CN204188962U - A kind of carrier-borne stable platform simulation test device - Google Patents
A kind of carrier-borne stable platform simulation test device Download PDFInfo
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- CN204188962U CN204188962U CN201420688267.XU CN201420688267U CN204188962U CN 204188962 U CN204188962 U CN 204188962U CN 201420688267 U CN201420688267 U CN 201420688267U CN 204188962 U CN204188962 U CN 204188962U
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Abstract
A kind of carrier-borne stable platform simulation test device of the utility model, can simulate the motion states such as ship rolling, pitching, heave, people can study carrier-borne stable platform by this device.Ear type joint I, ear type joint III and ear type joint V are connected in bottom platform I.Ear type joint II, ear type joint IV and ear type joint VI are connected in framework platform top.Electric cylinder I two ends are connected with ear type joint II with ear type joint I respectively.Electric cylinder II two ends are connected with ear type joint IV with ear type joint III respectively.Electric cylinder III two ends are connected with ear type joint VI with ear type joint V respectively.Ear type joint VII, ear type joint Ⅸ and ear type joint Ⅻ are connected in bottom framework platform.Ear type joint VIII, ear type joint Ⅹ and ear type joint Ⅺ are connected to platform II top.Electric cylinder IV two ends are connected with ear type joint VIII with ear type joint VII respectively.Electric cylinder V two ends are connected with ear type joint Ⅹ with ear type joint Ⅸ respectively.Electric cylinder VI two ends are connected with ear type joint Ⅺ with ear type joint Ⅻ respectively.
Description
Technical field
The utility model relates to a kind of carrier-borne Study system, more specifically to the carrier-borne stable platform simulation test device of one.
Background technology
By the effect of wave agitation factor, naval vessel can produce the effect of rolling, pitching, yawing, swaying, surging, heave 6 degree of freedom at sea.This motion brings serious impact to the launch accuracy of the landing safety of carrier-based helicopter, shipborne weapon and boats and ships seaborne supply etc.For adapting to the requirement of the military strategy for the new period, improving the ability that armament is fought at sea, therefore its platform stable systematic research just being become very necessary and there is strategic importance.In addition, carrier-borne stable platform also can be applied in oceanographic engineering field, it can isolate ship rolling, pitching, heave movement for the impact of the operations such as sea lifting, improves the safety and reliability of relevant operation, so its civilian meaning is also very extensive.But hip-based platform is different from other common platforms, its stability control techniques is not very ripe.The research in this direction domestic does not obtain outstanding achievement especially, and external research mostly is military concerning security matters project, so just more highlight the significance that we study this stable platform from this aspect.
Summary of the invention
The technical matters that the utility model mainly solves is: provide a kind of carrier-borne stable platform simulation test device, can simulate the motion states such as ship rolling, pitching, heave, people can study carrier-borne stable platform by this device.
For solving the problems of the technologies described above, the utility model relates to a kind of carrier-borne Study system, more specifically to the carrier-borne stable platform simulation test device of one, comprise platform I, ear type joint I, electric cylinder I, ear type joint II, ear type joint III, electric cylinder II, ear type joint IV, ear type joint V, electric cylinder III, ear type joint VI, framework platform, ear type joint VII, electric cylinder IV, ear type joint VIII, platform II, column, ear type joint Ⅸ, electric cylinder V, ear type joint Ⅹ, ear type joint Ⅺ, electric cylinder VI and ear type joint Ⅻ, ship rolling can be simulated, pitching, the motion of heave three degree of freedom, people can also realize the research to carrier-borne stable platform stability whereby.
Ear type joint I, ear type joint III and ear type joint V are all bolted bottom platform I.Ear type joint II, ear type joint IV and ear type joint VI are all connected to framework platform top.Electric cylinder I upper end is connected with ear type joint I, and lower end is connected with ear type joint II.Electric cylinder II upper end is connected with ear type joint III, and lower end is connected with ear type joint IV.Electric cylinder III upper end is connected with ear type joint V, and lower end is connected with ear type joint VI.Ear type joint VII, ear type joint Ⅸ and ear type joint Ⅻ are all connected to the bottom of framework platform.Ear type joint VIII, ear type joint Ⅹ and ear type joint Ⅺ are all bolted at the top of platform II.Electric cylinder IV upper end is connected with ear type joint VII, and lower end is connected with ear type joint VIII.Electric cylinder V upper end is connected with ear type joint Ⅸ, and lower end is connected with ear type joint Ⅹ.Electric cylinder VI upper end is connected with ear type joint Ⅻ, and lower end is connected with ear type joint Ⅺ.Column is fixed on bottom platform II.
As the further optimization of this programme, hole I on floor I on ear type joint I described in the utility model cooperatively interacts with the upper hole I on the screw rod I in electric cylinder I, ear type joint I and electric cylinder I are fixed through the hole I on floor I and the upper hole I on screw rod I by bolt, and use nut screwing clamping bolt.
As the further optimization of this programme, the center line in the upper hole I on screw rod I described in the utility model is mutually vertical with the center line of lower opening I.
As the further optimization of this programme, electric cylinder I described in the utility model and electric cylinder III are positioned at two Angle Position of framework platform.
As the further optimization of this programme, electric cylinder II described in the utility model is positioned at the centre of the opposite side on electric cylinder I and limit, electric cylinder III place.
As the further optimization of this programme, ear type joint II described in the utility model, ear type joint IV and ear type joint VI are all welded to connect with framework platform.
As the further optimization of this programme, ear type joint VII described in the utility model, ear type joint Ⅸ and ear type joint Ⅻ are all welded to connect with framework platform.
As the further optimization of this programme, electric cylinder IV described in the utility model and electric cylinder VI be positioned at framework platform two jiaos.
As the further optimization of this programme, electric cylinder V described in the utility model is positioned in the middle of the opposite side on electric cylinder IV and limit, electric cylinder VI place.
As the further optimization of this programme, electric cylinder I described in the utility model and electric cylinder V are positioned at framework platform two relative edge.
A kind of carrier-borne stable platform simulation test device of the utility model, by the motion simulation ship rolling of electric cylinder IV, electric cylinder V and electric cylinder IV, pitching, heave movement, the angle of inclination of obliquity sensor real-time detection block body panel roll and pitch, the dip angle signal that obliquity sensor collection is returned, through computing input control device, export control signal, electric cylinder I, electric cylinder II and electric cylinder III is driven to move, the motion of compensating analog boats and ships constantly, make platform I maintenance level motionless, and then reach the effect of stable platform I.
The utility model has the advantages that: can simulate the motion states such as ship rolling, pitching, heave, people can study carrier-borne stable platform by this device.
Accompanying drawing explanation
Below in conjunction with accompanying drawing and specific implementation method, the present invention will be further described in detail.
Fig. 1 is the structural representation of a kind of carrier-borne stable platform simulation test device of the utility model.
Fig. 2 is the stereographic map of a kind of carrier-borne stable platform simulation test device of the utility model.
Fig. 3 is the structural representation of the ear type joint II 2 of a kind of carrier-borne stable platform simulation test device of the utility model.
Fig. 4 is the side view of the ear type joint II 2 of a kind of carrier-borne stable platform simulation test device of the utility model.
Fig. 5 is the structural representation of the electric cylinder I 3 of a kind of carrier-borne stable platform simulation test device of the utility model.
Fig. 6 is the side view of the electric cylinder I 3 of a kind of carrier-borne stable platform simulation test device of the utility model.
In figure: platform I 1; Ear type joint I 2; Floor I 2-1; Hole I 2-1-1; Hole I 2-2; Electric cylinder I 3; Screw rod I 3-1; Upper hole I 3-1-1; Lower opening I 3-2; Ear type joint II 4; Ear type joint III 5; Electric cylinder II 6; Ear type joint IV 7; Ear type joint V 8; Electric cylinder III 9; Ear type joint VI 10; Framework platform 11; Ear type joint VII 12; Electric cylinder IV 13; Ear type joint VIII 14; Platform II 15; Column 16; Ear type joint Ⅸ 17; Electric cylinder V 18; Ear type joint Ⅹ 19; Ear type joint Ⅺ 20; Electric cylinder VI 21; Ear type joint Ⅻ 22.
Embodiment
At Fig. 1, 2, 3, 4, 5, in 6, the utility model relates to a kind of carrier-borne Study system, more specifically to the carrier-borne stable platform simulation test device of one, comprise platform I 1, ear type joint I 2, electric cylinder I 3, ear type joint II 4, ear type joint III 5, electric cylinder II 6, ear type joint IV 7, ear type joint V 8, electric cylinder III 9, ear type joint VI 10, framework platform 11, ear type joint VII 12, electric cylinder IV 13, ear type joint VIII 14, platform II 15, column 16, ear type joint Ⅸ 17, electric cylinder V 18, ear type joint Ⅹ 19, ear type joint Ⅺ 20, electric cylinder VI 21 and ear type joint Ⅻ 22, ship rolling can be simulated, pitching, the motion states such as heave, people can study carrier-borne stable platform by this device.
Ear type joint I 2, ear type joint III 5 and ear type joint V 8 are all bolted bottom platform I 1.Ear type joint II 4, ear type joint IV 7 and ear type joint VI 10 are welded to connect at framework platform 11 top.The center line of upper hole I 3-1-1 on screw rod I 3-1 in electric cylinder I 3 is mutually vertical with the center line of lower opening I 3-2, electric cylinder I 3 upper end is connected by bolt with ear type joint I 2, and upper hole I 3-1-1 matches with hole I 2-1-1, lower end is connected with ear type joint II 4, so ear type joint I 2 and ear type joint II 4 are also mutual at right angle settings, ear type joint I 2 and ear type joint II 4 had both served the effect of fixing electric cylinder, serve again the effect of universal joint, to ensure that electric cylinder I 3 can free movement and card does not occur within the scope of certain limit.Electric cylinder II 6 upper end is connected with ear type joint III 5, and lower end is connected with ear type joint IV 7.Electric cylinder III 9 upper end is connected with ear type joint V 8, and lower end is connected with ear type joint VI 10.Electric cylinder I 3 and electric cylinder III 9 are positioned at framework platform 11 two Angle Position on one side, electric cylinder II 6 is positioned at the centre of the opposite side on electric cylinder I 3 and limit, electric cylinder III 9 place, and platform I 1 can be made in the screw rod lifting process in electric cylinder I 3, electric cylinder II 6 and electric cylinder III 9 to keep horizontality.
Ear type joint VII 12, ear type joint Ⅸ 17 and ear type joint Ⅻ 22 are all welded to connect in the bottom of framework platform 11.Ear type joint VIII 14, ear type joint Ⅹ 19 and ear type joint Ⅺ 20 are all bolted with platform II 15.Electric cylinder IV 13 upper end is connected with ear type joint VII 12, and lower end is connected with ear type joint VIII 14.Electric cylinder V 18 upper end is connected with ear type joint Ⅸ 17, and lower end is connected with ear type joint Ⅹ 19.Electric cylinder VI 21 upper end is connected with ear type joint Ⅻ 22, and lower end is connected with ear type joint Ⅺ 20.Electric cylinder IV 13, electric cylinder V 18 and electric cylinder VI 21 are fixed between framework platform 11 and platform II 15.Column is welded on bottom platform II 15 and plays a supportive role.
When the screw rod in the screw rod in electric cylinder IV 13, electric cylinder V 18 and the screw rod in electric cylinder VI 21 constantly move up and down, and the height of three screw rod rise and fall is all different, framework platform 11 then can be made to do rolling, pitching and heave movement, thus the rolling of simulation boats and ships, pitching and heave, the dip angle signal that framework platform produces records through obliquity sensor and imports in single-chip microcomputer after A/D conversion, single-chip microcomputer carries out certain process to the data sent back, through pid control algorithm, export a control signal, be given to motor driver, after motor driver receives control signal, control electric cylinder I 3, motor action in electric cylinder II 6 and electric cylinder III 9, electric cylinder I 3 can be made, screw rod in electric cylinder II 6 and electric cylinder III 9 does corresponding rise and fall campaign, screw rod I 3-1 in electric cylinder I 3 is identical with the height of the screw rod rise and fall in electric cylinder VI 21 and synchronous, screw rod in electric cylinder II 6 is identical with the height of the screw rod rise and fall in electric cylinder V 18 and synchronous, screw rod in electric cylinder III 9 is identical with the height of the screw rod rise and fall in electric cylinder IV 13 and synchronous, so can ensure no matter how framework platform 11 moves, platform I 1 all remains level and highly constant, simulate ship rolling, pitching, the stationarity of boats and ships upper mounting plate in heave process.
A kind of carrier-borne stable platform simulation test device of the utility model, by the motion simulation ship rolling of electric cylinder IV 13, electric cylinder V 18 and electric cylinder VI 21, pitching, heave movement, the angle of inclination of obliquity sensor real-time detection block body panel roll and pitch, the dip angle signal that obliquity sensor collection is returned, through computing input control device, export control signal, drive the motion of electric cylinder I 3, electric cylinder II 6 and electric cylinder III 9, the motion of compensating analog boats and ships constantly, make platform I 1 maintenance level motionless, and then reach the effect of stable platform I 1.
Certain above-mentioned explanation is not limitation of the utility model; the utility model is also not limited only to above-mentioned citing; the change that those skilled in the art make in essential scope of the present utility model, remodeling, interpolation or replacement, also belong to protection domain of the present utility model.
Claims (10)
1. a carrier-borne stable platform simulation test device, comprise platform I (1), ear type joint I (2), electric cylinder I (3), ear type joint II (4), ear type joint III (5), electric cylinder II (6), ear type joint IV (7), ear type joint V (8), electric cylinder III (9), ear type joint VI (10), framework platform (11), ear type joint VII (12), electric cylinder IV (13), ear type joint VIII (14), platform II (15), column (16), ear type joint Ⅸ (17), electric cylinder V (18), ear type joint Ⅹ (19), ear type joint Ⅺ (20), electric cylinder VI (21) and ear type joint Ⅻ (22), it is characterized in that: ear type joint I (2), ear type joint III (5) and ear type joint V (8) are all bolted in platform I (1) bottom, ear type joint II (4), ear type joint IV (7) and ear type joint VI (10) are all connected to framework platform (11) top, electric cylinder I (3) upper end is connected with ear type joint I (2), and lower end is connected with ear type joint II (4), electric cylinder II (6) upper end is connected with ear type joint III (5), and lower end is connected with ear type joint IV (7), electric cylinder III (9) upper end is connected with ear type joint V (8), and lower end is connected with ear type joint VI (10), ear type joint VII (12), ear type joint Ⅸ (17) and ear type joint Ⅻ (22) are all connected to the bottom of framework platform (11), ear type joint VIII (14), ear type joint Ⅹ (19) and ear type joint Ⅺ (20) are all bolted at the top of platform II (15), electric cylinder IV (13) upper end is connected with ear type joint VII (12), and lower end is connected with ear type joint VIII (14), electric cylinder V (18) upper end is connected with ear type joint Ⅸ (17), and lower end is connected with ear type joint Ⅹ (19), electric cylinder VI (21) upper end is connected with ear type joint Ⅻ (22), and lower end is connected with ear type joint Ⅺ (20), column (16) is welded on platform II (15) bottom.
2. the carrier-borne stable platform simulation test device of one according to claim 1, it is characterized in that: the hole I (2-1-1) on the floor I (2-1) on described ear type joint I (2) cooperatively interacts with the upper hole I (3-1-1) on the screw rod I (3-1) in electric cylinder I (3), ear type joint I (2) and electric cylinder I (3) are fixed through the hole I (2-1-1) on floor I (2-1) and the upper hole I (3-1-1) on screw rod I (3-1) by bolt, and use nut screwing clamping bolt.
3. the carrier-borne stable platform simulation test device of one according to claim 2, is characterized in that: the center line in the upper hole I (3-1-1) on described screw rod I (3-1) is mutually vertical with the center line of lower opening I (3-2).
4. the carrier-borne stable platform simulation test device of one according to claim 1, is characterized in that: described electric cylinder I (3) and electric cylinder III (9) are positioned at two Angle Position of framework platform (11).
5. the carrier-borne stable platform simulation test device of one according to claim 1, is characterized in that: described electric cylinder II (6) is positioned at the centre of the opposite side on electric cylinder I (3) and electric cylinder III (9) limit, place.
6. the carrier-borne stable platform simulation test device of one according to claim 1, is characterized in that: described ear type joint II (4), ear type joint IV (7) and ear type joint VI (10) are all welded to connect with framework platform (11).
7. the carrier-borne stable platform simulation test device of one according to claim 1, is characterized in that: described ear type joint VII (12), ear type joint Ⅸ (17) and ear type joint Ⅻ (22) are all welded to connect with framework platform (11).
8. the carrier-borne stable platform simulation test device of one according to claim 1, is characterized in that: described electric cylinder IV (13) and electric cylinder VI (21) be positioned at framework platform (11) two jiaos.
9. the carrier-borne stable platform simulation test device of one according to claim 1, is characterized in that: described electric cylinder V (18) is positioned in the middle of the opposite side on electric cylinder IV (13) and electric cylinder VI (21) limit, place.
10. the carrier-borne stable platform simulation test device of one according to claim 1, is characterized in that: described electric cylinder I (3) and electric cylinder V (18) are positioned at framework platform (11) two relative edge.
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CN201420688267.XU CN204188962U (en) | 2014-11-17 | 2014-11-17 | A kind of carrier-borne stable platform simulation test device |
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CN201420688267.XU CN204188962U (en) | 2014-11-17 | 2014-11-17 | A kind of carrier-borne stable platform simulation test device |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
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CN105955068A (en) * | 2016-06-14 | 2016-09-21 | 大连海事大学 | Ship-borne stable platform experiment system and working method thereof |
CN108279576A (en) * | 2017-12-26 | 2018-07-13 | 湖北航天技术研究院总体设计所 | A kind of composite shaft target following emulation test system |
CN108303245A (en) * | 2018-02-28 | 2018-07-20 | 华中科技大学 | A kind of frame-type heave compensator test platform |
CN113353207A (en) * | 2021-06-03 | 2021-09-07 | 上海海事大学 | Comprehensive sea condition testing device for medical pod equipment of ship |
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2014
- 2014-11-17 CN CN201420688267.XU patent/CN204188962U/en not_active Expired - Fee Related
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105955068A (en) * | 2016-06-14 | 2016-09-21 | 大连海事大学 | Ship-borne stable platform experiment system and working method thereof |
CN108279576A (en) * | 2017-12-26 | 2018-07-13 | 湖北航天技术研究院总体设计所 | A kind of composite shaft target following emulation test system |
CN108279576B (en) * | 2017-12-26 | 2021-09-28 | 湖北航天技术研究院总体设计所 | Compound axle target tracking simulation test system |
CN108303245A (en) * | 2018-02-28 | 2018-07-20 | 华中科技大学 | A kind of frame-type heave compensator test platform |
CN108303245B (en) * | 2018-02-28 | 2024-04-02 | 华中科技大学 | Frame type heave compensation device test platform |
CN113353207A (en) * | 2021-06-03 | 2021-09-07 | 上海海事大学 | Comprehensive sea condition testing device for medical pod equipment of ship |
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CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150304 Termination date: 20151117 |