CN102840229B - Adjusting center screw shaft bearing apparatus - Google Patents
Adjusting center screw shaft bearing apparatus Download PDFInfo
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- CN102840229B CN102840229B CN201210317891.4A CN201210317891A CN102840229B CN 102840229 B CN102840229 B CN 102840229B CN 201210317891 A CN201210317891 A CN 201210317891A CN 102840229 B CN102840229 B CN 102840229B
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- bearing sleeve
- bearing
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- sleeve
- propeller
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Abstract
The present invention relates to a kind of adjusting center screw shaft bearing apparatus for boats and ships tail end.Comprise bearing support, be arranged on the propeller bearing of described bearing support inner chamber, it is characterized in that being installed on aligning bearing sleeve between bearing support lumen orifice seat and propeller bearing, described aligning bearing sleeve comprises periphery and arranges the outer bearing sleeve that the interior bearing sleeve of sphere and endoporus arrange corresponding ball seat, interior bearing sleeve is set in outer bearing sleeve endoporus, the periphery sphere of interior bearing sleeve and the ball seat phase configuration of outer bearing sleeve.The invention enables propeller bearing can do the swing fine setting of any direction, realize it with axle condition self-aligning function, propeller bearing is made to keep even contact with tailing axle in the axial direction, which not only improves the usability of propeller bearing, and can reduce wear, extend bearing working life, reduce and avoid the generation of noise, be also convenient to the installation of tailing axle and propeller bearing simultaneously.By lubricating oil pipeline pressure injection launching grease, realize the lubrication of aligning bearing sleeve and antirust, ensure the aligning function of aligning bearing sleeve.
Description
Technical field
The present invention relates to a kind of adjusting center screw shaft bearing apparatus for boats and ships tail end.
Background technique
Propeller cavitation is the visual plant of marine propuision system, and screw shaft bearing apparatus is for supporting the moiety by weight of propeller cavitation and axle system.Existing ship propeller bearing is made up of axle sleeve and the rubber strip that is arranged on inner hole of shaft sleeve, bearing be fixedly mounted in bearing support with tailing axle phase configuration.Because propeller cavitation sole mass is larger, and be arranged on tailing axle end portion, tailing axle end becomes cantilever-shaped, easily occur bending and deformation, and existing bearing maintains static, therefore easily make bearing contact with tailing axle in the axial direction uneven, cause local specific pressure bigger than normal, form " edge loading " phenomenon, cause bearing concentrated wear excessive, thus reduce bearing working life; And " edge loading " phenomenon makes cannot form good lubricating film between axle and bearing, produce dry friction and creeping phenomenon, cause pivot friction self-excited vibration, and then generation whistle, particularly when frictional vibration frequency is consistent with axle system or hull local frequencies, axle system or the resonance of hull partial structurtes can be caused, thus produce strong vibration noise, affect the recessive energy of sound on naval vessel.
Summary of the invention
Technical problem to be solved by this invention is to provide a kind of adjusting center screw shaft bearing apparatus, and it can improve the contact condition of propeller bearing and tailing axle, reduces wear, and improves usability and the life-span of propeller bearing, and reduces noise.
The technological scheme that the problem that the present invention is the above-mentioned proposition of solution is taked is: comprise bearing support, be arranged on the propeller bearing of described bearing support inner chamber, it is characterized in that being installed on aligning bearing sleeve between bearing support lumen orifice seat and propeller bearing, described aligning bearing sleeve comprises periphery and arranges the outer bearing sleeve that the interior bearing sleeve of sphere and endoporus arrange corresponding ball seat, interior bearing sleeve is set in outer bearing sleeve endoporus, the periphery sphere of interior bearing sleeve and the ball seat phase configuration of outer bearing sleeve.
By such scheme, the periphery sphere of described interior bearing sleeve is outer convex spherical, and the ball seat of described outer bearing sleeve is indent ball seat.
By such scheme, described interior bearing sleeve endoporus and the periphery phase configuration of propeller bearing, described outer bearing sleeve periphery and bearing support lumen orifice seat phase configuration.
By such scheme, described outer bearing sleeve is formed by two involutory connections of semicircular bearing shell.
By such scheme, described interior bearing sleeve evagination spherical diameter is greater than interior bearing sleeve outer circumference diameter, and interior bearing sleeve evagination spherical diameter is less than interior bearing sleeve axial length.
By such scheme, described outer bearing sleeve indent ball seat spherical diameter is identical with interior bearing sleeve evagination spherical diameter, and outer bearing sleeve indent ball seat spherical diameter is less than outer bearing sleeve outer circumference diameter.
By such scheme, described outer bearing sleeve indent ball seat sphere and the outer same centre of sphere of convex spherical of interior bearing sleeve, and the centre of sphere is positioned on the axis of described propeller bearing, described outer bearing sleeve indent ball seat area of spherical surface is less than interior bearing sleeve evagination area of spherical surface.
By such scheme, the outer convex spherical of described interior bearing sleeve is provided with oil groove, and described outer bearing sleeve indent ball seat ball correspondence offers the oilhole be connected with lubricant pipe.
By such scheme, described interior bearing sleeve and outer bearing sleeve are made up of ZCuAl10Fe3 material.
Beneficial effect of the present invention is: 1, by arranging aligning bearing sleeve, make propeller bearing can do the swing fine setting of any direction, realize it with axle condition self-aligning function, propeller bearing is made to keep even contact with tailing axle in the axial direction, which not only improves the usability of propeller bearing, and can reduce wear, extend bearing working life, reduce and avoid the generation of noise, be also convenient to the installation of tailing axle and propeller bearing simultaneously; 2, by the regular pressure injection launching grease of lubricating oil pipeline, stored in oil groove, realize aligning bearing sleeve sphere lubrication in the seawater and antirust, thus ensure the aligning function of aligning bearing sleeve; 3, the aligning bearing sleeve be made up of ZCuAl10Fe3 material has stronger wear-and corrosion-resistant ability, thus ensures further aligning bearing sleeve working life in the seawater.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is the sectional view of the A-A in Fig. 1.
Fig. 3 is the sectional view of the B-B in Fig. 2.
Embodiment
Embodiments of the present invention are further described below in conjunction with accompanying drawing.
Comprise the bearing support 1 connected firmly mutually with hull tailstock, aligning bearing sleeve is installed at bearing support lumen orifice seat, described aligning bearing sleeve comprises periphery and arranges the outer bearing sleeve 4 that the interior bearing sleeve 3 of sphere and endoporus arrange corresponding ball seat, the periphery sphere of described interior bearing sleeve is outer convex spherical 5, and the ball seat of described outer bearing sleeve is indent ball seat.Interior bearing sleeve evagination spherical diameter is greater than interior bearing sleeve outer circumference diameter, and interior bearing sleeve evagination spherical diameter is less than interior bearing sleeve axial length.Interior bearing sleeve is set in outer bearing sleeve endoporus, described outer bearing sleeve indent ball seat spherical diameter is identical with interior bearing sleeve evagination spherical diameter, the axial length of outer bearing sleeve is identical with interior bearing sleeve axial length, and interior bearing sleeve is by the indent ball seat phase configuration of outer convex spherical and outer bearing sleeve, outer bearing sleeve indent ball seat sphere 8 diameter is less than outer bearing sleeve outer circumference diameter.Described outer bearing sleeve indent ball seat sphere and the outer same centre of sphere of convex spherical of interior bearing sleeve, and the centre of sphere is positioned on the axis of described propeller bearing, and also outer bearing sleeve indent ball seat area of spherical surface is less than interior bearing sleeve evagination area of spherical surface.Outer bearing sleeve is formed by two involutory connections of semicircular bearing shell, is connected by clamping bolt 7.In addition, the outer convex spherical of interior bearing sleeve is provided with oil groove 9, and described outer bearing sleeve indent ball seat ball correspondence offers the oilhole 10 be connected with lubricant pipe 11.Described interior bearing sleeve and outer bearing sleeve are made up of ZCuAl10Fe3 material.Interior bearing sleeve endoporus suit propeller bearing 2, propeller bearing and tailing axle 6 phase configuration, tail the tip of the axis is installed on propeller cavitation 12.
Claims (9)
1. an adjusting center screw shaft bearing apparatus, comprise bearing support, be arranged on the propeller bearing of described bearing support inner chamber, aligning bearing sleeve is installed between bearing support lumen orifice seat and propeller bearing, described aligning bearing sleeve comprises periphery and arranges the outer bearing sleeve that the interior bearing sleeve of sphere and endoporus arrange corresponding ball seat, interior bearing sleeve is set in outer bearing sleeve endoporus, the periphery sphere of interior bearing sleeve and the ball seat phase configuration of outer bearing sleeve, it is characterized in that, certain interval is provided with between described interior bearing sleeve and outer bearing sleeve two ends, in this gap makes, annular chamber is formed between outer bearing sleeve, described annular chamber is communicated with outside seawater, this gap is less than interior bearing sleeve length, the length of described interior bearing sleeve equals the length of outer bearing sleeve.
2. adjusting center screw shaft bearing apparatus according to claim 1, is characterized in that the periphery sphere of described interior bearing sleeve is outer convex spherical, and the ball seat of described outer bearing sleeve is indent ball seat.
3. adjusting center screw shaft bearing apparatus according to claim 1 and 2, is characterized in that described interior bearing sleeve endoporus and the periphery phase configuration of propeller bearing, described outer bearing sleeve periphery and bearing support lumen orifice seat phase configuration.
4. adjusting center screw shaft bearing apparatus according to claim 1 and 2, is characterized in that described outer bearing sleeve is formed by two involutory connections of semicircular bearing shell.
5. adjusting center screw shaft bearing apparatus according to claim 2, it is characterized in that described interior bearing sleeve evagination spherical diameter is greater than interior bearing sleeve outer circumference diameter, interior bearing sleeve evagination spherical diameter is less than interior bearing sleeve axial length.
6. the adjusting center screw shaft bearing apparatus according to claim 2 or 5, it is characterized in that described outer bearing sleeve indent ball seat spherical diameter is identical with interior bearing sleeve evagination spherical diameter, and outer bearing sleeve indent ball seat spherical diameter is less than outer bearing sleeve outer circumference diameter.
7. adjusting center screw shaft bearing apparatus according to claim 6, it is characterized in that described outer bearing sleeve indent ball seat sphere and the outer same centre of sphere of convex spherical of interior bearing sleeve, and the centre of sphere is positioned on the axis of described propeller bearing, described outer bearing sleeve indent ball seat area of spherical surface is less than interior bearing sleeve evagination area of spherical surface.
8. adjusting center screw shaft bearing apparatus according to claim 7, is characterized in that the outer convex spherical of described interior bearing sleeve is provided with oil groove, and described outer bearing sleeve indent ball seat ball correspondence offers the oilhole be connected with lubricant pipe.
9. adjusting center screw shaft bearing apparatus according to claim 1 and 2, is characterized in that described interior bearing sleeve and outer bearing sleeve are made up of ZCuAl10Fe3 material.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201210317891.4A CN102840229B (en) | 2012-08-31 | 2012-08-31 | Adjusting center screw shaft bearing apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201210317891.4A CN102840229B (en) | 2012-08-31 | 2012-08-31 | Adjusting center screw shaft bearing apparatus |
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CN102840229A CN102840229A (en) | 2012-12-26 |
CN102840229B true CN102840229B (en) | 2015-11-18 |
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CN201210317891.4A Active CN102840229B (en) | 2012-08-31 | 2012-08-31 | Adjusting center screw shaft bearing apparatus |
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Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104196987A (en) * | 2014-08-08 | 2014-12-10 | 苏州苏净船用机械有限公司 | Lubrication structure of propeller bearing |
CN108953212A (en) * | 2018-08-16 | 2018-12-07 | 合肥恒大江海泵业股份有限公司 | A kind of transverse bearing of submersible pump adjusting center |
CN110239698A (en) * | 2019-06-24 | 2019-09-17 | 高峰 | A kind of non-maintaining ship rear driving system from centering |
CN115289135A (en) * | 2022-06-13 | 2022-11-04 | 中国船舶重工集团公司第七一九研究所 | Support bearing and ship propulsion system |
Citations (6)
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---|---|---|---|---|
FR1583685A (en) * | 1968-02-06 | 1969-11-28 | ||
US4005916A (en) * | 1975-11-07 | 1977-02-01 | Dillon Richard H F | Jacked hydrostatic bearing |
US4127080A (en) * | 1977-03-08 | 1978-11-28 | Lakiza Rostislav I | Tubular shaft of a marine line shafting |
DE4021053A1 (en) * | 1990-06-29 | 1992-01-09 | Mannesmann Ag | Axial-radial bearing for shaft - is for ship and has flange with at least hydraulic equalising chambers |
CN201391411Y (en) * | 2009-04-30 | 2010-01-27 | 天津市天发重型水电设备制造有限公司 | Automatic aligning type guide bearing structure |
CN102011796A (en) * | 2010-12-16 | 2011-04-13 | 武汉理工大学 | Self-aligning spherical plain water lubricated tail bearing for ships |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS50396B1 (en) * | 1970-09-14 | 1975-01-08 | ||
FI90869C (en) * | 1986-11-14 | 1994-04-11 | Tanabe Seiyaku Co | Process for the preparation of imidazolidinone derivatives useful as a medicament |
-
2012
- 2012-08-31 CN CN201210317891.4A patent/CN102840229B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1583685A (en) * | 1968-02-06 | 1969-11-28 | ||
US4005916A (en) * | 1975-11-07 | 1977-02-01 | Dillon Richard H F | Jacked hydrostatic bearing |
US4127080A (en) * | 1977-03-08 | 1978-11-28 | Lakiza Rostislav I | Tubular shaft of a marine line shafting |
DE4021053A1 (en) * | 1990-06-29 | 1992-01-09 | Mannesmann Ag | Axial-radial bearing for shaft - is for ship and has flange with at least hydraulic equalising chambers |
CN201391411Y (en) * | 2009-04-30 | 2010-01-27 | 天津市天发重型水电设备制造有限公司 | Automatic aligning type guide bearing structure |
CN102011796A (en) * | 2010-12-16 | 2011-04-13 | 武汉理工大学 | Self-aligning spherical plain water lubricated tail bearing for ships |
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CN102840229A (en) | 2012-12-26 |
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