CN112709777A - Damping platform and damping method - Google Patents
Damping platform and damping method Download PDFInfo
- Publication number
- CN112709777A CN112709777A CN202011400355.1A CN202011400355A CN112709777A CN 112709777 A CN112709777 A CN 112709777A CN 202011400355 A CN202011400355 A CN 202011400355A CN 112709777 A CN112709777 A CN 112709777A
- Authority
- CN
- China
- Prior art keywords
- platform
- vibration isolation
- flywheel
- damping
- flywheels
- 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
- 238000013016 damping Methods 0.000 title claims abstract description 64
- 238000000034 method Methods 0.000 title claims abstract description 13
- 238000002955 isolation Methods 0.000 claims abstract description 61
- 230000035939 shock Effects 0.000 claims description 25
- 229910000831 Steel Inorganic materials 0.000 claims description 3
- 239000010959 steel Substances 0.000 claims description 3
- 238000013461 design Methods 0.000 abstract description 5
- 230000000903 blocking effect Effects 0.000 abstract description 2
- 230000004044 response Effects 0.000 abstract description 2
- 238000010521 absorption reaction Methods 0.000 description 4
- 230000001276 controlling effect Effects 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000001259 photo etching Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/002—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion characterised by the control method or circuitry
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/022—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using dampers and springs in combination
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/023—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means
- F16F15/0232—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using fluid means with at least one gas spring
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
- F16F15/046—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means using combinations of springs of different kinds
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/02—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems
- F16F15/04—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means
- F16F15/06—Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems using elastic means with metal springs
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M5/00—Engine beds, i.e. means for supporting engines or machines on foundations
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2230/00—Purpose; Design features
- F16F2230/08—Sensor arrangement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F2230/00—Purpose; Design features
- F16F2230/18—Control arrangements
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The invention relates to a damping platform and a damping method, wherein the damping platform comprises a passive vibration isolation device, a flywheel damping device connected with the passive vibration isolation device and a control system electrically connected with the passive vibration isolation device and the flywheel damping device, the flywheel damping device comprises a box body for supporting a precision instrument and at least three flywheels arranged in the box body, the shells of the three flywheels are fixedly abutted against the inner wall of the box body, the central axes of the three flywheels are not parallel, the control system comprises a plurality of sensors and a controller electrically connected with the sensors, and the controller is electrically connected with the flywheels. Through the mode, the control bandwidth of the damping platform for blocking external vibration completely depends on the motor and the control system in the flywheel, the performance of the damping platform at low frequency, medium frequency and high frequency is strong, the torque of the flywheel depends on the motor and the driving design of the motor, the damping platform can be changed in size and freely, and the damping platform has strong adaptability and timely response to equipment with different sizes.
Description
Technical Field
The invention relates to the technical field of shock absorption, in particular to a shock absorption platform and a shock absorption method.
Background
On ships in various fields of application, it is common to equip the ships with high-precision equipment that is very sensitive to shock disturbances. These devices are extremely sensitive to external shock disturbances due to their very high accuracy of operation or measurement. The disturbance of the instrument in the direction of the vessel's shake is particularly acute due to the nature of the vessel's operation. This violent shaking can have a significant effect on the performance of the instrument, even in operation.
At present, two methods are mainly used for shock absorption of precision instruments: a passive vibration isolation device is adopted, and a spring and a damper are applied to isolate the influence of the vibration of a ship body on an instrument; adopt the vibration isolation revolving stage based on parallel mechanism.
As shown in fig. 1, the vibration isolation device using a spring and a damper can only reduce external vibration interference of a certain frequency or more due to the limitation of its operation principle, and theoretically cannot eliminate all external vibration influences. Thus, the external interference elimination effect on low frequency is poor; in addition, after the external vibration disappears, the system has residual vibration due to the characteristic of underdamping of the spring vibration isolation system.
As shown in fig. 2, in order to adopt the vibration isolation turntable based on the parallel mechanism, since 6 or more link mechanisms are required to shield the external vibration of the supported object, the control manner is complicated; in addition, because the driving force of the linear motor is small, a hydraulic connecting rod is required to be adopted for large-scale equipment, and the high-frequency vibration isolation response of the system is poor.
Based on this, it is desirable to provide a new shock absorbing platform and a shock absorbing method to solve the existing problems.
Disclosure of Invention
Based on the above, the invention provides a damping platform and a damping method, which are used for realizing better isolation effect on external shaking (angle) vibration.
The invention provides a shock-absorbing platform, comprising:
a passive vibration isolation device arranged on the deck, a flywheel damping device connected with the passive vibration isolation device and a control system electrically connected with the passive vibration isolation device and the flywheel damping device,
the flywheel damping device comprises a box body for supporting the precision instrument and at least three flywheels arranged in the box body, the shells of the three flywheels are abutted and fixed with the inner wall of the box body, the central shafts of the three flywheels are not parallel,
the control system comprises a plurality of sensors and a controller electrically connected with the sensors, and the controller is electrically connected with the flywheel.
Preferably, the central axes of three said flywheels intersect at a point.
Preferably, the central shafts of the three flywheels are arranged vertically in pairs.
Preferably, the box body is connected with the passive damping device in a ball hinge mode.
Preferably, the base of the box body, which is close to one side of the passive damping device, is a vertical cone, the vertex of the vertical cone is spherical, and the passive damping device is provided with a hinged shaft seat hinged with the vertex of the cone.
Preferably, the base of the box body on one side close to the passive damping device is a spherical surface, and the spherical surface is abutted and fixed with the passive damping device.
Preferably, the central axes of the three flywheels pass through the spherical center of the spherical surface.
Preferably, the passive vibration isolation device comprises a support platform, a plurality of vibration isolators uniformly arranged on one side of the support platform and dampers connected with the vibration isolators in series one by one, and the box body is arranged on the support platform.
Preferably, the vibration isolator comprises an air spring or a steel spring.
The invention also provides a damping method for the precise instrument, which comprises the following steps
Collecting a first sensing signal of the passive vibration isolation device, which is vibrated by a ship deck;
controlling the passive vibration isolation device according to the first sensing signal;
collecting a second sensing signal which passes through the passive vibration isolation device and then enters the flywheel damping device;
and controlling the rotating speeds of at least three flywheels according to the second sensing signals.
The invention has the beneficial effects that the damping platform comprises a passive vibration isolation device arranged on a deck, a flywheel damping device connected with the passive vibration isolation device and a control system electrically connected with the passive vibration isolation device and the flywheel damping device, wherein the flywheel damping device comprises a box body for supporting the precision instrument and at least three flywheels arranged in the box body, the shells of the three flywheels are fixedly abutted against the inner wall of the box body, the central shafts of the three flywheels are not parallel, the control system comprises a plurality of sensors and a controller electrically connected with the sensors, and the controller is electrically connected with the flywheels. Through the mode, the control bandwidth of the damping platform for blocking external vibration completely depends on the motor and the control system in the flywheel, the damping platform has excellent performance in low frequency, medium frequency and high frequency, and meanwhile, the torque of the flywheel completely depends on the motor and the driving design thereof, so that the damping platform can be changed in size and freely, has strong adaptability to different sizes of equipment and can respond in time.
Drawings
Fig. 1 is a schematic structural view of a first vibration isolating device in the prior art;
fig. 2 is a schematic structural view of a second vibration isolating device in the prior art;
FIG. 3 is a schematic view of a first structure of a damping platform according to an embodiment of the present invention;
FIG. 4 is a second structural diagram of a damping platform according to an embodiment of the present invention;
the meaning of the reference symbols in the drawings is: a shock absorbing platform 100; a passive vibration isolation device 1; a support table 11; the vibration isolator 12; a damper 13; a flywheel damping device 2; a case 21; a base 211; a cone apex 212; hinge shaft base 213; a flywheel 22; a control system 3; a precision instrument 200.
Detailed Description
To facilitate an understanding of the invention, the invention will now be described more fully with reference to the accompanying drawings. Preferred embodiments of the present invention are shown in the drawings. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention.
Referring to fig. 3 and 4, fig. 3 and 4 are two schematic structural views of a shock absorbing platform according to an embodiment of the present invention, in which the shock absorbing platform 100 is disposed on a deck of a ship and used for placing a precision instrument 200 on the ship to prevent the precision instrument 200 from being affected by external vibration. As shown in fig. 3, the vibration isolation platform 100 includes a passive vibration isolation device 1 disposed on a deck of a ship, a flywheel vibration isolation device 2 connected to the passive vibration isolation device 1, and a control system 3 electrically connected to the passive vibration isolation device 1 and the flywheel vibration isolation device 2.
The passive vibration isolation device 1 is arranged on a deck of a ship, and the passive vibration isolation device 1 comprises a supporting table 11, a plurality of vibration isolators 12 uniformly arranged on one side of the supporting table 11, and dampers 13 connected with the vibration isolators 12 in series one by one. Preferably, the vibration isolator 12 comprises an air spring or a steel spring. Flywheel damping device 2 is including supporting precision instrument 200's box 21 and locating at least three flywheel 22 in the box 21, box 21 is fixed in on the brace table 11, the shell of flywheel 22 with the inner wall butt of box 21 is fixed, and three the center pin of flywheel 22 is all unparallel, so that it is three flywheel 22 decouples along three direction along the rotation torque of rotation axis (center pin). The control system 3 comprises a plurality of sensors and a controller electrically connected with the sensors, and the controller is electrically connected with the flywheel. The sensors are respectively arranged on one side of the passive vibration isolation device 1, which is in contact with a ship deck, and are used for detecting a first sensing signal of external vibration; and the second sensing signal detection device is also arranged at the joint of the passive vibration isolation device 1 and the flywheel damping device 2, namely the joint of the box body and the support platform 11, and is used for detecting a second driving sensing signal entering the flywheel damping device 2 after being subjected to vibration isolation through the passive vibration isolation device 1. Preferably, the central axes of three of the flywheels 22 intersect at a point. Preferably, the central shafts of the three flywheels 22 are arranged vertically in pairs, so that decoupling is facilitated, and control and calculation of the platform are facilitated.
In the flywheel damping device 2 of the present invention, when the motor in the flywheel 22 performs acceleration and deceleration movement on the rotating flywheel, the flywheel stator and the housing need to apply a moment to the flywheel, according to the third law of newton, the flywheel housing must simultaneously bear a moment in the opposite direction, and the moment must be borne by the passive vibration isolation device 1 connected with the flywheel damping device 2. Therefore, by accelerating and decelerating the flywheel 22, the system can generate a corresponding controllable torque in the direction of the rotation axis (i.e. the central axis) of the flywheel 22 by using the principle to counteract the influence of the driving torque on the precision instrument 200 in the direction after passing through the passive vibration isolation device 1. Since the vibrations of the precision instrument 200 are caused by external forces and torques, maintaining zero rotation of the platform in this axial direction keeps the precision instrument 200 stationary in this axial direction. Since there are three directions for the external shaking vibrations, the system provides three flywheels 22 to meet the vibration isolation requirements on the three angular axes. The flywheel damping device 2 is matched with the passive vibration isolation device 1 for use, so that the bandwidth limitation of the passive vibration isolation device 1 can be completely eliminated, the swing of the precision instrument 200 is completely eliminated, and meanwhile, the linear vibration is greatly weakened.
According to the damping platform 100, firstly, vibration on a ship is damped for the first time through the passive vibration isolation device 1, external vibration interference above a certain frequency can be weakened, and then the weakened transmission and the vibration with lower frequency are damped through the flywheel damping device 2 so as to offset the influence of all external vibration. The damping effect of the flywheel damping device 2 in the damping platform 100 is mainly determined by the torque of the motors in the three flywheels 22, and the torque of the motors completely depends on the driving design of the motors and the driving design of the motors, so that the motors can be changed in size and freely.
In an optional embodiment, in order to facilitate the decoupling of the shaking vibration control and the linear vibration, the angle pose of the passive vibration isolation device 1 is completely controlled by the flywheel, and the angle pose can be controlled outside the vibration isolation function, that is, the pitching angle of the precision instrument 200 can be precisely driven to move. The base of the box 21 close to the supporting table 11 in the flywheel damping device 2 is connected with the supporting table 11 in the passive vibration isolation device 1 in a ball hinge manner, and with reference to fig. 3, the base 211 of the box 21 close to the supporting table 11 is a cone, the conical top 212 of the cone is processed into a sphere, and the supporting table 11 is provided with a hinge shaft seat 213 hinged with the conical top 212, so that the flywheel damping device 2 is hinged with the passive vibration isolation device 1.
In an alternative embodiment, in consideration of cost control, the spherical hinge structure shown in fig. 3 may be simplified to process the contact point between the flywheel damping device 2 and the passive vibration isolation device 1 into a spherical surface shape, and in particular, referring to fig. 4, the base 211 of the box 21 may be processed into a spherical surface, and the spherical surface 211 is abutted and fixed to the support table 11, so that the installation and maintenance costs of the damping platform 100 may be greatly reduced on the premise of ensuring the damping performance of the damping platform 100. Preferably, the central axes of the three flywheels 22 pass through the spherical center of the spherical surface.
Based on the damping platform 100, the invention also provides a damping method for the ship precision instrument, which specifically comprises the following steps:
step S1, collecting a first sensing signal of the passive vibration isolation device 1 which is vibrated by a ship deck;
step S2, controlling the passive vibration isolation device 1 according to the first sensing signal;
step S3, collecting a second sensing signal which passes through the passive vibration isolation device 1 and then enters the flywheel damping device 2;
and step S4, controlling the rotation speed of at least three flywheels 22 according to the second sensing signal.
According to the damping method of the precision instrument 200 on the ship deck, the passive vibration isolation device 1 is controlled to carry out vibration isolation through the first sensing signal of the vibration of the ship deck, the second sensing signal of the transmission after the vibration isolation is collected, the rotating speed of at least three flywheels 22 is controlled, and then the reaction force of the at least three flywheels 22 on the passive vibration isolation device 1 connected with the flywheel damping device 2 is regulated and controlled, and the reaction force is offset with the transmission force of the passive vibration isolation device 1 after the vibration isolation. Because the invention utilizes the action torque generated by the flywheel to the outside when accelerating and decelerating, the control bandwidth of the flywheel to the external vibration barrier completely depends on the bandwidths of the rotating motor and the control system thereof, and the flywheel has excellent performance in low frequency, medium frequency and high frequency. Meanwhile, the torque of the motor in the flywheel completely depends on the motor and the driving design thereof, the size of the motor can be changed freely, and the vibration isolation capability has strong adaptability to photoetching machines with different sizes and grades.
The above examples only express preferred embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.
Claims (10)
1. A shock absorbing platform, comprising:
a passive vibration isolation device arranged on the deck, a flywheel damping device connected with the passive vibration isolation device and a control system electrically connected with the passive vibration isolation device and the flywheel damping device,
the flywheel damping device comprises a box body for supporting the precision instrument and at least three flywheels arranged in the box body, the shells of the three flywheels are abutted and fixed with the inner wall of the box body, the central shafts of the three flywheels are not parallel,
the control system comprises a plurality of sensors and a controller electrically connected with the sensors, and the controller is electrically connected with the flywheel.
2. A shock absorbing platform as set forth in claim 1 wherein the central axes of three said flywheels intersect at a point.
3. A shock absorbing platform as set forth in claim 1, wherein the central axes of three said flywheels are arranged vertically two by two.
4. The shock absorbing platform of claim 1 wherein said housing is ball-hinged to said passive shock absorbing means.
5. A shock absorbing platform as set forth in claim 4, wherein the base of the box body on the side thereof adjacent to the passive shock absorbing device is a vertical cone, the vertex of the vertical cone is spherical, and the passive shock absorbing device is provided with a hinge shaft seat hinged to the vertex.
6. The shock absorbing platform of claim 1, wherein the base of the box on the side near the passive shock absorbing device is a spherical surface, and the spherical surface is fixed to the passive shock absorbing device in an abutting manner.
7. A shock absorbing platform as set forth in claim 6 wherein the central axes of three said flywheels pass through the spherical center of said spherical surface.
8. A shock absorbing platform as set forth in claim 1, wherein said passive vibration isolation means includes a support platform, a plurality of vibration isolators uniformly disposed on one side of said support platform, and dampers connected in series with said vibration isolators, said housing being disposed on said support platform.
9. The shock platform of claim 8, wherein the vibration isolator comprises an air spring or a steel spring.
10. A damping method for a precision instrument, the damping method comprising
Collecting a first sensing signal of the passive vibration isolation device, which is vibrated by a ship deck;
controlling the passive vibration isolation device according to the first sensing signal;
collecting a second sensing signal which passes through the passive vibration isolation device and then enters the flywheel damping device;
and controlling the rotating speeds of at least three flywheels according to the second sensing signals.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011400355.1A CN112709777A (en) | 2020-12-02 | 2020-12-02 | Damping platform and damping method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202011400355.1A CN112709777A (en) | 2020-12-02 | 2020-12-02 | Damping platform and damping method |
Publications (1)
Publication Number | Publication Date |
---|---|
CN112709777A true CN112709777A (en) | 2021-04-27 |
Family
ID=75542460
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202011400355.1A Pending CN112709777A (en) | 2020-12-02 | 2020-12-02 | Damping platform and damping method |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN112709777A (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0294130A2 (en) * | 1987-06-05 | 1988-12-07 | Eaton Corporation | Two mass flywheel assembly with relative rotation control |
CN103332301A (en) * | 2013-06-08 | 2013-10-02 | 北京航空航天大学 | Method for utilizing liquid filling variable inertial flywheel to control attitude of spacecraft and actuating mechanism thereof |
CN104158340A (en) * | 2013-05-14 | 2014-11-19 | 上海新跃仪表厂 | Novel three-shaft integrated micro flywheel |
WO2020182623A1 (en) * | 2019-03-08 | 2020-09-17 | Veoware Sprl | A modular and configurable attitude control system for a spacecraft |
CN111895039A (en) * | 2020-09-03 | 2020-11-06 | 宋文琦 | Vehicle-mounted vibration isolation platform for transporting precision instruments |
CN111981075A (en) * | 2020-08-21 | 2020-11-24 | 南京航空航天大学 | Quasi-zero rigidity vibration isolation system with bending moment resisting effect |
-
2020
- 2020-12-02 CN CN202011400355.1A patent/CN112709777A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0294130A2 (en) * | 1987-06-05 | 1988-12-07 | Eaton Corporation | Two mass flywheel assembly with relative rotation control |
CN104158340A (en) * | 2013-05-14 | 2014-11-19 | 上海新跃仪表厂 | Novel three-shaft integrated micro flywheel |
CN103332301A (en) * | 2013-06-08 | 2013-10-02 | 北京航空航天大学 | Method for utilizing liquid filling variable inertial flywheel to control attitude of spacecraft and actuating mechanism thereof |
WO2020182623A1 (en) * | 2019-03-08 | 2020-09-17 | Veoware Sprl | A modular and configurable attitude control system for a spacecraft |
CN111981075A (en) * | 2020-08-21 | 2020-11-24 | 南京航空航天大学 | Quasi-zero rigidity vibration isolation system with bending moment resisting effect |
CN111895039A (en) * | 2020-09-03 | 2020-11-06 | 宋文琦 | Vehicle-mounted vibration isolation platform for transporting precision instruments |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105547628B (en) | Vibration acceleration testing equipment vibration reaction force active balancing device | |
JP4045466B2 (en) | Apparatus and method for stabilizing a centrifuge rotor | |
US10794788B2 (en) | Dynamic balance testing device | |
CN109610673B (en) | Active moment of inertia drive control system | |
CN105204543B (en) | A kind of active-passive integrated vibration-isolating platforms of the Stewart of electromagnetic drive | |
CN207365823U (en) | A kind of Free Modal pilot system under guided missile autorotation | |
CN106369105A (en) | Eight-point damping system for optical fiber inertial unit of spacecraft | |
US20220154800A1 (en) | Motion sensor module and movable platform | |
US8740133B2 (en) | Aircraft including an engine controlled by synchrophasing | |
CN112709777A (en) | Damping platform and damping method | |
CN113184204B (en) | Unmanned aerial vehicle's damping cloud platform and unmanned aerial vehicle | |
US4977342A (en) | Electromagnetic vibration generators | |
JPH11159191A (en) | Damper | |
WO2009052549A1 (en) | Gyroscopic stabilisation apparatus and method | |
Rezaee et al. | Dynamics and stability of non-planar rigid rotor equipped with two ball-spring autobalancers | |
CN108547913B (en) | A kind of rotor-support-foundation system dynamic vibration absorber with varying stiffness member | |
Ziaran et al. | Analysis of the impact of different types of vibration isolation on the dynamic loading of machines and the surrounding environment | |
JPH0734721A (en) | Active shock absorber | |
CN112709778B (en) | Shock absorption photoetching machine and shock absorption method thereof | |
JPH0738748Y2 (en) | Rotating device | |
JP4052433B2 (en) | Rotational system vibration device | |
CN112590482B (en) | Vehicle suspension system and damping method thereof | |
CN109578507A (en) | A kind of main passive absorber of three axis rotation aerial camera | |
KR101637655B1 (en) | Device of damping vibration and Inertial measurement unit with device of damping vibration | |
CN114412962B (en) | Spherical self-stabilization posture adjustment platform and method |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for 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: 20210427 |