CN205256675U - Climb electronic aircraft of wall operation - Google Patents
Climb electronic aircraft of wall operation Download PDFInfo
- Publication number
- CN205256675U CN205256675U CN201520861178.5U CN201520861178U CN205256675U CN 205256675 U CN205256675 U CN 205256675U CN 201520861178 U CN201520861178 U CN 201520861178U CN 205256675 U CN205256675 U CN 205256675U
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- China
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- aircraft
- wall
- power
- climb
- management system
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Abstract
The utility model provides a climb electronic aircraft of wall operation. It is main including aircraft body, screw, motor system, supporting wheel and power management system. This aircraft can be stabilized and for a long time attached to on the wall to can accomplish the wall high altitude construction of specific kind. This aircraft can replace the artifical high altitude construction who accomplishes on the wall to avoid the personal safety risk and reduce the operating cost.
Description
Technical field
The utility model relates to Electric aircraft.
Background technology
The factor such as the body that known unmanned remote control Electric aircraft causes due to wind-force disturbance rocks and cruising time is short, be difficult to scouring, spraying etc. on wall to positioning accuracy request relatively high and long-term job task.
Summary of the invention
In order to solve, the existence of Electric aircraft body is rocked and cruising time is short, be difficult to the problem of long operation of high and duration of positioning accuracy request, the utility model provides a kind of and can be attached on wall and Electric aircraft that can be easily mobile, this aircraft can replace the work high above the ground manually completing on wall, thereby has avoided personal safety risk and reduced operating cost.
The Electric aircraft that the utility model provides, mainly comprises aircraft body, screw, electric motor system, support wheel and power-supply management system. Wherein electric motor system comprises the driver of motor and motor.
For aircraft can be attached on wall to improve positioning precision and can easily move, on aircraft provided by the utility model, be provided with support wheel, support wheel is connected with aircraft by its rotating shaft. In real work, the edge of support wheel is against on wall, aircraft tilts to wall, thereby there is the thrust component of a sensing wall in the thrust that makes screw generation, this thrust component makes support wheel and between the walls exist certain pressure, just can aircraft is attached on wall reposefully by the frictional force of support wheel and between the walls thus. Because support wheel can be around being positioned at carry-on rotating shaft rotation, therefore, by the rotation of support wheel, aircraft can slide to realize necessary position and move on wall.
Work continuously in order to realize for a long time, the power supply mode of aircraft provided by the utility model is: adopt long lead power taking from surface power supply equipment. For this reason, on aircraft provided by the utility model, be provided with power-supply management system. The power-supply management system that the utility model proposes, refer to the electrical system that electric energy is processed, this system has electrical input terminal and electric output, and there is buck functionality (being that the output voltage of system is lower than its input voltage), this system can will be processed from the relatively high electric energy of voltage of its input input, and output is applicable to the relatively low electric energy of voltage that electric motor system uses. Power-supply management system can be DC-DC power module. Power-supply management system is fixed on aircraft body.
Power supply unit is electrically connected with the input of carry-on power-supply management system by long lead, thus by the delivery of electrical energy of power supply unit to power-supply management system, the output of power-supply management system is electrically connected with the input of electric motor system. The electric energy that power-supply management system provides power supply unit is done, after necessary processing (as step-down, filtering), to offer electric motor system. Power supply unit can be generator.
Because power-supply management system has buck functionality, therefore when real work, the input voltage (being the output voltage of power supply unit) of power-supply management system can arrange very highly, its meaning is: between power supply unit and power-supply management system, can adopt less electric current to carry out delivery of electrical energy, thereby reduce the loss of electric energy on transfer wire.
In order to realize specific job task, on Electric aircraft provided by the utility model, specific power tool can be set, power tool can be wiper (for cleaning the windows etc.), can be also spray gun (for spraying operation), can be also giant (for cleaning). In the time that power tool is spray gun or hydraulic giant, can between power tool and ground, connect liquid transfer tube, for supplying required fluent material.
For the ease of the remote control in operation process, on Electric aircraft provided by the utility model, camera and wireless image transmission can be installed, thereby can monitor in real time operation process.
In order to realize flexible operation, on Electric aircraft provided by the utility model, mechanical arm can be installed, and power tool is fixed on mechanical arm. In order to reduce weight, mechanical arm can adopt carbon fibre material to make. Can also fixing camera on mechanical arm.
The beneficial effects of the utility model are: proposed a kind of Electric aircraft that is suitable for climbing wall operation, this aircraft can be stablized and be attached on wall for a long time, thereby can complete the wall work high above the ground of particular types. This aircraft can replace the work high above the ground manually completing on wall, to avoid personal safety risk and to reduce operating cost.
Brief description of the drawings
Fig. 1 is the side view of Electric aircraft that the utility model provides.
Fig. 2 is the top view of Electric aircraft that the utility model provides.
In figure, 1. aircraft body, 2. support bar, 3. screw (comprises screw 3.1, screw 3.2, screw 3.3, screw 3.4), 4. support wheel (comprising support wheel 4.1 and support wheel 4.2), 5. the spoke of support wheel (comprises spoke 5.1, spoke 5.2, spoke 5.3), 6. mechanical arm, 7. power tool (glass cleaner), 8. liquid memory, 9. woven hose, 10. shower nozzle, 11. cameras, 12. power-supply management systems, 13. wires, 14. power supply units, 15. joint of mechanical arm, 16. bodies of wall, 17. glass, the rotating shaft of 18. support wheels, 19. drive the electric motor system (comprising electric motor system 19.1 and electric motor system 19.2) of screw.
Detailed description of the invention
In Fig. 1, the plane at screw (3) place of four rotor Electric aircrafts (1) tilts, and the thrust that screw (3) produces has thus existed a lateral thrust component towards body of wall (16). It is upper that this lateral thrust makes support wheel (4) be against body of wall (16), and the frictional force between support wheel (4) and body of wall (16) is positioned on ad-hoc location aircraft (1) more reposefully, the drift of having avoided external disturbance (as wind is disturbed) to be caused. Power supply unit (14) rest on the ground, and the output of power supply unit (14) is electrically connected with the input of power-supply management system (12) by wire (13). The electric energy that power-supply management system (12) provides power supply unit (14) is done, after step-down processing, to offer electric motor system (19) and mechanical arm (6). The end of mechanical arm (6) is provided with power tool (7), and in the present embodiment, power tool (7) is glass cleaner. In addition, for auxiliary cleaning operation, be also provided with liquid memory (8) on aircraft (1), it is upper that the cleaning agent in liquid memory (8) is sprayed onto glass (17) by shower nozzle (10), in order to auxiliary cleaning operation. It is upper that camera (11) is arranged on mechanical arm (6), in order to real-time monitoring.
In the present embodiment, the V375B12C300AL module that power-supply management system (12) adopts Vicor company of the U.S. to produce, the input voltage of this series module is 375V, and output voltage is 12V, power output 300W, with inner filter circuit. Support wheel (4) is made of plastics with spoke (5), and the rotating shaft (18) of support wheel is carbon fiber pipe.
Claims (5)
1. climb wall operation Electric aircraft for one kind, mainly comprise aircraft body, electric motor system, screw, it is characterized in that: on aircraft, be provided with power-supply management system and the support wheel with buck functionality, wherein the output of power-supply management system and the input of electric motor system are electrically connected, and support wheel is connected with aircraft by its rotating shaft.
2. climb according to claim 1 wall operation Electric aircraft, it is characterized in that: on aircraft, be provided with mechanical arm.
3. climb according to claim 1 wall operation Electric aircraft, it is characterized in that: on aircraft, be provided with wiper and liquid storage device.
4. climb according to claim 1 wall operation Electric aircraft, it is characterized in that: on aircraft, be provided with shower nozzle.
5. climb according to claim 1 wall operation Electric aircraft, it is characterized in that: on aircraft, be provided with camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520861178.5U CN205256675U (en) | 2015-11-02 | 2015-11-02 | Climb electronic aircraft of wall operation |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520861178.5U CN205256675U (en) | 2015-11-02 | 2015-11-02 | Climb electronic aircraft of wall operation |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205256675U true CN205256675U (en) | 2016-05-25 |
Family
ID=55998220
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520861178.5U Expired - Fee Related CN205256675U (en) | 2015-11-02 | 2015-11-02 | Climb electronic aircraft of wall operation |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205256675U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107013018A (en) * | 2017-03-01 | 2017-08-04 | 浙江大学 | A kind of high-rise outer rendering robot |
-
2015
- 2015-11-02 CN CN201520861178.5U patent/CN205256675U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107013018A (en) * | 2017-03-01 | 2017-08-04 | 浙江大学 | A kind of high-rise outer rendering robot |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160525 Termination date: 20161102 |