CN109297370B - Elastic clamping type connector centering device - Google Patents
Elastic clamping type connector centering device Download PDFInfo
- Publication number
- CN109297370B CN109297370B CN201811157593.7A CN201811157593A CN109297370B CN 109297370 B CN109297370 B CN 109297370B CN 201811157593 A CN201811157593 A CN 201811157593A CN 109297370 B CN109297370 B CN 109297370B
- Authority
- CN
- China
- Prior art keywords
- frame
- connecting frame
- carriage
- swing arm
- docking
- 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
- 238000003032 molecular docking Methods 0.000 claims abstract description 43
- 230000007246 mechanism Effects 0.000 claims description 32
- 230000003068 static effect Effects 0.000 abstract description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 231100000331 toxic Toxicity 0.000 description 1
- 230000002588 toxic effect Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Conveying And Assembling Of Building Elements In Situ (AREA)
- Details Of Connecting Devices For Male And Female Coupling (AREA)
Abstract
一种弹性夹持式连接器对中装置,包括连接框组件、对接框、若干对中气缸等;底座上安装导轨,滑架安装在导轨上,主推进气缸驱动滑架沿导轨运动;对接框四角分别通过摆臂连接至滑架侧面,对接框通过摆臂相对滑架摆动;连接框组件中安装设备B,对接框通过边框两侧的支撑耳片与连接框组件上的滑轨配合,辅助推进气缸驱动连接框组件沿滑轨移动,移动方向与导轨方向一致;对接框上安装若干对中气缸,用于夹紧设备A,并调节设备A的位置与设备B对准。本发明可用于火箭加注用连接器与火箭上活门间的位置自动对中,也可用于其它静止或相对运动间物体的位置自动定位、跟随。
An elastic clamping type connector centering device, including a connecting frame assembly, a docking frame, a number of centering cylinders, etc.; a guide rail is installed on the base, a carriage is installed on the guide rail, and a main propulsion cylinder drives the carriage to move along the guide rail; the butting frame The four corners are respectively connected to the side of the carriage through the swing arm, and the docking frame swings relative to the carriage through the swing arm; the device B is installed in the connecting frame assembly, and the docking frame cooperates with the slide rails on the connecting frame assembly through the supporting lugs on both sides of the frame to assist The advancing cylinder drives the connecting frame assembly to move along the slide rail, and the moving direction is consistent with the direction of the guide rail; several alignment cylinders are installed on the docking frame to clamp equipment A and adjust the position of equipment A to align with equipment B. The invention can be used for the automatic alignment of the position between the rocket filling connector and the upper valve of the rocket, and can also be used for the automatic positioning and tracking of the position of other objects in static or relative motion.
Description
技术领域technical field
本发明属于运载火箭自动对接技术领域,涉及一种对中装置。The invention belongs to the technical field of automatic docking of launch vehicles, and relates to a centering device.
背景技术Background technique
在现有技术中,位于箭体底部的连接器较多采用了自动对接技术,基本实现了箭体尾部、低温燃料加注的自动对接,对接时连接器与活门位置相对静止,而在高空连接器与活门有较大相对运动速度情况下尚未见型号应用实例报道,位于高空的连接器大多在总装测试厂房内完成人工对接或半自动对接。In the prior art, the connector located at the bottom of the rocket body mostly adopts the automatic docking technology, which basically realizes the automatic docking of the tail of the rocket body and low-temperature fuel filling. When the relative movement speed of the valve and the valve is relatively large, there is no report on the application of the model. Most of the connectors located at high altitudes are manually docked or semi-automatically docked in the final assembly test workshop.
火箭加注用连接器与火箭上活门相对静止,连接一般靠人力对接,劳动强度大;在燃料泄漏等特殊情况下工作环境恶劣,危险性较大。The connector for rocket filling and the upper valve of the rocket are relatively static, and the connection is generally connected by manpower, which is labor-intensive; in special circumstances such as fuel leakage, the working environment is harsh and the danger is high.
发明内容SUMMARY OF THE INVENTION
本发明要解决的技术问题是:克服现有技术不足,提供一种弹性夹持式连接器对中装置,可用于火箭加注用连接器与火箭上活门间的位置自动对中,也可用于其它静止或相对运动间物体的位置自动定位、跟随。The technical problem to be solved by the present invention is to overcome the deficiencies of the prior art and provide an elastic clamping connector centering device, which can be used for automatic centering of the position between the rocket filling connector and the upper valve of the rocket, and can also be used for The position of other stationary or relative moving objects is automatically positioned and followed.
本发明所采用的技术方案是:一种弹性夹持式连接器对中装置,包括连接框组件、对接框、若干对中气缸、主推进气缸、辅助推进气缸、摆臂、滑架、导轨、底座;The technical scheme adopted in the present invention is: an elastic clamping connector centering device, comprising a connecting frame assembly, a docking frame, several centering cylinders, a main propulsion cylinder, an auxiliary propulsion cylinder, a swing arm, a sliding frame, a guide rail, base;
底座上安装导轨,滑架安装在导轨上,主推进气缸驱动滑架沿导轨运动;The guide rail is installed on the base, the carriage is installed on the guide rail, and the main propulsion cylinder drives the carriage to move along the guide rail;
对接框四角分别通过摆臂连接至滑架侧面,对接框通过摆臂相对滑架摆动;The four corners of the docking frame are respectively connected to the sides of the carriage through swing arms, and the docking frame swings relative to the carriage through the swing arms;
连接框组件中安装设备B,对接框通过边框两侧的支撑耳片与连接框组件上的滑轨配合,辅助推进气缸驱动连接框组件沿滑轨移动,移动方向与导轨方向一致;对接框上安装若干对中气缸,用于夹紧设备A,并调节设备A的位置与设备B对准。Device B is installed in the connecting frame assembly, the docking frame cooperates with the slide rails on the connecting frame assembly through the support lugs on both sides of the frame, and the auxiliary propelling cylinder drives the connecting frame assembly to move along the sliding rail, and the moving direction is consistent with the direction of the guide rail; Install several centering cylinders to clamp device A and adjust the position of device A to align with device B.
所述的弹性夹持式连接器对中装置,还包括下支撑气缸,下支撑气缸安装在滑架侧面,下支撑气缸的输出轴与摆臂的支撑杆接触,分别从下方调整摆臂的位置。The elastic clamping connector centering device also includes a lower support cylinder, the lower support cylinder is installed on the side of the carriage, the output shaft of the lower support cylinder is in contact with the support rod of the swing arm, and the position of the swing arm is adjusted from below. .
所述的弹性夹持式连接器对中装置,还包括侧支撑气缸,侧支撑气缸安装在滑架侧面,侧支撑气缸的输出轴与摆臂的支撑杆接触,从侧面调整摆臂的位置。The elastic clamping connector centering device further includes a side support cylinder installed on the side of the carriage, and the output shaft of the side support cylinder is in contact with the support rod of the swing arm to adjust the position of the swing arm from the side.
所述连接框组件包括滑轨、若干拉绳机构、连接框;连接框两侧安装滑轨,拉绳机构安装在连接框外壁上,用于拉紧安装在连接框内的设备B。The connecting frame assembly includes a sliding rail, several pulling rope mechanisms, and a connecting frame; the sliding rails are installed on both sides of the connecting frame, and the pulling rope mechanism is installed on the outer wall of the connecting frame for tightening the equipment B installed in the connecting frame.
所述拉绳机构包括压紧盖、弹簧、拉杆、钢丝绳、滚轮、滚轮座、弹簧座;钢丝绳一端与设备B连接,另一端绕过滚轮与拉杆连接,滚轮安装在连接框外壁上;拉杆穿过弹簧座中心孔,弹簧座安装在连接框上,压紧盖固定在拉杆上,压紧盖与弹簧座间安装弹簧,在弹簧作用下拉杆相对弹簧座滑动。The pulling rope mechanism includes a pressing cover, a spring, a pulling rod, a wire rope, a roller, a roller seat, and a spring seat; one end of the wire rope is connected to the equipment B, and the other end is connected to the pulling rod around the roller, and the roller is installed on the outer wall of the connection frame; Through the center hole of the spring seat, the spring seat is installed on the connecting frame, the pressing cover is fixed on the pull rod, the spring is installed between the pressing cover and the spring seat, and the rod slides relative to the spring seat under the action of the spring.
所述对接框的四边框中心处分别安装一个对中气缸,对中气缸的输出轴分别与对接框的各边框垂直,从上、下、左、右四个方向夹紧设备A。A centering cylinder is installed at the center of the four frames of the docking frame, and the output shaft of the centering cylinder is perpendicular to each frame of the docking frame, and the device A is clamped from four directions: top, bottom, left, and right.
所述摆臂包括滑块组件、支撑杆,支撑杆两端分别通过滑块组件与滑架、对接框连接。The swing arm includes a slider assembly and a support rod, and two ends of the support rod are respectively connected with the slide frame and the docking frame through the slider assembly.
所述滑块组件包括十字块、滑块座、销轴I、销轴II,十字块安装在支撑杆端部,十字块通过相互垂直的销轴I、销轴II与滑块座的安装孔配合,滑块座安装在对接框或滑架上。The slider assembly includes a cross block, a slider seat, a pin shaft I, and a pin shaft II. The cross block is installed at the end of the support rod, and the cross block passes through the mounting holes of the pin shaft I, the pin shaft II and the slider seat that are perpendicular to each other. Matching, the slider seat is installed on the docking frame or the sliding frame.
所述连接框的顶面安装两组拉绳机构,两组拉绳机构关于连接框的中心轴对称;每组包括两个沿连接框中心轴布置的拉绳机构,两个拉绳机构中的钢丝绳拉伸方向相反。Two sets of rope pulling mechanisms are installed on the top surface of the connecting frame, and the two sets of rope pulling mechanisms are symmetrical about the central axis of the connecting frame; each group includes two rope pulling mechanisms arranged along the central axis of the connecting frame, and one of the two rope pulling mechanisms The wire rope stretches in the opposite direction.
所述连接框的两侧面分别安装一组拉绳机构,每组包括两个沿连接框中心轴布置的拉绳机构,两个拉绳机构中的钢丝绳拉伸方向相反。Two sides of the connecting frame are respectively installed with a group of pulling rope mechanisms, each group includes two pulling rope mechanisms arranged along the central axis of the connecting frame, and the wire ropes in the two pulling rope mechanisms are drawn in opposite directions.
本发明与现有技术相比的优点在于:The advantages of the present invention compared with the prior art are:
(1)本发明可用于静止或运动中两物体的相对位置自动定位、跟随。如火箭加注连接器与火箭上活门的自动对接。特别适可用于如下场合,如:有毒等气体环境;应急处理系统,人工无法在规定时间内迅速完成工作;大雾、雨、雪等气候,人工不便处理。(1) The present invention can be used to automatically locate and follow the relative positions of two objects in motion or in motion. Such as the automatic docking of the rocket filling connector and the valve on the rocket. It is especially suitable for the following occasions, such as: toxic and other gas environments; emergency treatment system, manual work cannot be completed quickly within the specified time; heavy fog, rain, snow and other climates, manual processing is inconvenient.
(2)本发明方法可实现火箭加注连接器210与活门间的三个自由度位置精确自动调整跟踪,也可用于其它对夹持物体的三个自由度位置精确自动调整,并可根据需要与静止或运动中目标物的位置自动跟踪。(2) The method of the present invention can realize the precise automatic adjustment and tracking of the positions of the three degrees of freedom between the
(3)本发明控制原理简单,气缸实现对中调整。不需要位置检测元件,不需要伺服控制系统。系统可靠性高,环境适应性强。(3) The control principle of the present invention is simple, and the cylinder can realize centering adjustment. No position detection element is required, no servo control system is required. The system has high reliability and strong environmental adaptability.
附图说明Description of drawings
图1为本发明的对中装置的结构示意图;Fig. 1 is the structural representation of the centering device of the present invention;
图2为连接框的右视图;Fig. 2 is the right side view of the connection frame;
图3为连接框的主视图;Fig. 3 is the front view of the connection frame;
图4为滑块组件的俯视图。Figure 4 is a top view of the slider assembly.
具体实施方式Detailed ways
下面结合附图对本发明进行进一步说明。The present invention will be further described below with reference to the accompanying drawings.
如图1所示,对中装置包括连接框组件、对接框3、对中气缸4(包括上对中气缸、下对中气缸、侧对中气缸)、支撑气缸(包括下支撑气缸5、侧支撑气缸6)、主推进气缸、辅助推进气缸、摆臂1、滑架9、导轨8、底座7。As shown in Figure 1, the centering device includes a connecting frame assembly, a
底座7上安装导轨8,滑架9安装在导轨8上,主推进气缸驱动滑架9沿导轨8运动;对接框3四角分别通过摆臂1连接至滑架9侧面,对接框3通过摆臂1相对滑架9摆动;连接框组件中安装火箭加注用连接器210,对接框3通过边框两侧的支撑耳片与连接框组件上的滑轨21配合,辅助推进气缸驱动连接框组件沿滑轨21移动,移动方向与导轨8方向一致;对接框3上安装若干对中气缸4,用于夹紧火箭上活门,并调节火箭上活门的位置与火箭加注用连接器210对准;下支撑气缸5安装在滑架9侧面,下支撑气缸5的输出轴与摆臂1的支撑杆接触,分别从下方调整摆臂1的位置。侧支撑气缸6安装在滑架9侧面,侧支撑气缸6的输出轴与摆臂1的支撑杆接触,从侧面调整摆臂1的位置。The guide rail 8 is installed on the
连接框组件包括滑轨21、若干拉绳机构、连接框2;连接框2两侧安装滑轨21,拉绳机构安装在连接框2外壁上,用于拉紧安装在连接框2内的火箭加注用连接器210。连接框2如图2、图3所示,连接框2安装固定在对接框3上。连接框2上安装有滑轨21,在辅助推进气缸作用下可相对对接框3在图示左、右方向运动。连接框2的顶面安装两组拉绳机构、,两组拉绳机构关于连接框2的中心轴对称;连接框2的两侧面分别安装一组拉绳机构,每组包括两个沿连接框2中心轴布置的拉绳机构,两个拉绳机构中的钢丝绳25拉伸方向相反。The connecting frame assembly includes a
连接框2上安装有多组拉绳机构。图3所示,拉绳机构包括压紧盖28、弹簧27、拉杆26、钢丝绳25、滚轮24、滚轮座23、弹簧座22。钢丝绳25一端与火箭加注连接器210连接,另一端绕过滚轮24与拉杆26连接,滚轮24安装在连接框2外壁上。拉杆26穿过弹簧座22中心孔,弹簧座22安装在连接框2上,可相对弹簧座22滑动。压紧盖28与拉杆26固定在一起。压紧盖28与弹簧座22间安装有弹簧27。如图2所示,通过拉绳机构将火箭加注连接器210固定在连接框2中部位置。A plurality of groups of pulling rope mechanisms are installed on the
对接框3右侧上、下、左、右各安装有一组对中气缸4,当对接框3前端与火箭位置较近时,通过安装在对接框3上的四组气缸从上、下、左、右四个方向夹紧火箭上活门,实现连接框2与上活门的中心位置对中,火箭加注连接器210安装在连接框2的中部,从而实现火箭加注连接器210与上活门的位置对中。A set of centering cylinders 4 are installed on the upper, lower, left and right sides of the
对接框3与滑架9间通过四组摆臂1连接。四组摆臂1平行布置,两端均通过滑块组件分别与滑架9、对接框3连接,摆臂1包括滑块组件、支撑杆,支撑杆两端分别通过滑块组件与滑架9、对接框3连接。滑块组件见图4。滑块组件包括十字块13、滑块座14、销轴I11、销轴II12,十字块13安装在支撑杆端部,十字块13通过相互垂直的销轴I11、销轴II12与滑块座14的安装孔配合,滑块座14安装在对接框3或滑The
架9上。摆臂1左端通过滑块组件与支撑座连接。在外力作用下,通过四组摆臂1的协调控制作用,对接框3可相对滑架9摆动。on shelf 9. The left end of the swing arm 1 is connected with the support seat through the slider assembly. Under the action of external force, the
底座7上安装有主推进气缸,实现上方整个装置的前进、后退。A main propulsion cylinder is installed on the
火箭加注连接器210与活门位置对中工作原理:How the
初始位置,火箭加注连接器210与活门间保持一定距离。主推进气缸收回,使火箭加注连接器210位于远离活门位置。对中气缸4均收回。各支撑气缸均伸出,使摆臂1处于初始位置。通过拉绳机构,使火箭加注连接器210固定在连接框2中部位置。In the initial position, a certain distance is maintained between the
主推气缸伸出,推动滑架9等向图1所示左向运动。当对接框3前端顶紧在火箭表面,则停止前进。在进退气缸推动下,如火箭在图示左右方向摆动,对接框3右侧可保持始终均与火箭贴合。The main push cylinder is extended to push the carriage 9 to move to the left as shown in FIG. 1 . When the front end of the
各对中气缸4伸出,对中气缸4前端与火箭上活门周边贴合,保持气缸推力不变,可使对接框3始终与火箭上活门相对位置保持不变。Each centering cylinder 4 is extended, and the front end of the centering cylinder 4 is attached to the periphery of the rocket upper valve to keep the cylinder thrust unchanged, so that the relative position of the
辅助推进气缸前进,可推动火箭加注连接器210与活门贴合。当二者位置有差异特别是有小角度偏差时,火箭加注连接器210位置可通过拉绳机构微调,最后通过火箭加注连接器210的连接机构将火箭加注连接器210与活门连接在一起。The auxiliary propulsion cylinder moves forward, which can push the
火箭加注连接器210与活门解脱时,步骤与上述相反。When the
本发明未详细说明部分属于本领域技术人员公知技术。The parts of the present invention that are not described in detail belong to the well-known technology of those skilled in the art.
Claims (8)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811157593.7A CN109297370B (en) | 2018-09-30 | 2018-09-30 | Elastic clamping type connector centering device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811157593.7A CN109297370B (en) | 2018-09-30 | 2018-09-30 | Elastic clamping type connector centering device |
Publications (2)
Publication Number | Publication Date |
---|---|
CN109297370A CN109297370A (en) | 2019-02-01 |
CN109297370B true CN109297370B (en) | 2020-09-18 |
Family
ID=65161435
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201811157593.7A Active CN109297370B (en) | 2018-09-30 | 2018-09-30 | Elastic clamping type connector centering device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN109297370B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116294841B (en) * | 2023-02-13 | 2023-08-11 | 东方空间技术(山东)有限公司 | An automatic docking device for a rocket air conditioner winch |
CN116788528A (en) * | 2023-06-09 | 2023-09-22 | 重庆科技学院 | An automatic rocket fuel filling system |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101398277A (en) * | 2008-11-06 | 2009-04-01 | 上海交通大学 | Robot system for implementing amphibious automatic butt joint and releasing for rocket |
CN104613826A (en) * | 2015-02-06 | 2015-05-13 | 南京理工大学 | Automatic docking and falling connector with active follow-up function of carrier rocket |
CN105066795A (en) * | 2015-07-03 | 2015-11-18 | 北京航天发射技术研究所 | Connector rotation docking automatic shedding recovery device |
CN205589530U (en) * | 2016-03-22 | 2016-09-21 | 南京理工大学 | Automatic butt joint of carrier rocket adds lets out simple and easy position appearance compensation mechanism of connector |
CN105953666A (en) * | 2016-01-08 | 2016-09-21 | 璧电函 | Space docking error compensation mechanism |
CN107627259A (en) * | 2017-10-25 | 2018-01-26 | 北京航天发射技术研究所 | The adaptive centralising device in mechanical hydraulic servo position and method |
-
2018
- 2018-09-30 CN CN201811157593.7A patent/CN109297370B/en active Active
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN101398277A (en) * | 2008-11-06 | 2009-04-01 | 上海交通大学 | Robot system for implementing amphibious automatic butt joint and releasing for rocket |
CN104613826A (en) * | 2015-02-06 | 2015-05-13 | 南京理工大学 | Automatic docking and falling connector with active follow-up function of carrier rocket |
CN105066795A (en) * | 2015-07-03 | 2015-11-18 | 北京航天发射技术研究所 | Connector rotation docking automatic shedding recovery device |
CN105953666A (en) * | 2016-01-08 | 2016-09-21 | 璧电函 | Space docking error compensation mechanism |
CN205589530U (en) * | 2016-03-22 | 2016-09-21 | 南京理工大学 | Automatic butt joint of carrier rocket adds lets out simple and easy position appearance compensation mechanism of connector |
CN107627259A (en) * | 2017-10-25 | 2018-01-26 | 北京航天发射技术研究所 | The adaptive centralising device in mechanical hydraulic servo position and method |
Also Published As
Publication number | Publication date |
---|---|
CN109297370A (en) | 2019-02-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN109297370B (en) | Elastic clamping type connector centering device | |
CN111761349A (en) | A drive shaft press machine | |
CN110470453B (en) | Low-speed wind tunnel air refueling hose-taper sleeve dynamic characteristic test device | |
CN203804168U (en) | Floating-type sand-core clamping mechanism | |
CN109896049B (en) | A Cartesian coordinate flexible non-contact connector automatic docking device and method | |
CN112975794A (en) | Positioning and clamping device for outer wing of airplane | |
CN203473966U (en) | Movable sucker structure of clamping mechanism | |
CN107199554B (en) | Unmanned aerial vehicle maintains debugging robot fast | |
CN213013938U (en) | Bridge erects with supplementary interfacing apparatus convenient to align | |
CN117722551A (en) | Gas drainage pipe network leak hunting and leak repairing integrated device | |
CN117921583A (en) | Quick-mounting pipeline clamping equipment and pipeline machining device | |
CN206085056U (en) | Manipulator suitable for marine buoy automatic coupling | |
CN219624979U (en) | Automatic gas tightness detects frock | |
CN105666022A (en) | Rotatable parallel flexible clamp for thin sheets | |
CN202741998U (en) | Pipeline automatic fastening precise docking assembly and movable docking assembly | |
CN213921547U (en) | An automatic fixing device for aircraft wheels | |
CN212374270U (en) | A clamping and positioning device that can meet multiple specific rotation angles | |
CN107627259B (en) | Machine-hydraulic servo position self-adaptive centering device and method | |
CN208697220U (en) | Workpiece clamping platform with inner step feature | |
CN205630614U (en) | Three -branch six -degree -of -freedom robot | |
CN109373177B (en) | A connecting rod type three-degree-of-freedom position adjustment device | |
CN110844117A (en) | A Generalized Docking Test System Based on Multi-DOF Parallel Mechanism | |
CN218619040U (en) | Single-cylinder parallel clamping device | |
CN222732418U (en) | A recovery device for a water pipeline leakage detection robot | |
CN110398327A (en) | A PE saddle-type bypass pipe fittings airtightness testing machine |
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 |