CN202716171U - Multi-degree-of-freedom adjusting device - Google Patents
Multi-degree-of-freedom adjusting device Download PDFInfo
- Publication number
- CN202716171U CN202716171U CN2012202629847U CN201220262984U CN202716171U CN 202716171 U CN202716171 U CN 202716171U CN 2012202629847 U CN2012202629847 U CN 2012202629847U CN 201220262984 U CN201220262984 U CN 201220262984U CN 202716171 U CN202716171 U CN 202716171U
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- bulb
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- adjusting device
- supporting
- slide unit
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Abstract
The utility model relates to a multi-degree-of-freedom adjusting device. XY motion sliding tables are respectively arranged at the both ends above a supporting table; the supporting table and the XY motion sliding tables are connected through a transverse hand wheel screw rod pair and a longitudinal hand wheel screw rod pair; two lifting threaded pairs are symmetrically arranged on the upper surface of the XY motion sliding table at one end, and supporting bulbs are connected above the threaded pairs; an XY motion limiting sleeve is arranged between the two lifting threaded pairs; a limiting bulb I is arranged inside the XY motion limiting sleeve; the two supporting bulbs and the limiting bulb I commonly support one end of a product supporting table; a ball socket supporting oil cylinder is arranged on the upper surface of the XY motion sliding table at the other end; a limiting bulb II is arranged inside the ball socket supporting oil cylinder; and the other end of the product supporting table is supported by the upper part of the limiting bulb II. The multi-degree-of-freedom adjusting device provided by the utility model not only is simple in structure, but also can be used for accurately being in butt joint with a large-size part in actual operation, so that the production efficiency can be effectively improved.
Description
Technical field
The utility model relates to a kind of multiple degrees of freedom adjusting device, is used for the frock of heavy parts assembling location.
Background technology
At home, dock for Large Aircraft Components, the airplane tail mating operation of hanging down particularly, because the product component volume is large, quality is large, the means such as very difficult employing lifting are finished, must adopt possess support function, multiple degrees of freedom regulatory function the mechanical device guarantee safely, stablize, coordinate and keep away except adding stress etc., and be fit to development and batch production.
Summary of the invention
The technical problems to be solved in the utility model provides a kind of multiple degrees of freedom adjusting device, and this device is not only simple in structure, and can accurately dock heavy parts in real work, effectively raises production efficiency.
For overcoming the above problems, concrete technical scheme of the present utility model is as follows: a kind of multiple degrees of freedom adjusting device, and two ends are respectively equipped with XY motion slide unit above brace table, and brace table is connected by two horizontal and vertical handwheel screw pairs with XY motion slide unit; The upper surface of at one end XY motion slide unit is arranged with two elevating screw thread pairs, and the top of screw thread pair connects supports bulb; Between two elevating screw thread pairs, be provided with XY sports limiting sleeve, be provided with spacing bulb in the XY sports limiting sleeve, two ends that support bulb and a common support product brace table of spacing bulb; Upper surface at other end XY motion slide unit is provided with the ball-and-socket support cylinder, also is provided with spacing bulb in the ball-and-socket support cylinder, the other end of the top support product brace table of spacing bulb.
This multiple degrees of freedom adjusting device adopts the structure that XY motion slide unit, elevating screw thread are secondary, support bulb or spacing bulb, thereby but guaranteed product free adjustment on the product brace table, fully guarantee the degree of accuracy of rigging position.
Description of drawings
Fig. 1 is the structural representation of multiple degrees of freedom adjusting device.
Fig. 2 is multiple degrees of freedom adjusting device application distribution figure.
The specific embodiment
As shown in Figure 1, a kind of multiple degrees of freedom adjusting device, two ends are respectively equipped with XY motion slide unit 2 above brace table 1, and brace table 1 is connected by two horizontal and vertical handwheel screw pairs 3 with XY motion slide unit 2, thereby make the displacement that product brace table 9 can be horizontal and vertical; The upper surface of at one end XY motion slide unit 2 is arranged with two elevating screw thread pairs 5, and elevating screw thread pair 5 can be carried out the fine adjustments of upper-lower position, and the top of screw thread pair 5 connects supports bulb 8; Between two elevating screw thread pairs 5, be provided with XY sports limiting sleeve 4, be provided with 7, two ends that support bulb 8 and spacing bulb 7 common support product brace tables 9 of spacing bulb in the XY sports limiting sleeve 4; Upper surface at other end XY motion slide unit 2 is provided with ball-and-socket support cylinder 6, also is provided with spacing bulb 7 in the ball-and-socket support cylinder 6, the other end of the top support product brace table 9 of spacing bulb.
As shown in Figure 2, this device top arranges the aircraft vertical fin, keep balance with support part, at first shake handwheel and move XY motion slide unit, carry out the adjusting of horizontal level by measurement, and then carrying out rising the up-down adjustment of valency screw thread pair, product is adjusted to theory or anticipation position the most at last, locks at last each motion.
Claims (1)
1. multiple degrees of freedom adjusting device is characterized in that: be respectively equipped with XY motion slide unit (2) at two ends, brace table (1) top, brace table (1) is connected by horizontal and vertical two handwheel screw pairs (3) with XY motion slide unit (2); The upper surface of at one end XY motion slide unit (2) is arranged with two elevating screw thread pairs (5), and the top of screw thread pair (5) connects supports bulb (8); Between two elevating screw thread pairs (5), be provided with XY sports limiting sleeve (4), be provided with spacing bulb (7) in the XY sports limiting sleeve (4), two ends that support bulb (8) and the common support product brace table (9) of a spacing bulb (7); Upper surface at other end XY motion slide unit (2) is provided with ball-and-socket support cylinder (6), also is provided with spacing bulb (7) in the ball-and-socket support cylinder (6), the other end of the top support product brace table (9) of spacing bulb.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012202629847U CN202716171U (en) | 2012-06-06 | 2012-06-06 | Multi-degree-of-freedom adjusting device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012202629847U CN202716171U (en) | 2012-06-06 | 2012-06-06 | Multi-degree-of-freedom adjusting device |
Publications (1)
Publication Number | Publication Date |
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CN202716171U true CN202716171U (en) | 2013-02-06 |
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN2012202629847U Expired - Fee Related CN202716171U (en) | 2012-06-06 | 2012-06-06 | Multi-degree-of-freedom adjusting device |
Country Status (1)
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CN (1) | CN202716171U (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103252764A (en) * | 2013-05-16 | 2013-08-21 | 浙江吉利汽车研究院有限公司杭州分公司 | Space docking platform |
CN105345492A (en) * | 2015-11-27 | 2016-02-24 | 沈阳飞机工业(集团)有限公司 | Rapid positioning mechanism and method for plane intersection point finish machining table |
CN107651615A (en) * | 2017-09-25 | 2018-02-02 | 东莞理工学院 | Bearing type liftable omnidirectional support method and support base |
CN108857328A (en) * | 2018-09-12 | 2018-11-23 | 东莞中子科学中心 | Long-range ball-and-socket automatic positioning equipment and method |
CN110202501A (en) * | 2019-06-03 | 2019-09-06 | 苏州久协精工制造有限公司 | A kind of clamping fixture easy to use |
CN111322908A (en) * | 2020-03-05 | 2020-06-23 | 北京中科宇航技术有限公司 | Intelligent docking vehicle |
-
2012
- 2012-06-06 CN CN2012202629847U patent/CN202716171U/en not_active Expired - Fee Related
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103252764A (en) * | 2013-05-16 | 2013-08-21 | 浙江吉利汽车研究院有限公司杭州分公司 | Space docking platform |
CN103252764B (en) * | 2013-05-16 | 2015-09-02 | 浙江吉利汽车研究院有限公司杭州分公司 | Space articulation platform |
CN105345492A (en) * | 2015-11-27 | 2016-02-24 | 沈阳飞机工业(集团)有限公司 | Rapid positioning mechanism and method for plane intersection point finish machining table |
CN107651615A (en) * | 2017-09-25 | 2018-02-02 | 东莞理工学院 | Bearing type liftable omnidirectional support method and support base |
CN108857328A (en) * | 2018-09-12 | 2018-11-23 | 东莞中子科学中心 | Long-range ball-and-socket automatic positioning equipment and method |
CN108857328B (en) * | 2018-09-12 | 2020-04-24 | 东莞中子科学中心 | Remote ball socket automatic positioning device and method for high-radiation area equipment |
CN110202501A (en) * | 2019-06-03 | 2019-09-06 | 苏州久协精工制造有限公司 | A kind of clamping fixture easy to use |
CN111322908A (en) * | 2020-03-05 | 2020-06-23 | 北京中科宇航技术有限公司 | Intelligent docking vehicle |
CN111322908B (en) * | 2020-03-05 | 2022-04-29 | 北京中科宇航技术有限公司 | Intelligent docking vehicle |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130206 Termination date: 20150606 |
|
EXPY | Termination of patent right or utility model |