CN107505700B - Large-caliber telescope supporting system and tracking frame - Google Patents
Large-caliber telescope supporting system and tracking frame Download PDFInfo
- Publication number
- CN107505700B CN107505700B CN201710927196.2A CN201710927196A CN107505700B CN 107505700 B CN107505700 B CN 107505700B CN 201710927196 A CN201710927196 A CN 201710927196A CN 107505700 B CN107505700 B CN 107505700B
- Authority
- CN
- China
- Prior art keywords
- oil
- hydraulic
- support system
- telescope
- upright post
- 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.)
- Active
Links
Images
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B23/00—Telescopes, e.g. binoculars; Periscopes; Instruments for viewing the inside of hollow bodies; Viewfinders; Optical aiming or sighting devices
- G02B23/16—Housings; Caps; Mountings; Supports, e.g. with counterweight
Landscapes
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Telescopes (AREA)
- Magnetic Bearings And Hydrostatic Bearings (AREA)
Abstract
The invention discloses a large-caliber telescope supporting system, wherein a shaft system comprises a left upright post, a right upright post and the supporting system, and the supporting system comprises: the hydraulic support system comprises an oil cylinder, a hydrostatic pump, a hydraulic pipeline, a throttle valve, a first hydraulic oil cushion component and a second hydraulic oil cushion component; the first hydraulic cushion component and the left stand column limit a first oil cavity and form a first oil film, the second hydraulic cushion component and the right stand column limit a second oil cavity and form a second oil film, and the two oil cavities are communicated; the throttle valve is arranged on the hydraulic pipeline and controls the oil pressure of the two oil cavities. According to the invention, the hydraulic support structure is introduced into the pitching axis shaft system support system, the oil cavity pressure of the hydraulic pipeline is adjusted by adjusting the opening of the throttle valve, and the pressure of the two oil cavities is synchronously adjusted, so that the shaft heads on two sides of the horizontal shaft are in balanced load, the processing difficulty of the upper surface of the rotary table is reduced, the installation and adjustment time is reduced, and the construction cost of the telescope is effectively reduced.
Description
Technical Field
The invention relates to the structural design of a large-caliber telescope, in particular to a large-caliber telescope supporting system and a tracking frame.
Background
The mounting structure of the large-caliber telescope is also called a tracking frame structure, and the existing tracking frame structure has various structural forms, mainly including a horizontal type, a polar axis type, a horizontal type, a T-shaped frame structure, a six-rod universal platform type and the like. The first three structural forms are widely applied to structural design of the large-caliber foundation photoelectric telescope.
The three typical trackers differ greatly in structural design. The horizontal structure is single, two shafting forming the tracking frame are vertical to each other, the shafting vertical to the ground is called an azimuth shafting, and the shafting horizontally arranged and vertical to the azimuth axis is called a horizontal shafting (also called a pitch axis); the polar axis type tracking frame is also provided with two axes, namely a polar axis and a declination axis, wherein the polar axis is parallel to the zenith axis and points to the north pole; the horizontal tracking frame is also composed of two mutually perpendicular rotating shafts, one of which points to the north and south is called a warp beam, and the other is perpendicular to the warp beam and called a weft beam.
Taking the horizontal structure as an example, the pitch axis system generally consists of three parts: left stand, right stand and cross. In the large telescope, a left upright post and a right upright post both comprise a complete shafting. When the two components and the four-way component are integrated and then installed on the rotary table, due to the fact that factors such as unequal height of an installation plane and poor flatness exist, the axis of the installed pitching shaft deforms, and observation accuracy is lowered. It is also possible to have an effect on the bearing life of the pitch shaft if the deformation is large.
In order to solve the problem, conventionally, a bench worker and a detector are generally required to grind the upper surface of the rotary table together, and an autocollimator is used for real-time measurement so as to ensure that the directions of the axes of the shaft heads on the two sides are consistent. However, with the increasing aperture of the telescope, the span of the telescope tracking frame reaches the magnitude of more than 10 m. On one hand, the span is increased, so that the traditional detection means is difficult to reach the set precision; on the other hand, the large load capacity and span can generate considerable deflection under the action of gravity, so that the load of the motor can fluctuate greatly.
Disclosure of Invention
In view of the above, the invention provides a large-aperture telescope supporting system and a tracking frame, which realize balanced load of shaft heads on two sides of a horizontal shaft by introducing a hydraulic structure into a pitching shaft system supporting system, reduce moment fluctuation of horizontal shaft load, and improve low-speed tracking capability and pointing tracking precision of a telescope system.
In order to achieve the purpose, the technical scheme provided by the invention is as follows:
a large-caliber telescope supporting system is applied to a horizontal axis system of a horizontal structure and a weft axis system of the horizontal structure in a tracking frame structure, the axis systems comprise a left upright post (61), a right upright post (62) and the supporting system, and the supporting system comprises: the hydraulic support system comprises a lateral support system (5) and a hydraulic support system, wherein the hydraulic support system comprises an oil cylinder (11), a hydrostatic pump (13), a hydraulic pipeline (15), a throttle valve (16), a first hydraulic oil pad component (31) and a second hydraulic oil pad component (32);
the first hydraulic oil cushion assembly (31) is positioned below the left upright post (61), the left upright post (61) and the first hydraulic oil cushion assembly (31) jointly define a first oil chamber (81), and a first oil film is formed between the surfaces of the first hydraulic oil cushion assembly (31) opposite to the left upright post (61); the second hydraulic oil cushion assembly (32) is located below the right upright post (62), a second oil cavity (82) is defined by the right upright post (62) and the second hydraulic oil cushion assembly (32) together, a second oil film is formed between the surfaces of the second hydraulic oil cushion assembly (32) opposite to the right upright post (2), and the first oil cavity (81) is communicated with the second oil cavity (82);
the hydrostatic pump (13) is used for pumping the oil in the oil cylinder (11) into the hydraulic pipeline (15), and the throttle valve (16) is located on the hydraulic pipeline (15) and used for controlling the oil pressure of the first oil chamber (81) and the second oil chamber (82) so that the first oil film supports the left upright post (61) and the second oil film supports the right upright post (62).
Preferably, the method further comprises the following steps: a first hard spot mechanism (41) located within the first oil chamber (81), and a second hard spot mechanism (42) located within the second oil chamber (82).
Preferably, the first hard point mechanism (41) and the second hard point mechanism (42) are identical in structure, and the length of the first hard point mechanism (41) is not telescopic along the gravity direction.
Preferably, the first hard point mechanism (41) comprises a body of fixed length, and a pressure sensor provided at least at one end of the body.
Preferably, the hydraulic control system further comprises a controller, wherein the controller is used for adjusting the opening degree of the throttle valve (16) according to the stress conditions of the two ends of the first hard point mechanism (41) and the second hard point mechanism (42) so as to control the oil pressure of the first oil chamber (81) and the second oil chamber (82) and enable the stress of the two ends of the first hard point mechanism (41) and the second hard point mechanism (42) to be zero.
Preferably, the method further comprises the following steps: and one end of the electromagnetic overflow valve (14) is connected with the oil cylinder (11), and the other end of the electromagnetic overflow valve (14) is connected to a hydraulic pipeline between the hydrostatic pump (13) and the throttle valve (16).
Preferably, the method further comprises the following steps: and the oil temperature gauge (7) is arranged on the hydraulic pipeline between the first oil chamber (81) and the second oil chamber (82).
Preferably, the method further comprises the following steps: an oil filter (12), wherein one end of the oil filter (12) is communicated with the oil cylinder (11), and the other end is connected with the hydrostatic pump (13).
Preferably, oil pressures in the first oil chamber (81) and the second oil chamber (82) are 100 mpa, and the rigidity of the first oil film and the second oil film is several thousand mpa.
Preferably, the resonance frequency of the support system is 6HZ-8HZ for a telescope with a diameter of 8m-10m aperture, and the resonance frequency of the support system is 15HZ-20HZ for a telescope with a diameter of 2m-4m aperture.
The embodiment of the invention also discloses a tracking frame which is applied to the installation of the large-caliber telescope and is characterized by comprising an azimuth axis system (1), a rotary table (2) positioned above the azimuth axis system (1) and a horizontal axis system structure, wherein the horizontal axis system structure is arranged on the rotary table (2), and comprises a left upright post (61), a right upright post (62), a cross joint (7) and the large-caliber telescope supporting system.
Compared with the prior art, the technical scheme provided by the invention at least has the following advantages:
the invention provides a large-aperture telescope supporting system and a tracking frame, wherein a hydraulic while-tree structure is introduced into a pitching axis system supporting system, so that the mounting process of the pitching axis system conforms to the kinematic positioning principle, the oil cavity pressure of a hydraulic pipeline is adjusted by adjusting the opening of a throttle valve, and the oil cavities below a left upright post and a right upright post are communicated, and the oil cavity pressure is synchronously adjusted, so that the balanced load of shaft heads on two sides of a horizontal shaft is realized, the processing difficulty of the upper surface of a rotary table is reduced, the assembling and adjusting time is reduced, and the construction cost of a telescope can be effectively reduced.
In addition, a hard point mechanism is arranged in an oil cavity limited by the left stand column, the right stand column and the hydraulic oil pad together below the left stand column and the right stand column, the pressure of the oil cavity is adjusted according to the stress condition of the hard point adjusting mechanism, the installation and adjustment time is further reduced, the rigidity of the tracking frame is ensured by enough oil cavity pressure, the moment fluctuation of horizontal shaft load is reduced, and the low-speed tracking capability and the pointing tracking precision of the telescope system are improved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the provided drawings without creative efforts.
Fig. 1 is a front view of a tracking rack provided in an embodiment of the present application;
fig. 2 is a structure diagram of a hydraulic oil circuit of a large-caliber telescope support system according to an embodiment of the present disclosure;
fig. 3 is an enlarged view of the hard spot mechanism in fig. 2.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The embodiment of the invention discloses a large-aperture telescope supporting system, and the structure of the supporting system is explained by combining the structure of a tracking frame applying the system. The supporting system is applied to a horizontal axis of a horizontal structure in a tracking frame structure and a weft axis of the horizontal structure, and the horizontal axis is taken as an example, refer to fig. 1 and is a front view of the tracking frame.
The tracking frame is applied to the installation of a large-aperture telescope and comprises an azimuth axis system 1, a rotary table 2 positioned above the azimuth axis system 1 and a horizontal axis system structure. The horizontal axis structure in this embodiment is arranged on the turntable 2, and the horizontal axis structure includes a left column 61, a right column 62, a cross joint 7, and the large-caliber telescope support system disclosed in this embodiment.
As shown in fig. 2, a structural diagram of the support system of the large-aperture telescope is shown, and the support system comprises the following structures: the lateral supporting system 5 and the hydraulic supporting system, wherein the hydraulic supporting system comprises an oil cylinder 11, a hydrostatic pump 13, a hydraulic pipeline 15, a throttle valve 16, a first hydraulic cushion assembly 31 and a second hydraulic cushion assembly 32, and the components are matched to play a role in supporting the left upright post 61, the right upright post 62 and the four-way joint 7.
The first hydraulic oil cushion assembly 31 is located below the left upright post 61, the left upright post 61 and the first hydraulic oil cushion assembly 31 jointly define a first oil chamber 81, and a first oil film is formed between the surfaces of the first hydraulic oil cushion assembly 31 opposite to the left upright post 61; the second hydraulic cushion assembly 32 is located below the right upright column 62, a second oil cavity 82 is defined by the right upright column 62 and the second hydraulic cushion assembly 32 together, a second oil film is formed between the surfaces of the second hydraulic cushion assembly 32 opposite to the right upright column 2, and the first oil cavity 81 is communicated with the second oil cavity 82.
The hydrostatic pump 13 is connected to the cylinder 11, and is configured to pump the oil in the cylinder 11 into the hydraulic pipeline 15, the throttle valve 16 is located on the hydraulic pipeline 15, and is configured to control oil pressures of the first oil chamber 81 and the second oil chamber 82, so that the first oil film supports the left column 61, the second oil film supports the right column 62, and specifically, the oil pressures of the first oil chamber 81 and the second oil chamber 82 are adjusted by adjusting an opening degree of the throttle valve 16.
In addition, the supporting structure further comprises a hard point supporting system, the hard point supporting system comprises a first hard point mechanism 41 positioned in the first oil chamber 81 and a second hard point mechanism 42 positioned in the second oil chamber 82, the first hard point mechanism 41 and the second hard point mechanism 42 are identical in structure, as shown in fig. 2 and 3, wherein fig. 3 is an enlarged view of the first hard point mechanism 41.
It should be noted that the hard point mechanism is used for positioning a horizontal shaft of the large-caliber telescope, after the horizontal shaft system is initially installed, it is required to ensure that two ends of the hard point mechanism are not stressed, and in the installation process, the stress conditions at two ends of the hard point mechanism need to be detected in real time, so that the first oil cavity 81 and the second oil cavity 82 can be adjusted according to the stress conditions at two ends of the hard point mechanism, that is, the rigidity of the support system is ensured by adjusting the supporting force of oil films in the first oil cavity 81 and the second oil cavity 82.
In order to achieve the above-described function of the hard spot mechanism, the hard spot mechanism is freely movable within the corresponding oil chamber and does not block the oil passage inlet. Moreover, because of the requirement of the installation process, the hard point mechanisms in the prior art need to be retractable along the gravity direction, while the lengths of the two hard point mechanisms in the gravity direction in the embodiment are fixed, that is, the lengths of the first hard point mechanism 41 and the second hard point mechanism 42 are not retractable along the gravity direction. Specifically, taking the first hard spot mechanism 41 as an example, the hard spot mechanism includes a body with a fixed length and a pressure sensor at least disposed at one end of the body. In other embodiments, the pressure sensors in the first hard point mechanism 41 can be disposed at two ends of the body for better calibrating the force condition at two ends of the hard point mechanism.
It should be noted that, during the debugging process, the hard point mechanism may be in a state of contacting and being pressed by the left/right column or in a state of suspending in the oil chamber and having both ends away from the left/right column, and therefore, the pressure sensor disposed at one end or both ends of the hard point mechanism needs to be able to measure the pressure borne by the end of the hard point mechanism in the state of contacting and being pressed by the left/right column, and simultaneously needs to be able to detect the tensile force of the end of the hard point mechanism in the state of being away from the left/right column.
And, the hydraulic support system further includes a controller (not shown in the figure) for adjusting the opening of the throttle valve 16 according to the stress conditions at the two ends of the first hard point mechanism 41 and the second hard point mechanism 42 to control the oil pressure of the first oil chamber 81 and the second oil chamber 82 so that the stress at the two ends of the first hard point mechanism 41 and the second hard point mechanism 42 is zero.
Further, in order to ensure the stability of the oil pressure of the hydraulic system, the hydraulic support system in this embodiment further includes an electromagnetic overflow valve 14, and one end of the electromagnetic overflow valve 14 is connected to the oil cylinder 11, and the other end is connected to the hydraulic line between the hydrostatic pump 13 and the throttle valve 16.
And, in order to ensure the safety of the hydraulic pipeline, the hydraulic support system further comprises an oil temperature gauge 17 disposed on the hydraulic pipeline between the first oil chamber 81 and the second oil chamber 82 to measure the oil temperature in the hydraulic pipeline so as to control the temperature of the hydraulic pipeline in time.
Furthermore, in order to ensure the cleanness of oil in the hydraulic pipeline and ensure the stability of the system, the hydraulic support system also comprises an oil filter 12, one end of the oil filter 12 is communicated with the oil cylinder 11, and the other end of the oil filter 12 is connected with the hydrostatic pump 13, so that the oil in the oil cylinder 11 is filtered and then is input into the hydrostatic pump 13, and the stability of the system is improved.
The supporting system in the embodiment can be used for installing and supporting a telescope with the diameter of 8m-10m, the lateral supporting system 5, the hydraulic supporting system and the hard point supporting system are jointly supported and adjusted, the gravity of a horizontal shafting of the telescope is borne by oil films in the lateral supporting system 5 and the hydraulic supporting system, so that the resonant frequency of the installed supporting system is 6HZ-8HZ, and in addition, after the whole telescope supporting system is debugged subsequently, the control bandwidth of the supporting system can reach about one half to one quarter, preferably one third, of the resonant frequency of the supporting system.
The oil pressure in the first oil cavity 81 and the second oil cavity 82 in the hydraulic support system is 100 MPa, the rigidity of the first oil film and the second oil film can reach thousands of MPa, and the rigidity of the oil films is enough to support the gravity of a horizontal shaft of the large-caliber telescope. Specifically, in this embodiment, the surface area of the hydraulic oil pad assembly opposite to the left/right stand columns may be 10cm × 10cm, the oil pressure of the oil cavity is several tens of mpa, the contact area between the oil cavity and the left/right stand columns is large, and at this time, the rigidity of the oil film may reach several thousand mpa.
Similarly, the support system of the embodiment can also be used for supporting a telescope with a smaller caliber, such as a telescope with a diameter of 2m-4m, and the resonant frequency of the support system can reach 15HZ-20 HZ.
The adjusting mode of the horizontal shaft of the large-caliber telescope in the embodiment is that after two ends of the horizontal shaft of the large-caliber telescope are installed on the left upright post 61 and the right upright post 62, the lateral support systems 5 at two ends of the left upright post 61 and the right upright post 62 play a supporting role, then the opening degree of the throttle valve 16 is adjusted by monitoring the pressure detected by the pressure sensors at two ends of the first hard point mechanism and the second hard point mechanism to adjust the pressure of the static pressure oil cavity, and further adjust the stress condition of the oil film, namely adjust the rigidity of the oil film, so that the two ends of the first hard point mechanism and the second hard point mechanism are not stressed, namely adjust the rigidity of the oil film in the first oil cavity 81 and the second oil cavity 82 to a proper range, and thereby completing the adjustment of the horizontal shaft.
And the first oil chamber 81 and the second oil chamber 82 are communicated, the pressure of the first oil chamber and the second oil chamber is the same according to the principle of a communicating vessel, the pressure is synchronously adjusted, the bearing direction of the hydraulic support structure is consistent with the azimuth axis, the balanced and consistent stress of shaft heads on two sides of a horizontal shaft can be ensured, the balanced and consistent stress of a pitching shaft system is finally ensured, and the complexity of the adjusting process is reduced.
The invention provides a large-caliber telescope supporting system and a tracking frame, wherein the lateral supporting system and a hard point mechanism have the functions of providing enough axial and lateral rigidity for a horizontal shaft of a large-caliber telescope, and introducing a hydraulic while-tree structure (namely a hydraulic supporting structure) into a pitching shaft system supporting system to ensure that the mounting process of a pitching shaft system conforms to the kinematics positioning principle.
In addition, a hard point mechanism is arranged in an oil cavity limited by the left stand column, the right stand column and the hydraulic oil pad together below the left stand column and the right stand column, the pressure of the oil cavity is adjusted according to the stress condition of the hard point adjusting mechanism, the installation and adjustment time is further reduced, the rigidity of the tracking frame is ensured by enough oil cavity pressure, the moment fluctuation of horizontal shaft load is reduced, and the low-speed tracking capability and the pointing tracking precision of the telescope system are improved.
The hydraulic supporting structure is a static pressure supporting system, generates supporting force by depending on an oil film on a hydraulic cushion, has the characteristics of high rigidity and high sensitivity, and can detect the displacement of the left and right stand columns on the azimuth axis in real time, thereby ensuring that a hard point mechanism only plays a role in monitoring the position by adjusting the opening of the throttle valve without generating a supporting effect.
The embodiments in the present description are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other. The device disclosed by the embodiment corresponds to the method disclosed by the embodiment, so that the description is simple, and the relevant points can be referred to the method part for description.
The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (11)
1. The utility model provides a heavy-calibre telescope braced system which characterized in that, is applied to horizontal shafting and horizontal structure's of horizontal structure in the tracking frame structure horizontal shafting, the shafting includes left stand (61), right stand (62) and this braced system, and this braced system includes: the hydraulic support system comprises a lateral support system (5) and a hydraulic support system, wherein the hydraulic support system comprises an oil cylinder (11), a hydrostatic pump (13), a hydraulic pipeline (15), a throttle valve (16), a first hydraulic oil pad component (31) and a second hydraulic oil pad component (32);
the first hydraulic oil cushion assembly (31) is positioned below the left upright post (61), the left upright post (61) and the first hydraulic oil cushion assembly (31) jointly define a first oil chamber (81), and a first oil film is formed between the surfaces of the first hydraulic oil cushion assembly (31) opposite to the left upright post (61); the second hydraulic cushion assembly (32) is located below the right upright post (62), a second oil cavity (82) is defined by the right upright post (62) and the second hydraulic cushion assembly (32) together, a second oil film is formed between the surfaces, opposite to the right upright post (2), of the second hydraulic cushion assembly (32), the first oil cavity (81) is communicated with the second oil cavity (82), and the pressures of the first oil cavity and the second oil cavity are the same;
the hydrostatic pump (13) is used for pumping the oil in the oil cylinder (11) into the hydraulic pipeline (15), and the throttle valve (16) is positioned on the hydraulic pipeline (15) and used for synchronously controlling the oil pressure of the first oil chamber (81) and the second oil chamber (82) so that the first oil film supports the left upright post (61) and the second oil film supports the right upright post (62).
2. The large aperture telescope support system according to claim 1, further comprising: a first hard spot mechanism (41) located within the first oil chamber (81), and a second hard spot mechanism (42) located within the second oil chamber (82).
3. The support system for a large-caliber telescope according to claim 2, wherein the first hard point mechanism (41) and the second hard point mechanism (42) are identical in structure, and the length of the first hard point mechanism (41) is not telescopic in the direction of gravity.
4. The large aperture telescope support system according to claim 3, wherein the first hard point mechanism (41) comprises a body of fixed length, and a pressure sensor disposed at least at one end of the body.
5. The support system for a large-caliber telescope according to claim 4, wherein the support system further comprises a controller for adjusting the opening degree of the throttle valve (16) according to the stress on the two ends of the first hard point mechanism (41) and the second hard point mechanism (42) to control the oil pressure of the first oil chamber (81) and the second oil chamber (82) so that the stress on the two ends of the first hard point mechanism (41) and the second hard point mechanism (42) is zero.
6. The large aperture telescope support system according to claim 5, further comprising: and one end of the electromagnetic overflow valve (14) is connected with the oil cylinder (11), and the other end of the electromagnetic overflow valve (14) is connected to a hydraulic pipeline between the hydrostatic pump (13) and the throttle valve (16).
7. The large aperture telescope support system according to claim 6, further comprising: and the oil temperature gauge (17) is arranged on the hydraulic pipeline between the first oil chamber (81) and the second oil chamber (82).
8. The large aperture telescope support system according to claim 7, further comprising: an oil filter (12), wherein one end of the oil filter (12) is communicated with the oil cylinder (11), and the other end is connected with the hydrostatic pump (13).
9. The large-caliber telescope support system according to claim 8, wherein the oil pressure in the first oil chamber (81) and the second oil chamber (82) is 100 MPa, and the stiffness of the first oil film and the second oil film is several thousand MPa.
10. The large aperture telescope support system according to claim 9, wherein the support system has a resonant frequency of 6HZ to 8HZ for a telescope with an aperture of 8m to 10m, and 15HZ to 20HZ for a telescope with an aperture of 2m to 4 m.
11. A tracking frame is applied to installation of a large-caliber telescope and is characterized by comprising an azimuth axis system (1), a rotary table (2) located above the azimuth axis system (1) and a horizontal axis system structure, wherein the horizontal axis system structure is arranged on the rotary table (2), and comprises a left upright post (61), a right upright post (62), a four-way joint (7) and the large-caliber telescope supporting system as claimed in any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710927196.2A CN107505700B (en) | 2017-09-30 | 2017-09-30 | Large-caliber telescope supporting system and tracking frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710927196.2A CN107505700B (en) | 2017-09-30 | 2017-09-30 | Large-caliber telescope supporting system and tracking frame |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107505700A CN107505700A (en) | 2017-12-22 |
| CN107505700B true CN107505700B (en) | 2020-03-10 |
Family
ID=60699200
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710927196.2A Active CN107505700B (en) | 2017-09-30 | 2017-09-30 | Large-caliber telescope supporting system and tracking frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107505700B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111367040B (en) * | 2019-12-05 | 2021-12-24 | 中国科学院国家天文台南京天文光学技术研究所 | Hydraulic auxiliary control method and system for height shafting of large astronomical telescope |
| CN113719542A (en) * | 2021-09-16 | 2021-11-30 | 中国科学院国家天文台南京天文光学技术研究所 | Hydraulic damping vertical shock isolation device for large-scale foundation optical infrared telescope |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105479192A (en) * | 2016-01-22 | 2016-04-13 | 武汉樵薪机械制造有限公司 | Oil supply type static-pressure rectification system for support platform |
| CN106950690A (en) * | 2017-05-16 | 2017-07-14 | 谢秀娟 | A kind of primary mirror of astronomical telescope hydraulic support device |
-
2017
- 2017-09-30 CN CN201710927196.2A patent/CN107505700B/en active Active
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105479192A (en) * | 2016-01-22 | 2016-04-13 | 武汉樵薪机械制造有限公司 | Oil supply type static-pressure rectification system for support platform |
| CN106950690A (en) * | 2017-05-16 | 2017-07-14 | 谢秀娟 | A kind of primary mirror of astronomical telescope hydraulic support device |
Non-Patent Citations (1)
| Title |
|---|
| 地基大口径望远镜主镜主动支撑系统综述;胡佳宁等;《激光与红外》;20170131;第47卷(第1期);第5~12页 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107505700A (en) | 2017-12-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107238457B (en) | A kind of low thrust measuring device | |
| EP2613134B1 (en) | System and method for aligning a test article with a load | |
| CN107505700B (en) | Large-caliber telescope supporting system and tracking frame | |
| RU2554668C1 (en) | Rack for measurement of axial force of rocket engine traction | |
| CN107607248B (en) | Explosive explosion impulse and wind pressure load combined test device | |
| CN110895194B (en) | Engine shafting rigidity simulation and loading precision control device | |
| CN103790895A (en) | Hydraulic-cylinder lateral force testing device | |
| CN112683476B (en) | Turbofan engine fan blade multi-axis loading fatigue test stand and method | |
| CN109100420B (en) | Curved surface self-adaptive device for ultrasonic detection | |
| CN109342181B (en) | Brittle material three-dimensional tensile stress test method and replaceable bonding and stretching tool | |
| CN101719700A (en) | Moment motor driving shafting module for inner frame of airborne photoelectric platform | |
| CN103511481B (en) | Rotation positioning device | |
| CN111024310A (en) | Multi-dimensional air flotation follow-up system for satellite high-precision quality measurement | |
| CN105240452A (en) | Local bearing type active vibration isolation device capable of being applied to ultrahigh vacuum system | |
| EP4083590B1 (en) | Sensor assembly, force detection device and method, and construction machinery | |
| CN106425209B (en) | Electronic pillar | |
| WO2021126353A1 (en) | Cardan joint for inertially stabilizing a payload | |
| CN106840650B (en) | Rigidity detection device for rotary speed reducer | |
| CN104007032B (en) | The standard hardness machine of 2 high-precision force sensors of a kind of employing | |
| CN110682085A (en) | Shafting centering method | |
| EP2702295A1 (en) | An integral method for vibration compensation and misalignment prevention in rotor dynamic systems | |
| CN113494660B (en) | Stabilization device and method for stabilizing a fixing element | |
| CN209264312U (en) | Loader torque measures platform | |
| CN110273969B (en) | Flexible and adjustable elastic supporting device | |
| CN114526705A (en) | Method for measuring dynamic non-concentricity of double rotors of aero-engine |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |