CN212951184U - Airplane cleaning structure set device - Google Patents
Airplane cleaning structure set device Download PDFInfo
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- CN212951184U CN212951184U CN202020715837.5U CN202020715837U CN212951184U CN 212951184 U CN212951184 U CN 212951184U CN 202020715837 U CN202020715837 U CN 202020715837U CN 212951184 U CN212951184 U CN 212951184U
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Abstract
The utility model discloses an aircraft washs structure group device, including electrical system, longmen traveling system, AGV dolly, spraying system, automatic platform and drying system, electrical system should include PLC control system, servo transmission system, system human-computer interface and operating panel, longmen traveling system includes portal frame, removal robotic arm, flexible arm, servo motor and sensor, spraying system, automatic platform and drying system all install on the AGV dolly, spraying system comprises water pump, water pipeline and sprinkler bead, drying system comprises high pressure positive blower, tuber pipe and tuyere. The utility model discloses a be provided with control converter adjusting water pump, adjust water flow and pressure, and then make the cleaning performance of aircraft better, at abluent in-process, can carry out drying process to the surface of aircraft, and then make the cleaning of aircraft become automatic, it is extravagant to have reduced the manpower, makes work efficiency obtain improving convenient to use.
Description
Technical Field
The utility model relates to an aircraft washing technical field specifically is aircraft washing structure group device.
Background
In daily life, the airplane facilitates people going out from various places, when the airplane flies at high altitude, because the air temperature of the high altitude is low, ice is easily formed and adsorbed on the outer surface of the airplane when the air in the high altitude is contacted with the outer wall of the airplane, when ice, snow and frost are adhered to the surface of the airplane, the aerodynamic effect and the operation performance of the airplane are seriously affected, namely the lift force of the airplane is reduced, the ice, snow and frost are adhered to all air inlets of the airplane, the operation of airplane systems, engines or parts is abnormal, a captivity or a static pressure detecting port outside the airplane body can cause wrong flight data if blockage or deformation occurs, the misoperation of an automatic flight operation system can be caused, transparent ice on the airplane body falls off in the operation process of the airplane, the airplane body or the engines can be damaged, and therefore, when the airplane goes out, the outer wall of the airplane needs to be cleaned, therefore, when the airplane flies, substances such as ice, snow, frost and the like are prevented from being adsorbed on the outer surface of the airplane, the safety of the airplane during flying is further improved, and the airplane is convenient to use.
However, most of the existing methods for washing airplanes use manual cleaning and then use mechanical cleaning, which wastes a lot of manpower and material resources and a lot of time during each cleaning process, and further, the efficiency of washing airplanes is low and the use is inconvenient, so that an airplane washing structure set device is needed to solve the above problems.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an aircraft washs structure group device to the manual work that proposes in solving above-mentioned background washs the aircraft, extravagant problem of a large amount of manpowers and time.
In order to achieve the above object, the utility model provides a following technical scheme: aircraft washs structure group device, including electrical system, longmen traveling system, AGV dolly, spraying system, automatic platform and drying system, electrical system should include PLC control system, servo transmission system, system human-computer interface and operating panel, longmen traveling system includes portal frame, removal robotic arm, flexible arm, servo motor and sensor, spraying system, automatic platform and drying system all install on the AGV dolly, spraying system comprises water pump, water pipeline and sprinkler bead, drying system comprises high pressure positive blower, tuber pipe and tuyere.
Preferably, the PLC control system comprises a PLC main station and two remote local slave stations, the main station is placed in the control room, the remote local slave stations are respectively placed on two sides of the gantry, the main station and the slave stations are connected through the Ethernet, the slave stations respectively collect signals of the subsystems on two sides, the signals comprise water flow, pressure, limiting signals and encoder signals, control commands are sent, and the control commands comprise control of starting and stopping of a water pump, starting and stopping of a fan, movement of a mechanical arm and gantry walking.
Preferably, the human-computer interface, the operation panel, the display screen, the computer and the wireless router are placed in an operation room for centralized control, two operation rooms are arranged for remote control and remote or local operation, the two operation rooms are controlled in an interlocking mode and do not interfere with each other, the second operation room cannot be controlled when the first operation room is controlled, and the first operation room cannot be operated when the second operation room is controlled.
Preferably, the transmission system controls the operation of the servo motor and the water pump through a servo driver and a frequency converter, and the PLC controls the servo driver and the frequency converter through analog quantity signals, adjusts the frequency of the motor and controls the rotating speed of the motor, so that the movement of the mechanical arm and the flow of the water pump are controlled.
Preferably, 2 to 3 mobile mechanical arms are respectively arranged on the left side, the right side and the upper side of the portal frame, each mechanical arm is provided with a telescopic arm, each telescopic arm is provided with a rotating part, and the rotating part is provided with a high-pressure water spray head and a high-pressure air blowing nozzle or cleans a rotary mop.
Preferably, two walking gears are respectively arranged below the left frame and the right frame of the gantry, the electric control system controls the gantry to move and walk on the guide rail, the electric control system controls the mechanical arms to move up and down and left and right, controls the spraying system, the automatic platform and the drying system, and can respectively and simultaneously move the mechanical arms up and down and left and right and walk the gantry, control water spraying and air blowing, and respectively clean and dry the head, the middle part, the tail part, the side wings and the empennage of the airplane.
Preferably, every arm afterbody is equipped with the water spray nozzle, the blowout water is fan-shaped, the water pump passes through water pipeline to the clear water and reaches the shower nozzle, adjust discharge and water pressure through the converter, can install flow sensor and pressure sensor additional between water pump and the shower nozzle, flow value and pressure value feedback PLC to, PLC passes through logical operation, the control converter adjusts the water pump, adjust water flow and pressure, the position greasy dirt degree that the fan is different, different positions bear pressure or mechanical strength is different, the flow and the pressure of control water can satisfy above-mentioned demand.
Preferably, the drying and dehumidifying device consists of a high pressure fan, an air pipe and an air nozzle, high pressure gas blown out by the air heater is contacted with the drying and dehumidifying device to generate hot air, and the fan adopts two schemes: first, traditional contactor control fan starts, and the starting current ratio is great, causes great impact to the electric wire netting, probably causes the switch trip, and is also higher to the capacity requirement of the transformer that advances to net, consequently starts the fan through PLC logical operation, and the second, the converter starts the fan, can adjust amount of wind and wind pressure like this according to the demand.
Preferably, the automation platform is built by using an Ethernet, and a PLC, a human-computer interface, a remote local slave station, a mobile phone or a tablet computer exchange data through a router.
In a second aspect, embodiments of the present invention provide systems for aircraft cleaning structural groups, the systems comprising the aircraft cleaning structural group device and system of any one of the claims.
Compared with the prior art, the beneficial effects of the utility model are that: this aircraft washs structure group device is provided with belt cleaning device, and wherein belt cleaning device should include several major systems: electric control system, longmen traveling system, the AGV dolly, a spraying system, drying system, wherein electric control system control can drive operating panel and carry out self-cleaning system, electric control system can be respectively simultaneously to each arm about operation and longmen walking, control water spray and blow, respectively to aircraft head, middle part, afterbody, flank, the washing and the drying of fin, and then accomplish the self-cleaning process, the water pump passes through the water pipeline to the clear water and reaches the shower nozzle, adjust discharge and water pressure through the converter. Can install flow sensor and pressure sensor additional between water pump and the shower nozzle, feed back PLC to flow value and pressure value, PLC passes through logical operation, and control converter regulation water pump adjusts water flow and pressure, and then makes the cleaning performance of aircraft better, at abluent in-process, can carry out drying process to the surface of aircraft, and then makes the cleaning of aircraft work become automatic, has reduced the manpower extravagant, makes work efficiency obtain improving convenient to use.
Drawings
Fig. 1 is a schematic front view of the present invention;
fig. 2 is a schematic top view of the present invention;
fig. 3 is a schematic front view of the robot arm of the present invention;
fig. 4 is a schematic flow chart of the control system of the present invention;
fig. 5 is a schematic diagram of the control flow of the operating room system of the present invention.
In the figure: 1. a gantry; 2. a mechanical arm; 3. a servo motor; 4. a telescopic arm; 5. a gear guide rail; 6. A rotating assembly; 7. an electric telescopic rod; 8. a sprinkler head; 9. a blowing head; 10. scrubbing the mop.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-5, the present invention provides a first embodiment:
aircraft washs structure group device, including electrical system, longmen traveling system, the AGV dolly, spraying system, automated platform and drying system, electrical system should include PLC control system, servo transmission system, system human-computer interface and operating panel, PLC control system includes a PLC main website, and two long-range local slave stations, the main website is put at the control room, long-range local slave station is put respectively in the longmen both sides, main website and slave station pass through the ethernet and connect, the slave station gathers the signal of both sides branch system respectively, including discharge, pressure, spacing signal, the encoder signal, send control command, start including control water pump and stop, the fan opens and stops, 2 removal of arm and longmen walking, can put to wash for the surface to the aircraft entirely, and easy operation, high durability and convenient use, and abluent efficiency is higher, manual operation has been reduced, high durability and convenient use.
The human-computer interface, operating panel, the display screen, the computer, wireless router all puts an operation room centralized control, set up two operation room remote control, long-range or local operation, two operation rooms are interlocking control, mutual noninterference, operation room two can not be controlled during operation room one control, operation room one can not be operated during operation room two controls, can accomplish remote control and wash, make two operation rooms can not take place the condition of interference simultaneously, and then make control washing that the operation room can be better wash and dry mechanism washs the aircraft, the operation is simple, high durability and convenient use.
The gantry traveling system comprises a gantry frame 1, a movable mechanical arm, a telescopic arm 4, a servo motor 3 and a sensor, a transmission system controls the servo motor 3 and a water pump to operate by a servo driver and a frequency converter, a PLC controls the servo driver and the frequency converter through analog quantity signals, the frequency of the motor is adjusted, and the rotating speed of the motor is controlled, so that the mechanical arm 2 is controlled to move and the flow of the water pump is controlled, the water pump can be adjusted according to the actual cleaning condition, the cleaning effect of the cleaning mechanism on the airplane is better, and the use is convenient.
2 to 3 removal robotic arm are arranged respectively on a portal frame 1, the left side, the right, the last side both sides, have an arm that can stretch out and draw back on every arm 2, and install rotary part on every arm that can stretch out and draw back, install high pressure water sprayhead 8, high pressure blast nozzle on the rotary part or clean rotatory mop, can accomplish the back in the washing, clean and dry the outer wall machinery of aircraft, and then make the quick use of aircraft, easy operation, convenient to use.
Two walking gears are respectively arranged below a left frame and a right frame of the gantry, the electric control system controls the gantry to move and walk on the guide rail, the electric control system controls the mechanical arms 2 to move up and down and left and right, and controls the spraying system, the automatic platform and the drying system, the electric control system can respectively and simultaneously operate the mechanical arms 2 up and down, left and right and walk the gantry, control water spraying and air blowing, and respectively clean and dry the head, the middle part, the tail part, the side wings and the empennage of the airplane, so that the airplane is more complete in cleaning position, better in cleaning efficiency and convenient to.
2 afterbody of every arm is equipped with the water spray nozzle, the blowout water is fan-shaped, the water pump passes through water pipeline to the clear water and reaches the shower nozzle, adjust discharge and water pressure through the converter, can install flow sensor and pressure sensor additional between water pump and the shower nozzle, flow value and pressure value feedback PLC, PLC is through logical operation, control converter regulation water pump, adjust out water flow and pressure, the position greasy dirt degree that the fan is different, different positions bear pressure or mechanical strength different, the flow and the pressure of control water can satisfy above-mentioned demand, and then abluent cleaner, avoid some ice, snow and frost clearance are incomplete, and then make abluent more thorough.
Spraying system, automatic platform and drying system all install on the AGV dolly, and spraying system comprises water pump, water pipeline and sprinkler bead 8, and drying system comprises high pressure positive blower, tuber pipe and tuyere, and the high-pressure gas that blows off through the air heater contacts with dry dehydrating unit, produces hot-blastly, two kinds of schemes of this fan simultaneously: first, traditional contactor control fan starts, and the starting current is than great, causes great impact to the electric wire netting, probably causes the switch trip, and is also higher to the capacity requirement of the transformer that advances to net, consequently starts the fan through PLC logical operation, and the second, the converter starts the fan, can adjust amount of wind and wind pressure like this according to the demand, can carry out the strip to the efficiency of drying and adjust to make the efficiency of drying better, convenient to use.
The automatic platform is built through the Ethernet, the PLC, the human-computer interface, the remote local slave station, the mobile phone or the tablet personal computer exchange data through the router, and then the automatic platform terminal is enabled to control the cleaning mechanism and the drying mechanism, so that the cleaning process of the airplane is fully automated, the labor force is reduced, the cleaning efficiency of the airplane is improved, and the use is convenient.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (9)
1. Aircraft washs structure group device, its characterized in that: including electrical system, longmen traveling system, AGV dolly, spray system, automatic platform and drying system, electrical system includes PLC control system, servo transmission system, system human-computer interface and operating panel, longmen traveling system includes portal frame (1), removes robotic arm, flexible arm (4), servo motor (3) and sensor, spray system, automatic platform and drying system all install on the AGV dolly, spray system comprises water pump, water pipeline and sprinkler bead (8), drying system comprises high pressure positive blower, tuber pipe and tuyere.
2. An aircraft washing structure group arrangement according to claim 1, characterised in that: the PLC control system comprises a PLC master station and two remote local slave stations, the master station is placed in a control room, the remote local slave stations are placed on two sides of a gantry respectively, the master station and the slave stations are connected through an Ethernet, the slave stations collect signals of subsystems on two sides respectively, the signals comprise water flow, pressure, limiting signals and encoder signals, control commands are sent, and the control commands comprise control of starting and stopping of a water pump, starting and stopping of a fan, movement of a mechanical arm (2) and gantry walking.
3. An aircraft washing structure group arrangement according to claim 1, characterised in that: the human-computer interface, the operation panel, the display screen, the computer and the wireless router are placed in an operation room for centralized control, two operation rooms are arranged for remote control and remote or local operation, the two operation rooms are controlled in an interlocking mode and do not interfere with each other, the second operation room cannot be controlled when the first operation room is controlled, and the first operation room cannot be operated when the second operation room is controlled.
4. An aircraft washing structure group arrangement according to claim 1, characterised in that: the transmission system controls the operation of the servo motor (3) and the water pump through a servo driver and a frequency converter, and the PLC controls the servo driver and the frequency converter through analog quantity signals, adjusts the frequency of the motor, and controls the rotating speed of the motor, so that the movement of the mechanical arm (2) and the flow of the water pump are controlled.
5. An aircraft washing structure group arrangement according to claim 1, characterised in that: 2 to 3 mobile mechanical arms are respectively arranged on the left side, the right side and the upper side of the portal frame (1), each mechanical arm (2) is provided with a telescopic arm, each telescopic arm is provided with a rotating part, and the rotating parts are provided with high-pressure water spray heads (8) and high-pressure air blowing nozzles or are used for scrubbing rotating mops.
6. An aircraft washing structure group arrangement according to claim 5, characterised in that: two walking gears are respectively arranged below the left frame and the right frame of the gantry, the electric control system controls the gantry to move and walk on the guide rail, the electric control system controls the mechanical arms (2) to move up and down and left and right, controls the spraying system, the automatic platform and the drying system, and can respectively and simultaneously move the mechanical arms (2) up and down and left and right and walk the gantry, control water spraying and air blowing, and respectively clean and dry the head, the middle part, the tail part, the side wings and the empennage of the aircraft.
7. An aircraft washing structure group arrangement according to claim 1, characterised in that: every arm (2) afterbody is equipped with the water spray nozzle, the blowout water is fan-shaped, the water pump passes through water pipeline to the clear water and reaches the shower nozzle, adjust discharge and water pressure through the converter, can install flow sensor and pressure sensor additional between water pump and the shower nozzle, flow value and pressure value feedback PLC to, PLC passes through logical operation, control converter regulation water pump, adjust water flow and pressure, the position greasy dirt degree that the fan is different, different positions bear pressure or mechanical strength is different, the flow and the pressure of control water can satisfy above-mentioned demand.
8. An aircraft washing structure group arrangement according to claim 1, characterised in that: the drying and dehumidifying device is composed of a high-pressure fan, an air pipe and an air nozzle, high-pressure gas blown out by the air heater is in contact with the drying and dehumidifying device to generate hot air, and the fan adopts two schemes simultaneously: first, traditional contactor control fan starts, and the starting current ratio is great, causes great impact to the electric wire netting, probably causes the switch trip, and is also higher to the capacity requirement of the transformer that advances to net, consequently starts the fan through PLC logical operation, and the second, the converter starts the fan, can adjust amount of wind and wind pressure like this according to the demand.
9. An aircraft washing structure group arrangement according to claim 1, characterised in that: the automation platform is built by Ethernet, and a PLC, a human-computer interface, a remote local slave station, a mobile phone or a tablet computer exchange data through a router.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020715837.5U CN212951184U (en) | 2020-04-30 | 2020-04-30 | Airplane cleaning structure set device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020715837.5U CN212951184U (en) | 2020-04-30 | 2020-04-30 | Airplane cleaning structure set device |
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| CN212951184U true CN212951184U (en) | 2021-04-13 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113044235A (en) * | 2021-04-14 | 2021-06-29 | 中国航空规划设计研究总院有限公司 | Automatic surface treatment system for airplane and use method thereof |
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2020
- 2020-04-30 CN CN202020715837.5U patent/CN212951184U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113044235A (en) * | 2021-04-14 | 2021-06-29 | 中国航空规划设计研究总院有限公司 | Automatic surface treatment system for airplane and use method thereof |
| CN113044235B (en) * | 2021-04-14 | 2022-06-24 | 中国航空规划设计研究总院有限公司 | Automatic surface treatment system for airplane and using method thereof |
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