CN215462640U

CN215462640U - Double-deck concave joint machining center of aviation air supply

Info

Publication number: CN215462640U
Application number: CN202122100957.1U
Authority: CN
Inventors: 闵立志; 唐铭龙; 王真
Original assignee: Shaanxi Huachen Aviation Technology Co ltd
Current assignee: Shaanxi Huachen Aviation Technology Co ltd
Priority date: 2021-09-01
Filing date: 2021-09-01
Publication date: 2022-01-11
Anticipated expiration: 2031-09-01

Abstract

The utility model relates to the technical field of machining, in particular to an aviation air source double-layer concave joint machining center which reduces moisture attached to scrap iron through rotation of a spin dryer tube, improves the preservation time of the scrap iron, and improves the reliability and the practicability; the novel centrifugal drying machine comprises a base plate, a supporting box, a funnel, a sliding block, a lead screw, a motor, a supporting shaft, a connecting box, a first cone pulley, a second cone pulley, a first rotating shaft, a second rotating shaft, a spin dryer tube and a sealing door, supporting box fixed mounting is in the upper end of bottom plate, the inside of supporting box is provided with the cavity, the upper end of supporting box is provided with the multiunit through-hole, processingequipment is installed to the upper end of supporting box, funnel fixed mounting is in the upper end of supporting box cavity, slider horizontal sliding mounting is at the lower extreme of supporting box cavity, slider and lead screw spiral shell dress, the lead screw rotates and installs on supporting box, the left end of lead screw is connected with the output of motor, the back shaft rotates and installs on the slider.

Description

Double-deck concave joint machining center of aviation air supply

Technical Field

The utility model relates to the technical field of machining, in particular to a machining center for double-layer concave joints of an aviation air source.

Background

The machining center is an auxiliary device which can be used for machining double-layer female connectors and has application in the technical field of machining. The existing machining center finds that a large amount of cutting fluid is attached to collected machining scrap iron, the scrap iron and air are subjected to electrochemical reaction easily due to moisture in the cutting fluid, so that the scrap iron is rusted, the preservation time of the scrap iron is shortened, and the practicability and the reliability of the scrap iron are poor.

SUMMERY OF THE UTILITY MODEL

In order to solve the technical problem, the utility model provides the aviation air source double-layer female joint machining center which reduces the moisture attached to the scrap iron, improves the storage time of the scrap iron, and improves the reliability and the practicability through the rotation of the spin dryer tube.

The utility model relates to an aviation air source double-layer female joint machining center which comprises a bottom plate, a support box, a funnel, a sliding block, a screw rod, a motor, a support shaft, a connecting box, a first cone pulley, a second cone pulley, a first rotating shaft, a second rotating shaft, a spin dryer tube and a sealing door, wherein the support box is fixedly arranged at the upper end of the bottom plate, a cavity is arranged inside the support box, a plurality of groups of through holes are formed in the upper end of the support box, a machining device is arranged at the upper end of the support box, the funnel is fixedly arranged at the upper end of the cavity of the support box, the sliding block is arranged at the lower end of the cavity of the support box in a left-right sliding mode, the sliding block is in threaded connection with the screw rod, the screw rod is rotatably arranged on the support box, the left end of the screw rod is connected with the output end of the motor, the support shaft is rotatably arranged on the sliding block, the connecting box is fixedly arranged on the sliding block, the connecting box is rotatably arranged with the support shaft, the first cone pulley is fixedly arranged on the support shaft, the first cone pulley is meshed with the second cone pulley, second cone pulley fixed mounting is in the left end of first pivot, first pivot horizontal slip mounting is in the second pivot, connecting box and first pivot rotation installation, the second pivot is rotated and is installed on supporting box, the right-hand member of second pivot is connected with driving motor's output, spin-dry barrel fixed mounting is in the upper end of back shaft, the upper end of spin-dry barrel is the opening, be provided with the multiunit filtration pore on the lateral wall of spin-dry barrel, be provided with the collection mouth on the spin-dry barrel, it is provided with sealed lid outward to collect the mouth, be provided with row round pin mouth on the supporting box, sealing door installs the row round pin mouth department at supporting box.

The double-layer concave joint machining center for the aviation air source further comprises a suspension bracket, an air gun and an air pipe, wherein the suspension bracket is fixedly installed at the right end of the support box, the air gun is suspended on the support box, and the air gun is connected with an external air pump through the air pipe.

The double-layer female joint machining center for the aviation air source further comprises a cover plate and a bolt, wherein the support box is provided with an access hole, and the cover plate is installed on the outer side of the access hole through the bolt.

The double-layer concave joint machining center for the aviation air source further comprises a base, and the base is fixedly installed at the lower end of the bottom plate.

The double-layer concave joint machining center for the aviation air source further comprises a liquid level meter, and the liquid level meter is installed on the supporting box.

The double-layer female joint machining center for the aviation air source further comprises an illuminating lamp, and the illuminating lamp is installed on the supporting box.

The double-layer concave joint machining center for the aviation air source further comprises a limiting block, and the limiting block is fixedly installed on the screw rod.

The double-layer concave joint machining center for the aviation air source further comprises a reinforcing plate, and the reinforcing plate is fixedly installed on the funnel.

Compared with the prior art, the utility model has the beneficial effects that: firstly, a workpiece is processed through a processing device at the upper end of a supporting box, scrap iron and cutting fluid generated in the processing process can enter a spin dryer tube through a plurality of groups of through holes and a plurality of groups of funnels, then a driving motor is turned on, the driving motor drives a first rotating shaft to rotate at a high speed through a second rotating shaft, then the first rotating shaft drives a first cone pulley and a supporting shaft to rotate through a second cone pulley, then the supporting shaft drives the spin dryer tube to rotate at a high speed, the scrap iron in the spin dryer tube is subjected to huge centrifugal force by centrifugal force generated in the high-speed rotation process of the spin dryer tube, meanwhile, moisture attached to the scrap iron is discharged into a cavity of the supporting box through a plurality of groups of filtering holes in the spin dryer tube due to the huge centrifugal force, the scrap iron is remained in the spin dryer tube, after the moisture on the scrap iron is purified, the driving motor is turned off, the motor drives a screw rod to rotate, the screw rod drives the first rotating shaft through a sliding block, Connecting box, back shaft and spin dryer tube move left, move to the row's round pin mouth department of supporting box to the spin dryer tube, open the sealed lid on sealing door and the spin dryer tube, take out dry iron fillings in the spin dryer tube can, through the rotation of spin dryer tube, reduced adnexed moisture on the iron fillings in the spin dryer tube, improved the save time of iron fillings, improved reliability and practicality.

Drawings

FIG. 1 is a schematic front view of the present invention;

FIG. 2 is a schematic structural diagram of the connection of a motor, a screw rod, a sliding block and the like;

FIG. 3 is a schematic view showing a structure of coupling the slider, the coupling box, and the support shaft;

fig. 4 is a schematic structural view of the connection of the spin dryer tube, the support shaft and the first cone pulley;

in the drawings, the reference numbers: 1. a base plate; 2. a support box; 3. a through hole; 4. a funnel; 5. a slider; 6. a screw rod; 7. a motor; 8. a support shaft; 9. a connecting box; 10. a first cone pulley; 11. a second cone; 12. a first rotating shaft; 13. a second rotating shaft; 14. a spin dryer tube; 15. a sealing door; 16. a suspension bracket; 17. an air gun; 18. an air tube; 19. a cover plate; 20. a bolt; 21. a base; 22. a liquid level meter; 23. an illuminating lamp; 24. a limiting block; 25. a reinforcing plate.

Detailed Description

The following detailed description of embodiments of the present invention is provided in connection with the accompanying drawings and examples. The following examples are intended to illustrate the utility model but are not intended to limit the scope of the utility model.

As shown in fig. 1 to 4, the double-layer female joint machining center for an aviation air source comprises a bottom plate 1, a support box 2, a funnel 4, a sliding block 5, a screw rod 6, a motor 7, a support shaft 8, a connecting box 9, a first cone pulley 10, a second cone pulley 11, a first rotating shaft 12, a second rotating shaft 13, a spin dryer 14 and a sealing door 15, wherein the support box 2 is fixedly arranged at the upper end of the bottom plate 1, a cavity is arranged inside the support box 2, a plurality of groups of through holes 3 are arranged at the upper end of the support box 2, a machining device is arranged at the upper end of the support box 2, the funnel 4 is fixedly arranged at the upper end of the cavity of the support box 2, the sliding block 5 is arranged at the lower end of the cavity of the support box 2 in a left-right sliding manner, the sliding block 5 is screwed with the screw rod 6, the screw rod 6 is rotatably arranged on the support box 2, the left end of the screw rod 6 is connected with the output end of the motor 7, the support shaft 8 is rotatably arranged on the sliding block 5, the connecting box 9 is fixedly arranged on the sliding block 5, the connecting box 9 is rotatably mounted with the supporting shaft 8, the first cone pulley 10 is fixedly mounted on the supporting shaft 8, the first cone pulley 10 is meshed with the second cone pulley 11, the second cone pulley 11 is fixedly mounted at the left end of the first rotating shaft 12, the first rotating shaft 12 is slidably mounted on the second rotating shaft 13 left and right, the connecting box 9 is rotatably mounted with the first rotating shaft 12, the second rotating shaft 13 is rotatably mounted on the supporting box 2, the right end of the second rotating shaft 13 is connected with the output end of the driving motor, the spin-drying barrel 14 is fixedly mounted at the upper end of the supporting shaft 8, the upper end of the spin-drying barrel 14 is an opening, a plurality of groups of filter holes are formed in the side wall of the spin-drying barrel 14, a collecting port is formed in the spin-drying barrel 14, a sealing cover is arranged outside the collecting port, a pin discharging port is formed in the supporting box 2, and a sealing door 15 is mounted at the pin discharging port of the supporting box 2; firstly, a workpiece is processed through a processing device at the upper end of a support box 2, scrap iron and cutting fluid generated in the processing process enter a spin dryer tube 14 through a plurality of groups of through holes 3 and a plurality of groups of funnels 4, then a driving motor is turned on, the driving motor drives a first rotating shaft 12 to rotate at a high speed through a second rotating shaft 13, then the first rotating shaft 12 drives a first cone pulley 10 and a support shaft 8 to rotate through a second cone pulley 11, then the support shaft 8 drives the spin dryer tube 14 to rotate at a high speed, the scrap iron in the spin dryer tube 14 is subjected to huge centrifugal force by centrifugal force generated in the high-speed rotation process of the spin dryer tube 14, meanwhile, moisture attached to the scrap iron is discharged into a cavity of the support box 2 through a plurality of groups of filter holes in the spin dryer tube 14 due to the huge centrifugal force, the scrap iron is remained in the spin dryer tube 14, after the moisture on the scrap iron is dried, the driving motor is turned off, the motor 7 is turned on, the motor 7 drives a screw rod 6 to rotate, the lead screw 6 drives the first rotating shaft 12, the connecting box 9, the supporting shaft 8 and the spin dryer tube 14 to move leftwards through the sliding block 5, the spin dryer tube 14 moves to a pin arranging opening of the supporting box 2, the sealing door 15 and the sealing cover on the spin dryer tube 14 are opened, dry scrap iron in the spin dryer tube 14 can be taken out, through rotation of the spin dryer tube 14, attached moisture on the scrap iron in the spin dryer tube 14 is reduced, the preservation time of the scrap iron is prolonged, and reliability and practicability are improved.

The double-layer concave joint machining center for the aviation air source further comprises a suspension bracket 16, an air gun 17 and an air pipe 18, wherein the suspension bracket 16 is fixedly installed at the right end of the support box 2, the air gun 17 is suspended on the support box 2, and the air gun 17 is connected with an external air pump through the air pipe 18; through the setting, can blow the skin of supporting box 2 clean through air gun 17, improve the cleaning nature and the convenience in the use.

The double-layer concave joint machining center for the aviation air source further comprises a cover plate 19 and a bolt 20, wherein the support box 2 is provided with an access hole, and the cover plate 19 is arranged on the outer side of the access hole through the bolt 20; through the arrangement, the overhaul and the maintenance of the equipment in the cavity of the supporting box 2 are facilitated, and the convenience in the use process is improved.

The double-layer concave joint machining center for the aviation air source further comprises a base 21, wherein the base 21 is fixedly arranged at the lower end of the bottom plate 1; through the arrangement, the stability of the bottom plate 1 in the using process is improved.

The double-layer concave joint machining center for the aviation air source further comprises a liquid level meter 22, wherein the liquid level meter 22 is arranged on the support box 2; through the arrangement, the monitoring of the liquid level in the cavity of the supporting box 2 is facilitated, and the convenience in the use process is improved.

The double-layer female joint machining center for the aviation air source further comprises an illuminating lamp 23, wherein the illuminating lamp 23 is arranged on the support box 2; through the arrangement, the upper part of the supporting box 2 is brighter, the operation of workers is facilitated, and the convenience in the use process is improved.

The double-layer concave joint machining center for the aviation air source further comprises a limiting block 24, wherein the limiting block 24 is fixedly arranged on the screw rod 6; through the arrangement, the over-stroke movement of the sliding block 5 is prevented, and the reliability in the use process is improved.

The double-layer concave joint machining center for the aviation air source further comprises a reinforcing plate 25, wherein the reinforcing plate 25 is fixedly arranged on the funnel 4; through the arrangement, the firmness of the funnel 4 in the use process is improved.

The utility model relates to an aviation air source double-layer concave joint machining center, which comprises a support box 2, a first rotating shaft 12, a second rotating shaft 13, a first conical wheel 10, a second conical wheel 11, a first supporting shaft 8, a second rotating shaft 14, a driving motor, a second rotating shaft 13, a first rotating shaft 12, a second rotating shaft 8, a drying barrel 14, a centrifugal force generated by the drying barrel 14 in the high-speed rotation process, a plurality of groups of filtering holes in the drying barrel 14, and a plurality of groups of filtering holes in the drying barrel 14, and (3) closing the driving motor, opening the motor 7, driving the screw rod 6 to rotate by the motor 7, driving the first rotating shaft 12, the connecting box 9, the supporting shaft 8 and the spin dryer tube 14 to move leftwards by the screw rod 6 through the sliding block 5 until the spin dryer tube 14 moves to the pin arrangement opening of the supporting box 2, opening the sealing door 15 and the sealing cover on the spin dryer tube 14, and taking out dry scrap iron in the spin dryer tube 14.

According to the aviation air source double-layer female joint machining center, the installation mode, the connection mode or the arrangement mode are common mechanical modes, and the machining center can be implemented as long as the beneficial effects of the machining center can be achieved; the supporting box 2, the screw rod 6, the air gun 17, the liquid level meter 22 and the limiting block 24 of the double-layer concave joint machining center for the aviation air source are purchased from the market, and technicians in the industry only need to install and operate according to the attached operating instructions.

The above description is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, several modifications and variations can be made without departing from the technical principle of the present invention, and these modifications and variations should also be regarded as the protection scope of the present invention.

Claims

1. An aviation air source double-layer female joint machining center is characterized by comprising a bottom plate (1), a supporting box (2), a funnel (4), a sliding block (5), a screw rod (6), a motor (7), a supporting shaft (8), a connecting box (9), a first cone pulley (10), a second cone pulley (11), a first rotating shaft (12), a second rotating shaft (13), a spin dryer tube (14) and a sealing door (15), wherein the supporting box (2) is fixedly arranged at the upper end of the bottom plate (1), a cavity is arranged inside the supporting box (2), a plurality of groups of through holes (3) are formed in the upper end of the supporting box (2), a machining device is arranged at the upper end of the supporting box (2), the funnel (4) is fixedly arranged at the upper end of the cavity of the supporting box (2), the sliding block (5) is arranged at the lower end of the cavity of the supporting box (2) in a left-right sliding mode, the sliding mode is arranged at the lower end of the cavity of the supporting box (2), the sliding block (5) and is in a screw rod (6), the screw rod (6) is rotatably arranged on the supporting box (2), the left end of a screw rod (6) is connected with the output end of a motor (7), a support shaft (8) is rotatably arranged on a sliding block (5), a connecting box (9) is fixedly arranged on the sliding block (5), the connecting box (9) is rotatably arranged with the support shaft (8), a first cone pulley (10) is fixedly arranged on the support shaft (8), the first cone pulley (10) is meshed with a second cone pulley (11), the second cone pulley (11) is fixedly arranged at the left end of a first rotating shaft (12), the first rotating shaft (12) is slidably arranged on a second rotating shaft (13) left and right, the connecting box (9) is rotatably arranged with the first rotating shaft (12), the second rotating shaft (13) is rotatably arranged on a support box (2), the right end of the second rotating shaft (13) is connected with the output end of a driving motor, a spin dryer drum (14) is fixedly arranged at the upper end of the support shaft (8), the upper end of the spin dryer drum (14) is open, and a plurality of groups of filter holes are formed in the side wall of the spin dryer drum (14), the spin dryer tube (14) is provided with a collecting opening, a sealing cover is arranged outside the collecting opening, the support box (2) is provided with a pin arranging opening, and the sealing door (15) is arranged at the pin arranging opening of the support box (2).

2. The double-layer concave joint machining center for the aviation air source as claimed in claim 1, further comprising a suspension bracket (16), an air gun (17) and an air pipe (18), wherein the suspension bracket (16) is fixedly installed at the right end of the support box (2), the air gun (17) is suspended on the support box (2), and the air gun (17) is connected with an external air pump through the air pipe (18).

3. The double-layer female joint machining center for the aviation air supply as claimed in claim 1, further comprising a cover plate (19) and a bolt (20), wherein the support box (2) is provided with an access opening, and the cover plate (19) is installed on the outer side of the access opening through the bolt (20).

4. The double-layer female connector machining center for the air supply of the aviation according to claim 1, further comprising a base (21), wherein the base (21) is fixedly installed at the lower end of the bottom plate (1).

5. The double-deck female joint machining center of an air supply of an aircraft according to claim 1, further comprising a liquid level gauge (22), wherein the liquid level gauge (22) is mounted on the support box (2).

6. The double-layer female connector machining center for an aviation air supply according to claim 1, further comprising an illuminating lamp (23), wherein the illuminating lamp (23) is installed on the support box (2).

7. The machining center for the double-layer female connector of the aviation air source as claimed in claim 1, further comprising a limiting block (24), wherein the limiting block (24) is fixedly installed on the screw rod (6).

8. The double-layer female connector machining center for the air supply of aviation according to claim 1, further comprising a reinforcing plate (25), wherein the reinforcing plate (25) is fixedly installed on the funnel (4).