CN105716840A - Ship-borne stabilized platform simulation experiment device - Google Patents
Ship-borne stabilized platform simulation experiment device Download PDFInfo
- Publication number
- CN105716840A CN105716840A CN201410733528.XA CN201410733528A CN105716840A CN 105716840 A CN105716840 A CN 105716840A CN 201410733528 A CN201410733528 A CN 201410733528A CN 105716840 A CN105716840 A CN 105716840A
- Authority
- CN
- China
- Prior art keywords
- electric cylinder
- type joint
- ear type
- platform
- ear
- 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
Landscapes
- Testing Electric Properties And Detecting Electric Faults (AREA)
Abstract
The invention discloses a ship-borne stabilized platform simulation experiment device. A platform I, a frame platform and a platform II form two layers, and an electric cylinder I, an electric cylinder II and an electric cylinder III are disposed between the platform I and the frame platform through ear-shaped connectors. Similarly, an electric cylinder IV, an electric cylinder V and an electric cylinder VI are disposed between the platform II and the frame platform through ear-shaped connectors. The device simulates the rolling and pitching and rising and falling movement of a ship through the movement of the electric cylinder IV, the electric cylinder V and the electric cylinder VI. A tilt angle sensor detects the tilt angles of the rolling and pitching of the frame platform in real time, and the tilt angle signals collected by the tilt angle sensor is calculated and processed and inputted into a controller. A control signal is outputted to drive the electric cylinder I, the electric cylinder II and the electric cylinder III to move, thereby achieving the continuous compensation and simulation of the movement of the ship, enabling the platform I to remain level and stationary, and achieving an effect of stabilizing the platform I.
Description
Technical field
The present invention relates to a kind of carrier-borne Study system, more specifically to a kind of carrier-borne stabilized platform simulation test device.
Background technology
By the effect of wave agitation factor, naval vessel at sea can produce the effect of rolling, pitching, yawing, swaying, surging, 6 degree of freedom of heave.This motion brings serious impact to the launch accuracy and boats and ships seaborne supply etc. of the landing safety of carrier-based helicopter, shipborne weapon.For adapting to the requirement of the military strategy for the new period, improve the ability that armament is at sea fought, it is very necessary therefore its platform stable systematic research just to be become and there is strategic importance.In addition, carrier-borne stabilized platform can also be applied in ocean engineering field, and 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 prominent achievement especially, and external research mostly is military concerning security matters project, so seeing that just more highlighting us studies the significance of this stabilized platform from this point on.
Summary of the invention
What present invention mainly solves technical problem is that: provide a kind of carrier-borne stabilized platform simulation test device, it is possible to the kinestates such as simulation ship rolling, pitching, heave, people can study carrier-borne stabilized platform by this device.
For solving above-mentioned technical problem, present invention employs techniques below scheme:
A kind of carrier-borne stabilized platform simulation test device, including platform I, ear type joint I, ear type joint III, ear type joint V, electric cylinder I, electric cylinder II, electric cylinder III, ear type joint IV, ear type joint V, ear type joint VI, framework platform, ear type joint VII, ear type joint Ⅸ, ear type joint Ⅻ, electric cylinder IV, electric cylinder V, electric cylinder VI, ear type joint VIII, ear type joint Ⅹ, ear type joint Ⅺ, platform II and column
Ear type joint I, ear type joint III and ear type joint V are each through being bolted to bottom platform I；Ear type joint II, ear type joint IV and ear type joint VI are both 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 both connected to the bottom of framework platform；Ear type joint VIII, ear type joint Ⅹ and ear type joint Ⅺ are each through the top being bolted to 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 welded on bottom platform II.
Further, hole I on floor I on described ear type joint I cooperates with the upper hole I on the screw rod I in electric cylinder I, ear type joint I and electric cylinder I are fixed by bolt through the hole I on floor I and the upper hole I on screw rod I, and use nut screwing clamping bolt.
Further, the centrage in upper hole I on described screw rod I and the centrage of lower opening I are mutually perpendicular to.
Further, described electric cylinder I and electric cylinder III are positioned at two Angle Position of framework platform.
Further, described electric cylinder II is positioned at the centre of the opposite side on electric cylinder I and limit, electric cylinder III place.
Further, described electric cylinder IV and electric cylinder VI be positioned at framework platform two jiaos.
Further, described electric cylinder V is positioned in the middle of the opposite side on electric cylinder IV and limit, electric cylinder VI place.
Further, described electric cylinder I and electric cylinder V are positioned at framework platform two relative edge.
The invention have the advantage that
Present configuration is simple, and degree of freedom is big, it is possible to the kinestates such as simulation ship rolling, pitching, heave, people can study carrier-borne stabilized platform by this device.
Accompanying drawing explanation
Fig. 1 is the structural representation of a kind of carrier-borne stabilized platform simulation test device of the present invention.
Fig. 2 is the axonometric chart of a kind of carrier-borne stabilized platform simulation test device of the present invention.
Fig. 3 is the structural representation of the ear type joint II of a kind of carrier-borne stabilized platform simulation test device of the present invention.
Fig. 4 is the side view of the ear type joint II of a kind of carrier-borne stabilized platform simulation test device of the present invention.
Fig. 5 is the structural representation of the electric cylinder I of a kind of carrier-borne stabilized platform simulation test device of the present invention.
Fig. 6 is the side view of the electric cylinder I of a kind of carrier-borne stabilized platform simulation test device of the present invention.
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.
Detailed description of the invention
As shown in Fig. 1,2,3,4,5 and 6, a kind of carrier-borne stabilized platform simulation test device, including platform I 1, ear type joint I 2, ear type joint III 5, ear type joint V 8, electric cylinder I 3, electric cylinder II 6, electric cylinder III 9, ear type joint II 4, ear type joint IV 7 and ear type joint VI 10, framework platform 11, ear type joint VII 12, ear type joint Ⅸ 17, ear type joint Ⅻ 22, electric cylinder IV 13, electric cylinder V 18, electric cylinder VI 21, ear type joint VIII 14, ear type joint Ⅹ 19, ear type joint Ⅺ 20, platform II 15 and column 16；
Ear type joint I 2, ear type joint III 5 and ear type joint V 8 are each through being bolted to bottom platform I 1；Ear type joint II 4, ear type joint IV 7 and ear type joint VI 10 are both 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 both 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 each through the top being bolted to 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 bottom platform II 15.
Further, hole I 2-1-1 on floor I 2-1 on described ear type joint I 2 cooperates with upper hole I 3-1-1 on screw rod I 3-1 in electric cylinder I 3, ear type joint I 2 and electric cylinder I 3 are fixed by bolt through hole I 2-1-1 on floor I 2-1 and upper hole I 3-1-1 on screw rod I 3-1, and use nut screwing clamping bolt.
Further, the centrage of upper hole I 3-1-1 on described screw rod I 3-1 and the centrage of lower opening I 3-2 are mutually perpendicular to.
Further, described electric cylinder I 3 and electric cylinder III 9 are positioned at two Angle Position of framework platform 11.
Further, described 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.
Further, described electric cylinder IV 13 and electric cylinder VI 21 be positioned at framework platform 11 two jiaos.
Further, described electric cylinder V 18 is positioned in the middle of the opposite side on electric cylinder IV 13 and limit, electric cylinder VI 21 place.
Further, described electric cylinder I 3 and electric cylinder V 18 are positioned at 11 liang of relative edges of framework platform.
Operation principle and process:
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 centrage of upper hole I 3-1-1 on screw rod I 3-1 in electric cylinder I 3 and the centrage of lower opening I 3-2 are mutually perpendicular to, 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 be mutually perpendicular to installation, 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, with ensure electric cylinder I 3 can within the scope of certain limit freely-movable and there is not card.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, can so that platform I 1 keeps level in the screw rod lifting process in electric cylinder I 3, electric cylinder II 6 and electric cylinder III 9.
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 simulating the rolling of boats and ships, pitching and heave, the dip angle signal that framework platform produces records and in incoming single-chip microcomputer after A/D changes through obliquity sensor；The single-chip microcomputer data to sending back carry out certain process, through pid control algorithm, export a control signal, it is 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 synchronizes, 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 synchronizes, 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 synchronizes, so can ensure that 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.
By electric cylinder IV 13, electric cylinder V 18 and the motion simulation ship rolling of electric cylinder VI 21, pitching, heave movement, the angle of inclination of the real-time detection block body panel roll and pitch of obliquity sensor, the dip angle signal that obliquity sensor collection is returned, controller is inputted through computing, output control signal, drives electric cylinder I 3, electric cylinder II 6 and electric cylinder III 9 motion, compensates the motion of simulation boats and ships constantly, make platform I 1 maintenance level motionless, and then reach the effect of stabilized platform I 1.
Claims (8)
1. a carrier-borne stabilized platform simulation test device, including platform I, ear type joint I, ear type joint III, ear type joint V, electric cylinder I, electric cylinder II, electric cylinder III, ear type joint IV, ear type joint V, ear type joint VI, framework platform, ear type joint VII, ear type joint Ⅸ, ear type joint Ⅻ, electric cylinder IV, electric cylinder V, electric cylinder VI, ear type joint VIII, ear type joint Ⅹ, ear type joint Ⅺ, platform II and column, it is characterised in that:
Ear type joint I, ear type joint III and ear type joint V are each through being bolted to bottom platform I；Ear type joint II, ear type joint IV and ear type joint VI are both 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 both connected to the bottom of framework platform；Ear type joint VIII, ear type joint Ⅹ and ear type joint Ⅺ are each through the top being bolted to 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 welded on bottom platform II.
2. the carrier-borne stabilized platform simulation test device of one according to claim 1, it is characterized in that: the hole I on the floor I on described ear type joint I cooperates with the upper hole I on the screw rod I in electric cylinder I, ear type joint I and electric cylinder I are fixed by bolt through the hole I on floor I and the upper hole I on screw rod I, and use nut screwing clamping bolt.
3. the carrier-borne stabilized platform simulation test device of one according to claim 1, it is characterised in that: the centrage in the upper hole I on described screw rod I and the centrage of lower opening I are mutually perpendicular to.
4. the carrier-borne stabilized platform simulation test device of one according to claim 1, it is characterised in that: described electric cylinder I and electric cylinder III are positioned at two Angle Position of framework platform.
5. the carrier-borne stabilized platform simulation test device of one according to claim 1, it is characterised in that: described electric cylinder II is positioned at the centre of the opposite side on electric cylinder I and limit, electric cylinder III place.
6. the carrier-borne stabilized platform simulation test device of one according to claim 1, it is characterised in that: described electric cylinder IV and electric cylinder VI be positioned at framework platform two jiaos.
7. the carrier-borne stabilized platform simulation test device of one according to claim 1, it is characterised in that: described electric cylinder V is positioned in the middle of the opposite side on electric cylinder IV and limit, electric cylinder VI place.
8. the carrier-borne stabilized platform simulation test device of one according to claim 1, it is characterised in that: described electric cylinder I and electric cylinder V are positioned at framework platform two relative edge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410733528.XA CN105716840A (en) | 2014-12-04 | 2014-12-04 | Ship-borne stabilized platform simulation experiment device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410733528.XA CN105716840A (en) | 2014-12-04 | 2014-12-04 | Ship-borne stabilized platform simulation experiment device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105716840A true CN105716840A (en) | 2016-06-29 |
Family
ID=56143552
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410733528.XA Pending CN105716840A (en) | 2014-12-04 | 2014-12-04 | Ship-borne stabilized platform simulation experiment device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105716840A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106991865A (en) * | 2017-02-09 | 2017-07-28 | 沈阳工业大学 | Slide block connecting rod tilter |
| CN107014631A (en) * | 2017-03-20 | 2017-08-04 | 中国船舶科学研究中心（中国船舶重工集团公司第七0二研究所） | Lift by crane Hardware-in-loop Simulation Experimentation device in a kind of deep-sea |
| CN108303245A (en) * | 2018-02-28 | 2018-07-20 | 华中科技大学 | A kind of frame-type heave compensator test platform |
| CN111111807A (en) * | 2019-12-30 | 2020-05-08 | 武昌船舶重工集团有限公司 | Ship experiment platform |
-
2014
- 2014-12-04 CN CN201410733528.XA patent/CN105716840A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106991865A (en) * | 2017-02-09 | 2017-07-28 | 沈阳工业大学 | Slide block connecting rod tilter |
| CN107014631A (en) * | 2017-03-20 | 2017-08-04 | 中国船舶科学研究中心（中国船舶重工集团公司第七0二研究所） | Lift by crane Hardware-in-loop Simulation Experimentation device in a kind of deep-sea |
| 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 |
| CN111111807A (en) * | 2019-12-30 | 2020-05-08 | 武昌船舶重工集团有限公司 | Ship experiment platform |
| CN111111807B (en) * | 2019-12-30 | 2021-11-30 | 武昌船舶重工集团有限公司 | Ship experiment platform |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105047041B (en) | Wave heaves systems stabilisation and its control method | |
| CN105716840A (en) | Ship-borne stabilized platform simulation experiment device | |
| CN104890830B (en) | Deep water dynamic positioning semisubmersible platform tuning heave plate, which subtracts to shake to subtract, swings control system | |
| CN204188962U (en) | A kind of carrier-borne stable platform simulation test device | |
| US20210247419A1 (en) | Ship Real Wind Measuring Device Calibration Method | |
| CN2887748Y (en) | Underwater robot for underwater monitoring platform | |
| CN109733530B (en) | Series-parallel connection six-degree-of-freedom active wave compensation platform | |
| CN106828886A (en) | A kind of aircraft center of gravity dynamically balancing device | |
| CN103935482A (en) | Automatic navigation control system improving seakeeping performance of ship | |
| GB201207999D0 (en) | Offshore aquaculture system | |
| CN107600354A (en) | A kind of flow-disturbing system for reducing ship rolling motion | |
| CN102904017B (en) | Hemispherical work spatial domain parallel antenna structure system | |
| CN104149959A (en) | Sea glider driven by wave force | |
| CN109094817B (en) | Carrier-based helicopter self-adaptive landing gear landing simulation system | |
| CN105689174A (en) | Automatic ship spraying robot | |
| CN110937076B (en) | Ship comfort control system based on model prediction design of two-channel parameters and control method thereof | |
| CN105022414B (en) | A kind of multifunctional control method and control device suitable for Swaying Test Platform | |
| CN107942731A (en) | A kind of walkaround active wave compensating device and method based on prediction | |
| CN110568814A (en) | Wave signal simulation device suitable for active heave compensation | |
| CN202923841U (en) | Boarding ladder | |
| CN203332373U (en) | Underwater platform with automatic horizontal adjustment function | |
| CN112798224B (en) | Ship model plane motion measurement method | |
| CN201882244U (en) | Open shelf type fluctuation towed vehicle close to sea bottom | |
| CN106769153B (en) | Ship's crane automatic experiment system | |
| CN204008006U (en) | A kind of pipeline internal force balance system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160629 |