CN215566871U - Integrated aerodynamic system device - Google Patents

Integrated aerodynamic system device Download PDF

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Publication number
CN215566871U
CN215566871U CN202122284470.3U CN202122284470U CN215566871U CN 215566871 U CN215566871 U CN 215566871U CN 202122284470 U CN202122284470 U CN 202122284470U CN 215566871 U CN215566871 U CN 215566871U
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China
Prior art keywords
box
worm
system device
fixed plate
hasp
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CN202122284470.3U
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Chinese (zh)
Inventor
钱称心
刘凤华
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Kesuo Compressor Shanghai Co ltd
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Kesuo Compressor Shanghai Co ltd
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Abstract

The utility model provides an integrated aerodynamic system device, and relates to the technical field of compressors. This integral type aerodynamic system device includes the box, box one side is provided with the worm, worm one side meshing is connected with the worm wheel, the inside fixedly connected with dwang of worm wheel, dwang outside fixedly connected with rotates the hasp, the bar groove has been seted up to the box opposite side. This integral type aerodynamic system device, the worm rotates and drives the worm wheel rotation, and then the worm wheel rotates and drives the dwang and rotate, because rotate hasp fixed connection in the dwang outside, and then the dwang rotates and drives the rotation hasp and rotate, rotate the hasp and rotate and then can make and rotate the hasp and break away from and then enter into the bar inslot portion from the spacing inslot portion, can stimulate the fixed plate left this moment, and then can take out the fixed plate, this structure is of value to and takes out the fixed plate fast, moreover, the steam generator is simple in structure, and convenient for operation saves time, and saves manpower.

Description

Integrated aerodynamic system device
Technical Field
The utility model relates to a power system device, in particular to an integrated air power system device, and belongs to the technical field of compressors.
Background
An existing aerodynamic system device, such as an air compressor unit, an air compressor is a device for compressing air. The air compressor is constructed similarly to a water pump. Most air compressors are of the reciprocating piston type, rotating vane or rotating screw type, and centrifugal compressors are very large applications, which can be divided into three main categories according to the working principle: the compressor is characterized by comprising a volume type compressor, a power type compressor (a speed type compressor or a turbine type compressor) and a thermal type compressor, wherein when the compressor works, air is sucked through a self-cleaning air filter, the air enters a first-stage compression mode after being automatically adjusted through an inlet guide vane through a PLC (programmable logic controller) automatic cleaning filter, the temperature of the air after the first-stage compression is higher, and then the air enters an intercooler for cooling.
When traditional integral type aerodynamic system device generally need examine aerodynamic system device, general power device system all fixes the baffle through the bolt, and when fixing through the screw thread, often need use specialized tool to dismantle when dismantling, it is very inconvenient to dismantle, and because the volume ratio of bolt is less, and then take place easily after dismantling the bolt and lose, and then still need go again to match new bolt and fix, the waste time, extravagant manpower, cause certain trouble, consequently, need improve this integral type aerodynamic system device.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
The utility model aims to provide an integrated air power system device to solve the problems, and aims to solve the problems that in the prior art, when a common power system is fixed by a bolt and fixed by a thread, a special tool is usually required to be used for dismounting during dismounting, dismounting is very inconvenient, and due to the fact that the bolt is small in size, the bolt is easy to lose after being dismounted, and further needs to be matched with a new bolt again for fixing, time and labor are wasted, and certain troubles are caused.
(II) technical scheme
In order to achieve the purpose, the utility model is realized by the following technical scheme: integral type aerodynamic force system device, the power distribution box comprises a box body, box one side is provided with the worm, worm one side meshing is connected with the worm wheel, the inside fixedly connected with dwang of worm wheel, dwang outside fixedly connected with rotates the hasp, the bar groove has been seted up to the box opposite side, the spacing groove has been seted up to bar groove both sides, the box opposite side is provided with seal assembly.
Preferably, seal assembly includes the sealing strip, the sealing strip sets up in the box opposite side, the ring channel has been seted up to the box opposite side, sealing strip and ring channel phase-match through being provided with the sealing strip, and then be convenient for seal the aerodynamic system device, and then reduce the vibrations of aerodynamic system device, consequently can reduce the noise of aerodynamic system device, through being provided with sealing strip and ring channel phase-match, and then can increase the leakproofness of box.
Preferably, sealing strip opposite side fixedly connected with fixed plate, three damping spring of fixed plate one side difference fixedly connected with, through being provided with the fixed plate, and then be convenient for seal the box, through being provided with damping spring, and then be convenient for carry out the shock attenuation to the box, reduce the vibrations of box, consequently can reduce aerodynamic system device's noise.
Preferably, the dwang runs through the fixed plate and rotates with the fixed plate to be connected, rotate the hasp and set up in fixed plate one side, through being provided with the dwang, and then be convenient for drive and rotate the hasp and rotate, and then be convenient for seal the box, be convenient for fix the fixed plate, avoid using the bolt fastening, consequently need use specialized tool to dismantle, the bolt ratio takes place easily to lose, waste time, extravagant manpower.
Preferably, the box front side is opened and is equipped with the louvre, box internally mounted has the axis of rotation, rotor blade is installed in the axis of rotation outside, and through being provided with the louvre, and then is convenient for dispel the heat to the box, avoids the inside electrical components high temperature damage of box, reduces electrical components's life.
Preferably, fixed plate opposite side fixedly connected with backup pad, the backup pad rotates to be connected in the worm outside, through being provided with the backup pad, and then is convenient for support the worm, and the worm of being convenient for moves more stably, and then can drive and rotate the hasp and rotate, and then can fix the fixed plate, seals the box, avoids using the bolt.
Preferably, the worm outside fixedly connected with handle, spacing groove and rotation hasp interference fit, the cavity has been seted up to box inside, and through being provided with the handle, and then be convenient for drive the worm and rotate, carries out interference fit through being provided with the spacing groove and rotating the hasp, and then can seal fixedly to the box, and then avoid using the bolt fastening.
The utility model provides an integrated aerodynamic system device, which has the following beneficial effects:
1. this integral type aerodynamic system device, the worm rotates and drives the worm wheel rotation, because worm wheel fixed connection is in the dwang outside, and then the worm wheel rotates and drives the dwang rotation, because rotate hasp fixed connection in the dwang outside, and then the dwang rotates and drives the rotation hasp and rotate, it rotates the hasp and then can make the rotation hasp break away from and then enter into the bar inslot portion from the spacing inslot portion, can stimulate the fixed plate left this moment, and then can take out the fixed plate, this structure is of value to and takes out the fixed plate fast, moreover, the steam generator is simple in structure, and the steam generator is convenient to operate, and the time is saved, and the manpower is saved.
2. This integral type aerodynamic system device, because fixed plate one side fixedly connected with sealing strip, the sealing strip cooperatees with the ring channel, and then is convenient for seal the box, consequently can fall the noise to the box, because fixed plate one side fixedly connected with damping spring, and then be convenient for carry out the shock attenuation to the box, consequently can reach a absorbing effect equally, the noise reduction.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is an enlarged view of the portion A of FIG. 1 according to the present invention;
FIG. 3 is a schematic view of a fixing plate according to the present invention;
FIG. 4 is a schematic view of the spring structure of the present invention;
FIG. 5 is an enlarged view of the portion B of FIG. 3 according to the present invention.
In the figure: 1. a box body; 2. a worm; 3. a worm gear; 4. rotating the rod; 5. rotating the lock catch; 6. a strip-shaped groove; 7. a limiting groove; 8. a sealing strip; 9. a damping spring; 10. a support plate; 11. a handle; 12. a fixing plate; 13. heat dissipation holes; 14. an annular groove; 15. a rotating shaft; 16. a rotor blade; 17. a cavity.
Detailed Description
The embodiment of the utility model provides an integrated aerodynamic system device.
Please refer to fig. 1, fig. 2, fig. 3, fig. 4 and fig. 5, including box 1, 1 one side of box is provided with worm 2, 2 one side meshing of worm is connected with worm wheel 3, 3 inside fixedly connected with dwang 4 of worm wheel, 4 outside fixedly connected with of dwang rotates hasp 5, bar groove 6 has been seted up to 1 opposite side of box, spacing groove 7 has been seted up to 6 both sides of bar groove, 1 opposite side of box is provided with seal assembly, dwang 4 runs through fixed plate 12 and is connected with fixed plate 12 rotation, it sets up in 12 one sides of fixed plate to rotate hasp 5, 12 opposite side fixedly connected with backup pad 10 of fixed plate, backup pad 10 rotates and connects in the 2 outsides of worm, 2 outside fixedly connected with handles 11 of worm, spacing groove 7 and 5 interference fit of rotation hasp, cavity 17 has been seted up to 1 inside of box.
Specifically, the method comprises the following steps: when the power system device needs to be used and needs to be disassembled and maintained, the handle 11 can be rotated, the handle 11 is fixedly connected to the outer side of the worm 2, and then the handle 11 is rotated to drive the worm 2 to rotate, because the worm wheel 3 is meshed with one side of the worm 2, and then the worm 2 is rotated to drive the worm wheel 3 to rotate, because the worm wheel 3 is fixedly connected to the outer side of the rotating rod 4, and then the worm wheel 3 is rotated to drive the rotating rod 4 to rotate, because the rotating lock catch 5 is fixedly connected to the outer side of the rotating rod 4, and then the rotating lock catch 4 is rotated to drive the rotating lock catch 5 to rotate, and the rotating lock catch 5 is rotated to enable the rotating lock catch 5 to be separated from the inner part of the limiting groove 7 and enter the inner part of the strip-shaped groove 6, and then the fixing plate 12 can be pulled leftwards, and then the fixing plate 12 can be taken out, the structure is beneficial to quickly taking out the fixing plate 12, and has simple structure, the operation is convenient, the time is saved, and the labor is saved.
Referring to fig. 3 and 4 again, the sealing assembly includes a sealing strip 8, the sealing strip 8 is disposed on the other side of the box body 1, an annular groove 14 is formed on the other side of the box body 1, the sealing strip 8 is matched with the annular groove 14, a fixing plate 12 is fixedly connected to the other side of the sealing strip 8, and three damping springs 9 are fixedly connected to one side of the fixing plate 12 respectively.
Specifically, the method comprises the following steps: meanwhile, because fixed plate 12 one side fixedly connected with sealing strip 8, sealing strip 8 cooperatees with ring channel 14, and then is convenient for seal box 1, consequently can fall the noise to box 1, because fixed plate 12 one side fixedly connected with damping spring 9, and then is convenient for carry out the shock attenuation to box 1, consequently can reach a absorbing effect equally, the noise reduction.
Referring to fig. 3 again, heat dissipation holes 13 are formed in the front side of the box 1, a rotation shaft 15 is installed inside the box 1, and rotating blades 16 are installed outside the rotation shaft 15.
Specifically, the method comprises the following steps: through being provided with louvre 13, and then be convenient for dispel the heat to box 1, avoid because the inside electrical components high temperature of box 1 causes electrical components's damage, through being provided with backup pad 10, and then can support worm 2, the worm 2 operation of being convenient for is more stable.
The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. 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 (7)

1. Integral type aerodynamic system device, including box (1), its characterized in that: box (1) one side is provided with worm (2), worm (2) one side meshing is connected with worm wheel (3), inside fixedly connected with dwang (4) of worm wheel (3), dwang (4) outside fixedly connected with rotates hasp (5), bar groove (6) have been seted up to box (1) opposite side, spacing groove (7) have been seted up to bar groove (6) both sides, box (1) opposite side is provided with seal assembly.
2. The integrated aerodynamic system device of claim 1, wherein: the sealing assembly comprises a sealing strip (8), the sealing strip (8) is arranged on the other side of the box body (1), an annular groove (14) is formed in the other side of the box body (1), and the sealing strip (8) is matched with the annular groove (14).
3. The integrated aerodynamic system device of claim 2, wherein: the sealing strip (8) opposite side fixedly connected with fixed plate (12), fixed plate (12) one side fixedly connected with three damping spring (9) respectively.
4. The integrated aerodynamic system device of claim 1, wherein: dwang (4) run through fixed plate (12) and rotate with fixed plate (12) and be connected, rotation hasp (5) set up in fixed plate (12) one side.
5. The integrated aerodynamic system device of claim 1, wherein: the box body (1) front side is opened and is equipped with louvre (13), box body (1) internally mounted has axis of rotation (15), rotating blade (16) are installed to axis of rotation (15) outside.
6. The integrated aerodynamic system device of claim 3, wherein: the other side of the fixing plate (12) is fixedly connected with a supporting plate (10), and the supporting plate (10) is rotatably connected to the outer side of the worm (2).
7. The integrated aerodynamic system device of claim 1, wherein: the worm (2) outside fixedly connected with handle (11), spacing groove (7) and rotation hasp (5) interference fit, cavity (17) have been seted up to box (1) inside.
CN202122284470.3U 2021-09-22 2021-09-22 Integrated aerodynamic system device Active CN215566871U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202122284470.3U CN215566871U (en) 2021-09-22 2021-09-22 Integrated aerodynamic system device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202122284470.3U CN215566871U (en) 2021-09-22 2021-09-22 Integrated aerodynamic system device

Publications (1)

Publication Number Publication Date
CN215566871U true CN215566871U (en) 2022-01-18

Family

ID=79851568

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202122284470.3U Active CN215566871U (en) 2021-09-22 2021-09-22 Integrated aerodynamic system device

Country Status (1)

Country Link
CN (1) CN215566871U (en)

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