CN102501064A - Wire drawing positioning device for air rudder - Google Patents
Wire drawing positioning device for air rudder Download PDFInfo
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- CN102501064A CN102501064A CN2011103606819A CN201110360681A CN102501064A CN 102501064 A CN102501064 A CN 102501064A CN 2011103606819 A CN2011103606819 A CN 2011103606819A CN 201110360681 A CN201110360681 A CN 201110360681A CN 102501064 A CN102501064 A CN 102501064A
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Abstract
The invention relates to a wire drawing positioning device for an air rudder, which is characterized by comprising a longitudinal platform. A jig frame is arranged on the longitudinal platform, and three struts are arranged at each of two ends of the jig frame. A bottom plate and an adjusting plate are disposed at the upper end of each of first struts, shaft holes are disposed at four corners of each of the bottom plates and the adjusting plates, and a first bolt and a nut are arranged between each pair of shaft holes. Screw holes and second bolts are disposed at four corners of each adjusting plate. Rudder spindle fixing blocks are arranged at two ends of each adjusting plate, and round holes are disposed on the rudder spindle fixing blocks. Positioning circular plates and first small center holes are arranged in the round holes. Adjusting rings are arranged at upper ends of second struts, and screw holes and third bolts are uniformly distributed on peripheries of the adjusting rings. Light target tubes are arranged in the adjusting ring, and inner ends of the third bolts are abutted to the light target tubes. A sealing plate and a second small center hole are disposed at one end of each light target tube. Screw holes are arranged at upper ends of third struts, and fourth bolts are arranged in the screw holes. A steel wire is arranged between the third struts, and two ends of the steel wire are respectively connected with the fourth bolts after sequentially penetrating through the second small center holes and the first small center holes. The wire drawing positioning device is applicable to calibration positioning of rudder spindles of air rudders.
Description
Technical field
The present invention relates to a kind of rudder for ship production equipment.Specifically, be in the hollow rudder production process, to be used for rudderpost calibrated making two rudderposts be in the airvane backguy positioner on the same straight line.
Background technology
All know at shipbuilding industry; Used airvane is connected with conduit through last neck bearing on the amphibious ship; In the 3.5m length range; Require up and down that the center line of rudderpost is equal to or less than 0.5mm in the installation deviation of side of a ship length direction, be equal to or less than 0.3mm in the installation deviation of rudder blade thickness direction, the rudderpost installation accuracy of visible hollow rudder requires very high.Conventional method is earlier the rudder body to be placed on the moulding bed, just two rudderposts directly is connected with the upper and lower side of bolt with the rudder body without any calibration.Owing to just two rudderposts directly are connected on the upper and lower side of rudder body without any calibration, can't satisfy the requirement of installation accuracy, make that the hollow rudder of producing is second-rate.
Summary of the invention
The problem that the present invention will solve provides a kind of airvane backguy positioner.Adopt this device to produce hollow rudder, can satisfy the installation accuracy requirement, improved the quality of hollow rudder greatly.
For addressing the above problem, take following technical scheme:
Airvane backguy positioner characteristics of the present invention are to comprise vertical platform; Vertically the platform middle part is useful on the moulding bed of placing the rudder body; First pillar, second pillar and the 3rd pillar are all arranged on vertical platform at moulding bed two ends from inside to outside successively, and the lower end of this first, second and third pillar all is connected with vertical platform mutually.First pillar upper end is fixed with base plate, and adjustable plate is arranged on the base plate, on four jiaos of correspondence positions of base plate and adjustable plate axis hole is arranged all, between corresponding a pair of axis hole first bolt is arranged all, and the outer end of first bolt is rotary with nut.Four jiaos of the joint plate all have the screw and second bolt, and said second bolt screws in the screw above adjustable plate and the second bolt lower end and base plate are offseted, and makes and leaves spacing between base plate and adjustable plate.Outer, the inner of joint plate all are fixed with the rudderpost fixed block; This rudderpost fixed block contains piece and following piece; Up and down the adjacent one side of piece be circular arc and up and down piece link together through screw; Form a circular hole that is used to place rudderpost by the circular arc of piece adjacent side up and down, and said circular hole is on the same straight line.In the said circular hole positioning disc is arranged, first central small hole is arranged on the positioning disc, this first central small hole is concentric with the circular hole on the fixed block.Second pillar upper end is fixed with the adjustment annulus, is evenly equipped with screw around the adjustment annulus, is rotary with the 3rd bolt in the screw.Adjustment has the light target pipe in the annulus, and the inner end of the 3rd bolt all offsets with the lateral surface of light target pipe.Light target Guan Yiduan has shrouding, and second central small hole is arranged on the shrouding, and this second central small hole is concentric with the light target pipe.There is screw the 3rd pillar upper end, and the 4th bolt is arranged in the screw.Individual the 3rd intercolumniation has steel wire, links to each other with the 4th bolt of the 3rd pillar upper end respectively after second central small hole that homonymy is all passed at the two ends of this steel wire successively and first central small hole.
Take such scheme, have the following advantages:
Can find out by such scheme; Because airvane backguy positioner of the present invention comprises vertical platform; Vertically the platform middle part is useful on the moulding bed of placing the rudder body; First pillar, second pillar and the 3rd pillar are all arranged on vertical platform at moulding bed two ends from inside to outside successively, and the lower end of this first, second and third pillar all is connected with vertical platform mutually.First pillar upper end fixed base plate has adjustable plate on the base plate, on four jiaos of correspondence positions of base plate and adjustable plate axis hole is arranged all, between corresponding a pair of axis hole first bolt is arranged all, and the outer end of first bolt is rotary with nut.Four jiaos of adjustable plate all have the screw and second bolt, and said second bolt screws in the screw above adjustable plate and the second bolt lower end and base plate are offseted, and makes and leaves spacing between base plate and adjustable plate.All there is the rudderpost fixed block outer, the inner of adjustable plate, be used to place the circular hole of rudderpost on the fixed block, and said circular hole is on the same straight line.Second pillar upper end is fixed with the adjustment annulus, is evenly equipped with screw around the adjustment annulus, is rotary with the 3rd bolt in the screw.Adjustment has the light target pipe in the annulus, and the inner end of the 3rd bolt all offsets with the side of light target pipe.There is screw the 3rd pillar upper end, and the 4th bolt is arranged in the screw.Two the 3rd intercolumniations have steel wire, and the two ends of this steel wire link to each other with the 4th bolt of the 3rd pillar upper end respectively after all passing circular hole on the corresponding rudderpost fixed block, light target pipe successively.Before two rudderposts are installed, earlier vertical platform is adjusted to horizontal level, regulate the 4th bolt in the screw of the 3rd pillar upper end again, steel wire is stretching.Regulate the light target pipe with four the 3rd bolts then, make the horizontal reference line parallel on steel wire and the moulding bed.Afterwards, regulate the second adjusting bolt on first bolt and the adjustable plate between two first pillars top base plates and adjustable plate, make steel wire all be in the first central small hole center on four positioning discs.At last, unload steel wire, four last pieces and four positioning discs, can two rudderposts be installed in the two ends of rudder body.Go up piece with four again and be fixed together, promptly accomplished the location of the rudderpost at rudder body and its two ends with screw and corresponding piece down.Only need screw bolt, just can realize the location of two rudderposts and rudder body.Can satisfy the installation accuracy requirement, guarantee the quality of hollow rudder.
Description of drawings
Fig. 1 is an airvane backguy positioning device structure sketch map of the present invention;
Fig. 2 is that the A of Fig. 1 is to view;
Fig. 3 is the I point enlarged diagram of Fig. 1;
Fig. 4 is that sketch map is looked on the left side of Fig. 3.
The specific embodiment
Like Fig. 1, Fig. 2, Fig. 3 and shown in Figure 4; Airvane backguy positioner of the present invention comprises vertical platform 11; Vertically platform 11 middle parts are useful on the moulding bed 5 of placing the rudder body; First pillar 10, second pillar 9 and the 3rd pillar 1 are all arranged on vertical platform 11 at moulding bed 5 two ends from inside to outside successively, and the lower end of this first, second and third pillar all is connected with vertical platform 11 mutually.Said first pillar 10, second pillar 9 and the 3rd pillar 1 all process with angle steel.First pillar, 10 upper ends are fixed with base plate 13; Base plate 13 is provided with adjustable plate 12; All be processed with axis hole on four jiaos of correspondence positions of base plate 13 and adjustable plate 12, all connect with first bolt 21 between corresponding a pair of axis hole, the outer end of first bolt 21 is stretched out on adjustable plate 12 and is rotary with nut 20.Four jiaos of adjustable plate 12 all are processed with screw, all are furnished with second bolt 20 in each screw, and said second bolt 20 screws in the screw above adjustable plate 12 and second bolt, 20 lower ends and base plate 13 are offseted, and makes 12 of base plate 13 and adjustable plates leave spacing.Outer, the inner fixed block that is used for fixing rudderpost that all is fixed with of adjustable plate 12; This rudderpost fixed block contains piece 6 and following piece 7; Upper and lower adjacent one side is promptly gone up following and last piece 7 bottoms of piece 6 and is all processed and be circular arc and upper and lower and link together through screw 22; Form a circular hole that is used to place rudderpost by the circular arc of upper and lower adjacent side, and said circular hole is on the same straight line.Positioning disc 21 is installed in the said circular hole, is processed with first central small hole 22 on the positioning disc 21, this first central small hole is concentric with the circular hole on the fixed block.Second pillar, 9 upper ends are fixed with adjustment annulus 4, are evenly equipped with screw around the adjustment annulus 4, are rotary with the 3rd bolt 3 in the screw.The inner end that adjustment is provided with light target pipe 21, the three bolts 3 in the annulus 4 all offsets with the lateral surface of light target pipe 21.Light target pipe 21 1 ends wherein are processed with the shrouding 20 that forms as one with it, are processed with second central small hole 22 on the shrouding 20, and this second central small hole is concentric with light target pipe 21.The 3rd pillar 1 upper end is processed with screw, is furnished with the 4th bolt 2 in the screw.Two the 3rd 1 on pillars are provided with steel wire 8, link to each other with the 4th bolt 2 of the 3rd pillar 1 upper end respectively after second central small hole 22 that homonymy is all passed at the two ends of this steel wire successively and first central small hole 22.
In the airvane production process, earlier vertical platform 11 is adjusted to horizontal level, regulate the 4th bolt 2 in the 3rd pillar 1 upper end screw again, steel wire 8 is stretching.Regulate light target pipe 21 with four the 3rd bolts 3 then, make the horizontal reference line parallel on steel wire 8 and the moulding bed 5.Afterwards, regulate first bolt 21 of 12 of two first pillar 10 top base plates 13 and adjustable plates and second bolt 20 on the adjustable plate 12, make steel wire 8 all be in first central small hole, 22 centers on four positioning discs 21.At last, unload steel wire 8, four and go up piece 6 and four positioning discs 21, can two rudderposts be installed in the two ends of rudder body.Go up piece 7 usefulness screws 22 with four again and be fixed together, promptly accomplished the location of the rudderpost at rudder body and its two ends with corresponding piece 6 down.
Claims (2)
1. airvane backguy positioner; It is characterized in that comprising vertical platform (11); Vertically platform (11) middle part is useful on the moulding bed (5) of placing the rudder body; First pillar (10), second pillar (9) and the 3rd pillar (1) are all arranged on vertical platform (11) at moulding bed (5) two ends from inside to outside successively, and the lower end of this first, second and third pillar all is connected with vertical platform (11) mutually; First pillar (10) upper end is fixed with base plate (13); Adjustable plate (12) is arranged on the base plate (13); On four jiaos of correspondence positions of base plate (13) and adjustable plate (12) axis hole is arranged all; Between corresponding a pair of axis hole first bolt (21) is arranged all, the outer end of first bolt (21) is rotary with nut (20); Four jiaos of adjustable plate (12) all have screw and second bolt (20); Said second bolt (20) screws in the screw above adjustable plate (12) and second bolt (20) lower end and base plate (13) is offseted, and makes and leaves spacing between base plate (13) and adjustable plate (12); Outer, the inner of adjustable plate (12) all are fixed with the rudderpost fixed block; This rudderpost fixed block contains piece (6) and following piece (7); Up and down the adjacent one side of piece be circular arc and up and down piece link together through screw (22); Form a circular hole that is used to place rudderpost by the circular arc of piece adjacent side up and down, and the center of circle of said circular hole is on the same straight line; Positioning disc (21) is arranged in the said circular hole, first central small hole (22) is arranged on the positioning disc (21), this first central small hole is concentric with the circular hole on the fixed block; Second pillar (9) upper end is fixed with adjustment annulus (4), is evenly equipped with screw around the adjustment annulus (4), is rotary with the 3rd bolt (3) in the screw; In adjustment annulus (4) light target pipe (12) is arranged, the inner end of the 3rd bolt (3) all offsets with the lateral surface of light target pipe (12); Light target pipe (12) one ends wherein have shrouding (20), and second central small hole (22) is arranged on the shrouding (21), and this second central small hole is concentric with light target pipe (12); There is screw the 3rd pillar (3) upper end, and the 4th bolt (2) is arranged in the screw; Steel wire (8) is arranged between two the 3rd pillars (1), link to each other with the 4th bolt (2) of the 3rd pillar (1) upper end respectively after second central small hole (22) that homonymy is all passed at the two ends of this steel wire successively and first central small hole (22).
2. airvane backguy positioner according to claim 1 is characterized in that said first pillar (10), second pillar (9) and the 3rd pillar (1) are angle steel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110360681.9A CN102501064B (en) | 2011-11-15 | 2011-11-15 | Wire drawing positioning device for air rudder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110360681.9A CN102501064B (en) | 2011-11-15 | 2011-11-15 | Wire drawing positioning device for air rudder |
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| Publication Number | Publication Date |
|---|---|
| CN102501064A true CN102501064A (en) | 2012-06-20 |
| CN102501064B CN102501064B (en) | 2014-04-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201110360681.9A Active CN102501064B (en) | 2011-11-15 | 2011-11-15 | Wire drawing positioning device for air rudder |
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| CN (1) | CN102501064B (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105750828A (en) * | 2014-12-15 | 2016-07-13 | 江南造船(集团)有限责任公司 | Manufacturing and installation technology of marine aerial rudder blade |
| CN105775035A (en) * | 2014-12-15 | 2016-07-20 | 江南造船(集团)有限责任公司 | Installation technology for marine air rudder |
| CN109131737A (en) * | 2018-09-21 | 2019-01-04 | 江门市南洋船舶工程有限公司 | A kind of regulating device for hole central pull |
| CN110030984A (en) * | 2018-01-11 | 2019-07-19 | 中航国际船舶发展（中国）有限公司 | A kind of irradiation platform with light target frame |
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| US6383041B1 (en) * | 2001-01-30 | 2002-05-07 | Peter D. Keefe | Rudder mechanism for jet propelled personal watercraft |
| EP1434030A2 (en) * | 2002-12-20 | 2004-06-30 | The Boeing Company | Laser alignment tool |
| CN101537510A (en) * | 2008-03-21 | 2009-09-23 | 上海船厂船舶有限公司 | Method for processing large-sized rudder blade |
| CN201559059U (en) * | 2009-05-07 | 2010-08-25 | 中冶天工上海十三冶建设有限公司 | Wire-hanging type aligner |
| CN202447874U (en) * | 2011-11-15 | 2012-09-26 | 无锡德林船舶设备有限公司 | Aerial rudder pull positioning device |
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2011
- 2011-11-15 CN CN201110360681.9A patent/CN102501064B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
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| DD118581A1 (en) * | 1975-03-27 | 1976-03-12 | ||
| DE3441017A1 (en) * | 1984-11-09 | 1986-05-15 | Vladimir Isaakovič Drut | Method of assembling ship steering gear |
| US6383041B1 (en) * | 2001-01-30 | 2002-05-07 | Peter D. Keefe | Rudder mechanism for jet propelled personal watercraft |
| EP1434030A2 (en) * | 2002-12-20 | 2004-06-30 | The Boeing Company | Laser alignment tool |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105750828A (en) * | 2014-12-15 | 2016-07-13 | 江南造船(集团)有限责任公司 | Manufacturing and installation technology of marine aerial rudder blade |
| CN105775035A (en) * | 2014-12-15 | 2016-07-20 | 江南造船(集团)有限责任公司 | Installation technology for marine air rudder |
| CN105775035B (en) * | 2014-12-15 | 2017-09-01 | 江南造船(集团)有限责任公司 | The mounting process of airvane peculiar to vessel |
| CN105750828B (en) * | 2014-12-15 | 2017-10-27 | 江南造船(集团)有限责任公司 | The manufacture mounting process of airvane rudder blade peculiar to vessel |
| CN110030984A (en) * | 2018-01-11 | 2019-07-19 | 中航国际船舶发展（中国）有限公司 | A kind of irradiation platform with light target frame |
| CN110030984B (en) * | 2018-01-11 | 2023-11-03 | 招商局邮轮研究院(上海)有限公司 | Lighting table with light target frame |
| CN109131737A (en) * | 2018-09-21 | 2019-01-04 | 江门市南洋船舶工程有限公司 | A kind of regulating device for hole central pull |
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| Publication number | Publication date |
|---|---|
| CN102501064B (en) | 2014-04-30 |
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Address after: 214191, No. 22 east section of northeast Tanggu Road, Tin Road, Xishan District, Jiangsu, Wuxi Patentee after: Wuxi sea nuclear equipment Technology Co., Ltd. Address before: 214191, No. 8 East Harbour Road, Xishan District, Jiangsu, Wuxi Patentee before: Wuxi Delin Ship Equipment Co., Ltd. |
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Address after: No. 203, Furong Zhongsi Road, Xishan District, Wuxi City, Jiangsu Province Patentee after: WUXI HAIHE EQUIPMENT TECHNOLOGY Co.,Ltd. Address before: 214191, No. 22 east section of northeast Tanggu Road, Tin Road, Xishan District, Jiangsu, Wuxi Patentee before: WUXI HAIHE EQUIPMENT TECHNOLOGY Co.,Ltd. |