CN204183452U - A kind of part holding device - Google Patents

A kind of part holding device Download PDF

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Publication number
CN204183452U
CN204183452U CN201420597266.4U CN201420597266U CN204183452U CN 204183452 U CN204183452 U CN 204183452U CN 201420597266 U CN201420597266 U CN 201420597266U CN 204183452 U CN204183452 U CN 204183452U
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CN
China
Prior art keywords
pedestal
connecting hole
push rod
base
support bar
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Expired - Lifetime
Application number
CN201420597266.4U
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Chinese (zh)
Inventor
韩美洲
张旭
王坤
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AVIC Aircraft Corp Ltd
AVIC Xian Aircraft Industry Group Co Ltd
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AVIC Aircraft Corp Xian Aircraft Branch
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Publication date
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Priority to CN201420597266.4U priority Critical patent/CN204183452U/en
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Publication of CN204183452U publication Critical patent/CN204183452U/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Abstract

一种零件顶紧装置,含有基座、支撑杆和顶杆,所述的基座是一个圆柱状体,其上部中心有连接孔,支撑杆的下端间隙插接在基座的连接孔内,另有一个压紧螺钉将支撑杆与基座固定,支撑杆的上端是一个有连接孔的叉耳结构,有一个销轴铰接在叉耳的连接孔上,顶杆是一个带外螺纹的长螺杆,顶杆螺接在销轴中部的螺纹孔内,顶杆的前端连接有顶块。

A component tightening device, comprising a base, a support rod and a push rod, the base is a cylindrical body with a connecting hole in the center of the upper part, and the lower end of the support rod is inserted into the connecting hole of the base, There is also a compression screw to fix the support rod and the base. The upper end of the support rod is a fork lug structure with a connecting hole, and a pin is hinged on the connecting hole of the fork lug. The ejector rod is a long Screw rod, the push rod is screwed in the threaded hole in the middle part of the pin shaft, and the front end of the push rod is connected with a top block.

Description

一种零件顶紧装置A part clamping device

技术领域technical field

本申请涉及飞机零件生产中所使用的顶紧装置,尤其适用于任意型面及任意角度的可旋转顶紧装置。The application relates to a clamping device used in the production of aircraft parts, and is especially suitable for a rotatable clamping device with any profile and any angle.

背景技术Background technique

在零件的生产制造过程中,为满足零件的精度要求,通常需要通过夹具对零件进行定位、压紧。而螺钉支座顶紧装置是夹具中一种常用的压紧方式。飞机零件庞杂多样,需要顶紧的面可分为平面、多角度平面、曲面。对于与夹具某一面平行的面可用通用的螺钉支座进行顶紧。但对于多角度平面、曲面顶紧需要专用的顶紧机构,方能使顶紧机构顶紧面与零件被顶紧面充分贴合。这种专用顶紧机构使用过程中,由于每个顶紧位置的型面不同,致使顶紧机构不同。如此,对于外廓尺寸较大、型面复杂的零件,顶紧机构不能批量制造,不能互换使用,造成生产成本偏高。并且在零件加工使用过程中,每个顶紧机构的位置是固定的。如果顶紧机构可卸,容易造成混淆使用,易致使零件变形,使用极为不方便,且装夹零件时间长。对于批量生产的零件来说,现有的专用顶紧机构的缺点在于通用性差,利用率低,增加零件的加工成本,降低生产效率。In the manufacturing process of parts, in order to meet the precision requirements of the parts, it is usually necessary to position and compress the parts through fixtures. The screw support jacking device is a commonly used pressing method in the fixture. Aircraft parts are complex and diverse, and the surfaces that need to be tightened can be divided into flat surfaces, multi-angle flat surfaces, and curved surfaces. For the surface parallel to a certain surface of the fixture, it can be tightened with a general-purpose screw support. However, a special clamping mechanism is required for multi-angle plane and curved surface clamping, so that the clamping surface of the clamping mechanism can fully fit the clamped surface of the part. During the use of this special tightening mechanism, due to the different profiles of each tightening position, the tightening mechanism is different. In this way, for parts with large external dimensions and complex profiles, the jacking mechanism cannot be mass-produced and cannot be used interchangeably, resulting in high production costs. And in the process of parts processing, the position of each clamping mechanism is fixed. If the jacking mechanism is detachable, it is easy to cause confusion and deformation of the parts, which is extremely inconvenient to use and takes a long time to clamp the parts. For parts produced in batches, the disadvantages of the existing special clamping mechanism are poor versatility, low utilization rate, increased processing cost of parts, and reduced production efficiency.

发明内容Contents of the invention

本申请的目的在于提供一种通用性好的零件顶紧装置。The purpose of this application is to provide a component clamping device with good versatility.

一种零件顶紧装置,含有基座、支撑杆和顶杆,其特征在于,所述的基座是一个圆柱状体,基座的下端有带外螺纹的固定柄,基座的上部中心有连接孔,基座上有一个垂直于连接孔孔壁的螺纹压紧孔,支撑杆的下端是连接柄,连接柄上有环形压紧槽,支撑杆的连接柄可以间隙插接在基座的连接孔内,另有一个压紧螺钉通过基座的压紧孔进入支撑杆连接柄的压紧槽,将支撑杆与基座固定,支撑杆的上端是一个有连接孔的叉耳结构,有一个销轴铰接在叉耳的连接孔上,顶杆是一个带外螺纹的长螺杆,顶杆螺接在销轴中部的螺纹孔内,顶杆的前端连接有顶块。A part tightening device, comprising a base, a support rod and a push rod, characterized in that the base is a cylindrical body, the lower end of the base has a fixed handle with external threads, and the upper center of the base has a Connecting hole, there is a threaded pressing hole perpendicular to the wall of the connecting hole on the base, the lower end of the support rod is a connecting handle, and there is an annular pressing groove on the connecting handle, the connecting handle of the supporting rod can be inserted into the base In the connection hole, another compression screw enters the compression groove of the connection handle of the support rod through the compression hole of the base to fix the support rod and the base. The upper end of the support rod is a fork ear structure with a connection hole. A pin shaft is hinged on the connecting hole of the fork ear, the push rod is a long screw rod with external thread, the push rod is screwed in the threaded hole in the middle part of the pin shaft, and the front end of the push rod is connected with a top block.

本申请的有益效果在于:顶杆的顶紧方向可以任意多角度的调整,支撑杆相对于基座可以在水平方向任意角度旋转,顶杆相对于支撑杆可以在垂直方向转动顶紧角度,大大拓展了顶紧零件的通用性。The beneficial effect of the present application is that: the tightening direction of the ejector rod can be adjusted at any angle, the support rod can rotate at any angle in the horizontal direction relative to the base, and the ejector rod can rotate in the vertical direction relative to the support rod at a tightening angle, greatly Expand the versatility of the jacking parts.

以下结合实施例附图对本申请做进一步详细描述。The present application will be further described in detail below in conjunction with the accompanying drawings of the embodiments.

附图说明Description of drawings

图1是零件顶紧装置的结构示意Figure 1 is a schematic diagram of the structure of the parts clamping device

图2是零件顶紧装置使用状态的剖面示意Figure 2 is a schematic cross-sectional view of the working state of the part clamping device

图中编号说明:1基座、2支撑杆、3顶杆、4固定柄、5压紧螺钉、6叉耳、7销轴、8顶块、9螺纹压紧孔、10环形压紧槽、11工装体、12零件Description of numbers in the figure: 1 base, 2 support rods, 3 ejector rods, 4 fixed handles, 5 compression screws, 6 fork ears, 7 pin shafts, 8 top blocks, 9 thread compression holes, 10 annular compression grooves, 11 tooling body, 12 parts

具体实施方式Detailed ways

参见附图,零件顶紧装置,含有基座1、支撑杆2和顶杆3,所述的基座1是一个圆柱状体,基座1的下端有带外螺纹的固定柄4,该固定柄4可以将基座固定在零件12装配用的工装体11的定位孔上,基座1的上部中心有连接孔,支撑杆的下端与该连接孔间隙配合,支撑杆相对于连接孔可以在水平方向转动,以达到调节顶杆的水平顶紧方向,为了固定支撑杆与基座的相对位置,在基座上有一个垂直于连接孔孔壁的螺纹压紧孔9,支撑杆2的下端是连接柄,连接柄上有环形压紧槽10,用于限定连接柄的上限位移,支撑杆2的连接柄插接在基座1的连接孔内,另有一个压紧螺钉5通过基座1的螺纹压紧孔9进入支撑杆连接柄的环形压紧槽10,将支撑杆2与基座1固定;支撑杆2的上端是一个有连接孔的叉耳6,有一个销轴7铰接在叉耳6的连接孔上,该销轴可以在叉耳的连接孔内轴向转动,顶杆3是一个带外螺纹的长螺杆,顶杆3螺接在销轴7中部的螺纹孔内,顶杆的前端连接有顶块8。Referring to the accompanying drawings, the part tightening device includes a base 1, a support rod 2 and a push rod 3. The base 1 is a cylindrical body, and the lower end of the base 1 has a fixed handle 4 with external threads. The handle 4 can fix the base on the positioning hole of the tooling body 11 used for assembling the parts 12. The upper center of the base 1 has a connection hole, and the lower end of the support rod is clearance-fitted with the connection hole. The support rod can be positioned relative to the connection hole Rotate in the horizontal direction to adjust the horizontal tightening direction of the ejector rod. In order to fix the relative position of the support rod and the base, there is a threaded pressing hole 9 perpendicular to the wall of the connecting hole on the base. The lower end of the support rod 2 It is a connecting handle, and there is an annular compression groove 10 on the connecting handle, which is used to limit the upper limit displacement of the connecting handle. The connecting handle of the support rod 2 is inserted into the connecting hole of the base 1, and another compression screw 5 passes through the base The threaded pressing hole 9 of 1 enters the annular pressing groove 10 of the connecting handle of the supporting rod, and the supporting rod 2 and the base 1 are fixed; the upper end of the supporting rod 2 is a fork ear 6 with a connecting hole, and a pin shaft 7 is hinged On the connection hole of the fork lug 6, the pin shaft can rotate axially in the connection hole of the fork lug, the push rod 3 is a long screw with external thread, and the push rod 3 is screwed in the threaded hole in the middle of the pin shaft 7 , the front end of the push rod is connected with a top block 8.

本申请结构简单,操作方便、省时省力,顶紧灵活、顶紧力足够,成本较低,通用性好,可用于多角度平面及大曲率型面的顶紧,因此实用性好,易于推广应用,具有较大的实用价值。The application has the advantages of simple structure, convenient operation, time-saving and labor-saving, flexible jacking, sufficient jacking force, low cost, good versatility, and can be used for jacking of multi-angle planes and large-curvature profiles, so it has good practicability and is easy to popularize application, has great practical value.

Claims (1)

1. a part holding device, containing pedestal, support bar and push rod, it is characterized in that, described pedestal is a cylinder, there is the externally threaded fixed handle of band the lower end of pedestal, the central upper portion of pedestal has connecting hole, pedestal there is one perpendicular to the screw thread hold-down apertures of connecting hole hole wall, the lower end of support bar is connection handle, connection handle there is ring compression groove, the connection handle of support bar can be plugged in the connecting hole of pedestal in gap, a housing screw is separately had to be entered the pressing groove of support bar connection handle by the hold-down apertures of pedestal, support bar and pedestal are fixed, the upper end of support bar is a fork ear structure having connecting hole, there is a hinge on the connecting hole of fork ear, push rod is an externally threaded long bolt of band, push rod is screwed onto in the screwed hole in the middle part of bearing pin, the front end of push rod is connected with jacking block.
CN201420597266.4U 2014-10-15 2014-10-15 A kind of part holding device Expired - Lifetime CN204183452U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420597266.4U CN204183452U (en) 2014-10-15 2014-10-15 A kind of part holding device

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Application Number Priority Date Filing Date Title
CN201420597266.4U CN204183452U (en) 2014-10-15 2014-10-15 A kind of part holding device

Publications (1)

Publication Number Publication Date
CN204183452U true CN204183452U (en) 2015-03-04

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106181832A (en) * 2016-09-23 2016-12-07 江西洪都航空工业集团有限责任公司 Belt lock catch clamp termination joint
CN109552664A (en) * 2018-12-07 2019-04-02 江西洪都航空工业集团有限责任公司 A kind of adjustable limit holding device in direction
CN110695896A (en) * 2019-11-26 2020-01-17 中国航发沈阳黎明航空发动机有限责任公司 An aero-engine junction ring assembly support fixture and its assembly process
CN114833536A (en) * 2022-07-04 2022-08-02 保定康强医疗器械制造有限公司 Femoral medullary cavity filing process and primary milling tool

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106181832A (en) * 2016-09-23 2016-12-07 江西洪都航空工业集团有限责任公司 Belt lock catch clamp termination joint
CN109552664A (en) * 2018-12-07 2019-04-02 江西洪都航空工业集团有限责任公司 A kind of adjustable limit holding device in direction
CN110695896A (en) * 2019-11-26 2020-01-17 中国航发沈阳黎明航空发动机有限责任公司 An aero-engine junction ring assembly support fixture and its assembly process
CN110695896B (en) * 2019-11-26 2021-04-16 中国航发沈阳黎明航空发动机有限责任公司 An aero-engine junction ring assembly support fixture and its assembly process
CN114833536A (en) * 2022-07-04 2022-08-02 保定康强医疗器械制造有限公司 Femoral medullary cavity filing process and primary milling tool

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP03 Change of name, title or address
CP03 Change of name, title or address

Address after: No. 710089 in Shaanxi province Xi'an city Yanliang District West Avenue

Patentee after: AVIC Xi'an Aircraft Industry Group Co.,Ltd.

Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee before: AVIC AIRCRAFT Corp.

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20210617

Address after: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee after: AVIC AIRCRAFT Corp.

Address before: 1 No. 710089 Shaanxi province Xi'an city Yanliang District West Avenue

Patentee before: XI'AN AIRCRAFT BRANCH OF XI'AN AIRCRAFT INTERNATIONAL Corp.

CX01 Expiry of patent term
CX01 Expiry of patent term

Granted publication date: 20150304