CN107186623A - Airvane grinding hand-operated clamping fixture - Google Patents
Airvane grinding hand-operated clamping fixture Download PDFInfo
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- CN107186623A CN107186623A CN201710546750.2A CN201710546750A CN107186623A CN 107186623 A CN107186623 A CN 107186623A CN 201710546750 A CN201710546750 A CN 201710546750A CN 107186623 A CN107186623 A CN 107186623A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B24—GRINDING; POLISHING
- B24B—MACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
- B24B41/00—Component parts such as frames, beds, carriages, headstocks
- B24B41/06—Work supports, e.g. adjustable steadies
- B24B41/065—Steady rests
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Abstract
空气舵磨削加工手动夹紧夹具,包括底板、主板、中间板、锁止套筒、入口套、拉紧组件;主板竖直固接在底板上端;中间板平行于主板,并与主板相对固定,其上设有方孔;入口套安装在主板的安装孔中并与主板固接,其一端伸入到主板与中间板之间的区间内;锁止套筒位于主板与中间板之间的区间内,并通过其内孔中的光孔段活动套装在入口套的外壁上,其内孔与入口套的内孔连通并正对中间板的方孔;拉紧组件安装在中间板上并与锁止套筒关联,其可拉动锁止套筒向中间板移动,并使锁止套筒与中间板在彼此相对距离最近时保持相对固定。本发明只需一套夹具便可实现空气舵磨削加工时的装夹定位,解决了现有的空气舵磨削加工夹具成本偏高的问题。
Manual clamping fixture for air rudder grinding, including base plate, main plate, middle plate, locking sleeve, inlet sleeve, and tensioning assembly; the main plate is vertically fixed on the top of the base plate; the middle plate is parallel to the main plate and fixed relative to the main plate , there is a square hole on it; the inlet sleeve is installed in the installation hole of the main board and is fixedly connected with the main board, and one end of it extends into the interval between the main board and the middle board; the locking sleeve is located between the main board and the middle board In the interval, and through the light hole section in the inner hole, it is movably fitted on the outer wall of the inlet sleeve, and its inner hole communicates with the inner hole of the inlet sleeve and is facing the square hole of the middle plate; the tensioning component is installed on the middle plate and Associated with the locking sleeve, it can pull the locking sleeve to move toward the middle plate, and keep the locking sleeve and the middle plate relatively fixed when they are relatively closest to each other. The invention only needs one set of fixtures to realize the clamping and positioning during the air rudder grinding process, and solves the problem of relatively high cost of the existing air rudder grinding process fixtures.
Description
技术领域technical field
本发明涉及一种夹具,特别是一种空气舵磨削加工手动夹紧夹具。The invention relates to a fixture, in particular to a manual clamping fixture for air rudder grinding.
背景技术Background technique
空气舵是导弹上的方向控制部件,用来控制导弹飞行姿态和飞行轨迹。其结构如图7所示,包括三角板101、锥台102、螺纹杆103及四方块104;三角板101的前端面和后端面均为直角三角形,前、后端面之间通过底面、左侧面和右侧面连接;锥台102直径大的一端连接在三角板101的底面上;螺纹杆103一端连接在锥台102直径小的一端的端面上,另一端的端面上连接有四方块104。The air rudder is the direction control part on the missile, which is used to control the flight attitude and flight trajectory of the missile. Its structure is as shown in Figure 7, comprises triangular plate 101, truncated cone 102, threaded rod 103 and square block 104; The right side is connected; one end with a large diameter of the frustum 102 is connected to the bottom surface of the triangular plate 101; one end of the threaded rod 103 is connected to the end face of the small end of the diameter of the frustum 102, and the end face of the other end is connected with a square block 104.
空气舵的三角板101的底面及左侧面需要磨削加工,目前是采用两套夹具,通过两次装夹实现三角板101的底面及左侧面的磨削。先通过第一套夹具装夹,实现三角板101底面的磨削,再通过第二套夹具装夹,实现三角板101左侧面的磨削。The bottom surface and the left side of the triangular plate 101 of the air rudder need to be ground. At present, two sets of fixtures are used to realize the grinding of the bottom surface and the left side of the triangular plate 101 through two clampings. Grinding the bottom surface of the triangular plate 101 is achieved by first clamping the first set of fixtures, and then grinding the left side of the triangular plate 101 by clamping the second set of fixtures.
即为了磨削空气舵要用两套夹具,造成生产成本偏高。That is, two sets of fixtures are used for grinding the air rudder, resulting in high production costs.
发明内容Contents of the invention
本发明的目的是克服现有技术的不足,而提供一种空气舵磨削加工手动夹紧夹具,它只需一套夹具便可实现空气舵底面及左侧面磨削加工时的装夹定位,解决了现有的空气舵磨削加工需要用到两套夹具,生产成本偏高的问题。The purpose of the present invention is to overcome the deficiencies of the prior art, and provide a manual clamping fixture for air rudder grinding, which only needs one set of fixtures to realize the clamping and positioning of the air rudder bottom surface and left side grinding process , which solves the problem that the existing air rudder grinding process needs to use two sets of fixtures and the production cost is relatively high.
本发明的技术方案是:空气舵磨削加工手动夹紧夹具,包括底板、主板、中间板、锁止套筒、入口套、拉紧组件;The technical solution of the present invention is: the air rudder grinding and processing manual clamping fixture, including the bottom plate, the main board, the middle plate, the locking sleeve, the inlet sleeve, and the tensioning assembly;
主板竖直固接在底板上端,其上设有供入口套装入的安装孔,安装孔贯通主板的两端面;The main board is vertically fixed on the top of the bottom plate, and there are mounting holes for the inlet sleeve to be inserted on it, and the mounting holes penetrate the two ends of the main board;
中间板平行于主板,并与主板相对固定,其上设有方孔,所述方孔与空气舵四方块外形相适应;The middle plate is parallel to the main board and relatively fixed with the main board, and is provided with a square hole on it, and the square hole is adapted to the four-square shape of the air rudder;
入口套内孔为锥形孔并与空气舵锥台的锥度相适应,入口套安装在主板的安装孔中并与主板固接,其一端伸入到主板与中间板之间的区间内;The inner hole of the inlet sleeve is a tapered hole and adapts to the taper of the air rudder cone. The inlet sleeve is installed in the mounting hole of the main board and fixedly connected with the main board, and one end of it extends into the interval between the main board and the middle board;
锁止套筒的外壁上设有环形槽,环形槽内设有多个翘拨孔;锁止套筒的内孔为阶梯孔,阶梯孔一段为螺纹孔段,另一段为光孔段,螺纹孔段可与空气舵螺纹杆的外螺纹相配合;锁止套筒位于主板与中间板之间的区间内,并通过其内孔中的光孔段活动套装在入口套的外壁上,其内孔与入口套的内孔连通并正对中间板的方孔;There is an annular groove on the outer wall of the locking sleeve, and a plurality of warping holes are arranged in the annular groove; the inner hole of the locking sleeve is a stepped hole, and one section of the stepped hole is a threaded hole section, and the other section is a smooth hole section. The hole section can match the external thread of the air rudder threaded rod; the locking sleeve is located in the interval between the main board and the middle plate, and is movably fitted on the outer wall of the inlet sleeve through the light hole section in the inner hole. The hole communicates with the inner hole of the inlet sleeve and faces the square hole of the middle plate;
拉紧组件安装在中间板上并与锁止套筒关联,其可拉动锁止套筒向中间板移动,并使锁止套筒与中间板在彼此相对距离最近时保持相对固定。The tensioning component is installed on the middle plate and is associated with the locking sleeve, which can pull the locking sleeve to move toward the middle plate, and keep the locking sleeve and the middle plate relatively fixed when the relative distance is closest to each other.
本发明进一步的技术方案是:中间板上设有拉杆孔;拉紧组件包括活动板、气缸及L形拉杆;L形拉杆一端伸入锁止套筒的环形槽内,另一端杆体穿过中间板上的拉杆孔后固接在活动板上,L形拉杆的数量不少于二根,其与锁止套筒的接触点呈环形均布在环形槽上;气缸固定安装在中间板上,其活塞杆与活动板固定连接。The further technical solution of the present invention is: a tie rod hole is provided on the middle plate; the tension assembly includes a movable plate, a cylinder and an L-shaped tie rod; one end of the L-shaped tie rod extends into the annular groove of the locking sleeve, and the other end of the rod body passes through the middle The tie rod holes on the plate are fixed on the movable plate, and the number of L-shaped tie rods is not less than two, and their contact points with the locking sleeve are evenly distributed on the annular groove in a ring shape; the cylinder is fixedly installed on the middle plate, Its piston rod is fixedly connected with the movable plate.
本发明再进一步的技术方案是:锁止套筒上的翘拨孔的数量为六个,六个翘拨孔以锁止套筒的中心为中心,呈环形均布在环形槽的底部,翘拨孔的轴心线垂直于锁止套筒内孔的轴心线。A further technical solution of the present invention is: the number of warping holes on the locking sleeve is six, and the six warping holes center on the center of the locking sleeve and are evenly distributed in the bottom of the annular groove in a ring shape. The axis line of the dial hole is perpendicular to the axis line of the inner hole of the locking sleeve.
本发明更进一步的技术方案是:底板与主板之间设有加强筋板,加强筋板一侧与底板固接,另一侧与主板固接。A further technical solution of the present invention is: a rib plate is provided between the base plate and the main plate, one side of the rib plate is fixedly connected to the base plate, and the other side is fixedly connected to the main plate.
本发明更进一步的技术方案是:中间板的方孔在四角处设有弧形避让槽,弧形避让槽向方孔外侧延伸。A further technical solution of the present invention is: the square hole of the middle plate is provided with arc-shaped escape grooves at the four corners, and the arc-shaped escape grooves extend to the outside of the square hole.
本发明与现有技术相比具有如下优点:Compared with the prior art, the present invention has the following advantages:
本发明只需一套夹具便可实现空气舵磨削加工时的装夹定位,解决了现有的空气舵磨削加工夹具成本偏高的问题。The invention only needs one set of fixtures to realize the clamping and positioning during the air rudder grinding process, and solves the problem of relatively high cost of the existing air rudder grinding process fixtures.
以下结合图和实施例对本发明作进一步描述。Below in conjunction with figure and embodiment the present invention will be further described.
附图说明Description of drawings
图1为本发明的结构示意图;Fig. 1 is a structural representation of the present invention;
图2为本发明的爆炸图;Fig. 2 is an explosion diagram of the present invention;
图3为锁止套筒的立体结构示意图;Fig. 3 is a three-dimensional structural schematic diagram of a locking sleeve;
图4中间板的立体结构示意图;The schematic diagram of the three-dimensional structure of the middle plate of Fig. 4;
图5为中间板在另一视角下的立体结构示意图;5 is a schematic diagram of the three-dimensional structure of the middle plate under another viewing angle;
图6为本发明装夹空气舵时的状态示意图;Fig. 6 is a schematic diagram of the state when the air rudder is clamped according to the present invention;
图7为空气舵的立体结构图。Fig. 7 is a three-dimensional structure diagram of the air rudder.
具体实施方式detailed description
实施例1:Example 1:
如图1-4所示,空气舵磨削加工手动夹紧夹具,包括主板1、底板2、中间板3、锁止套筒5、入口套4及拉紧组件。As shown in Figure 1-4, the manual clamping fixture for air rudder grinding includes main board 1, bottom board 2, middle board 3, locking sleeve 5, inlet sleeve 4 and tensioning components.
主板1竖直焊接固定在底板2上端,其上设有供入口套装入的安装孔11,安装孔11贯通主板1的两端面。The main board 1 is vertically welded and fixed on the upper end of the base plate 2, and is provided with a mounting hole 11 for the inlet sleeve to be inserted, and the mounting hole 11 runs through both ends of the main board 1.
中间板3平行于主板1,并在四角处通过螺栓与主板1相对固定,中间板3上设有方孔31和拉杆孔32,所述方孔31与空气舵的四方块104外形相适应。The middle plate 3 is parallel to the main board 1, and is relatively fixed with the main board 1 by bolts at the four corners. The middle plate 3 is provided with a square hole 31 and a tie rod hole 32. The square hole 31 is adapted to the shape of the square 104 of the air rudder.
入口套4内孔为锥形孔并与空气舵的锥台102的锥度相适应,入口套4安装在主板1的安装孔11中并通过螺栓与主板1固接,其一端伸入到主板1与中间板3之间的区间内。具体地说,入口套4一端设有径向伸出的凸台41,凸台41上设有螺栓孔,主板1的安装孔11中设有台阶面111,台阶面111上设有与凸台41上的螺栓孔对应的螺纹孔。当入口套4装入主板1的安装孔11中,凸台41与台阶面111相抵而定位,再通过螺栓将入口套4与主板1固定连接。The inner hole of the inlet sleeve 4 is a tapered hole and is adapted to the taper of the cone 102 of the air rudder. The inlet sleeve 4 is installed in the mounting hole 11 of the main board 1 and is fixedly connected to the main board 1 by bolts, and one end thereof extends into the main board 1 and the middle plate 3 in the interval. Specifically, one end of the inlet sleeve 4 is provided with a radially protruding boss 41, and the boss 41 is provided with a bolt hole, and the mounting hole 11 of the main board 1 is provided with a stepped surface 111, and the stepped surface 111 is provided with a boss 41. The threaded holes corresponding to the bolt holes on the 41. When the inlet sleeve 4 is installed in the mounting hole 11 of the main board 1, the boss 41 is positioned against the step surface 111, and then the inlet sleeve 4 is fixedly connected with the main board 1 by bolts.
锁止套筒5的外壁上设有环形槽51,环形槽51内设有多个翘拨孔511。锁止套筒5的内孔为阶梯孔,阶梯孔一段为螺纹孔段521,另一段为光孔段522,螺纹孔段521可与空气舵的螺纹杆103上的外螺纹相配合。锁止套筒5位于主板1与中间板3之间的区间内,并通过其内孔中的光孔段522活动套装在入口套4的外壁上,其内孔与入口套4的内孔连通并正对中间板3的方孔31。An annular groove 51 is arranged on the outer wall of the locking sleeve 5 , and a plurality of warping holes 511 are arranged in the annular groove 51 . The inner hole of the locking sleeve 5 is a stepped hole, one section of the stepped hole is a threaded hole section 521, and the other section is a light hole section 522, and the threaded hole section 521 can cooperate with the external thread on the threaded rod 103 of the air rudder. The locking sleeve 5 is located in the interval between the main board 1 and the middle board 3, and is movably fitted on the outer wall of the inlet sleeve 4 through the light hole section 522 in its inner hole, and its inner hole communicates with the inner hole of the inlet sleeve 4 And facing the square hole 31 of the middle plate 3.
拉紧组件安装在中间板3上并与锁止套筒5关联,其可拉动锁止套筒5向中间板3移动,并使锁止套筒5与中间板3在彼此相对距离最近时保持相对固定。拉紧组件包括活动板6、气缸7及L形拉杆8。L形拉杆8一端伸入锁止套筒5的环形槽51内,另一端穿过中间板3的拉杆孔32后固接在活动板6上,L形拉杆8的数量有两根,其与锁止套筒5的接触点呈环形均布在环形槽51上。气缸7固定安装在中间板3上,其活塞杆71与活动板6固定连接。The tensioning assembly is installed on the middle plate 3 and is associated with the locking sleeve 5, which can pull the locking sleeve 5 to move toward the middle plate 3, and keep the locking sleeve 5 and the middle plate 3 when they are closest to each other. relatively fixed. The tensioning assembly includes a movable plate 6, a cylinder 7 and an L-shaped tie rod 8. One end of the L-shaped tie rod 8 extends into the annular groove 51 of the locking sleeve 5, and the other end passes through the tie rod hole 32 of the middle plate 3 and is fixedly connected to the movable plate 6. There are two L-shaped tie rods 8, which are the same as The contact points of the locking sleeve 5 are evenly distributed on the annular groove 51 in an annular shape. The cylinder 7 is fixedly mounted on the middle plate 3 , and its piston rod 71 is fixedly connected with the movable plate 6 .
优选,锁止套筒5上的翘拨孔511的数量为六个,六个翘拨孔511沿锁止套筒5的中心呈环形均布在环形槽51的底部,翘拨孔511的轴心线垂直于锁止套筒5内孔的轴心线。Preferably, the number of warping holes 511 on the locking sleeve 5 is six, and the six warping holes 511 are evenly distributed in the bottom of the annular groove 51 in a ring along the center of the locking sleeve 5, and the axis of the warping holes 511 The center line is perpendicular to the axis line of the inner hole of the locking sleeve 5 .
优选,底板2与主板1之间设有加强筋板9,加强筋板9一侧与底板2固接,另一侧与主板1固接。Preferably, a rib plate 9 is provided between the bottom plate 2 and the main board 1 , one side of the rib plate 9 is fixedly connected to the bottom plate 2 , and the other side is fixedly connected to the main board 1 .
优选,中间板3的方孔31在四角处设有弧形避让槽311,弧形避让槽311向方孔31外侧延伸。Preferably, the square hole 31 of the middle plate 3 is provided with arc-shaped escape grooves 311 at four corners, and the arc-shaped escape grooves 311 extend to the outside of the square hole 31 .
简述本发明的使用:将底板2平放于机床工作台面,用百分表找正,然后将底板2紧固于机床台面。将空气舵水平装入夹具,通过入口套4的内孔和中间板3的方孔31实现空气舵的定位(如图6所示),再将内六方扳手插入锁止套筒5的翘拨孔511中,人工转动锁止套筒5,使其与空气舵的螺纹杆103旋配并拧紧。之后启动气缸7,气缸的活塞杆71伸出,从而推动活动板6移动,活动板6与L形拉杆8连接从而带动L形拉杆8移动,L形拉杆8拉动锁止套筒5向靠近中间板3的方向移动,完成对空气舵的压紧,最后对刀加工,磨削空气舵的三角板101的底面及左侧面。Briefly describe the use of the present invention: place the bottom plate 2 flat on the machine tool table, align it with a dial indicator, and then fasten the bottom plate 2 to the machine tool table. Put the air rudder horizontally into the fixture, realize the positioning of the air rudder through the inner hole of the inlet sleeve 4 and the square hole 31 of the middle plate 3 (as shown in Figure 6), and then insert the hexagonal wrench into the locking sleeve 5. In the hole 511, manually rotate the locking sleeve 5 to screw it with the threaded rod 103 of the air rudder and tighten it. Then start the cylinder 7, the piston rod 71 of the cylinder stretches out, thereby pushing the movable plate 6 to move, the movable plate 6 is connected with the L-shaped pull rod 8 to drive the L-shaped pull rod 8 to move, and the L-shaped pull rod 8 pulls the locking sleeve 5 toward the middle The direction of plate 3 is moved to complete the compression of the air rudder, and finally the knife is processed to grind the bottom surface and the left side of the triangular plate 101 of the air rudder.
Claims (6)
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| CN201710546750.2A CN107186623B (en) | 2017-07-06 | 2017-07-06 | Air Rudder Grinding Manual Clamping Fixture |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN107717712A (en) * | 2017-10-18 | 2018-02-23 | 深圳市华盛源机电有限公司 | Sleeve part inwall honing tool |
| CN114011665A (en) * | 2021-11-09 | 2022-02-08 | 山西钢科碳材料有限公司 | Clamp for air rudder |
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| EP0007887A1 (en) * | 1978-07-31 | 1980-02-06 | TORNOS S.A. Fabrique de machines Moutier | Pulled double-conical collet |
| US5788249A (en) * | 1995-05-26 | 1998-08-04 | Tagami; Tetsuro | Cutting tool chuck for chucking cutting tool |
| US6238152B1 (en) * | 1999-04-13 | 2001-05-29 | Fanuc Ltd. | Tool clamping mechanism and pull stud |
| CN2629886Y (en) * | 2003-06-18 | 2004-08-04 | 河南石油勘探局南阳石油机械厂 | Bevel gear chucking device |
| CN203304954U (en) * | 2013-05-29 | 2013-11-27 | 重庆旭源摩托车工业有限公司 | Drilling pneumatic tool |
| CN103394935A (en) * | 2013-08-09 | 2013-11-20 | 合肥长源液压股份有限公司 | Pneumatic expansion type clamp |
| CN203875613U (en) * | 2013-12-27 | 2014-10-15 | 大连瑞谷科技有限公司 | Ultra-light thin-walled copper cage and special-purpose fixture thereof for pocket hole |
| CN205888120U (en) * | 2016-07-20 | 2017-01-18 | 江苏腾旋科技股份有限公司 | Formula that rises outward anchor clamps |
| CN207206167U (en) * | 2017-07-06 | 2018-04-10 | 南华大学 | Airvane grinding hand-operated clamping fixture |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107717712A (en) * | 2017-10-18 | 2018-02-23 | 深圳市华盛源机电有限公司 | Sleeve part inwall honing tool |
| CN114011665A (en) * | 2021-11-09 | 2022-02-08 | 山西钢科碳材料有限公司 | Clamp for air rudder |
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| CN107186623B (en) | 2023-04-14 |
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Application publication date: 20170922 Assignee: Hengyang Wentai Electronic Technology Co.,Ltd. Assignor: University OF SOUTH CHINA Contract record no.: X2024980033162 Denomination of invention: Manual clamping fixture for air rudder grinding processing Granted publication date: 20230414 License type: Common License Record date: 20241209 |
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