CN209191911U - A kind of aircarrier aircraft wheel self-filler - Google Patents
A kind of aircarrier aircraft wheel self-filler Download PDFInfo
- Publication number
- CN209191911U CN209191911U CN201821803947.6U CN201821803947U CN209191911U CN 209191911 U CN209191911 U CN 209191911U CN 201821803947 U CN201821803947 U CN 201821803947U CN 209191911 U CN209191911 U CN 209191911U
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- air inlet
- inlet pipe
- electric box
- gas
- charging connection
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Abstract
The utility model discloses a kind of aircarrier aircraft wheel self-fillers, belong to airplane wheel air charging system technical field.It is provided with inflator in the middle part of the device noumenon, and device noumenon two sides are provided with explosion-proof cage；Two sides are provided with alarm lamp at the top of the electric box, and touch screen and emergency stop switch are provided on the chamber door of electric box, the electric box is internally provided with air inlet pipe and control power supply, and air inlet pipe runs through electric box, the aircarrier aircraft wheel self-filler is designed as binary channels output, configuration is suitble to the quick-release gas-charging connection of each wheel charging valve, the wheel of two different model different pressures demands can be inflated simultaneously, the blowing pressure is set as required according to different wheels, it is automatically controlled using PLC, meet client's diversity requirement, improves work efficiency；The wheel self-filler, highest output pressure meet all airline carriers of passengers wheel the blowing pressures up to 275PSI.
Description
Technical field
The utility model relates to a kind of aircarrier aircraft wheel self-fillers, belong to airplane wheel air charging system technology neck
Domain.
Background technique
Aircarrier aircraft wheel the blowing pressure maximum pressure reaches 235PSI, and traditional automatic aerator highest the blowing pressure is about
200PSI is unable to satisfy the wheel inflation of institute's organic type, and is single channel output, is only a tyre inflating every time,
Working efficiency is low.
Summary of the invention
In view of the above-mentioned problems, the technical problem to be solved by the present invention is to provide a kind of aircarrier aircraft wheel automatic inflatings
Device.
The aircarrier aircraft wheel self-filler of the utility model, it includes device noumenon, inflator and explosion-proof cage, institute
It is provided with inflator in the middle part of the device noumenon stated, and device noumenon two sides are provided with explosion-proof cage；
The inflator includes alarm lamp, electric box, touch screen, air inlet pipe, pressure reducer, solenoid valve, check valve, first
Internal thread threeway, pressure sensor, the second internal thread threeway, internal-screw ball valve, tracheae, cable assembly, 8V1 gas-charging connection, 12V1 inflation
Connector, waterproof connector, emergency stop switch and control power supply, two sides are provided with alarm lamp at the top of the electric box, and electric box
Touch screen and emergency stop switch are provided on chamber door, the electric box is internally provided with air inlet pipe and control power supply, and air inlet pipe
Through electric box, the air inlet pipe is equipped with two groups altogether, and air inlet pipe and electric box junction are provided with waterproof connector, described
The inlet end of air inlet pipe is disposed with pressure reducer, solenoid valve, check valve, pressure sensor and internal-screw ball valve, the pressure
Sensor is connect by the first internal thread threeway with air inlet pipe, and the internal-screw ball valve is connected by the second internal thread threeway and air inlet pipe
It connects, the outlet side of the air inlet pipe is connect with tracheae, and the tracheae front end is provided with 8V1 gas-charging connection and 12V1 inflation connects
Head, and 8V1 gas-charging connection and 12V1 gas-charging connection are fixed by cable assembly and air inlet pipe.
Preferably, the air inlet pipe is connect with nitrogen cylinder.
Preferably, the solenoid valve is fixedly connected by mounting plate with electrical box body.
Preferably, being connected between the 8V1 gas-charging connection, 12V1 gas-charging connection and tracheae by male and female quick union
It connects.
Preferably, the solenoid valve, pressure sensor are electrically connected with touch screen.
Compared with prior art, the utility model has the beneficial effects that the aircarrier aircraft wheel self-filler designs
For binary channels output, configuration is suitble to the quick-release gas-charging connection of each wheel charging valve, can be simultaneously to two different model difference pressures
The wheel of power demand is inflated, and the blowing pressure is set as required according to different wheels, is automatically controlled using PLC, meets client
Diversity requirement improves work efficiency；The wheel self-filler, highest output pressure meet all up to 275PSI
Airline carriers of passengers wheel the blowing pressure.
Detailed description of the invention
Fig. 1 is the overall structure diagram of the utility model；
Fig. 2 is the inflator schematic diagram of internal structure of the utility model；
Fig. 3 is the air inlet pipe piping diagram of the utility model.
Appended drawing reference: device noumenon 1, explosion-proof cage 3, alarm lamp 4, electric box 5, touch screen 6, air inlet pipe 7, subtracts inflator 2
Depressor 8, solenoid valve 9, check valve 10, the first internal thread threeway 11, pressure sensor 12, the second internal thread threeway 13, internal-screw ball valve 14,
Tracheae 15, cable assembly 16,8V1 gas-charging connection 17,12V1 gas-charging connection 18, waterproof connector 19, emergency stop switch 20, control power supply
21。
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
As shown in Figure 1-Figure 3, present embodiment uses following technical scheme: it includes device noumenon 1, inflator 2
With explosion-proof cage 3, inflator 2 is provided in the middle part of the device noumenon 1, and 1 two sides of device noumenon are provided with explosion-proof cage 3；
The inflator 2 includes alarm lamp 4, electric box 5, touch screen 6, air inlet pipe 7, pressure reducer 8, solenoid valve 9, unidirectional
Valve 10, the first internal thread threeway 11, pressure sensor 12, the second internal thread threeway 13, internal-screw ball valve 14, tracheae 15, cable assembly 16,
8V1 gas-charging connection 17,12V1 gas-charging connection 18, waterproof connector 19, emergency stop switch 20 and control power supply 21, the electric box 5
Top two sides are provided with alarm lamp 4, and touch screen 6 and emergency stop switch 20 are provided on the chamber door of electric box 5, the electric box
5 are internally provided with air inlet pipe 7 and control power supply 21, and air inlet pipe 7 runs through electric box 5, and the air inlet pipe 7 and nitrogen cylinder connect
Connect, the air inlet pipe 7 is equipped with two groups altogether, and air inlet pipe 7 and 5 junction of electric box are provided with waterproof connector 19, it is described into
The inlet end of tracheae 7 is disposed with pressure reducer 8, solenoid valve 9, check valve 10, pressure sensor 12 and internal-screw ball valve 14, described
Solenoid valve 9 be fixedly connected by mounting plate with 5 cabinet of electric box, the pressure sensor 12 pass through the first internal thread threeway 11
It is connect with air inlet pipe 7, the internal-screw ball valve 14 is connect by the second internal thread threeway 13 with air inlet pipe 7, the air inlet pipe 7
Outlet side is connect with tracheae 15, and 15 front end of tracheae is provided with 8V1 gas-charging connection 17 and 12V1 gas-charging connection 18, and 8V1
Gas-charging connection 17 and 12V1 gas-charging connection 18 are fixed by cable assembly 16 and air inlet pipe 7, the 8V1 gas-charging connection 17,
It is connected between 12V1 gas-charging connection 18 and tracheae 15 by male and female quick union.
The solenoid valve 9, pressure sensor 12 are electrically connected with touch screen 6, are filled using high-precision pressure sensor detection
Air pressure force value sets the blowing pressure according to different wheels using PLC all-in-one machine programming Control as required, is automatically performed inflation and makees
Industry meets all airline carriers of passengers wheel inflation requirements.
Working principle: first use will inflator installation with by upper position, pressure reducer 8 directly connects when inflation among side
Nitrogen cylinder is connect, pneumatic head one end enters in cage from steel plate mesh, opens the cage door of explosion-proof cage 3, is pushed into tire, pneumatic head and wheel
Tire connection, can start to inflate after locking explosion-proof 3 cage door of cage.
Pressure reducer 8 connects nitrogen cylinder, powers on, and opens nitrogen cylinder, and pressure regulator valve recalls atmospheric pressure slightly larger than needed for tire
Pressurising power connects pneumatic head and wheel air inflation nozzle；After powering on, touch screen 6 shows main interface, unscrews emergency stop switch 20, clicks boundary
Face, successively sets bound, the blowing pressure upper limit value needed for inputting by " Enter " (if pressure needed for tire is 221PSI, on
Limit is set as 222, lower limit set 220), it clicks " starting " and starts to inflate；When inflation, the corresponding Amber Alerts lamp of alarm lamp 4
It lights, Amber Alerts lamp extinguishes after the completion of inflation, and green is lighted prompting inflation and completed, and clicks " stopping " after the completion of inflation, green
Warning lamp extinguishes, and opens inflation cage door, pulls up gas-charging connection；Gas source is closed, is pressed " emergency stop switch ", cutting inflation electromechanical source.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (5)
1. a kind of aircarrier aircraft wheel self-filler, it is characterised in that: it includes device noumenon (1), inflator (2) and prevents
Quick-fried cage (3), the device noumenon (1) middle part is provided with inflator (2), and device noumenon (1) two sides are provided with explosion-proof cage
(3)；
The inflator (2) includes alarm lamp (4), electric box (5), touch screen (6), air inlet pipe (7), pressure reducer (8), electromagnetism
Valve (9), check valve (10), the first internal thread threeway (11), pressure sensor (12), the second internal thread threeway (13), internal-screw ball valve
(14), tracheae (15), cable assembly (16), 8V1 gas-charging connection (17), 12V1 gas-charging connection (18), waterproof connector (19), emergency stop
(20) and control power supply (21) are switched, two sides are provided with alarm lamp (4) at the top of the electric box (5), and the case of electric box (5)
Touch screen (6) and emergency stop switch (20) are provided on door, the electric box (5) is internally provided with air inlet pipe (7) and control electricity
Source (21), and air inlet pipe (7) runs through electric box (5), the air inlet pipe (7) is equipped with two groups, and air inlet pipe (7) and electric box altogether
(5) junction is provided with waterproof connector (19), and the inlet end of the air inlet pipe (7) is disposed with pressure reducer (8), solenoid valve
(9), check valve (10), pressure sensor (12) and internal-screw ball valve (14), the pressure sensor (12) pass through the first internal thread
Threeway (11) is connect with air inlet pipe (7), and the internal-screw ball valve (14) is connected by the second internal thread threeway (13) and air inlet pipe (7)
It connects, the outlet side of the air inlet pipe (7) is connect with tracheae (15), and the tracheae (15) front end is provided with 8V1 gas-charging connection
(17) and 12V1 gas-charging connection (18), and 8V1 gas-charging connection (17) and 12V1 gas-charging connection (18) by cable assembly (16) with
Air inlet pipe (7) is fixed.
2. a kind of aircarrier aircraft wheel self-filler according to claim 1, it is characterised in that: the air inlet pipe
(7) it is connect with nitrogen cylinder.
3. a kind of aircarrier aircraft wheel self-filler according to claim 1, it is characterised in that: the solenoid valve
(9) it is fixedly connected by mounting plate with electric box (5) cabinet.
4. a kind of aircarrier aircraft wheel self-filler according to claim 1, it is characterised in that: the 8V1 fills
It is connect between gas connector (17), 12V1 gas-charging connection (18) and tracheae (15) by male and female quick union.
5. a kind of aircarrier aircraft wheel self-filler according to claim 1, it is characterised in that: the solenoid valve
(9), pressure sensor (12) is electrically connected with touch screen (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821803947.6U CN209191911U (en) | 2018-11-03 | 2018-11-03 | A kind of aircarrier aircraft wheel self-filler |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821803947.6U CN209191911U (en) | 2018-11-03 | 2018-11-03 | A kind of aircarrier aircraft wheel self-filler |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209191911U true CN209191911U (en) | 2019-08-02 |
Family
ID=67410262
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821803947.6U Active CN209191911U (en) | 2018-11-03 | 2018-11-03 | A kind of aircarrier aircraft wheel self-filler |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209191911U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115046135A (en) * | 2022-06-21 | 2022-09-13 | 上海航天精密机械研究所 | High-compatibility portable emission tube nitrogen filling equipment suitable for complex environment |
-
2018
- 2018-11-03 CN CN201821803947.6U patent/CN209191911U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN115046135A (en) * | 2022-06-21 | 2022-09-13 | 上海航天精密机械研究所 | High-compatibility portable emission tube nitrogen filling equipment suitable for complex environment |
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