CN216332857U - Active work recognition device for airplane deicing vehicle - Google Patents
Active work recognition device for airplane deicing vehicle Download PDFInfo
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- CN216332857U CN216332857U CN202122750651.0U CN202122750651U CN216332857U CN 216332857 U CN216332857 U CN 216332857U CN 202122750651 U CN202122750651 U CN 202122750651U CN 216332857 U CN216332857 U CN 216332857U
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- deicing
- deicing vehicle
- bevel gear
- fixedly installed
- protective frame
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Abstract
The utility model discloses an active work recognition device of an airplane deicing vehicle, which comprises a deicing vehicle main body, a protective frame and an electric lifting rod, wherein the protective frame and the electric lifting rod are fixedly installed at the top of the deicing vehicle main body; the top of the supporting table is rotatably connected with a rotating table, a transmission bevel gear is fixedly installed at the bottom of the rotating table, a motor groove is formed in the side wall of the supporting table, a speed reducing motor is fixedly installed in the motor groove, a drive bevel gear is fixedly sleeved on the periphery of an output shaft of the speed reducing motor, and the drive bevel gear is in meshing transmission with the transmission bevel gear; and a support column is fixedly arranged at the top of the rotating table. The deicing device can detect the thickness of a deicing part and feed back a deicing operation picture so as to control and adjust the using amount of the deicing agent, save the deicing agent, reduce the using cost, facilitate adjustment and change of a deicing operation position, and has high flexibility and higher safety during operation.
Description
Technical Field
The utility model relates to the technical field of airplane deicing auxiliary equipment, in particular to an active work recognition device for an airplane deicing vehicle.
Background
Airplane deicing efficiency and airport runway deicing efficiency are key factors influencing the forward flight rate and safe flight in winter. At present, airplane deicing liquid adding proportioning stations and runway deicing liquid adding stations are successively built in large and medium airports in China, so that the liquid adding speed of the deicing liquid is increased, and the overall efficiency of deicing operation is improved.
The existing airplane surface deicing operation mostly adopts a mode of manually spraying an airplane deicing agent to deice, and because the thickness of an ice layer on the surface of an airplane is different, the quantity of deicing liquid required to be used is different, so that the waste of the airplane deicing agent is easily caused.
Therefore, the active work recognition device for the airplane deicing vehicle is provided.
SUMMERY OF THE UTILITY MODEL
The utility model mainly aims to provide an active work recognition device of an airplane deicing vehicle, which can effectively solve the problems in the background technology.
In order to achieve the purpose, the utility model adopts the technical scheme that:
an active work recognition device of an airplane deicing vehicle comprises a deicing vehicle main body, a protective frame and an electric lifting rod, wherein the protective frame and the electric lifting rod are fixedly installed at the top of the deicing vehicle main body, and a support table is fixedly installed at the top of the electric lifting rod;
the top of the supporting table is rotatably connected with a rotating table, a transmission bevel gear is fixedly installed at the bottom of the rotating table, a motor groove is formed in the side wall of the supporting table, a speed reducing motor is fixedly installed in the motor groove, a drive bevel gear is fixedly sleeved on the periphery of an output shaft of the speed reducing motor, and the drive bevel gear is in meshing transmission with the transmission bevel gear;
the top installation of revolving stage is fixed with the support column, the top structure of support column has perpendicular groove, erects and is fixed with the extension rod through the bolt installation between the lateral wall in groove, the tip installation of extension rod is fixed with the end plate, the lateral wall installation of extension rod is fixed with the identification plate, infrared sensor and camera are installed to the bottom of identification plate, the cleaner shower nozzle is installed to the bottom of end plate.
Furthermore, intelligent touch-control display screen is installed at the top of protection frame, intelligent touch-control display screen respectively with electric lift pole and gear motor electric connection, intelligent touch-control display screen embeds has intelligent treater, can accept the signal of handling infrared sensor feedback to send work order to electric lift pole and gear motor.
Furthermore, a ladder stand is fixedly arranged at the tail part of the deicing vehicle main body, so that the deicing vehicle is convenient to operate
The worker gets on the top of the deicing vehicle main body and enters the protective frame to operate.
Furthermore, the cross-section structure of protection frame is the U font, and the outer wall of protection frame has the rail through damping hinge connection, through rail and protection frame that can close, security when having improved the operating personnel operation.
Furthermore, a lock catch is movably connected between the fence and the protective frame.
Compared with the prior art, the utility model has the following beneficial effects: the infrared sensor and the camera are arranged, so that the thickness of a deicing part can be conveniently detected, a deicing operation picture can be conveniently fed back, and the timely control and adjustment of the using amount of the deicing agent are facilitated, so that the deicing agent is saved, and the using cost is reduced; the angle and the position of deicing operation can be conveniently adjusted and changed by the arranged speed reducing motor, the driving bevel gear, the transmission bevel gear and the rotating table, so that the flexibility of deicing operation is higher, and the deicing efficiency is improved; through the arrangement of the protective frame and the fence,
the safety of operating personnel during operation is higher, avoids taking place the incident.
Drawings
Fig. 1 is a schematic overall structure diagram of an active work recognition device of an aircraft deicing vehicle according to the present invention.
Fig. 2 is a schematic structural diagram of a rotating table of the active work recognition device of the aircraft deicing vehicle.
Fig. 3 is an enlarged view of a structure a in fig. 1 of an active work recognition device of an aircraft deicing vehicle according to the present invention.
Fig. 4 is an enlarged view of a structure B in fig. 1 of the active work recognition device of the aircraft deicing vehicle according to the present invention.
In the figure: 1. a deicing vehicle main body; 2. a protective frame; 3. a fence; 4. an intelligent touch display screen; 5. an electric lifting rod; 6. a support table; 7. a reduction motor; 8. a drive bevel gear; 9. a drive bevel gear; 10. a rotating table; 11. a support pillar; 12. an extension pole; 13. an end plate; 14. a cleaning agent spray head; 15. a recognition board; 16. An infrared sensor.
Detailed Description
In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the utility model easy to understand, the utility model is further described with the specific embodiments.
As shown in fig. 1-4, an active work recognition device for an aircraft deicing vehicle comprises a deicing vehicle main body 1, a protective frame 2 and an electric lifting rod 5, wherein the protective frame 2 and the electric lifting rod 5 are fixedly installed on the top of the deicing vehicle main body 1, and a support table 6 is fixedly installed on the top of the electric lifting rod 5;
the top of the supporting table 6 is rotatably connected with a rotating table 10, the bottom of the rotating table 10 is fixedly provided with a transmission bevel gear 9, the side wall of the supporting table 6 is provided with a motor groove, a speed reducing motor 7 is fixedly arranged in the motor groove, the periphery of an output shaft of the speed reducing motor 7 is fixedly sleeved with a drive bevel gear 8, and the drive bevel gear 8 is in meshing transmission with the transmission bevel gear 9;
the top installation of revolving stage 10 is fixed with support column 11, the top structure of support column 11 has perpendicular groove, erects and is fixed with extension rod 12 through the bolt installation between the lateral wall in groove, the tip installation of extension rod 12 is fixed with end plate 13, the lateral wall installation of extension rod 12 is fixed with identification plate 15, infrared sensor 16 and camera are installed to identification plate 15's bottom, cleaner shower nozzle 14 is installed to end plate 13's bottom.
Wherein, intelligent touch-control display screen 4 is installed at the top of protective frame 2, intelligent touch-control display screen 4 respectively with electric lift rod 5 and gear motor 7 electric connection, intelligent touch-control display screen 4 embeds has intelligent treater, can accept the signal of handling the 16 feedbacks of infrared sensor to send work order to electric lift rod 5 and gear motor 7.
The crawling ladder is fixedly arranged at the tail of the deicing vehicle main body 1, so that an operator can conveniently climb onto the top of the deicing vehicle main body 1 and enter the protection frame 2 for operation.
The cross-section structure of the protection frame 2 is U-shaped, the outer wall of the protection frame 2 is connected with a fence 3 through a damping hinge, and the safety of an operator during operation is improved through the closable fence 3 and the protection frame 2.
Wherein, a lock catch is movably connected between the fence 3 and the protective frame 2.
The active work recognition device for the airplane deicing vehicle comprises a cleaning agent spray head 14 and a cleaning pump which are communicated before use, when the active work recognition device is used, a driver drives the deicing vehicle body 1 to approach the airplane, an operator climbs the top of the deicing vehicle body 1 through a ladder and closes the fence 3 to lock the fence after entering the protective frame 2, the intelligent touch display screen 4 controls the electric lifting rod 5 and the speed reducing motor 7 to work, meanwhile, the infrared sensor 16 and the camera feed back monitoring signals in time, and the electric lifting rod 5 can change the cleaning mode
The cleaning height of the cleaning agent spray head 14, the output shaft of the speed reducing motor 7 drives the driving bevel gear 8 to rotate, the driving bevel gear 8 and the driving bevel gear 9 are in meshed transmission, and the cleaning position of the cleaning agent spray head 14 is changed.
The foregoing shows and describes the fundamental principles and principal features of the utility model, together with the examples
With novel advantages. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed. The scope of the utility model is defined by the appended claims and equivalents thereof.
Claims (5)
1. An active work recognition device of an airplane deicing vehicle comprises a deicing vehicle main body (1) and is characterized by further comprising a protective frame (2) and an electric lifting rod (5), wherein the protective frame (2) and the electric lifting rod (5) are fixedly installed at the top of the deicing vehicle main body (1), and a support table (6) is fixedly installed at the top of the electric lifting rod (5);
the top of the supporting table (6) is rotatably connected with a rotating table (10), a transmission bevel gear (9) is fixedly installed at the bottom of the rotating table (10), a motor groove is formed in the side wall of the supporting table (6), a speed reduction motor (7) is fixedly installed in the motor groove, a drive bevel gear (8) is fixedly sleeved on the periphery of an output shaft of the speed reduction motor (7), and the drive bevel gear (8) is in meshing transmission with the transmission bevel gear (9);
the top installation of revolving stage (10) is fixed with support column (11), the top structure of support column (11) has perpendicular groove, erects and is fixed with extension rod (12) through the bolt installation between the lateral wall in groove, the tip installation of extension rod (12) is fixed with end plate (13), the lateral wall installation of extension rod (12) is fixed with identification plate (15), infrared sensor (16) and camera are installed to the bottom of identification plate (15), cleaner shower nozzle (14) are installed to the bottom of end plate (13).
2. An aircraft deicing vehicle active operation identification device as claimed in claim 1, wherein: intelligent touch display screen (4) are installed at the top of protective frame (2), intelligent touch display screen (4) respectively with electric lift pole (5) and gear motor (7) electric connection.
3. An aircraft deicing vehicle active operation identification device as claimed in claim 1, wherein: the tail part of the deicing vehicle main body (1) is fixedly provided with a ladder stand.
4. An aircraft deicing vehicle active operation identification device as claimed in claim 1, wherein: the cross-section structure of protection frame (2) is the U font, and the outer wall of protection frame (2) has rail (3) through damping hinge connection.
5. An aircraft deicing vehicle active operation identification device as claimed in claim 4, wherein: a lock catch is movably connected between the fence (3) and the protective frame (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122750651.0U CN216332857U (en) | 2021-11-11 | 2021-11-11 | Active work recognition device for airplane deicing vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122750651.0U CN216332857U (en) | 2021-11-11 | 2021-11-11 | Active work recognition device for airplane deicing vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216332857U true CN216332857U (en) | 2022-04-19 |
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ID=81137338
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122750651.0U Active CN216332857U (en) | 2021-11-11 | 2021-11-11 | Active work recognition device for airplane deicing vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216332857U (en) |
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2021
- 2021-11-11 CN CN202122750651.0U patent/CN216332857U/en active Active
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