CN105000184A - Throwing cabin opening mechanism for throwing type micro robot - Google Patents
Throwing cabin opening mechanism for throwing type micro robot Download PDFInfo
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- CN105000184A CN105000184A CN201510406469.XA CN201510406469A CN105000184A CN 105000184 A CN105000184 A CN 105000184A CN 201510406469 A CN201510406469 A CN 201510406469A CN 105000184 A CN105000184 A CN 105000184A
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- throwing
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- hatch door
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Abstract
本发明公开了一种抛投式微小型机器人抛投舱的开舱机构,该机构包括电机、舱门以及舱门挂钩。本发明安装于微小型机器人抛投舱上,用于在将微小型机器人抛投在特定区域内。本发明针对微小型机器人应用领域设计,机构简单,效率高,维修方便。适合山区探测、搜寻等作业,尤其适用于地震灾区,辐射地区等特殊区域应用。
The invention discloses a mechanism for opening a throwing cabin of a throwing miniature robot, which comprises a motor, a hatch and a hook for the hatch. The invention is installed on the miniature robot throwing cabin, and is used for throwing the miniature robot in a specific area. The invention is designed for the application field of miniature robots, and has simple mechanism, high efficiency and convenient maintenance. It is suitable for detection and search operations in mountainous areas, especially for special areas such as earthquake-stricken areas and radiation areas.
Description
技术领域technical field
本发明属于机器人技术和航空航天领域。特别涉及到一种抛投式两轮机器人抛投舱的开舱机构。针对微小型机器人应用领域设计,适合山区探测、搜寻等作业,尤其适用于地震灾区,辐射地区等特殊区域应用。The invention belongs to the field of robot technology and aerospace. In particular, it relates to a cabin opening mechanism of a throwing two-wheeled robot throwing cabin. Designed for the application field of micro-robots, it is suitable for detection and search operations in mountainous areas, especially for special areas such as earthquake-stricken areas and radiation areas.
背景技术Background technique
以山区探测、搜寻,地震救灾,核化泄漏等特殊场景为应用背景。由于区域内环境未知,人无法直接参与区域作业或无法保证工作人员安全,在类似情景下要求能够对该区域进行预探测工作。该机构针对微小型机器人所设计,能够在预定地点上空将微小型机器人准确无误地投放于特定区域。The application background is in special scenarios such as detection and search in mountainous areas, earthquake relief, and nuclear leakage. Due to the unknown environment in the area, people cannot directly participate in the area operations or cannot guarantee the safety of the staff. In similar scenarios, it is required to be able to carry out pre-detection work in the area. The agency is designed for micro-robots, which can accurately place micro-robots in a specific area over a predetermined location.
发明内容Contents of the invention
本发明在于提供了一种抛投式两轮机器人抛投舱开舱机构,针对现有的抛投方式给出了一种简单易用的实施方案。本发明成本低,安装维修方便。本发明如下所述实现。The present invention provides a throwing two-wheel robot throwing cabin opening mechanism, and provides a simple and easy-to-use implementation scheme for the existing throwing methods. The invention has low cost and convenient installation and maintenance. The present invention is realized as described below.
一种开舱机构,包括电机、凸轮机构、舱门挂钩、舱门以及微动开关等。其特征在于:A hatch opening mechanism includes a motor, a cam mechanism, a hatch hook, a hatch, and a micro switch. It is characterized by:
所述电机为直流电机,通过外置电源以及PLC控制箱驱动。The motor is a DC motor driven by an external power supply and a PLC control box.
所述凸轮机构由电机带动凸轮,凸轮位于凸轮槽内,工作时凸轮槽带动舱门挂钩绕舱门挂钩转轴着做杠杆运动。Described cam mechanism is driven cam by motor, and cam is positioned at cam groove, and cam groove drives hatch door hook to do lever motion around the hatch hook rotating shaft during work.
所述舱门在舱门挂钩动作到位后与舱门挂钩脱开,在弹簧作用下绕着舱门转轴运动,从而实现开舱动作。The hatch door is disengaged from the hatch door hook after the hatch door hook moves in place, and moves around the hatch door shaft under the action of the spring, thereby realizing the opening action.
所述微动开关用于舱门挂钩到位时断开电机电源。The microswitch is used to disconnect the motor power supply when the hatch hook is in place.
根据上述,所述凸轮槽为长方形槽,作用在于保证了舱门在误动作下的开舱危险。According to the above, the cam groove is a rectangular groove, which is used to ensure the danger of opening the cabin door under malfunction.
根据上述,所述弹簧用于在开舱后将舱门拉回到舱体上,避免其可能引起的妨碍机器人出舱、妨碍飞机飞行安全等问题。According to the above, the spring is used to pull the hatch door back to the cabin body after the cabin is opened, so as to avoid possible problems such as preventing the robot from getting out of the cabin and hindering the flight safety of the aircraft.
根据上述,所述微动开关在舱门关闭到位时动作,保证飞行中舱门的安全性。According to the above, the microswitch acts when the cabin door is fully closed to ensure the safety of the cabin door in flight.
根据上述,本发明是基于功能和实际使用所设计,电机、舱门、舱门挂钩等部件都是由卡扣固定于舱体上的,建构简单,安装方便。According to the above, the present invention is designed based on functions and actual use. The components such as the motor, hatch door, and hatch hook are all fixed on the cabin body by buckles, and the structure is simple and easy to install.
附图说明Description of drawings
图1是开舱机构示意图Figure 1 is a schematic diagram of the opening mechanism
图2是凸轮部位剖视示意图Figure 2 is a schematic cross-sectional view of the cam part
其中附图中标记含义如下:The meanings of the marks in the accompanying drawings are as follows:
1、弹簧 2、舱门转轴 3、舱门固定座 4、舱体 5、舱门 6、舱门挂钩 7、舱门挂钩转轴 8、微动开关 9、凸轮槽 10、凸轮 11、电机 12、电机固定架 13、卡扣 14、紧定螺钉1. Spring 2. Hatch door shaft 3. Hatch door fixing seat 4. Cabin body 5. Hatch door 6. Hatch door hook 7. Hatch door hook shaft 8. Micro switch 9. Cam groove 10. Cam 11. Motor 12. Motor fixing frame 13, buckle 14, set screw
具体实施方式Detailed ways
图1为本发明的安装示意图。其中电机11和微动开关8连接于外置电源以及PLC控制箱。工作时PLC给出信号导通电源驱使电机转动。Fig. 1 is the installation diagram of the present invention. Wherein the motor 11 and the micro switch 8 are connected to an external power supply and a PLC control box. When working, the PLC gives a signal to turn on the power supply to drive the motor to rotate.
凸轮10由紧定螺钉14固定于电机11轴上,电机转动时凸轮10转动从而驱动凸轮槽9带动舱门挂钩6绕着舱门挂钩转轴7转动,凸轮10旋转180°时舱门5在弹簧1作用下绕舱门转轴2翻转,从而实现开舱过程。Cam 10 is fixed on the motor 11 shaft by set screw 14, and when motor rotates, cam 10 rotates thereby driving cam groove 9 to drive hatch door hook 6 to rotate around hatch hook rotating shaft 7, and hatch door 5 is on spring when cam 10 rotates 180 °. 1 under the action of flipping around the door shaft 2, thereby realizing the process of opening the cabin.
在重新抛投需关闭舱门时,手工接通电机电源,当舱门挂钩6勾住舱门5后微动开关8动作,使电源断电从而达到精确关舱门过程。When the hatch door needs to be closed for throwing again, the motor power supply is switched on manually, and when the hatch door hook 6 catches the hatch door 5, the micro switch 8 moves, so that the power supply is cut off and thus reaches the process of accurately closing the hatch door.
图2为本发明凸轮部位的剖视图。Fig. 2 is a sectional view of the cam part of the present invention.
Claims (6)
Priority Applications (1)
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CN201510406469.XA CN105000184A (en) | 2015-07-12 | 2015-07-12 | Throwing cabin opening mechanism for throwing type micro robot |
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CN201510406469.XA CN105000184A (en) | 2015-07-12 | 2015-07-12 | Throwing cabin opening mechanism for throwing type micro robot |
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CN201510406469.XA Pending CN105000184A (en) | 2015-07-12 | 2015-07-12 | Throwing cabin opening mechanism for throwing type micro robot |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106044688A (en) * | 2016-07-31 | 2016-10-26 | 于卫华 | Express fuel hover filling technology and device of unmanned aerial vehicle and implementation method |
CN107089331A (en) * | 2017-06-09 | 2017-08-25 | 娄文忠 | A kind of the fire extinguisher bomb jettison system carried and its method of jettisoninging |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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US3677506A (en) * | 1970-11-23 | 1972-07-18 | Mc Donnell Douglas Corp | Store rack hook assembly |
US5350135A (en) * | 1992-01-30 | 1994-09-27 | The Boeing Company | Latch pin inhibitor for folding wing-tip aircraft |
WO2001008972A2 (en) * | 1999-07-14 | 2001-02-08 | Transtechnology Corporation | Downlock-pin actuator apparatus |
US6460445B1 (en) * | 2002-01-07 | 2002-10-08 | Eric P. Young | Playload dispensing system |
CN103015837A (en) * | 2011-09-26 | 2013-04-03 | 梅西耶-布加蒂-道提公司 | Device for operating the door of an aircraft landing gear on the ground |
-
2015
- 2015-07-12 CN CN201510406469.XA patent/CN105000184A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3677506A (en) * | 1970-11-23 | 1972-07-18 | Mc Donnell Douglas Corp | Store rack hook assembly |
US5350135A (en) * | 1992-01-30 | 1994-09-27 | The Boeing Company | Latch pin inhibitor for folding wing-tip aircraft |
WO2001008972A2 (en) * | 1999-07-14 | 2001-02-08 | Transtechnology Corporation | Downlock-pin actuator apparatus |
US6460445B1 (en) * | 2002-01-07 | 2002-10-08 | Eric P. Young | Playload dispensing system |
CN103015837A (en) * | 2011-09-26 | 2013-04-03 | 梅西耶-布加蒂-道提公司 | Device for operating the door of an aircraft landing gear on the ground |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106044688A (en) * | 2016-07-31 | 2016-10-26 | 于卫华 | Express fuel hover filling technology and device of unmanned aerial vehicle and implementation method |
CN107089331A (en) * | 2017-06-09 | 2017-08-25 | 娄文忠 | A kind of the fire extinguisher bomb jettison system carried and its method of jettisoninging |
CN107089331B (en) * | 2017-06-09 | 2019-04-02 | 娄文忠 | A kind of fire extinguisher bomb jettison system carried and its method of jettisoninging |
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