CN101733672A - Flexible positioning pin - Google Patents
Flexible positioning pin Download PDFInfo
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- CN101733672A CN101733672A CN201010102069A CN201010102069A CN101733672A CN 101733672 A CN101733672 A CN 101733672A CN 201010102069 A CN201010102069 A CN 201010102069A CN 201010102069 A CN201010102069 A CN 201010102069A CN 101733672 A CN101733672 A CN 101733672A
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- workbench
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- positioning pin
- shop bolt
- movable block
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Abstract
The invention relates to a flexible positioning pin which comprises two one-dimensional motion working platforms, a rotary working platform and a positioning pin device, wherein each one-dimensional motion working platform comprises a vertical motion working platform and a horizontal motion working platform; the positioning pin device comprises a base (4) and a positioning pin (3); the positioning pin (3) is connected with the base (4) by interference fit; and the rotary working platform comprises a support disk (2), a rotary disk (6), an adjusting screw (7) and a locking screw (5). The invention can be used for a flexible clamp for processing aircraft skin tools and positioning a workpiece.
Description
Technical field
The present invention relates to flexible positioning pin, be specifically related to the flexible positioning pin on a kind of clamp body of aircraft skin use for machining parts.
Technical background
Covering is the strength member that guarantees the aircraft aerodynamics performance, and the aircraft skin stochastic pattern is different with covering residing position on airframe and present different shapes and specification.Because covering specification, shape, change in size are many, the clamping of workpiece, to adjust shared ratio very high, influenced the raising of working (machining) efficiency.If according to traditional clamping means, will design numerous anchor clamps, and have problems such as bad adaptability, cost increase and management difficulty are big, must adopt flexible fixture to adapt to the requirement of different workpieces, and aircraft skin class part is because size and curvature of curved surface different, position of dowel hole and size are also fixing above it, how to set up accurate localization concerns it is the key that guarantees crudy between workpiece and the anchor clamps.
At present, the alignment pin on the aircraft skin class part clamp all adopts fixing mode, can't adjust its position and angle, causes a kind of anchor clamps can only process one or more workpiece of the same type, causes very big waste.Therefore, a kind of can be according to different, the dowel hole position of surface of the work shape and size and size different, can freely adjust the position and the angle of alignment pin, make that the dowel hole axis overlaps fully on shop bolt and the workpiece, the position can be current active demand to aircraft skin class part processing location by exactly determined flexible positioning pin between workpiece and the clamp body, to guarantee the crudy of workpiece.
Summary of the invention
The purpose of this invention is to provide the flexible positioning pin on a kind of clamp body that is used for the aircraft skin use for machining parts.Move both vertically workbench and horizontal movement motion workbench of dowel device of the present invention, rotary table, one formed, have easy to adjust, precision is high, characteristics such as widely applicable.Among the present invention, the dowel device of being made up of pedestal 4 and shop bolt 3 is fixed on the workbench that moves both vertically by screw, and shop bolt 3 and pedestal 4 are connected by interference fit, can change the size of shop bolt 3 according to the size of workpiece dowel hole; The rotary table of being made up of supporting disk 2, rolling disc 6, set screw 7 and lock screw 5 is fixed on the workbench that moves both vertically by contiguous block 8, by turning set screw 7, can drive rolling disc 6 and fixed thereon 's dowel device rotation, thus adjustable angle of adjusting a pin 3.After having adjusted, can rolling disc 6 be fixed on the supporting disk 2 by lock screw 5; By back-up block 1, movable block 9, micrometer 10, and the workbench that moves both vertically formed of the lock-screw of side be fixed on the horizontal movement workbench by contiguous block 11, by turning micrometer 10, can drive movable block 9 and move in vertical direction, thereby adjust shop bolt 3 position in vertical direction with rotary table.After having adjusted, can movable block 9 be fixed on the back-up block 1 by lock screw; The horizontal movement workbench of being made up of back-up block 14, movable block 12, micrometer 15 and lock-screw 13 can be connected and fixed by relevant apparatus and clamp body, by turning micrometer 15, can drive movable block 12 and move in the horizontal direction, thereby adjust shop bolt 3 position in the horizontal direction with the workbench that moves both vertically.After having adjusted, can movable block 12 be fixed on the back-up block 14 by lock screw 13.Shop bolt 3 can be demarcated by laser tracker in advance with the initial position of clamp body, difference according to different workpieces dowel hole position, can make the axis direction and the dead in line of workpiece dowel hole of shop bolt 3 by the motion of two one dimension workbench and rotary table.The position that shop bolt 3 moves and the angle of rotation can be obtained by the scale on two one dimension workbench and the rotary table, can calculate the particular location of shop bolt 3 in clamp body according to the software that weaves again, this flexible positioning pin generally has 2~3 to be used, thereby can accurately determine the position of workpiece in clamp body.By the present invention have easy to adjust, precision is high, characteristics such as widely applicable, the location when being particularly suitable for the aircraft skin class part processing of different sizes and curved surface, the definite position of setting up between workpiece and the clamp body concerns.
Description of drawings
Fig. 1 flexible positioning pin graphics of the present invention;
Fig. 2 flexible positioning pin front view of the present invention;
Fig. 3 flexible positioning pin left view of the present invention;
Fig. 4 flexible positioning pin vertical view of the present invention.
Specific implementation method
Specific implementation method of the present invention is: dowel device is made up of pedestal 4 and shop bolt 3, shop bolt 3 links together by interference fit and pedestal 4, shop bolt 3 can be changed according to the size of the dowel hole of workpiece, and it can eject shop bolt 3 by the screw of 4 li of pedestals when changing from pedestal 4.Rotary table is made up of supporting disk 2, rolling disc 6, set screw 7 and lock screw 5.By turning set screw 7, can drive rolling disc 6 and fixed thereon 's dowel device rotation, thus adjustable angle of adjusting a pin 3.After having adjusted, can rolling disc 6 be fixed on the supporting disk 2 by lock screw 5.Move both vertically workbench by back-up block 1, movable block 9, micrometer 10, and the lock-screw of side form.Rotary table is fixed together by the movable block 9 of contiguous block 8 with the workbench that moves both vertically.By turning micrometer 10, can drive movable block 9 and move in vertical direction, thereby adjust shop bolt 3 position in vertical direction with rotary table.After having adjusted, can movable block 9 be fixed on the back-up block 1 by lock screw.The horizontal movement workbench is made up of back-up block 14, movable block 12, micrometer 15 and lock-screw 13.The workbench that moves both vertically is fixed together by the movable block 12 of contiguous block 8 with the horizontal movement workbench.By turning micrometer 15, can drive movable block 12 and move in the horizontal direction, thereby adjust shop bolt 3 position in the horizontal direction with the workbench that moves both vertically.After having adjusted, can movable block 12 be fixed on the back-up block 14 by lock screw 13.Back-up block 14 can be connected and fixed by relevant apparatus and clamp body.According to the shape and the size of workpiece to be machined, can select 2~3 these flexible positioning pins to be used, accurately to determine the position relation between workpiece and the anchor clamps.
Claims (5)
1. flexible positioning pin, by two motion in one dimension workbench, rotary table and dowel device are formed, it is characterized in that: described motion in one dimension workbench comprises move both vertically a workbench and a horizontal movement workbench, described dowel device is made up of pedestal (4) and shop bolt (3), shop bolt (3) links together by interference fit and pedestal (4), shop bolt (3) is along with its locus and angle are adjusted in the motion of workbench, overlap with workpiece pin hole axis direction with the axis direction that guarantees shop bolt (3), described rotary table is by supporting disk (2), rolling disc (6), set screw (7) and lock screw (5) are formed, by turning set screw (7), drive rolling disc (6) and fixed thereon 's dowel device rotation, thus the angle of an adjustable pin (3) of adjusting.
2. flexible positioning pin as claimed in claim 1 is characterized in that: described shop bolt (3) is changed according to the size of the dowel hole of workpiece, and the screw by pedestal (4) lining when it is changed ejects shop bolt (3) from pedestal (4).
3. flexible positioning pin as claimed in claim 1, it is characterized in that: described move both vertically workbench by back-up block (1), movable block (9), micrometer (10), and the lock-screw of side form, rotary table is fixed together by the movable block (9) of contiguous block (8) with the workbench that moves both vertically, by turning micrometer (10), driving movable block (9) moves in vertical direction with rotary table, thereby adjust shop bolt (3) position in vertical direction, after having adjusted, movable block (9) is fixed on the back-up block (1) by lock screw.
4. flexible positioning pin as claimed in claim 1, it is characterized in that: described horizontal movement workbench is by back-up block (14), movable block (12), micrometer (15) and lock-screw (13) are formed, the workbench that moves both vertically is fixed together by the movable block (12) of contiguous block (8) with the horizontal movement workbench, by turning micrometer (15), driving movable block (12) moves in the horizontal direction with the workbench that moves both vertically, thereby adjust shop bolt (3) position in the horizontal direction, after having adjusted, by lock screw (13) movable block (12) is fixed on the back-up block (14), back-up block (14) is connected and fixed by relevant apparatus and clamp body.
5. flexible positioning pin as claimed in claim 1 is characterized in that: according to the shape and the size of workpiece to be machined, select 2~3 described flexible positioning pins to be used, accurately to determine the position relation between workpiece and the anchor clamps.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201010102069A CN101733672A (en) | 2010-01-28 | 2010-01-28 | Flexible positioning pin |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201010102069A CN101733672A (en) | 2010-01-28 | 2010-01-28 | Flexible positioning pin |
Publications (1)
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CN101733672A true CN101733672A (en) | 2010-06-16 |
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Family Applications (1)
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CN201010102069A Pending CN101733672A (en) | 2010-01-28 | 2010-01-28 | Flexible positioning pin |
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Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103418971A (en) * | 2013-08-23 | 2013-12-04 | 芜湖奕辰模具科技有限公司 | Easy-to-adjust positioning bin |
CN103464946A (en) * | 2013-08-23 | 2013-12-25 | 芜湖奕辰模具科技有限公司 | Spirally-adjusted type positioning pin |
CN103624609A (en) * | 2013-11-06 | 2014-03-12 | 大连机床(数控)股份有限公司 | Adjustable positioning pin mechanism |
CN103921041A (en) * | 2014-03-31 | 2014-07-16 | 大连奥托股份有限公司 | Floating pin mechanism |
CN104034221A (en) * | 2014-07-07 | 2014-09-10 | 南通大地电气有限公司 | Device for fixing micrometer to workbench |
CN104889912A (en) * | 2015-06-19 | 2015-09-09 | 江西洪都航空工业集团有限责任公司 | Flexible presser |
CN109551406A (en) * | 2019-01-21 | 2019-04-02 | 柳州沪信汽车科技有限公司 | Flexible positioning system |
CN109605290A (en) * | 2019-01-25 | 2019-04-12 | 江苏塔帝思智能科技有限公司 | A kind of flexibility positioning table |
CN113858081A (en) * | 2021-10-29 | 2021-12-31 | 中国航空制造技术研究院 | Array type multi-point flexible positioning tool capable of being split, moved and recombined and positioning method |
CN114161446A (en) * | 2021-12-17 | 2022-03-11 | 北京星航机电装备有限公司 | Titanium alloy weak-rigidity variable-curvature wing rudder skin gripping device and gripping method |
-
2010
- 2010-01-28 CN CN201010102069A patent/CN101733672A/en active Pending
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103418971A (en) * | 2013-08-23 | 2013-12-04 | 芜湖奕辰模具科技有限公司 | Easy-to-adjust positioning bin |
CN103464946A (en) * | 2013-08-23 | 2013-12-25 | 芜湖奕辰模具科技有限公司 | Spirally-adjusted type positioning pin |
CN103464946B (en) * | 2013-08-23 | 2015-12-23 | 芜湖奕辰模具科技有限公司 | A kind of rotary adjustment type alignment pin |
CN103418971B (en) * | 2013-08-23 | 2016-01-20 | 芜湖奕辰模具科技有限公司 | One easily regulates alignment pin |
CN103624609A (en) * | 2013-11-06 | 2014-03-12 | 大连机床(数控)股份有限公司 | Adjustable positioning pin mechanism |
CN103921041A (en) * | 2014-03-31 | 2014-07-16 | 大连奥托股份有限公司 | Floating pin mechanism |
CN104034221A (en) * | 2014-07-07 | 2014-09-10 | 南通大地电气有限公司 | Device for fixing micrometer to workbench |
CN104889912A (en) * | 2015-06-19 | 2015-09-09 | 江西洪都航空工业集团有限责任公司 | Flexible presser |
CN109551406A (en) * | 2019-01-21 | 2019-04-02 | 柳州沪信汽车科技有限公司 | Flexible positioning system |
CN109605290A (en) * | 2019-01-25 | 2019-04-12 | 江苏塔帝思智能科技有限公司 | A kind of flexibility positioning table |
CN113858081A (en) * | 2021-10-29 | 2021-12-31 | 中国航空制造技术研究院 | Array type multi-point flexible positioning tool capable of being split, moved and recombined and positioning method |
CN114161446A (en) * | 2021-12-17 | 2022-03-11 | 北京星航机电装备有限公司 | Titanium alloy weak-rigidity variable-curvature wing rudder skin gripping device and gripping method |
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Open date: 20100616 |