CN105965251A - Shaft flange assembly hole alignment structure and alignment method - Google Patents
Shaft flange assembly hole alignment structure and alignment method Download PDFInfo
- Publication number
- CN105965251A CN105965251A CN201610476677.1A CN201610476677A CN105965251A CN 105965251 A CN105965251 A CN 105965251A CN 201610476677 A CN201610476677 A CN 201610476677A CN 105965251 A CN105965251 A CN 105965251A
- Authority
- CN
- China
- Prior art keywords
- flange
- tapered sleeve
- pilot hole
- flanges
- hole
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 238000000034 method Methods 0.000 title claims abstract description 10
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052802 copper Inorganic materials 0.000 claims abstract description 16
- 239000010949 copper Substances 0.000 claims abstract description 16
- 239000000463 material Substances 0.000 claims abstract description 6
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 238000010030 laminating Methods 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 239000004519 grease Substances 0.000 claims 1
- 238000003780 insertion Methods 0.000 abstract description 3
- 230000037431 insertion Effects 0.000 abstract description 3
- 238000009434 installation Methods 0.000 abstract 2
- 208000037805 labour Diseases 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000005299 abrasion Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 125000004122 cyclic group Chemical group 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000010079 rubber tapping Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/10—Aligning parts to be fitted together
- B23P19/12—Alignment of parts for insertion into bores
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Abstract
The invention discloses a shaft flange assembly hole alignment structure and an alignment method thereof. The assembly hole alignment of two connected flanges is realized through matching between a copper taper sleeve and a taper rod; as the taper sleeve adopts a copper material, the plasticity is good; the taper sleeve outwards expands in the radial direction through interference fit installation of the taper rod and the taper sleeve, so that the two flanges can relatively rotate to force alignment of assembly holes of the flanges; as the outer diameter of the taper sleeve is smaller than the aperture of the assembly holes of the flanges, the taper sleeve can be easily inserted in the corresponding assembly holes of the flanges to prevent damage of dowel pins and the flanges caused by direct collision of insertion ends of the copper dowel pins on the end surfaces of the flanges due to no alignment of the assembly holes of the two flanges in a traditional installation structure; and as the assembly holes of the adjacently connected flanges are aligned through an expansion mode of the taper sleeve and the taper rod, the assembly time and labors are saved, the working efficiency is high, and the precise alignment is realized through repeated adjustment without needing manual operations.
Description
Technical field
The present invention relates to marine shafting flange bolt hole align structures and alignment methods.
Background technology
nullIn the boats and ships of conventional tail type，For by jackshaft、The Propulsion Systems that propeller shaft and main frame flywheel are formed，Flange opening (GAP) in shaft and skew (SAG) adjust after examination terminates，Need to be integrated above three parts assembly connection，By adjusting the height of the temporary support below jackshaft，Thus regulate the longitudinally height of jackshaft，Main frame flywheel or propeller shaft is moved subsequently by dish，Make the pilot hole on the flange of the pilot hole on the flange of main frame flywheel end or propeller shaft end turn to the pilot hole on jackshaft corresponding end flange to be directed at，After alignment, copper alignment pin is inserted in the pilot hole of two alignments，Jackshaft is made to be fixed with one with propeller shaft with main frame flywheel and jackshaft in an interference fit，Owing to jackshaft and main frame flywheel and jackshaft are to be connected by interference fit with propeller shaft，Therefore，Required precision to pilot hole is the highest，Once pilot hole precision does not reaches standard，During then causing assembling，Alignment pin inserts the end face of end and withstands on the end face of flange on jackshaft、On the end face of main frame flywheel flange or on the end face of propeller shaft flange，During constantly tapping alignment pin，Alignment pin end face is caused to clash into end face of flange，Cause alignment pin damage and cause the flange on main frame flywheel、Flange on jackshaft or the flange on propeller shaft damage，Cause and need to change parts，And again make alignment pin，Cost is caused drastically to raise；For solving the problems referred to above, need to take time and effort by manually not stopping the flange on adjustment jackshaft and the Aligning degree of the pilot hole on corresponding main frame flywheel flange and propeller shaft flange；Further, since alignment pin outside dimension must be to close according to matching size after pilot hole polish, therefore, this kind of speciality alignment pin cannot recycle, and therefore, causes each sleeve system to need one group of specific assembly tool, causes cost significantly to raise.
Summary of the invention
It is desirable to provide a kind of can alignment flange pilot hole quick, accurate and the axle system flange pilot hole align structures of reusable edible and alignment methods, it is provided that assembly work efficiency, time saving and energy saving, reduce manufacturing cost.
A kind of axle system of the present invention flange pilot hole align structures, including the copper tapered sleeve inserted in two flange pilot holes and the cone rod matched with tapered sleeve, described tapered sleeve is column, tapered sleeve outer surface diameter is less than flange pilot hole aperture, tapered sleeve inner surface is conical through-hole, described cone rod is tapered, and one end of cone rod major diameter is inserted by minor diameter one end of the conical through-hole within tapered sleeve, and the end face of described cone rod minor diameter one end is provided with rotating rod.
A kind of axle system of the present invention flange pilot hole alignment methods, its step is as follows:
1) manual adjustment, makes main frame flywheel flange somewhat be directed at jackshaft corresponding end flange with jackshaft corresponding end flange and propeller shaft flange；
2) copper tapered sleeve is inserted in the pilot hole that adjacent two flanges are corresponding；
3) cone rod major diameter one end is inserted from the conical through-hole minor diameter one end within tapered sleeve；
4) artificial turn rotating rod, makes the conical through-hole surface laminating of cone rod outer surface and tapered sleeve；
5) manually rotate one group of rotating rod of homonymy simultaneously, cone rod is made to axially move relative to the conical through-hole of tapered sleeve, cone rod radially swell tapered sleeve, make tapered sleeve outer surface push against on the inner surface of flange pilot hole, make two flange relative movements of connection, thus the pilot hole on two flanges is directed at.
A kind of axle system flange pilot hole align structures of the present invention and alignment methods thereof, by copper tapered sleeve and excellent the coordinating of cone, realize the pilot hole alignment on two flanges connected, owing to tapered sleeve uses copper material, therefore, plasticity is good, can be installed by the interference fit of cone rod with tapered sleeve, tapered sleeve is made radially to extend out, so that two flanges can relatively rotate, flange pilot hole is forced to be directed at, owing to tapered sleeve external diameter is less than flange pilot hole aperture, therefore, can easily tapered sleeve be inserted in the pilot hole that two flanges are corresponding, avoid in original mounting structure, because the pilot hole of two flanges is not aligned with, and make the insertion end of copper alignment pin directly impinge upon on end face of flange, to damage alignment pin and flange；Owing to making the flange pilot hole of adjacent connection be directed at by the tensioner mode of tapered sleeve with cone rod, therefore, it is time saving and energy saving to assemble, and work efficiency is high, it is not necessary to manually realize precisely being directed at by repeatedly regulating；Owing to tapered sleeve uses copper material, its plasticity is good, therefore, in the case of tapered sleeve is without damaging, for the axle system flange that the aperture of flange pilot hole is close, this align structures can be recycled, further significantly reduce manufacturing cost, and owing to tapered sleeve takes through-hole structure, therefore, making tapered sleeve material few, cost is lower.
Accompanying drawing explanation
Fig. 1 is present configuration schematic diagram.
Fig. 2 is Fig. 1 part A partial enlarged drawing.
Detailed description of the invention
A kind of axle system flange pilot hole align structures, as depicted in figs. 1 and 2, including the copper tapered sleeve 2 inserted in two flange 1 pilot holes and the cone rod 3 matched with tapered sleeve 2, described tapered sleeve 2 is in column, tapered sleeve 2 outer surface diameter is less than flange 1 pilot hole aperture, and tapered sleeve 2 inner surface is conical through-hole, and described cone rod 3 is tapered, the one end boring excellent 3 major diameters is inserted by minor diameter one end of the conical through-hole within tapered sleeve 2, and the end face of the excellent 3 minor diameter one end of described cone is provided with rotating rod 4.
The range of taper of the conical through-hole of described tapered sleeve 2 is 1:15 ~ 1:25, such as 1:15,1:18,1:20,1:22,1:25 etc., preferably 1:20；Range of taper 1:15 ~ the 1:25 of described cone rod 3, such as 1:15,1:18,1:20,1:22,1:25 etc., preferably 1:20.Under this tapering, the alignment of the flange pilot hole that this align structures is widely used in marine shafting can be made, improve the cyclic utilization rate of align structures, reduce manufacturing cost.
Described rotating rod 4 is threaded bar, nut 5 is tightened in threaded bar, by arranging nut 5, it is simple to artificial rotation rotating rod 4, simple to operate, time saving and energy saving, meanwhile, by arranging nut 5, the flange that can also make two connections is fastened as a whole, avoid boats and ships to produce vibration in running, and make align structures loosen, make the flange 1 of two connections depart from.
Described tapered sleeve 2 length thickness sum less than two flanges 1 and the thickness more than single flange 1, it is arranged with copper stop washer 6 in the threaded bar between nut 5 and tapered sleeve 2 end face in described threaded bar, described stop washer 6 is in T shape, by tightening nut 5, major diameter one end end face of stop washer 6 pushes against in flange 1 surface, minor diameter one end of stop washer 6 is stretched in flange 1 pilot hole, its end face pushes against in tapered sleeve 2 end face, thus flange 1 of avoiding wearing and tearing in nut 5 rotation process, also avoid tapered sleeve 2 to move axially simultaneously.
Excellent 3 materials of described cone are steel, and owing to cone rod 3 can bear certain puller system extruding force, therefore, the cone rod 3 made by steel during assembling, its intensity is high, and stress is good.
A kind of axle system of the present invention flange pilot hole alignment methods, the steps include: (1) manual adjustment, makes main frame flywheel flange somewhat be directed at jackshaft corresponding end flange with jackshaft corresponding end flange and propeller shaft flange；(2) copper tapered sleeve 2 is inserted in the pilot hole of adjacent two flange 1 correspondences；(3) at the conical through-hole inner surface of tapered sleeve 2 and bore excellent 3 surface greases, it is beneficial to the two and relatively slides, reduce abrasion, increase the service life, bore excellent 3 major diameter one end from conical through-hole minor diameter one end insertion tapered sleeve 2 within；(4) artificial turn rotating rod 4, makes the conical through-hole surface laminating of cone rod 3 outer surfaces and tapered sleeve 2；(5) manually rotate one group of rotating rod 4 of homonymy simultaneously, cone rod 3 is made to axially move relative to the conical through-hole of tapered sleeve 2, cone rod 3 radially swell tapered sleeve 2, tapered sleeve 2 outer surface is made to push against on the inner surface of flange 1 pilot hole, make two flange 1 relative movements of connection, thus the pilot hole on two flanges 1 is directed at.
Claims (8)
1. an axle system flange pilot hole align structures, it is characterized in that: include the copper tapered sleeve (2) inserting in two flanges (1) pilot hole and cone rod (3) matched with tapered sleeve (2), described tapered sleeve (2) is in column, tapered sleeve (2) outer surface diameter is less than flange (1) pilot hole aperture, tapered sleeve (2) inner surface is conical through-hole, described cone rod (3) is tapered, one end of cone rod (3) major diameter is inserted by minor diameter one end of the conical through-hole of tapered sleeve (2) inside, and the end face of described cone rod (3) minor diameter one end is provided with rotating rod (4).
A kind of axle system the most according to claim 1 flange pilot hole align structures, it is characterised in that: the range of taper of the conical through-hole of described tapered sleeve (2) is 1:15 ~ 1:25；Range of taper 1:15 ~ the 1:25 of described cone rod (3).
A kind of axle system the most according to claim 2 flange pilot hole align structures, it is characterised in that: the preferred 1:20 of tapering of the conical through-hole of described tapered sleeve (2)；The preferred 1:20 of tapering of described cone rod (3).
A kind of axle system the most according to claim 1 flange pilot hole align structures, it is characterised in that: described rotating rod (4) is threaded bar, and nut (5) is tightened in threaded bar.
A kind of axle system the most according to claim 4 flange pilot hole align structures, it is characterized in that: described tapered sleeve (2) length thickness sum less than two flanges (1) and the thickness more than single flange (1), it is arranged with copper stop washer (6) in the threaded bar between nut (5) and tapered sleeve (2) end face in described threaded bar, described stop washer (6) is in T shape, by tightening nut (5), major diameter one end end face of stop washer (6) pushes against in flange (1) surface, minor diameter one end of stop washer (6) is stretched in flange (1) pilot hole, its end face pushes against in tapered sleeve (2) end face.
6. according to a kind of axle system flange pilot hole align structures described in claim 1-5 any one, it is characterised in that: described cone rod (3) material is steel.
7. an axle system flange pilot hole alignment methods, it is characterised in that step is as follows:
1) manual adjustment, makes main frame flywheel flange somewhat be directed at jackshaft corresponding end flange with jackshaft corresponding end flange and propeller shaft flange；
2) copper tapered sleeve (2) is inserted in the pilot hole that adjacent two flanges (1) are corresponding；
3) cone rod (3) major diameter one end is inserted from conical through-hole minor diameter one end that tapered sleeve (2) is internal；
4) artificial turn rotating rod (4), makes the conical through-hole surface laminating of cone rod (3) outer surface and tapered sleeve (2)；
5) manually rotate one group of rotating rod (4) of homonymy simultaneously, cone rod (3) is made to axially move relative to the conical through-hole of tapered sleeve (2), cone rod (3) radially swell tapered sleeve (2), tapered sleeve (2) outer surface is made to push against on the inner surface of flange (1) pilot hole, make two flanges (1) relative movement of connection, thus the pilot hole on two flanges (1) is directed at.
A kind of axle system the most according to claim 7 flange pilot hole align structures, it is characterised in that: in step 3), at conical through-hole inner surface and cone rod (3) surface grease of tapered sleeve (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610476677.1A CN105965251A (en) | 2016-06-27 | 2016-06-27 | Shaft flange assembly hole alignment structure and alignment method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610476677.1A CN105965251A (en) | 2016-06-27 | 2016-06-27 | Shaft flange assembly hole alignment structure and alignment method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105965251A true CN105965251A (en) | 2016-09-28 |
Family
ID=57019231
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610476677.1A Pending CN105965251A (en) | 2016-06-27 | 2016-06-27 | Shaft flange assembly hole alignment structure and alignment method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105965251A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107030479A (en) * | 2016-12-26 | 2017-08-11 | 北京金风科创风电设备有限公司 | Dislocation adjusting device and flange dislocation adjusting method |
| CN110434547A (en) * | 2019-08-12 | 2019-11-12 | 哈尔滨电机厂有限责任公司 | A kind of coaxial pin hole interference localization method of hydraulic turbine |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU1794582C (en) * | 1991-06-13 | 1993-02-15 | Харьковский авиационный институт им.Н.Е.Жуковского | Method for making riveted joint |
| CN2460785Y (en) * | 2001-01-19 | 2001-11-21 | 王少恩 | Combined locating pin |
| CN201916314U (en) * | 2010-12-16 | 2011-08-03 | 渤海船舶重工有限责任公司 | Connecting bolt for ship main engine shaft and flange |
| CN203993074U (en) * | 2014-07-17 | 2014-12-10 | 常州爱普超高压液压系统有限公司 | Flange connecting screw hole centering tooling |
| CN205764838U (en) * | 2016-06-27 | 2016-12-07 | 广州文冲船厂有限责任公司 | A kind of axle system flange pilot hole align structures |
-
2016
- 2016-06-27 CN CN201610476677.1A patent/CN105965251A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU1794582C (en) * | 1991-06-13 | 1993-02-15 | Харьковский авиационный институт им.Н.Е.Жуковского | Method for making riveted joint |
| CN2460785Y (en) * | 2001-01-19 | 2001-11-21 | 王少恩 | Combined locating pin |
| CN201916314U (en) * | 2010-12-16 | 2011-08-03 | 渤海船舶重工有限责任公司 | Connecting bolt for ship main engine shaft and flange |
| CN203993074U (en) * | 2014-07-17 | 2014-12-10 | 常州爱普超高压液压系统有限公司 | Flange connecting screw hole centering tooling |
| CN205764838U (en) * | 2016-06-27 | 2016-12-07 | 广州文冲船厂有限责任公司 | A kind of axle system flange pilot hole align structures |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107030479A (en) * | 2016-12-26 | 2017-08-11 | 北京金风科创风电设备有限公司 | Dislocation adjusting device and flange dislocation adjusting method |
| CN107030479B (en) * | 2016-12-26 | 2019-05-24 | 北京金风科创风电设备有限公司 | Dislocation adjustment device and flange dislocation adjustment method |
| CN110434547A (en) * | 2019-08-12 | 2019-11-12 | 哈尔滨电机厂有限责任公司 | A kind of coaxial pin hole interference localization method of hydraulic turbine |
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| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160928 |