CN214565206U - Electric clear water vehicle for airplane - Google Patents
Electric clear water vehicle for airplane Download PDFInfo
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- CN214565206U CN214565206U CN202120205539.6U CN202120205539U CN214565206U CN 214565206 U CN214565206 U CN 214565206U CN 202120205539 U CN202120205539 U CN 202120205539U CN 214565206 U CN214565206 U CN 214565206U
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Abstract
The utility model discloses an electronic driving waterwheel for aircraft relates to aircraft waterwheel technical field, to the current not good problem of electronic waterwheel working property for aircraft, now proposes following scheme, and it includes the waterwheel main part, the top fixedly connected with clean water tank of waterwheel main part, the first water pump of top fixedly connected with of clean water tank, the input of first water pump is connected with the inlet tube, the one end that first water pump was kept away from to the inlet tube extends to the inside of clean water tank, the output of first water pump is connected with the outlet pipe, the top fixedly connected with sewage case of waterwheel main part, the left end of sewage case is equipped with the storage water tank. The utility model discloses can the efficient wash aircraft water inlet department, guarantee when adding water to the aircraft, the clear water can not receive the pollution to can retrieve the sewage after wasing, can not discharge at will on the ground at airport, lead to the ground humidity to skid, influence the security.
Description
Technical Field
The utility model relates to an aircraft clear water car technical field especially relates to an electronic clear water car for aircraft.
Background
In civil aviation transportation field, need use clean drinking water on the aircraft, need supply the clear water to it after every aircraft falls to the ground, aircraft clear water car is the airport ground professional equipment that provides the drinking water to the aircraft, and the product has the drinking water and supplies with the function, consequently need save a large amount of water sources in the clear water car carriage.
The aircraft need wash the water inlet of aircraft earlier before replenishing the clear water to guarantee can not receive the pollution when carrying the clear water, do not possess on the current clear water car and carry out abluent device to it, need the manual water lift of staff to utilize to wipe the water inlet, the operation is complicated, brings inconvenience for the user, for this reason we have proposed an electronic clear water car for aircraft.
SUMMERY OF THE UTILITY MODEL
The utility model provides a pair of electronic clear water car for aircraft has solved the current not good problem of electronic clear water car working property for the aircraft.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
an electric clear water vehicle for an airplane comprises a clear water vehicle main body, wherein a clear water tank is fixedly connected to the top of the clear water vehicle main body, a first water pump is fixedly connected to the top of the clear water tank, the input end of the first water pump is connected with a water inlet pipe, one end, away from the first water pump, of the water inlet pipe extends into the clear water tank, the output end of the first water pump is connected with a water outlet pipe, a sewage tank is fixedly connected to the top of the clear water vehicle main body, a water storage tank is arranged at the left end of the sewage tank, the bottom of the water storage tank is fixedly connected to the top of the clear water vehicle main body, a placing plate is arranged above the sewage tank, vertically arranged hydraulic rods are fixedly connected to four corners of the top of the sewage tank, a piston end of each hydraulic rod is fixedly connected to the bottom of the placing plate, a cleaning tank is fixedly connected to the top of the placing plate, and an annular inner cavity is formed in the peripheral inner wall of the cleaning tank, wash case inner wall all around and seted up a plurality of purge holes, purge hole and annular inner chamber cooperation work, the bottom of wasing the case is connected with the blow off pipe, the top at the sewage case is connected to the one end that the case was washd in the blow off pipe keeping away from, the top fixedly connected with second water pump of storage water tank, the input of second water pump is connected with the raceway, the one end that the second water pump was kept away from to the raceway extends to the inside of storage water tank, the output of second water pump is connected with the drain pipe, the one end that the second water pump was kept away from to the drain pipe is connected at the left end of wasing the case.
Preferably, the top of the clean water tank is provided with a connecting hole, the inner wall of the connecting hole is fixedly connected with a sealing ring along the circumferential direction, the water inlet pipe is connected inside the connecting hole in a sliding manner, and the top of the clean water tank is fixedly connected with a water inlet valve.
Preferably, the top of the water storage tank is provided with a mounting hole, the inner wall of the mounting hole is fixedly connected with a sealing ring along the circumferential direction, and the water delivery pipe is slidably connected inside the mounting hole.
Preferably, the placing plate is provided with a positioning hole, and the sewage draining pipe is connected inside the positioning hole in a sliding manner.
Preferably, the outer wall of the water storage tank is fixedly connected with an input water valve, and the outer wall of the sewage tank is fixedly connected with a drain valve.
Preferably, guard rails are fixedly connected to two sides of the top of the main body of the clean water vehicle.
The utility model discloses in:
through the cooperation of the clean water vehicle main body, the clean water tank, the first water pump, the water inlet pipe, the water outlet pipe, the sewage tank, the water storage tank, the placing plate, the hydraulic rod, the cleaning tank, the annular inner cavity, the blow-off pipe, the positioning hole, the second water pump, the water delivery pipe, the mounting hole, the drain pipe, the input water valve, the drain valve, the protective guard and the connecting hole, on one hand, the clean water vehicle can move through the piston end of the operating hydraulic rod to drive the placing plate to move upwards to drive the cleaning tank to be sleeved outside the airplane water inlet, and through the operation of the second water pump, the clean water in the water storage tank flows into the second water pump from the water delivery pipe and flows into the annular inner cavity through the drain pipe, the water is discharged through the cleaning hole, the periphery of the airplane water inlet positioned in the cleaning tank is comprehensively cleaned, and the cleaned sewage flows into the sewage tank through the blow-off pipe to be recycled, the airplane water adding device can not be randomly arranged on the ground of an airport, so that the ground is wet and slippery, the safety is affected, and on the other hand, when workers add water to an airplane on a water truck main body, the protective guard can be used for enclosing the workers, so that the protective effect is achieved.
To sum up, the utility model discloses can the efficient wash aircraft water inlet department, guarantee when adding water to the aircraft, the clear water can not receive the pollution to can retrieve the sewage after wasing, can not discharge at will on the ground in airport, lead to the ground humidity to skid, influence the security.
Drawings
Fig. 1 is a schematic structural view of an electric clear water vehicle for an aircraft according to the present invention;
FIG. 2 is a schematic structural view of a sewage tank in an electric clear water vehicle for an aircraft according to the present invention;
fig. 3 is the utility model provides a structural schematic diagram of annular inner chamber in electronic clear water wagon for aircraft.
Reference numbers in the figures: 1. a clean water vehicle main body; 2. a clear water tank; 3. a first water pump; 4. a water inlet pipe; 5. a water outlet pipe; 6. a sewage tank; 7. a water storage tank; 8. placing the plate; 9. a hydraulic lever; 10. a cleaning tank; 11. an annular inner cavity; 12. a blow-off pipe; 13. positioning holes; 14. a second water pump; 15. a water delivery pipe; 16. mounting holes; 17. a drain pipe; 18. an input water valve; 19. a drain valve; 20. protecting the fence; 21. and connecting the holes.
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.
Referring to fig. 1-3, an electric clear water vehicle for an airplane comprises a clear water vehicle main body 1, a clear water tank 2 is fixedly connected to the top of the clear water vehicle main body 1, a first water pump 3 is fixedly connected to the top of the clear water tank 2, an input end of the first water pump 3 is connected with a water inlet pipe 4, one end of the water inlet pipe 4, which is far away from the first water pump 3, extends into the clear water tank 2, an output end of the first water pump 3 is connected with a water outlet pipe 5, a sewage tank 6 is fixedly connected to the top of the clear water vehicle main body 1, a water storage tank 7 is arranged at the left end of the sewage tank 6, the bottom of the water storage tank 7 is fixedly connected to the top of the clear water vehicle main body 1, a placing plate 8 is arranged above the sewage tank 6, hydraulic rods 9 which are vertically arranged are fixedly connected to four corners of the top of the sewage tank 6, a piston end of the hydraulic rod 9 is fixedly connected to the bottom of the placing plate 8, a cleaning tank 10 is fixedly connected to the top of the placing plate 8, the inner wall around the cleaning box 10 is provided with an annular inner cavity 11, the inner wall around the cleaning box 10 is provided with a plurality of cleaning holes, the cleaning holes are matched with the annular inner cavity 11 for work, the bottom of the cleaning box 10 is connected with a blow-off pipe 12, the blow-off pipe 12 is an extensible hose, one end of the blow-off pipe 12, which is far away from the cleaning box 10, is connected to the top of the sewage box 6, the top of the water storage box 7 is fixedly connected with a second water pump 14, the input end of the second water pump 14 is connected with a water pipe 15, one end of the water pipe 15, which is far away from the second water pump 14, extends into the water storage box 7, the output end of the second water pump 14 is connected with a drain pipe 17, the drain pipe 17 is an extensible hose, one end of the drain pipe 17, which is far away from the second water pump 14, is connected to the left end of the cleaning box 10, after the airplane lands, the clear water needs to be supplemented to the inside, firstly, the airplane needs to be supplemented with the clear water, firstly, the piston end of the hydraulic rod 9 is operated to move, the placing plate 8 is driven to move upwards, the cleaning box 10 is driven to be sleeved outside the water inlet of the airplane, the clean water in the water storage tank 7 flows into the second water pump 14 from the water delivery pipe 15 by operating the second water pump 14, then flows into the annular inner cavity 11 through the drain pipe 17, water is discharged through the cleaning hole, the periphery of the airplane water inlet positioned in the cleaning box 10 is comprehensively cleaned, the cleaned sewage flows into the sewage tank 6 through the drain pipe 12 to be recycled, the sewage cannot be randomly discharged on the ground of an airport, the ground is wet and slippery, the safety is affected, when the cleaning is finished, the piston end of the hydraulic rod 9 is operated to move downwards, the cleaning box 10 is moved away from the water inlet of the airplane, at the moment, the end part of the water outlet pipe 5 can be connected into the water inlet of the airplane to be discharged, through operation first water pump 3 for the inside clear water of clear water tank 2 gets into in the first water pump 3 through inlet tube 4, and rethread outlet pipe 5 gets into the water inlet of aircraft, saves to the inside of aircraft.
The top of the clean water tank 2 is provided with a connecting hole 21, the inner wall of the connecting hole 21 is fixedly connected with a sealing ring along the circumferential direction, the water inlet pipe 4 is connected inside the connecting hole 21 in a sliding manner, the top of the clean water tank 2 is fixedly connected with a water inlet valve, and the clean water tank 2 is added with clean water by utilizing the water inlet valve.
The working principle is as follows: after the airplane lands on the ground, clear water needs to be supplemented to the interior of the airplane, firstly, the clear water vehicle main body 1 is driven to the airplane needing to be supplemented with the clear water, firstly, the piston end of the operation hydraulic rod 9 moves to drive the placing plate 8 to move upwards and drive the cleaning box 10 to move upwards, the cleaning box 10 is driven to be sleeved outside the airplane water inlet, by operating the second water pump 14, the clear water in the water storage tank 7 flows into the second water pump 14 from the water delivery pipe 15 and then flows into the annular inner cavity 11 through the water discharge pipe 17, water is discharged through the cleaning hole, the periphery of the airplane water inlet in the cleaning box 10 is comprehensively cleaned, and the cleaned sewage flows into the sewage tank 6 through the sewage discharge pipe 12 to be recovered, so that the ground in an airport can not be discharged at will, the ground is moist and slippery, the safety is influenced, after the cleaning is finished, the piston end of the operation hydraulic rod 9 moves downwards, the cleaning tank 10 is moved away from the water inlet outlet of the airplane, the end part of the water outlet pipe 5 can be connected to the water inlet outlet of the airplane, clean water in the clean water tank 2 enters the first water pump 3 through the water inlet pipe 4 by operating the first water pump 3, and then enters the water inlet of the airplane through the water outlet pipe 5 to be stored in the airplane.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are only for convenience of description and to simplify the description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (6)
1. An electric clear water vehicle for an airplane comprises a clear water vehicle main body (1) and is characterized in that a clear water tank (2) is fixedly connected to the top of the clear water vehicle main body (1), a first water pump (3) is fixedly connected to the top of the clear water tank (2), an input end of the first water pump (3) is connected with a water inlet pipe (4), one end, far away from the first water pump (3), of the water inlet pipe (4) extends into the clear water tank (2), an output end of the first water pump (3) is connected with a water outlet pipe (5), a sewage tank (6) is fixedly connected to the top of the clear water vehicle main body (1), a water storage tank (7) is arranged at the left end of the sewage tank (6), the bottom of the water storage tank (7) is fixedly connected to the top of the clear water vehicle main body (1), a placing plate (8) is arranged above the sewage tank (6), and vertically arranged hydraulic rods (9) are fixedly connected to four corners of the top of the sewage tank (6), the piston end of the hydraulic rod (9) is fixedly connected with the bottom of the placing plate (8), the top of the placing plate (8) is fixedly connected with a cleaning box (10), the inner wall around the cleaning box (10) is provided with an annular inner cavity (11), the inner wall around the cleaning box (10) is provided with a plurality of cleaning holes, the cleaning holes are matched with the annular inner cavity (11) to work, the bottom of the cleaning box (10) is connected with a blow-off pipe (12), one end, far away from the cleaning box (10), of the blow-off pipe (12) is connected with the top of the sewage tank (6), the top of the water storage tank (7) is fixedly connected with a second water pump (14), the input end of the second water pump (14) is connected with a water conveying pipe (15), one end, far away from the second water pump (14), of the water conveying pipe (15) extends to the inside of the water storage tank (7), the output end of the second water pump (14) is connected with a water discharging pipe (17), and one end of the drain pipe (17) far away from the second water pump (14) is connected to the left end of the cleaning box (10).
2. The electric clear water vehicle for the aircraft as claimed in claim 1, wherein a connecting hole (21) is formed in the top of the clear water tank (2), a sealing ring is fixedly connected to the inner wall of the connecting hole (21) along the circumferential direction, the water inlet pipe (4) is slidably connected to the inside of the connecting hole (21), and a water inlet valve is fixedly connected to the top of the clear water tank (2).
3. The electric clear water vehicle for the aircraft as claimed in claim 1, wherein a mounting hole (16) is formed at the top of the water storage tank (7), a sealing ring is fixedly connected to the inner wall of the mounting hole (16) along the circumferential direction, and the water pipe (15) is slidably connected to the inside of the mounting hole (16).
4. The electric clear water vehicle for the aircraft as claimed in claim 1, wherein the placing plate (8) is provided with a positioning hole (13), and the sewage discharge pipe (12) is slidably connected inside the positioning hole (13).
5. An electric clear water vehicle for an aircraft according to claim 1, characterized in that the outer wall of the water storage tank (7) is fixedly connected with an input water valve (18), and the outer wall of the sewage tank (6) is fixedly connected with a drain valve (19).
6. An electric clear water vehicle for aircraft according to claim 1, characterized in that guard rails (20) are fixedly connected to both sides of the top of the clear water vehicle main body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120205539.6U CN214565206U (en) | 2021-01-26 | 2021-01-26 | Electric clear water vehicle for airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120205539.6U CN214565206U (en) | 2021-01-26 | 2021-01-26 | Electric clear water vehicle for airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214565206U true CN214565206U (en) | 2021-11-02 |
Family
ID=78371153
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120205539.6U Active CN214565206U (en) | 2021-01-26 | 2021-01-26 | Electric clear water vehicle for airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214565206U (en) |
-
2021
- 2021-01-26 CN CN202120205539.6U patent/CN214565206U/en active Active
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