CN109649702A - Double super satellite platform ground simulation equipment of the vertical control of differential type air bearing - Google Patents
Double super satellite platform ground simulation equipment of the vertical control of differential type air bearing Download PDFInfo
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- CN109649702A CN109649702A CN201910075425.1A CN201910075425A CN109649702A CN 109649702 A CN109649702 A CN 109649702A CN 201910075425 A CN201910075425 A CN 201910075425A CN 109649702 A CN109649702 A CN 109649702A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G7/00—Simulating cosmonautic conditions, e.g. for conditioning crews
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Abstract
The present invention provides a kind of, and double super satellite platform ground simulation equipment based on the vertical control of differential type air bearing belong to spacecraft physical emulation field, Rx, Ry and Rz freedom degree rotation of rotatable platform are realized by air-floating ball bearing, X the and Y freedom degree movement of load cabin air floating platform and platform cabin air floating platform is realized by plane air-bearing, support post passes through the throttle orifice that is arranged on support post and horizontal shifting platform gas supply composition air floating structure, realizes the gas suspension support of support post, is vertically directed and pressure control driving straight up；The throttle orifice of thrust plate setting is oriented to by air bearing, realize being vertically directed and pressure control driving straight down to support post, and then it realizes and the differential type air bearing catenary motion of support post is controlled, have many advantages, such as that six degree of freedom non-contact support drives, stability is high and response is fast, can be used for attitude-simulating, big swing angle maneuvering characteristics and dynamic middle imaging ground validation of double super satellite platforms etc..
Description
Technical field
The present invention relates to spacecraft physicals to emulate field, and in particular, to a kind of vertical control of differential type air bearing it is double super
Satellite platform ground simulation equipment.
Background technique
Along with the rapid development of science and technology, space flight earth observation remote sensing task is gradually towards high spatial resolution and high efficiency side
To development, and observe the high spatial resolution of remote sensing and high efficiency depend primarily on the pointing accuracy of satellite load, stability and
Quick mobility.In traditional satellite platform, the flexible appendages such as large-scale solar array and flywheel, gyro, driving mechanism
Equal movable parts are the main reason for influencing satellite load posture pointing accuracy, stability and quick mobility.
In conventional satellite design, load cabin and platform cabin are connected, and posture follows satellite platform to be controlled, load cabin
Attitude accuracy depends primarily on the attitude control accuracy of satellite platform, and the large-scale flexible appendage on satellite platform influences indirectly
The control precision of load cabin.Therefore it is difficult to realize the ultra-high stable of load posture simultaneously in such a way that load and platform are connected
Degree, superelevation pointing accuracy and superelevation agility performance.In order to improve the pointing accuracy and stability of satellite load, have to vibration
The isolation and inhibition of effect by using platform and load to be carried out to the two-body satellite form of physical separation, and then realize load
High-precision high-speed movement, it has also become one of the hot spot technology of next-generation satellite platform.In order to realize to the in-orbit of two-body satellite platform
Performance verification, the ground simulation experiment for carrying out simulated weightlessness and micro- disturbance torque space environment just become particularly important.Therefore, it needs
The ground physical emulation ground testing system for meeting movement needs is provided.
Patent document CN103514792A refers to that a kind of space six degree of freedom air bearing follow-up motion platform, the platform pass through gas
Floating technology realization two-freedom translation and three degree of freedom rotation, and it is vertical servo-actuated using the realization of fluid balance method, and then obtain
Obtain the movement simulation of spacecraft attitude under space microgravity environment.But the hydraulic-driven structure type that the patent document uses,
Due to hydraulic oil high viscosity and cause biggish viscous damping to be interfered, while being promoted using one-way hydraulic cylinder and being put down with air bearing campaign
The open type control mode that the gravity of platform balances each other has seriously undermined the response frequency and stability of plateform system；Patent document
CN104875907A refers to that a kind of narrow space heavy equipment transports installation six degree of freedom air-floated vehicle, passes through plane gas foot, front and back
The combination of one-movement-freedom-degree device, vertical shift freedom degree device and the freedom degree device that swings, realizes the six of heavy equipment
Freedom degree transports installation, but vertically moving in the air-floated vehicle, front and back overturning, left-right swinging mechanism are all made of direct contact type
Motion guide rail, and then biggish frictional force is brought, it is unable to satisfy the ground simulation requirement of micro- disturbance torque environment of spacecraft；Specially
One of sharp document CN105321398A six degree of freedom air-flotation type motion simulator, by a spherical surface air-bearing, three
Plane air-bearing and a lifting column assembly realize the six-freedom motion of platform, but the lifting column assembly in the patent is logical
The form connection outer support column and balance weight for crossing wirerope and pulley blocks, can bring biggish frictional force to interfere, and due to steel wire
Elastic deformation cause catenary motion control precision it is low, stablize the time it is long.Therefore need to design a kind of fast response time, perturbed force
Square is small, and is adapted to the novel six freedom physical simulation of verifying two-body satellite pointing accuracy, stability and quick mobility
Ground test device.
Summary of the invention
For the defects in the prior art, the object of the present invention is to provide a kind of the double super of vertical control of differential type air bearing to defend
Star platform ground simulation equipment.
A kind of double super satellite platform ground simulation equipment of the vertical control of differential type air bearing provided according to the present invention, including
Platform cabin air floating platform, load cabin air floating platform, magnetic floating mechanism；Platform cabin air floating platform and load cabin air floating platform are floating by magnetic
Mechanism connection, platform cabin air floating platform and load cabin air floating platform carry out power transmitting by magnetic floating mechanism.
Preferably, the magnetic floating mechanism include magnetic floating mechanism coil, magnetic floating mechanism magnet steel, magnetic floating mechanism coil support plate,
Magnetic floating mechanism magnet steel support plate；
Magnetic floating mechanism coil support plate is fastenedly connected with platform cabin air floating platform；
Magnetic floating mechanism magnet steel support plate is fastenedly connected with load cabin air floating platform；
Magnetic floating mechanism coil is fastenedly connected with magnetic floating mechanism magnet steel support plate；
Magnetic floating mechanism magnet steel is fastenedly connected with magnetic floating mechanism magnet steel support plate.
Preferably, platform cabin air floating platform includes rotatable platform, air-floating ball bearing component；
Air-floating ball bearing component is fastenedly connected with rotatable platform.
Preferably, the air-floating ball bearing component includes air floatation ball, air bearing ball-and-socket, gas sealing plate；
Air floatation ball is fastenedly connected with rotatable platform；
It is provided with the groove that shape and air floatation ball match on air bearing ball-and-socket, air floatation ball can be accommodated and be arranged in air bearing ball-and-socket
On；
Air bearing ball-and-socket is arranged in vertically below in gas sealing plate, can support air bearing ball-and-socket and be arranged in air floatation ball fossa slot
Air floatation ball.
Preferably, platform cabin air floating platform includes support post, air-bearing structural body；
The lower section of air-floating ball bearing component is arranged in support post；
Air-bearing structural body is connect with support post vertical direction, and driving support post carries out the vertical fortune of differential type air bearing
It is dynamic.
Preferably, the air-bearing structural body includes horizontal shifting platform, the throttle orifice being arranged on support post, gas
Floating guiding thrust plate, the throttle orifice being arranged on air bearing guiding thrust plate vertical direction；
The vertical lower of support post is arranged in horizontal shifting platform, forms closed gas with the vertical lower end of support post
Cavity；
Air bearing is oriented to thrust plate and is arranged in support post radial direction or axial direction.
Preferably, double super satellite platform ground simulation equipment of the vertical control of differential type air bearing, including lower layer's gas
Bottle, plane air-bearing；
Plane air-bearing is fastenedly connected with air-bearing structural body, is arranged in horizontal direction；
Plane air-bearing is provided with multiple；
Lower layer's gas cylinder is connected with air-bearing structural body.
Preferably, ring-type is arranged radial throttle orifice at air bearing guiding thrust plate internal orifice dimension, air bearing be oriented to thrust plate with
Support post air film clearance seal.
Preferably, the multiple rows of radial throttle orifice of the vertical lower end ring-type setting of the support post, support post and horizontal shifting
Moving platform air film clearance seal.
Compared with prior art, the present invention have it is following the utility model has the advantages that
1, realize that six degree of freedom non-contact motion, motion artifacts are generated by air viscosity, rubbed using air-floating ball bearing structure
It is extremely low to wipe power, and there is unlimited service life；
2, the enclosed volume formed to support post lower end and horizontal shifting platform carries out pressure control gas supply, to described
Air bearing guiding thrust plate and the enclosed volume that is formed of support post upper surface carry out pressure control gas supply, pass through accurate control in real time
The difference of both systems air pressure, realizes the gravity compensation of the catenary motion component of platform cabin air floating platform, overcomes one direction gas suspension
The Low rigidity of gravity compensation support and stablize time long problem, fast response time, stability is good, catenary motion high stability and
Height response.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon:
Fig. 1 is general structure schematic diagram of the invention；
Fig. 2 is load cabin structural schematic diagram of the invention；
Fig. 3 is that vertical suspension support drives schematic diagram.
It is shown in figure: 1-platform cabin air floating platform；2-load cabin air floating platforms；3-magnetic floating mechanism coils；4-magnetic are floating
Mechanism magnet steel；5-magnetic floating mechanism coil support plates；6-magnetic floating mechanism magnet steel support plates；7-rotatable platforms；8-air floatation balls；
9-air bearing ball-and-sockets；10-upper layer gas cylinders；11-gas sealing plates；12-support posts；13-lower layer's gas cylinders；14-move horizontally it is flat
Platform；15-plane air-bearings；16-air bearing thrust guide plates；17-thrusters；18-radial throttle orifices；19-vertical directions
Throttle orifice.
Specific embodiment
The present invention is described in detail combined with specific embodiments below.Following embodiment will be helpful to the technology of this field
Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill of this field
For personnel, without departing from the inventive concept of the premise, several changes and improvements can also be made.These belong to the present invention
Protection scope.
A kind of double super satellite platform ground simulation equipment of the vertical control of differential type air bearing provided according to the present invention, including
Platform cabin air floating platform 1, load cabin air floating platform 2, magnetic floating mechanism；Platform cabin air floating platform 1 passes through with load cabin air floating platform 2
Magnetic floating mechanism connection, platform cabin air floating platform 1 and load cabin air floating platform 2 carry out power transmitting by magnetic floating mechanism.
Specifically, the magnetic floating mechanism includes magnetic floating mechanism coil 3, magnetic floating mechanism magnet steel 4, magnetic floating mechanism coil support plate
5, magnetic floating mechanism magnet steel support plate 6；Magnetic floating mechanism coil support plate 5 is fastenedly connected with platform cabin air floating platform 1；Magnetic floating mechanism magnetic
Steel bracing plate 6 is fastenedly connected with load cabin air floating platform 2；Magnetic floating mechanism coil 3 and the fastening of magnetic floating mechanism magnet steel support plate 6 connect
It connects；Magnetic floating mechanism magnet steel 4 is fastenedly connected with magnetic floating mechanism magnet steel support plate 6.
Specifically, platform cabin air floating platform 1 includes rotatable platform 7, air-floating ball bearing component；Air-floating ball bearing component
It is fastenedly connected with rotatable platform 7.
Specifically, the air-floating ball bearing component includes air floatation ball 8, air bearing ball-and-socket 9, gas sealing plate 11；Air floatation ball 8 and rotation
Platform 7 is fastenedly connected；It is provided with the groove that shape and air floatation ball 8 match on air bearing ball-and-socket 9, the setting of air floatation ball 8 can be accommodated
On air bearing ball-and-socket 9；Air bearing ball-and-socket 9 is arranged in vertically below in gas sealing plate 11, can support air bearing ball-and-socket 9 and be arranged in air bearing
Air floatation ball 8 in 9 groove of ball-and-socket.
Specifically, platform cabin air floating platform 1 includes support post 12, air-bearing structural body；Support post 12 is set
It sets in the lower section of air-floating ball bearing component；Air-bearing structural body is connect with 12 vertical direction of support post, drives support post
12 carry out differential type air bearing catenary motion.
Specifically, the air-bearing structural body include horizontal shifting platform 14, the throttling that is arranged on support post 12
Hole, air bearing guiding thrust plate 16, the throttle orifice being arranged on air bearing guiding 16 vertical direction of thrust plate；Horizontal shifting platform 14 is set
The vertical lower in support post 12 is set, forms closed air cavity with the vertical lower end of support post 12；Air bearing is oriented to thrust
Plate 16 is arranged in 12 radial direction of support post or axial direction.
Specifically, double super satellite platform ground simulation equipment of the vertical control of differential type air bearing, further include lower layer
Gas cylinder 13, plane air-bearing 15；Plane air-bearing 15 is fastenedly connected with air-bearing structural body, is arranged in horizontal direction；
Plane air-bearing 15 is provided with multiple；Lower layer's gas cylinder 13 is connected with air-bearing structural body.
Specifically, radial throttle orifice is arranged in ring-type at air bearing guiding 16 internal orifice dimension of thrust plate, and air bearing is oriented to thrust plate
16 with 12 air film clearance seal of support post.
Specifically, the multiple rows of radial throttle orifice of the support post 12 vertical lower end ring-type setting, support post 12 and water
Translate 14 air film clearance seal of moving platform.
Rotatable platform 7 by the air-floating ball bearing component that air floatation ball 8, air bearing ball-and-socket 9 and gas sealing plate 11 form can realize Rx,
Ry and Rz is moved to non-contact rotation freedom degree, can realize X and Y-direction by the plane air-bearing for being fixed on horizontal shifting platform
Non-contact one-movement-freedom-degree movement, support post passes through the throttle orifice being arranged on support post and horizontal shifting platform supplies structure
At air-bearing structure, realizes the non-contact gas suspension gravity compensation support of support post and be vertically directed；
The present invention realizes that Rx, Ry and Rz freedom degree of rotatable platform rotate by air-floating ball bearing, passes through plane air-bearing shafts
X the and Y freedom degree movement for realizing load cabin air floating platform and platform cabin air floating platform is held, support post is vertical in support by setting
Throttle orifice and horizontal shifting platform gas supply composition air floating structure on column, realize the gas suspension support of support post, are vertically directed
Pressure straight up controls driving；It is oriented to the throttle orifice of thrust plate setting by air bearing, realizes to the vertical of support post
Guiding and pressure straight down control driving, and then realize and control the differential type air bearing catenary motion of support post, have
The driving of six degree of freedom non-contact support, the advantages that stability is high and response is fast can be used for the attitude-simulating, big of double super satellite platforms
Pivot angle maneuvering characteristics and dynamic middle imaging ground validation etc..It is floating that the present invention passes through the magnetic being arranged on platform cabin air floating platform 1
The magnetic floating mechanism of actuator coil and the magnetic floating mechanism magnet steel 4 being arranged on load cabin air floating platform 2 composition is realized in double super satellites
Load cabin and the power in platform cabin are transmitted, and magnetic floating mechanism coil 3 is installed on by way of being fixed on magnetic floating mechanism coil support plate 5
Platform cabin air floating platform, magnetic floating mechanism magnet steel 4 are installed on load cabin gas by way of being fixed on magnetic floating mechanism magnet steel support plate 6
Floating platform, for platform cabin air floating platform, rotatable platform is fixed in air floatation ball, and by by air floatation ball, air bearing ball-and-socket and envelope
Gas board group realizes that Rx, Ry and Rz of rotatable platform are rotated at air-floating ball bearing component, the upper layer gas cylinder being installed on rotatable platform
Supply gas pressure is provided to thruster, the top of support post is arranged in air-floating ball bearing, and support post is vertical in support by setting
Throttle orifice and horizontal shifting platform on column constitute air-bearing structure, realize being vertically directed for support post, are existed by setting
The seal air cavity that the vertical lower end of support post and horizontal shifting platform are formed constitutes thrust cylinder form and realizes to support post
Gas suspension is supported and is driven straight up, and the setting of horizontal shifting platform upper surface has to the radial and axial application gas of support post
The air bearing of body pressure is oriented to thrust plate, and the arrangement of the vertical direction throttle orifice of thrust plate is oriented to by air bearing, realizes vertical to support
The driving straight down of column drives by the driving straight up to support post and straight down, realizes to support post
The control of differential type air bearing catenary motion, the high pressure gas provided by lower layer's gas cylinder are more on horizontal shifting platform to being fixed on
A plane air-bearing is supplied, and realizes that the X of horizontal shifting platform and Y-direction are mobile.
Double super satellite platform ground simulation equipment based on the vertical control of differential type air bearing, are oriented to thrust along air bearing
Radial throttle orifice is arranged in ring-type at panel aperture, is arranged by the radial throttle orifice that air bearing is oriented to thrust plate, realizes that air bearing guiding is stopped
The air film clearance seal and guiding of push plate and support post, in the multiple rows of radial throttling of the vertical lower end ring-type setting of support post
Hole is arranged by the radial throttle orifice of support post, is realized the air film clearance seal of support post and horizontal shifting platform and is led
To.
Double super satellite platform ground simulation equipment based on the vertical control of differential type air bearing, it is vertical to the support
The enclosed volume that column lower end and horizontal shifting platform are formed carries out pressure control gas supply, to the air bearing guiding thrust plate with
The enclosed volume that support post upper surface is formed carries out pressure control gas supply, and the difference by both accurate control air pressure in real time is real
The gravity compensation of the catenary motion component of existing platform cabin air floating platform.
Double super satellite platform ground simulation equipment based on the vertical control of differential type air bearing, the plane air bearing
Bearing can use planar annular thrust orifice restriction air-bearing, Porous air-bearing or other plane thrust air bearings
Bearing type, and it is not limited to above-described plane thrust air-bearing form, it is made of air floatation ball, air bearing ball-and-socket and gas sealing plate
Air-floating ball bearing component and plane air-bearing can be supplied simultaneously with identical supply gas pressure, can also be to different confessions
Atmospheric pressure supplies air-floating ball bearing component and plane air-bearing respectively.
The present invention is described in further detail below in conjunction with the accompanying drawings:
Double super satellite platform ground simulation equipment based on the vertical control of differential type air bearing, the ground simulation equipment include flat
Platform cabin air floating platform 1 and load cabin air floating platform 2 by the magnetic floating mechanism coil 3 being arranged on platform cabin air floating platform 1 and are set
It sets and realizes load cabin and platform in double super satellites in the magnetic floating mechanism that the magnetic floating mechanism magnet steel 4 on load cabin air floating platform 2 forms
The power in cabin is transmitted, and it is flat that magnetic floating mechanism coil 3 is installed on the air bearing of platform cabin by way of being fixed on magnetic floating mechanism coil support plate 5
Platform 1, magnetic floating mechanism magnet steel 4 is installed on load cabin air floating platform 2 by way of being fixed on magnetic floating mechanism magnet steel support plate 6, right
In platform cabin air floating platform 1, rotatable platform 7 is fixed in air floatation ball 8, and by by air floatation ball 8, air bearing ball-and-socket 9 and gas sealing plate
11 composition air-floating ball bearing components realize Rx, Ry and Rz rotation of rotatable platform 7, the upper layer gas cylinder being installed on rotatable platform 7
10 pairs of thrusters 17 provide supply gas pressure, form the setting of air-floating ball bearing component by air floatation ball 8, air bearing ball-and-socket 9 and gas sealing plate 11
On the top of support post 12, support post 12 passes through radial throttle orifice 18 and the horizontal shifting platform being arranged on support post
14 constitute air-bearing structures, realize that support post 12 is vertically directed, by setting support post 12 vertical lower end with
The seal air cavity of the formation of horizontal shifting platform 14, composition thrust cylinder form is to the realization gas suspension support of support post 12 and vertically
It drives up, the setting of 14 upper surface of horizontal shifting platform has the air bearing for applying gas pressure radial and axial to support post 12
It is oriented to thrust plate 16, the arrangement of the vertical direction throttle orifice 19 of thrust plate 16 is oriented to by air bearing, is realized to support post 12
It drives, drives by the driving straight up to support post 12 and straight down straight down, realize to support post 12
The control of differential type air bearing catenary motion, the high pressure gas provided by lower layer's gas cylinder 13, to being fixed on horizontal shifting platform 14
Multiple plane air-bearings 15 supplied, realize that the X of horizontal shifting platform 14 and Y-direction are mobile.
Double super satellite platform ground simulation equipment based on the vertical control of differential type air bearing, are oriented to thrust along air bearing
Radial throttle orifice is arranged in ring-type at 16 internal orifice dimension of plate, is arranged by the radial throttle orifice that air bearing is oriented to thrust plate 16, realizes air bearing
It is oriented to the air film clearance seal and guiding of thrust plate 16 and support post 12, is arranged in the vertical lower end ring-type of support post 12 more
Radial throttle orifice is arranged, is arranged by the radial throttle orifice of support post 12, realizes support post 12 and horizontal shifting platform 14
Air film clearance seal and guiding.
Double super satellite platform ground simulation equipment based on the vertical control of differential type air bearing, it is vertical to the support
The enclosed volume that 12 lower end of column and horizontal shifting platform 14 are formed carries out pressure control gas supply, is oriented to thrust to the air bearing
The enclosed volume that plate 16 and 12 upper surface of support post are formed carries out pressure control gas supply, passes through both accurate control air pressure in real time
Difference realize platform cabin air floating platform 1 catenary motion component gravity compensation.
Double super satellite platform ground simulation equipment based on the vertical control of differential type air bearing, the plane air bearing
Bearing 15 can use planar annular thrust orifice restriction air-bearing, Porous air-bearing or other plane thrust gas
Floating bearing type, and it is not limited to above-described plane thrust air-bearing form, by air floatation ball 8, air bearing ball-and-socket 9 and gas sealing plate
11 composition air-floating ball bearing components and plane air-bearing 15 can be supplied simultaneously with identical supply gas pressure, can also to
Different supply gas pressures supplies air-floating ball bearing component and plane air-bearing 15 respectively.
In the description of the present application, it is to be understood that term " on ", "front", "rear", "left", "right", " is erected at "lower"
Directly ", the orientation or positional relationship of the instructions such as "horizontal", "top", "bottom", "inner", "outside" is orientation based on the figure or position
Relationship is set, description the application is merely for convenience of and simplifies description, rather than the device or element of indication or suggestion meaning are necessary
It with specific orientation, is constructed and operated in a specific orientation, therefore should not be understood as the limitation to the application.
Specific embodiments of the present invention are described above.It is to be appreciated that the invention is not limited to above-mentioned
Particular implementation, those skilled in the art can make a variety of changes or modify within the scope of the claims, this not shadow
Ring substantive content of the invention.In the absence of conflict, the feature in embodiments herein and embodiment can any phase
Mutually combination.
Claims (9)
1. a kind of double super satellite platform ground simulation equipment of vertical control of differential type air bearing, which is characterized in that including platform cabin
Air floating platform (1), load cabin air floating platform (2), magnetic floating mechanism；Platform cabin air floating platform (1) and load cabin air floating platform (2) are logical
Magnetic floating mechanism connection is crossed, platform cabin air floating platform (1) and load cabin air floating platform (2) pass through magnetic floating mechanism progress power transmitting.
2. double super satellite platform ground simulation equipment of the vertical control of differential type air bearing according to claim 1, feature
It is, the magnetic floating mechanism includes magnetic floating mechanism coil (3), magnetic floating mechanism magnet steel (4), magnetic floating mechanism coil support plate (5), magnetic
Float means magnet steel support plate (6)；
Magnetic floating mechanism coil support plate (5) is fastenedly connected with platform cabin air floating platform (1)；
Magnetic floating mechanism magnet steel support plate (6) is fastenedly connected with load cabin air floating platform (2)；
Magnetic floating mechanism coil (3) is fastenedly connected with magnetic floating mechanism magnet steel support plate (6)；
Magnetic floating mechanism magnet steel (4) is fastenedly connected with magnetic floating mechanism magnet steel support plate (6).
3. double super satellite platform ground simulation equipment of the vertical control of differential type air bearing according to claim 1, feature
It is, platform cabin air floating platform (1) includes rotatable platform (7), air-floating ball bearing component；
Air-floating ball bearing component is fastenedly connected with rotatable platform (7).
4. double super satellite platform ground simulation equipment of the vertical control of differential type air bearing according to claim 3, feature
It is, the air-floating ball bearing component includes air floatation ball (8), air bearing ball-and-socket (9), gas sealing plate (11)；
Air floatation ball (8) is fastenedly connected with rotatable platform (7)；
It is provided with the groove that shape matches with air floatation ball (8) on air bearing ball-and-socket (9), air floatation ball (8) can be accommodated and be arranged in gas
On floating ball nest (9)；
Gas sealing plate (11) setting air bearing ball-and-socket (9) vertically below, can support air bearing ball-and-socket (9) and setting in air bearing ball-and-socket
(9) air floatation ball in groove (8).
5. double super satellite platform ground simulation equipment of the vertical control of differential type air bearing according to claim 3, feature
It is, platform cabin air floating platform (1) includes support post (12), air-bearing structural body；
The lower section of air-floating ball bearing component is arranged in support post (12)；
Air-bearing structural body is connect with support post (12) vertical direction, and driving support post (12) carries out differential type air bearing and hangs down
To movement.
6. double super satellite platform ground simulation equipment of the vertical control of differential type air bearing according to claim 5, feature
It is, the air-bearing structural body includes horizontal shifting platform (14), the throttle orifice being arranged on support post (12), air bearing
It is oriented to the throttle orifice of thrust plate (16), setting on air bearing guiding thrust plate (16) vertical direction；
The vertical lower in support post (12), the vertical lower end shape with support post (12) is arranged in horizontal shifting platform (14)
At closed air cavity；
Air bearing is oriented to thrust plate (16) and is arranged in support post (12) radial direction or axial direction.
7. double super satellite platform ground simulation equipment of the vertical control of differential type air bearing according to claim 3, feature
It is, including lower layer's gas cylinder (13), plane air-bearing (15)；
Plane air-bearing (15) is fastenedly connected with air-bearing structural body, is arranged in horizontal direction；
Plane air-bearing (15) is provided with multiple；
Lower layer's gas cylinder (13) is connected with air-bearing structural body.
8. double super satellite platform ground simulation equipment of the vertical control of differential type air bearing according to claim 6, feature
It is, radial throttle orifice is arranged in ring-type at described air bearing guiding thrust plate (16) internal orifice dimension, and air bearing is oriented to thrust plate (16) and branch
Support column (12) air film clearance seal.
9. double super satellite platform ground simulation equipment of the vertical control of differential type air bearing according to claim 6, feature
Be, the multiple rows of radial throttle orifice of the vertical lower end ring-type setting of the support post (12), support post (12) with move horizontally
Platform (14) air film clearance seal.
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| CN201910075425.1A CN109649702B (en) | 2019-01-25 | 2019-01-25 | Differential air-floatation vertical control double-super satellite platform ground simulation equipment |
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| CN201910075425.1A CN109649702B (en) | 2019-01-25 | 2019-01-25 | Differential air-floatation vertical control double-super satellite platform ground simulation equipment |
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| CN109649702B CN109649702B (en) | 2021-11-23 |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111024310A (en) * | 2019-12-24 | 2020-04-17 | 北京卫星制造厂有限公司 | Multi-dimensional air flotation follow-up system for satellite high-precision quality measurement |
| CN111157199A (en) * | 2019-12-16 | 2020-05-15 | 上海卫星工程研究所 | Flexible cable rigidity determination test method, system and medium |
| CN111487570A (en) * | 2020-04-15 | 2020-08-04 | 中国科学院空间应用工程与技术中心 | Magnetic levitation guidance testing device, system and method |
| CN113406887A (en) * | 2021-06-25 | 2021-09-17 | 日照坤仑智能科技有限公司 | Self-adaptive six-degree-of-freedom air floatation simulation test bed and calculation method thereof |
| CN113619818A (en) * | 2021-08-16 | 2021-11-09 | 哈尔滨工业大学 | Six-degree-of-freedom microgravity test system based on air floatation pulley |
| CN113636116A (en) * | 2021-08-16 | 2021-11-12 | 哈尔滨工业大学 | Dumbbell-shaped reducing air-float pulley longitudinal gravity compensation device |
| CN114572430A (en) * | 2022-04-28 | 2022-06-03 | 中国人民解放军火箭军工程大学 | Multi-degree-of-freedom test system |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104960676A (en) * | 2015-07-13 | 2015-10-07 | 哈尔滨工业大学 | Multi-degree of freedom air floated platform pressure stabilizing device and pressure stabilizing method |
| CN105109712A (en) * | 2015-08-21 | 2015-12-02 | 哈尔滨工业大学 | Air floating shaft based on Z-direction control of six-freedom-degree air floating table |
| KR20160079404A (en) * | 2014-12-26 | 2016-07-06 | 한국항공우주연구원 | Satellite Loading Apparatus For Thermal Vacuum Chamber |
| CN106467175A (en) * | 2016-09-08 | 2017-03-01 | 上海卫星工程研究所 | The double super satellite ground Proof-Of Principle system of double five degree of freedom air supporting master-slave mode noncontacts |
| CN108177802A (en) * | 2017-11-30 | 2018-06-19 | 北京卫星制造厂 | A kind of constant force device and its application method based on air spring |
| CN207709886U (en) * | 2017-09-20 | 2018-08-10 | 广州市昊志机电股份有限公司 | Cylinder assembly and air-flotation electric spindle |
-
2019
- 2019-01-25 CN CN201910075425.1A patent/CN109649702B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20160079404A (en) * | 2014-12-26 | 2016-07-06 | 한국항공우주연구원 | Satellite Loading Apparatus For Thermal Vacuum Chamber |
| CN104960676A (en) * | 2015-07-13 | 2015-10-07 | 哈尔滨工业大学 | Multi-degree of freedom air floated platform pressure stabilizing device and pressure stabilizing method |
| CN105109712A (en) * | 2015-08-21 | 2015-12-02 | 哈尔滨工业大学 | Air floating shaft based on Z-direction control of six-freedom-degree air floating table |
| CN106467175A (en) * | 2016-09-08 | 2017-03-01 | 上海卫星工程研究所 | The double super satellite ground Proof-Of Principle system of double five degree of freedom air supporting master-slave mode noncontacts |
| CN207709886U (en) * | 2017-09-20 | 2018-08-10 | 广州市昊志机电股份有限公司 | Cylinder assembly and air-flotation electric spindle |
| CN108177802A (en) * | 2017-11-30 | 2018-06-19 | 北京卫星制造厂 | A kind of constant force device and its application method based on air spring |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111157199A (en) * | 2019-12-16 | 2020-05-15 | 上海卫星工程研究所 | Flexible cable rigidity determination test method, system and medium |
| CN111024310A (en) * | 2019-12-24 | 2020-04-17 | 北京卫星制造厂有限公司 | Multi-dimensional air flotation follow-up system for satellite high-precision quality measurement |
| CN111024310B (en) * | 2019-12-24 | 2021-11-16 | 北京卫星制造厂有限公司 | Multi-dimensional air flotation follow-up system for satellite high-precision quality measurement |
| CN111487570A (en) * | 2020-04-15 | 2020-08-04 | 中国科学院空间应用工程与技术中心 | Magnetic levitation guidance testing device, system and method |
| CN113406887A (en) * | 2021-06-25 | 2021-09-17 | 日照坤仑智能科技有限公司 | Self-adaptive six-degree-of-freedom air floatation simulation test bed and calculation method thereof |
| CN113619818A (en) * | 2021-08-16 | 2021-11-09 | 哈尔滨工业大学 | Six-degree-of-freedom microgravity test system based on air floatation pulley |
| CN113636116A (en) * | 2021-08-16 | 2021-11-12 | 哈尔滨工业大学 | Dumbbell-shaped reducing air-float pulley longitudinal gravity compensation device |
| CN113636116B (en) * | 2021-08-16 | 2023-04-28 | 哈尔滨工业大学 | Longitudinal gravity compensation device for dumbbell variable-diameter air-float pulley |
| CN114572430A (en) * | 2022-04-28 | 2022-06-03 | 中国人民解放军火箭军工程大学 | Multi-degree-of-freedom test system |
| CN114572430B (en) * | 2022-04-28 | 2024-02-27 | 中国人民解放军火箭军工程大学 | Multi-degree-of-freedom test system |
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