected with a fix bar one end, and described two fix bars are expansion link, described two solid Connected between fixed pole by fixing device.
The beneficial effects of the utility model are:
1. fixing device of the present utility model and two fix bars are used cooperatively the part or folder that can fix required processing Tool, while two fix bars are slided and are rotatablely connected by sliding block and slideway, use is more flexible, can be conveniently adjusted two fixations The distance between bar, when not in use, two fix bars can be placed in the groove of hanging plate, save space, and without prejudice to work Make personnel's operation.
2. threaded rod one of the present utility model and sleeve one are used cooperatively, platen height can be adjusted, is easy to different height Staff use, it is and easy to operate.
Brief description of the drawings
Fig. 1:The utility model structure diagram;
Fig. 2:The utility model sliding block and fixed rod structure schematic diagram;
Fig. 3:The utility model fixture structure schematic diagram;
Wherein:1- bases;2- sleeves one;3- threaded rods one;4- rubber sleeves;5- platens;6- hanging plates;6-1- grooves;7- is slided Block;8- fix bars;9- fixing devices;9-1- handgrips;9-2- sleeves two;9-3- threaded rods two;10- multi-layer drawers;11- gaps.
Embodiment
As shown in Fig. 1 ~ Fig. 3, a kind of airplane parts composite processing support meanss, including platen 5, hanging plate 6, fixation 9, two, the device fix bar 8, four of sliding block 7, two sleeve 1 of threaded rod one 3, four and four bases 1;The water of platen 5 Flat to set, described four upper surfaces of threaded rod 1 being vertically arranged are fixedly connected with the bottom surface of platen 5, four threaded rods 1,3 one-tenth squares Shape arranges, and each lower end of threaded rod 1 respectively sets female sleeve 1 with one and is threadedly coupled, and four bases 1 are set Below four sleeves 1, it is rotatablely connected between four bases 1 and corresponding sleeve 1, the bottom of hanging plate 6 being vertically arranged With being fixedly connected on rear side of the upper surface of platen 5, the leading flank lower end of hanging plate 6 offers groove 6-1, the groove 6- in the horizontal direction in face 1 upper and lower ends face offers slide rail in the horizontal direction, and described two upper and lower ends of sliding block 7 are slided with two slide rails of groove 6-1 Dynamic and rotation connection, each lateral surface of sliding block 7 are respectively fixedly connected with the one end of fix bar 8, and described two fix bars 8 are to stretch Contracting bar, connected by fixing device 9 between described two fix bars 8.
The fixing device 9 includes two 9-2 and two 9-3 of threaded rod two, sleeve handgrip 9-1;The 9-3 mono- of threaded rod two End is connected with the 9-2 threaded one ends of sleeve two, and the 9-3 other ends of threaded rod two and the 9-2 other ends of sleeve two are respectively consolidated with a handgrip 9-1 Fixed connection, described two handgrip 9-1 are used to fix two fix bars 8.
The airplane parts composite processing also includes four rubber sleeves 4 with support meanss, each threaded rod 1 Lateral surface is set with rubber sleeve 4, and each upper surface of rubber sleeve 4 is fixedly connected with the bottom surface of platen 5, each rubber sleeve 4 Bottom surface is fixedly connected with the corresponding upper surface of sleeve 1, between four rubber sleeves 4 are provided between corresponding threaded rod 1 Gap 11.
Airplane parts composite processing support meanss also include multi-layer drawers 10, the upper end of multi-layer drawers 10 Face is fixedly connected with the bottom surface of platen 5.
Application method:
For processed needed for fixation part or fixture when, by two fix bars 8 by sliding block 7 slide into processing part or Behind fixture both sides, the length of two fix bars 8 is adjusted, two handgrips are adjusted further according to the distance between two fix bars 8 9-1 distance, two handgrip 9-1 are fixed in two fix bars 8, spiral shell can adjust by the 9-2 of turnbarrel two in addition The 9-3 of rasp bar two outreach, so as to adjust two handgrip 9-1 distance;
After the completion of use, two fix bars 8 are rotated in rearward recess 6-1 by sliding block 7;
Adjust the height of platen 5, it is only necessary to which turnbarrel 1 adjusts the lifting of threaded rod 1.
The leading flank of hanging plate 6 is provided with multiple hole slots, the instrument used for hooking staff etc..
Preferred embodiment of the present utility model is the foregoing is only, is not limited to the utility model, for this For the technical staff in field, the utility model can have various modifications and variations.It is all in the spirit and principles of the utility model Within, any modification, equivalent substitution and improvements made etc., it should be included within the scope of protection of the utility model.

Claims (4)

  1. A kind of 1. airplane parts composite processing support meanss, it is characterised in that:Including platen(5), hanging plate(6), it is fixed Device(9), two sliding blocks(7), two fix bars(8), four threaded rods one(3), four sleeves one(2)And four bases(1); The platen(5)It is horizontally disposed, described four threaded rods one being vertically arranged(3)Upper surface and platen(5)Bottom surface is fixedly connected, Four threaded rods one(3)Rectangular arrangement, each threaded rod one(3)Lower end respectively sets female sleeve one with one(2)Spiral shell Line connects, four bases(1)It is arranged on four sleeves one(2)Lower section, four bases(1)With corresponding sleeve one(2)It Between be rotatablely connected, the hanging plate being vertically arranged(6)Bottom surface and platen(5)It is fixedly connected on rear side of upper surface, hanging plate(6)Leading flank Lower end offers groove in the horizontal direction(6-1), the groove(6-1)Upper and lower ends face offers slide rail in the horizontal direction, Described two sliding blocks(7)Upper and lower ends are and groove(6-1)Two slide rails are slided and are rotatablely connected, each sliding block(7)Lateral surface Respectively with a fix bar(8)One end is fixedly connected, described two fix bars(8)It is expansion link, described two fix bars(8)It Between pass through fixing device(9)Connection.
  2. A kind of 2. airplane parts composite processing support meanss according to claim 1, it is characterised in that:It is described solid Determine device(9)Including threaded rod two(9-3), sleeve two(9-2)And two handgrips(9-1);The threaded rod two(9-3)One end with Sleeve two(9-2)Threaded one end connects, threaded rod two(9-3)The other end and sleeve two(9-2)The other end respectively with a handgrip(9- 1)It is fixedly connected, described two handgrips(9-1)For fixing two fix bars(8).
  3. A kind of 3. airplane parts composite processing support meanss according to claim 1, it is characterised in that:It is described to fly Machine part composite processing also includes four rubber sleeves with support meanss(4), each threaded rod one(3)Lateral surface covers Equipped with rubber sleeve(4), each rubber sleeve(4)Upper surface is and platen(5)Bottom surface is fixedly connected, each rubber sleeve(4)Bottom Face with corresponding sleeve one(2)Upper surface is fixedly connected, four rubber sleeves(4)With corresponding threaded rod one(3)Between set There is gap(11).
  4. A kind of 4. airplane parts composite processing support meanss according to claim 1, it is characterised in that:It is described to fly Machine part composite processing also includes multi-layer drawers with support meanss(10), the multi-layer drawers(10)Upper surface and platen (5)Bottom surface is fixedly connected.
CN201720608888.6U 2017-05-27 2017-05-27 A kind of airplane parts composite processing support meanss Expired - Fee Related CN206717785U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720608888.6U CN206717785U (en) 2017-05-27 2017-05-27 A kind of airplane parts composite processing support meanss

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720608888.6U CN206717785U (en) 2017-05-27 2017-05-27 A kind of airplane parts composite processing support meanss

Publications (1)

Publication Number Publication Date
CN206717785U true CN206717785U (en) 2017-12-08

Family

ID=60511251

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720608888.6U Expired - Fee Related CN206717785U (en) 2017-05-27 2017-05-27 A kind of airplane parts composite processing support meanss

Country Status (1)

Country Link
CN (1) CN206717785U (en)

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20171208

Termination date: 20180527

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