CN103203699A - Telescopic fine-adjustment positioning support mechanism - Google Patents
Telescopic fine-adjustment positioning support mechanism Download PDFInfo
- Publication number
- CN103203699A CN103203699A CN2013101014007A CN201310101400A CN103203699A CN 103203699 A CN103203699 A CN 103203699A CN 2013101014007 A CN2013101014007 A CN 2013101014007A CN 201310101400 A CN201310101400 A CN 201310101400A CN 103203699 A CN103203699 A CN 103203699A
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- China
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- support
- termination
- latch
- support bar
- seat board
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Abstract
The invention discloses a telescopic fine-adjustment positioning support mechanism which comprises a support base plate. A support tube is fixedly connected on the support base plate, one end of a support rod is inserted into the support tube, a guide sleeve is arranged between the support rod and the support tube, at least two insertion holes are arranged on one side face of the support tube, an axial slot hole is arranged on the other side face of the support tube, a radial bolt is arranged between the insertion end of the support rod and the support tube, one end of the bolt is matched with the insertion holes, the other end of the bolt extends out of the slot hole and connected with a handle, an outer tip of the support rod is connected with a support head, and a clamping ejecting tightening mechanism is arranged on the support base plate. The telescopic fine-adjustment positioning support mechanism is simple in integral structure, convenient to adjust, and stable and firm when used for positioning and supporting parts.
Description
Technical field
The present invention relates to a kind of telescopic fine setting positioning supports mechanism, be mainly used in the part processing industry and relatively large part is supported realize the processing fitting operation.
Background technology
Some heavy parts all is to adopt relevant clamping mechanism that part is carried out clamping in the processing install operation process at present, sometimes also needing to have corresponding support component to carry out assist location supports, assist location all is to select for use the suitable frock of trying one's best to make up when supporting temporarily, very trouble wastes time and energy.
Summary of the invention
The purpose of this invention is to provide a kind of simple in structure, easy to adjust, stablize firm telescopic fine setting positioning supports mechanism, overcome the deficiencies in the prior art.
Telescopic fine setting positioning supports of the present invention mechanism, comprise the support seat board, be fixedly connected with the support body at the support seat board, one end of support bar is inserted into and supports in the body, between support bar and support body, be provided with guide pin bushing, a side of supporting body is provided with at least two jacks, the another side of supporting body is provided with axial long hole, be provided with the latch that radially arranges between the insertion end of support bar and the support body, one end and the jack of latch match, the other end of latch to slotted hole stretches out and takes over handle, and the external end head of support bar connects supporting member, and the support seat board is provided with the clamping jacking mechanism.
Be positioned at the outside, termination of support bar and the outside of latch in the described support body and be set with cushion collar; Described clamping jacking mechanism is to be provided with nut sleeve in support seat board end, and screw mandrel one termination that matches with nut sleeve has spanner, and the other end is connected to and leans the termination, the termination of supporting body be provided with end plate and with lean the termination and be oppositely arranged.
Telescopic fine setting positioning supports of the present invention mechanism, rotate spanner during use and screw mandrel is driven lean that move the termination and be clamped on the corresponding frame relatively with end plate, the pulling handle makes the termination of latch shift out from jack, this moment support bar, latch, cushion collar, handle can be with respect to the stay pipe axon to movement, handle slides in slotted hole, the supporting member of support bar termination is pressed against on the part, latch is inserted in the corresponding jack lock then.Played the positioning supports effect to part, overall structure is simple, and is easy to adjust, firmly stable.
Description of drawings
Fig. 1 is the structural representation of the specific embodiment of the invention;
Fig. 2 is the cross-sectional schematic along support bar and support body longitudinal centre line shown in Figure 1.
The specific embodiment
As shown in Figure 1, 2: 1 is the support seat board, is fixedly connected with at support seat board 1 and supports body 2, and an end of support bar 6 is inserted into and supports in the body 2, is provided with guide pin bushing 5 between support bar 6 and support body 2, and guide pin bushing 5 fixedly is embedded in and supports inboard, body 2 termination.A side of supporting body 2 is provided with at least two jacks 10, the another side of supporting body 2 is provided with axial long hole 9, be provided with the latch 4 that radially arranges between the insertion end of support bar 6 and the support body 2, one end and the jack 10 of latch 4 match, and the other end of latch 4 to slotted hole 9 stretches out and fixedly connected handle 8.The outside of supporting the outside, termination that is positioned at support bar 6 in the body 2 and latch 4 is set with the cushion collar 3 of colloidal materials.The external end head of support bar 6 connects supporting member 7.Support seat board 1 is provided with the clamping jacking mechanism, the clamping jacking mechanism is to be provided with nut sleeve 13 in support seat board 1 end, screw mandrel 14 1 terminations that match with nut sleeve 13 have spanner 12 and are furnished with locking nut 16, the other end is connected to and leans termination 15, the termination of supporting body 2 fixedly have end plate 11 and with lean termination 15 and be oppositely arranged.
Telescopic fine setting positioning supports of the present invention mechanism, rotate spanner 12 during use and screw mandrel 14 is driven lean that move termination 15 and be clamped on the corresponding frame relatively with end plate 11, pulling handle 8 makes the termination of latch 4 shift out from jack 10, support bar 6, latch 4, cushion collar 3, handle 8 can move axially with respect to supporting body 2 at this moment, handle 8 slides in slotted hole, the supporting member 7 of support bar 6 terminations is pressed against on the part, then latch 4 is inserted locking in the corresponding jack 10.Played the positioning supports effect to part, overall structure is simple, and is easy to adjust, firmly stable.
Claims (2)
1. telescopic fine setting positioning supports mechanism, it is characterized in that: comprise support seat board (1), be fixedly connected with support body (2) at support seat board (1), one end of support bar (6) is inserted into and supports in the body (2), between support bar (6) and support body (2), be provided with guide pin bushing (5), a side of supporting body (2) is provided with at least two jacks (10), the another side of supporting body (2) is provided with axial long hole (9), be provided with the latch (4) that radially arranges between the insertion end of support bar (6) and the support body (2), one end of latch (4) and jack (10) match, the other end of latch (4) to slotted hole (9) stretches out and takes over handle (8), the external end head of support bar (6) connects supporting member (7), and support seat board (1) is provided with the clamping jacking mechanism.
2. telescopic fine setting positioning supports according to claim 1 mechanism is characterized in that: be positioned at the outside, termination of support bar (6) and the outside of latch (4) in the described support body (2) and be set with cushion collar (3); Described clamping jacking mechanism is to be provided with nut sleeve (13) in support seat board (1) end, screw mandrel (14) one terminations that match with nut sleeve (13) have spanner (12), the other end is connected to and leans termination (15), the termination of supporting body (2) be provided with end plate (11) and with lean termination (15) and be oppositely arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101014007A CN103203699A (en) | 2013-03-27 | 2013-03-27 | Telescopic fine-adjustment positioning support mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101014007A CN103203699A (en) | 2013-03-27 | 2013-03-27 | Telescopic fine-adjustment positioning support mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103203699A true CN103203699A (en) | 2013-07-17 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013101014007A Pending CN103203699A (en) | 2013-03-27 | 2013-03-27 | Telescopic fine-adjustment positioning support mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103203699A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104162888A (en) * | 2014-08-01 | 2014-11-26 | 大连四达高技术发展有限公司 | Six-freedom-degree floating mechanism |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2663090Y (en) * | 2003-10-08 | 2004-12-15 | 上海新月工具有限公司 | Double end G-shape clip |
| CN101100050A (en) * | 2007-07-25 | 2008-01-09 | 长春轨道客车股份有限公司 | Bidirectional synchronous telescopic positioning method and device |
| CN201329514Y (en) * | 2008-11-07 | 2009-10-21 | 寿震森 | Slight-adjustment positioning seat |
| KR100922588B1 (en) * | 2003-03-11 | 2009-10-21 | 한국항공우주산업 주식회사 | Apparatus supporting a part for machining |
| CN201632951U (en) * | 2010-03-09 | 2010-11-17 | 上海北特金属制品有限公司 | Cylinder fine-tuning and precise-positioning device |
| CN201900424U (en) * | 2010-11-24 | 2011-07-20 | 理想能源设备有限公司 | Load adjusting and positioning device |
| CN201960481U (en) * | 2010-12-17 | 2011-09-07 | 上海宇航系统工程研究所 | Regulation and positioning device for mobile carrier |
| CN202609094U (en) * | 2012-03-22 | 2012-12-19 | 沈阳飞机工业（集团）有限公司 | Adjustable support mechanism for assembling tools |
| CN203156621U (en) * | 2013-03-27 | 2013-08-28 | 大连四达高技术发展有限公司 | Telescopic fine adjustment locating and supporting mechanism |
-
2013
- 2013-03-27 CN CN2013101014007A patent/CN103203699A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100922588B1 (en) * | 2003-03-11 | 2009-10-21 | 한국항공우주산업 주식회사 | Apparatus supporting a part for machining |
| CN2663090Y (en) * | 2003-10-08 | 2004-12-15 | 上海新月工具有限公司 | Double end G-shape clip |
| CN101100050A (en) * | 2007-07-25 | 2008-01-09 | 长春轨道客车股份有限公司 | Bidirectional synchronous telescopic positioning method and device |
| CN201329514Y (en) * | 2008-11-07 | 2009-10-21 | 寿震森 | Slight-adjustment positioning seat |
| CN201632951U (en) * | 2010-03-09 | 2010-11-17 | 上海北特金属制品有限公司 | Cylinder fine-tuning and precise-positioning device |
| CN201900424U (en) * | 2010-11-24 | 2011-07-20 | 理想能源设备有限公司 | Load adjusting and positioning device |
| CN201960481U (en) * | 2010-12-17 | 2011-09-07 | 上海宇航系统工程研究所 | Regulation and positioning device for mobile carrier |
| CN202609094U (en) * | 2012-03-22 | 2012-12-19 | 沈阳飞机工业（集团）有限公司 | Adjustable support mechanism for assembling tools |
| CN203156621U (en) * | 2013-03-27 | 2013-08-28 | 大连四达高技术发展有限公司 | Telescopic fine adjustment locating and supporting mechanism |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104162888A (en) * | 2014-08-01 | 2014-11-26 | 大连四达高技术发展有限公司 | Six-freedom-degree floating mechanism |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130717 |