CN104973246A - Casting cabin opening mechanism of novel casting type six-wheel robot - Google Patents
Casting cabin opening mechanism of novel casting type six-wheel robot Download PDFInfo
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- CN104973246A CN104973246A CN201510406708.1A CN201510406708A CN104973246A CN 104973246 A CN104973246 A CN 104973246A CN 201510406708 A CN201510406708 A CN 201510406708A CN 104973246 A CN104973246 A CN 104973246A
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- China
- Prior art keywords
- hatch door
- cabin
- robot
- wheel robot
- casting
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- Power-Operated Mechanisms For Wings (AREA)
Abstract
本发明公开了一种新型抛投式六轮机器人抛投舱的开舱机构，该机构包括电机、舱门挂钩、舱门等。本发明安装于六轮机器人抛投舱上外壳壁上。本发明针对六轮机器人以及六轮机器人抛投舱结构所设计。强度高，结构简单，维修更换方便。能够有效抵抗运输过程中的振动，确保六轮机器人抛投舱中的机器人安全。适合地震灾区等人员无法到达的特殊区域应用。
The invention discloses a cabin opening mechanism of a novel throwing type six-wheel robot throwing cabin. The mechanism includes a motor, a hatch door hook, a hatch door and the like. The invention is installed on the shell wall of the throwing cabin of the six-wheel robot. The present invention is designed for the structure of the six-wheel robot and the throwing cabin of the six-wheel robot. High strength, simple structure, easy maintenance and replacement. It can effectively resist the vibration during transportation and ensure the safety of the robot in the throwing cabin of the six-wheeled robot. It is suitable for applications in special areas where people cannot reach, such as earthquake-stricken areas.
Description
Technical field
The invention belongs to the field such as aerospace and disaster relief detection.Be particularly useful for needing robot to replace operating personnel cannot enter the situation in feature region.Be related specifically to a kind of throwing type six wheel robot to jettisoning the mechanism of opening the cabin in cabin.
Background technology
With earthquake relief, coring leakage and Special section scouting etc. for application background.Because region environment is unknown, staff cannot enter Active workings safely, creates the robot replacing people's operation in this case.Six wheel robots can be invested in the predetermined area by the present invention like clockwork, guarantee safe while be robot continuation of the journey provide guarantee.
Summary of the invention
The invention reside in and provide a kind of throwing type six wheel robot cabin of jettisoninging and to open the cabin mechanism, give a kind of embodiment be simple and easy to for the existing mode of jettisoninging.Cost of the present invention is low, and installation and maintenance are convenient.The present invention's realization as described below.
One is opened the cabin mechanism, comprises motor, cam mechanism, hatch door hook, hatch door and micro-switch etc.It is characterized in that:
Described motor is DC machine, is driven by external power supply and PLC control cabinet.
Described cam mechanism is by driven by motor cam, and cam is positioned at cam path, and during work, cam path drives hatch door hook around the rotating shaft of hatch door hook and does lever motion.
Described hatch door is high strength elastic cloth, and its one end is fixed on body side, cabin, and opposite side is linked up with by hatch door and caught on, and its intensity can ensure the safety of six wheel robots in transportation, and elastic behavior counteracts the vibration hidden danger that may exist to a certain extent.
The intensity of described high strength elastic cloth is by robot weight and to be equipped on aircraft maximum vibration in flight map and to determine.
Described high strength elastic cloth is designed by the airborne vibration rule of actual experiment parameter, robot weight and aircraft, can use under complex environment.Further, its superior performance is in other materials in actual use, installs easily simultaneously.
Described micro-switch is arranged on hatch door hook base, disconnects motor power when putting in place for hatch door hook.
Accompanying drawing explanation
Fig. 1 closes cabin schematic diagram
Fig. 2 is the schematic diagram that opens the cabin
Fig. 3 is hatch door fixed end enlarged diagram
Wherein mark implication in accompanying drawing as follows:
1, hatch door pressing plate 2, hatch door adapter plate 3, hatch door 4, hatch door hook 5, hatch door button 6, elastic strip
Detailed description of the invention
Fig. 1 is hatch door closed condition schematic diagram of the present invention.Wherein one end of hatch door 3 is fixed on hatch door adapter plate 2 by hatch door pressing plate 1, and the other end of hatch door 3 is fixed with hatch door button 5, and during closedown hatch door, hatch door hook 4 catches on hatch door button 5.Because hatch door 3 is special material, it has good elasticity, also has enough intensity to ensure the safety of cabin inner component simultaneously.
Fig. 2 is hatch door open mode schematic diagram of the present invention.The rear door 3 that opens the cabin is contracted in together under elastic strip 6 acts on, and actv. avoids it to hinder the problems such as Flight Safety.
Fig. 3 is the enlarged drawing of this hatch door fixed end.Rounding place has been done at the arris place that adapter plate 2 contacts with hatch door 3.
Claims (3)
1. open the cabin a mechanism in novel throwing type six wheel robot cabin of jettisoninging, and it is characterized in that: comprise motor, hatch door hook and special hatch door; Motor is linked up with hatch door and is connected by cam mechanism.
2. motor described in is DC machine, is driven by external power supply and PLC control cabinet; Described cam mechanism drives hatch door hook to do lever swing by cam path and realizes opening the cabin.
3. hatch door described in is high strength elastic cloth, and it has good elasticity, also has enough intensity to ensure the safety of cabin inner component simultaneously.Hatch door one end is fixed on jettisonings on cabin, and the other end hangs on hatch door hook.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510406708.1A CN104973246A (en) | 2015-07-12 | 2015-07-12 | Casting cabin opening mechanism of novel casting type six-wheel robot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510406708.1A CN104973246A (en) | 2015-07-12 | 2015-07-12 | Casting cabin opening mechanism of novel casting type six-wheel robot |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104973246A true CN104973246A (en) | 2015-10-14 |
Family
ID=54270324
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510406708.1A Pending CN104973246A (en) | 2015-07-12 | 2015-07-12 | Casting cabin opening mechanism of novel casting type six-wheel robot |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104973246A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818984A (en) * | 2016-05-16 | 2016-08-03 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle satellite intercom with robot device |
| CN106428562A (en) * | 2016-12-01 | 2017-02-22 | 北京理工大学 | Landing buffer device used for rapid laying of laying type detecting robot in the sky |
| CN114735222A (en) * | 2022-05-18 | 2022-07-12 | 安徽工程大学 | A cargo-throwing integrated unmanned aerial vehicle based on carbon fiber sheets |
Citations (7)
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|---|---|---|---|---|
| GB534331A (en) * | 1939-06-01 | 1941-03-05 | John Alfred Richard Goode | Improvements in or relating to grip-and-release devices |
| GB740174A (en) * | 1949-10-12 | 1955-11-09 | Saunders Roe Ltd | Improvements in flying boats |
| US3506222A (en) * | 1967-11-24 | 1970-04-14 | Bell Aerospace Corp | Aircraft supporting device |
| GB1221220A (en) * | 1967-11-10 | 1971-02-03 | Alkan R & Cie | Improvements in or relating to automatic-release retaining devices |
| US3677506A (en) * | 1970-11-23 | 1972-07-18 | Mc Donnell Douglas Corp | Store rack hook assembly |
| US5988567A (en) * | 1997-06-30 | 1999-11-23 | Mcdonnell Douglas | Conformable weapons platform |
| WO2001008972A2 (en) * | 1999-07-14 | 2001-02-08 | Transtechnology Corporation | Downlock-pin actuator apparatus |
-
2015
- 2015-07-12 CN CN201510406708.1A patent/CN104973246A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB534331A (en) * | 1939-06-01 | 1941-03-05 | John Alfred Richard Goode | Improvements in or relating to grip-and-release devices |
| GB740174A (en) * | 1949-10-12 | 1955-11-09 | Saunders Roe Ltd | Improvements in flying boats |
| GB1221220A (en) * | 1967-11-10 | 1971-02-03 | Alkan R & Cie | Improvements in or relating to automatic-release retaining devices |
| US3506222A (en) * | 1967-11-24 | 1970-04-14 | Bell Aerospace Corp | Aircraft supporting device |
| US3677506A (en) * | 1970-11-23 | 1972-07-18 | Mc Donnell Douglas Corp | Store rack hook assembly |
| US5988567A (en) * | 1997-06-30 | 1999-11-23 | Mcdonnell Douglas | Conformable weapons platform |
| WO2001008972A2 (en) * | 1999-07-14 | 2001-02-08 | Transtechnology Corporation | Downlock-pin actuator apparatus |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818984A (en) * | 2016-05-16 | 2016-08-03 | 苏州金建达智能科技有限公司 | Unmanned aerial vehicle satellite intercom with robot device |
| CN106428562A (en) * | 2016-12-01 | 2017-02-22 | 北京理工大学 | Landing buffer device used for rapid laying of laying type detecting robot in the sky |
| CN114735222A (en) * | 2022-05-18 | 2022-07-12 | 安徽工程大学 | A cargo-throwing integrated unmanned aerial vehicle based on carbon fiber sheets |
| CN114735222B (en) * | 2022-05-18 | 2024-09-20 | 安徽工程大学 | Cargo transporting, throwing and throwing integrated unmanned aerial vehicle based on carbon fiber sheet |
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Legal Events
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|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20151014 |
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| WD01 | Invention patent application deemed withdrawn after publication |