CN104476227A - Tool clamp for fast replacing and clamping and locating plurality of aeronautical parts - Google Patents

Tool clamp for fast replacing and clamping and locating plurality of aeronautical parts Download PDF

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Publication number
CN104476227A
CN104476227A CN201410649992.0A CN201410649992A CN104476227A CN 104476227 A CN104476227 A CN 104476227A CN 201410649992 A CN201410649992 A CN 201410649992A CN 104476227 A CN104476227 A CN 104476227A
Authority
CN
China
Prior art keywords
plate
clamping
locating
header board
positioning
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.)
Pending
Application number
CN201410649992.0A
Other languages
Chinese (zh)
Inventor
陈勇
何波
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.)
Chengdu Siwi High Tech Industrial Park Co Ltd
Original Assignee
Chengdu Siwi High Tech Industrial Park 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 Chengdu Siwi High Tech Industrial Park Co Ltd filed Critical Chengdu Siwi High Tech Industrial Park Co Ltd
Priority to CN201410649992.0A priority Critical patent/CN104476227A/en
Publication of CN104476227A publication Critical patent/CN104476227A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q3/00Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/02Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
    • B23Q3/06Work-clamping means
    • B23Q3/061Work-clamping means adapted for holding a plurality of workpieces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q3/00Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/02Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
    • B23Q3/06Work-clamping means
    • B23Q3/062Work-clamping means adapted for holding workpieces having a special form or being made from a special material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Jigs For Machine Tools (AREA)

Abstract

The invention discloses a tool clamp for fast replacing and clamping and locating a plurality of aeronautical parts. The tool clamp comprises a bottom plate, a front plate, a part die plate and a rear plate; a plurality of V-shaped grooves, which are in a direction from the front to back, are formed from left to right at intervals in the upper parts of the part die plate; two locating holes are formed in the bottom part of the part die plate; two locating columns in match with the locating holes are arranged on the top part of the bottom plate; the front plate and the rear plate are respectively fixed to the front part and the rear part of the part die late through fixing bolts; a plurality of compressing bars which are in the direction from front to back are in threaded connection to the front plate, corresponding to the V-shaped grooves. The tool clamp has the beneficial effects that the plurality of aeronautical parts can be clamped at a time, and the clamping is performed at the outside of a machine tool, so that the production efficiency can be raised, and the utilization rate of a numerically-controlled machine tool can be raised; the clamping is simple, the labor intensity of frequently clamping components is greatly reduced, and the production cost is saved.

Description

A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning
Technical field
The present invention relates to a kind of frock clamp, particularly a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, belong to Computerized Numerical Control processing technology field.
Background technology
Our unit is at present at a certain aviation part of processing, and its structure as shown in Figure 1, 2.The production lot of this aviation part is large, and quality requirement is high, and each part must by process operation person self-inspection after production completes, and the qualified rear dish of self-inspection can be delivered to special inspection place and recheck, thus strict guarantee product quality.
In process, because part is little, process time is short, need on digital controlled processing central machine tool frequent renewal part Set and Positioning.Continuous replacing like this, constantly Set and Positioning mode also exist following weak point:
One, the machining accuracy of part not easily ensures;
The effective rate of utilization of two, actual production efficiency and numerical control machine tool is very low;
Three, the labour intensity of process operation person is also large.
Because this part needs production fast in enormous quantities, therefore, how to enhance productivity, ensure that product quality is a very important problem simultaneously.
Summary of the invention
Goal of the invention of the present invention is: for the demand proposed in background technology, provides a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, can meet the demands.
The technical solution used in the present invention is such:
A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, comprise base plate, header board, part template and rear plate, described part template top is the some V-type grooves of spaced set from left to right, V-type groove groove is to being fore-and-aft direction, two locating holes are set bottom part template, described base plate top arranges two locating dowels and mates with locating hole, described front and rear panels are separately fixed at the front and rear of part template by set bolt, some sagittal compressions that described header board is also threaded rod corresponding each V-type groove.
As preferably, described V-type groove has six.
As preferably, described set bolt has the six roots of sensation, arranges two respectively in left, center, right portion.
As preferably, described compression rod is divided into screw rod and pressing plate two parts, and to being threaded on header board before and after screw rod, pressing plate is fixedly connected on spiro rod rear end.
In sum, owing to have employed technique scheme, the invention has the beneficial effects as follows:
1, can the multiple aviation part of clamped one time, and clamping process is carried out outside lathe, improves actual production efficiency and Digit Control Machine Tool utilization rate;
2, clamping is simple, considerably reduces the labour intensity of frequent clamping workpiece, has saved the production cost of my unit;
3, product quality can obtain good guarantee.
Accompanying drawing explanation
Fig. 1 is the front view of aviation part to be detected.
Fig. 2 is the right view of aviation part to be detected.
Fig. 3 is three-dimensional structure diagram of the present invention.
Mark in figure: 1 is base plate, and 2 is locating dowel, and 3 is set bolt, and 4 is header board, and 5 is part template, and 6 is rear plate, and 7 is V-type groove, 8 for compressing rod.
Detailed description of the invention
Below in conjunction with accompanying drawing, the present invention is described in detail.
Embodiment:
As shown in Figure 3, a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, comprise base plate 1, header board 4, part template 5 and rear plate 6, described part template 5 top is the some V-type grooves 7 of spaced set from left to right, V-type groove 7 groove is to being fore-and-aft direction, two locating holes are set bottom part template 5, described base plate 1 top arranges two locating dowels 2 and mates with locating hole, described header board 4 and rear plate 6 are separately fixed at the front and rear of part template 5 by set bolt 3, some sagittal compressions that described header board 4 is also threaded rod 8 corresponding each V-type groove 7.
Described V-type groove 6 has six.
Described set bolt 3 has the six roots of sensation, arranges two respectively in left, center, right portion.
Described compression rod 8 is divided into screw rod and pressing plate two parts, and to being threaded on header board 4 before and after screw rod, pressing plate is fixedly connected on spiro rod rear end.
Part shown in Fig. 1, Fig. 2 is positioned over part template 5 each V-type groove 7 in, then rotate compress rod 8, part is pushed against on rear plate 6.After part installs, header board 4, part template 5, rear plate 6 and each part entirety are put on base plate 1, the locating hole allowing locating dowel 2 insert bottom part template 5 positions.
The foregoing is only preferred embodiment of the present invention, not in order to limit the present invention, all any amendments done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within protection scope of the present invention.

Claims (4)

1. one kind for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, it is characterized in that: comprise base plate (1), header board (4), part template (5) and rear plate (6), described part template (5) top is the some V-type grooves (7) of spaced set from left to right, V-type groove (7) groove is to being fore-and-aft direction, part template (5) bottom arranges two locating holes, described base plate (1) top arranges two locating dowels (2) and mates with locating hole, described header board (4) and rear plate (6) are separately fixed at the front and rear of part template (5) by set bolt (3), some sagittal compressions rod (8) that described header board (4) is also threaded corresponding each V-type groove (7).
2. according to claim 1 a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, it is characterized in that: described V-type groove (6) has six.
3. according to claim 1 a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, it is characterized in that: described set bolt (3) has the six roots of sensation, arranges two respectively in left, center, right portion.
4. according to claim 1 a kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning, it is characterized in that; Described compression rod (8) is divided into screw rod and pressing plate two parts, and to being threaded on header board (4) before and after screw rod, pressing plate is fixedly connected on spiro rod rear end.
CN201410649992.0A 2014-11-17 2014-11-17 Tool clamp for fast replacing and clamping and locating plurality of aeronautical parts Pending CN104476227A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410649992.0A CN104476227A (en) 2014-11-17 2014-11-17 Tool clamp for fast replacing and clamping and locating plurality of aeronautical parts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410649992.0A CN104476227A (en) 2014-11-17 2014-11-17 Tool clamp for fast replacing and clamping and locating plurality of aeronautical parts

Publications (1)

Publication Number Publication Date
CN104476227A true CN104476227A (en) 2015-04-01

Family

ID=52750901

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410649992.0A Pending CN104476227A (en) 2014-11-17 2014-11-17 Tool clamp for fast replacing and clamping and locating plurality of aeronautical parts

Country Status (1)

Country Link
CN (1) CN104476227A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107756099A (en) * 2016-08-23 2018-03-06 苏州昊信精密机械有限公司 Shape extrusion fixture
CN109202491A (en) * 2018-11-20 2019-01-15 陕西海力特精密机械有限公司 Process the linear orientation clamping tooling of chuck jaws
CN115178813A (en) * 2022-08-02 2022-10-14 威海华邦精冲科技股份有限公司 Thread milling device and machining method thereof

Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2869433A (en) * 1957-04-25 1959-01-20 Aldege L Dery Loading magazine for a work holding fixture
US3091452A (en) * 1959-03-09 1963-05-28 North American Phillips Compan Holder for pluralities of objects
CN101081477A (en) * 2006-06-02 2007-12-05 鸿富锦精密工业(深圳)有限公司 Rolling circle smelting tool
CN201833206U (en) * 2010-09-28 2011-05-18 深圳市金三维模具有限公司 Hexagonal device processing clamp
CN202174420U (en) * 2011-08-04 2012-03-28 海南丰兴精密产业股份有限公司 Threaded cable clamp processing fixture
CN202224956U (en) * 2011-09-15 2012-05-23 河源职业技术学院 Multi-workpiece linear cutting machining linkage clamp
CN202846411U (en) * 2012-09-19 2013-04-03 铜陵辉腾模具科技有限公司 Locating clamping device used for pipe fitting machining
CN203282401U (en) * 2013-05-16 2013-11-13 苏州创丰精密五金有限公司 Riveting jig
CN203471398U (en) * 2013-08-27 2014-03-12 天津东义镁制品股份有限公司 Sacrificial anode milling machine die
CN203579271U (en) * 2013-09-12 2014-05-07 西安志越机电科技有限公司 Hydraulic driving type multi-station milling fixture
CN204235174U (en) * 2014-11-17 2015-04-01 成都四威高科技产业园有限公司 A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning

Patent Citations (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2869433A (en) * 1957-04-25 1959-01-20 Aldege L Dery Loading magazine for a work holding fixture
US3091452A (en) * 1959-03-09 1963-05-28 North American Phillips Compan Holder for pluralities of objects
CN101081477A (en) * 2006-06-02 2007-12-05 鸿富锦精密工业(深圳)有限公司 Rolling circle smelting tool
CN201833206U (en) * 2010-09-28 2011-05-18 深圳市金三维模具有限公司 Hexagonal device processing clamp
CN202174420U (en) * 2011-08-04 2012-03-28 海南丰兴精密产业股份有限公司 Threaded cable clamp processing fixture
CN202224956U (en) * 2011-09-15 2012-05-23 河源职业技术学院 Multi-workpiece linear cutting machining linkage clamp
CN202846411U (en) * 2012-09-19 2013-04-03 铜陵辉腾模具科技有限公司 Locating clamping device used for pipe fitting machining
CN203282401U (en) * 2013-05-16 2013-11-13 苏州创丰精密五金有限公司 Riveting jig
CN203471398U (en) * 2013-08-27 2014-03-12 天津东义镁制品股份有限公司 Sacrificial anode milling machine die
CN203579271U (en) * 2013-09-12 2014-05-07 西安志越机电科技有限公司 Hydraulic driving type multi-station milling fixture
CN204235174U (en) * 2014-11-17 2015-04-01 成都四威高科技产业园有限公司 A kind of for multiple aviation part quick-replaceable and the frock clamp of Set and Positioning

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107756099A (en) * 2016-08-23 2018-03-06 苏州昊信精密机械有限公司 Shape extrusion fixture
CN109202491A (en) * 2018-11-20 2019-01-15 陕西海力特精密机械有限公司 Process the linear orientation clamping tooling of chuck jaws
CN115178813A (en) * 2022-08-02 2022-10-14 威海华邦精冲科技股份有限公司 Thread milling device and machining method thereof

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Application publication date: 20150401

RJ01 Rejection of invention patent application after publication