CN217991854U - Cooling system of aviation screw tapping machine - Google Patents

Cooling system of aviation screw tapping machine Download PDF

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Publication number
CN217991854U
CN217991854U CN202220893352.4U CN202220893352U CN217991854U CN 217991854 U CN217991854 U CN 217991854U CN 202220893352 U CN202220893352 U CN 202220893352U CN 217991854 U CN217991854 U CN 217991854U
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China
Prior art keywords
rose box
tapping machine
cooling system
filter
pivot
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Active
Application number
CN202220893352.4U
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Chinese (zh)
Inventor
郭弘
胡维嘉
汪浩
张炳刚
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Xinyang Yicheng Aviation Technology Co ltd
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Xinyang Yicheng Aviation Technology Co ltd
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Priority to CN202220893352.4U priority Critical patent/CN217991854U/en
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Publication of CN217991854U publication Critical patent/CN217991854U/en
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Abstract

The utility model relates to an aviation screw tapping machine cooling system, the setting is on the tapping machine, including spraying the mechanism, circulation mechanism and filter mechanism, circulation mechanism includes water tank and circulating pump, it includes the sprinkler bead to spray the mechanism, the sprinkler bead adopts the pipe connection with circulation mechanism, filter mechanism includes the rose box, the rose box top is provided with inserts the unloading funnel of establishing in the rose box, unloading funnel lower extreme installation valve, the rose box lower extreme is provided with the fluid-discharge tube with the water tank intercommunication, the level is provided with multiunit filter unit in the rose box, filter unit includes the installing frame, the installing frame right-hand member rotates the pivot that sets up along the fore-and-aft direction extension, the pivot left side is connected with the filter screen, the rose box outside is provided with the slewing mechanism that each pivot is connected, the rose box lateral wall of filter unit below rotates and is provided with the deflector, the rose box side of keeping away from the deflector articulates there is the discharge door. The utility model has the advantages of can in time discharge clastic.

Description

Cooling system of aviation screw tapping machine
Technical Field
The utility model relates to a screw rod production facility field especially relates to an aviation screw tapping machine cooling system.
Background
Need utilize the tapping machine to carry out the tapping to the screw surface in screw rod production, the tapping in-process can produce a large amount of heats, if not cooling the screw rod, can lead to a screw rod cutter overheated, produce the substandard product, consequently, need cool off screw rod and cutter in the tapping in-process, the common mode of cooling is that utilize endless coolant liquid to wash out the screw rod thereby take away the heat, in the tapping, can produce the piece, the piece can be along with the coolant liquid downward flow, need utilize filtration system to filter these pieces out, it clears up in unison when waiting for the workman to hand over, but because the tapping machine continuous operation, the piece that produces is more, consequently just need great space to filter the piece and hold the piece, occupation space is great, therefore it is just obvious especially necessary to develop an aviation screw rod tapping machine cooling system that can in time discharge the piece.
SUMMERY OF THE UTILITY MODEL
The utility model provides an aviation screw tapping machine cooling system has the clastic advantage of can in time discharging.
The technical scheme is as follows:
the utility model provides an aviation screw tapping machine cooling system, the setting is on the tapping machine, including spraying the mechanism, circulation mechanism and filter mechanism, circulation mechanism includes water tank and circulating pump, it includes the sprinkler bead to spray the mechanism, the sprinkler bead adopts the pipe connection with circulation mechanism, filter mechanism includes the rose box, the rose box top is provided with inserts the unloading funnel of establishing in the rose box, unloading funnel lower extreme installation valve, the rose box lower extreme is provided with the fluid-discharge tube with the water tank intercommunication, the level is provided with multiunit filter unit in the rose box, filter unit includes the installing frame, the installing frame right-hand member rotates the pivot that sets up along fore-and-aft direction extension, the pivot left side is connected with the filter screen, the rose box outside is provided with the slewing mechanism that each pivot is connected, the rose box lateral wall of filter unit below rotates and is provided with the deflector, the rose box side of keeping away from the deflector articulates there is the discharge door.
Preferably, slewing mechanism include rack and a plurality of gear, the gear is installed respectively at the tip of each pivot, rack horizontal slip sets up in the gear below and all meshes with each gear, the rose box outside level is provided with the electric telescopic handle of being connected with the rack.
Preferably, the free end of the guide plate is connected with a connecting rope, and one end of the connecting rope, which is far away from the guide plate, is connected with the discharge door.
Preferably, the valve is an electric gate valve.
Preferably, the lower ends of the filter screens are provided with electromagnets.
Preferably, the upper end of the filter screen is provided with a rubber sealing ring.
Compared with the prior art, the beneficial effects are that:
the utility model discloses the utilization can pivoted filter screen and filter screen below can the pivoted deflector, utilizes the switching of valve, regularly clears up the piece, does not need very big rose box, practices thrift the space, and has the clastic advantage of in time discharging.
Drawings
FIG. 1 is a schematic structural diagram of a cooling system of an aviation screw tapping machine of the present invention,
figure 2 is a schematic view of the structure at a in figure 1,
FIG. 3 is a schematic structural diagram of a rotating mechanism of the cooling system of the aviation screw tapping machine of the present invention,
in the figure: 1. the water tank, 2, the circulating pump, 3, the sprinkler bead, 4, the rose box, 5, unloading funnel, 6, the valve, 7, the installing frame, 8, the pivot, 9, the filter screen, 10, the gear, 11, the rack, 12, electric telescopic handle, 13, the deflector, 14, the discharge door, 15, connect the rope, 16, the electro-magnet.
Detailed Description
The present invention will be further described with reference to the following specific embodiments, as shown in fig. 1 to 3: a cooling system of an aviation screw tapping machine is arranged on the tapping machine and comprises a spraying mechanism, a circulating mechanism and a filtering mechanism, wherein the circulating mechanism comprises a water tank 1 and a circulating pump 2, the spraying mechanism comprises a water spray head 3, the water spray head 3 is connected with the circulating mechanism through a pipeline, cooling liquid is contained in the water tank 1, the circulating pump 2 conveys the cooling liquid to the water spray head 3, the water spray head 3 flushes the cooling liquid onto a screw rod to take away heat generated by tapping,
the filtering mechanism comprises a filtering box 4, a discharging funnel 5 inserted in the filtering box 4 is arranged above the filtering box 4, a valve 6 is arranged at the lower end of the discharging funnel 5, a liquid discharge pipe communicated with the water tank 1 is arranged at the lower end of the filtering box 4, the discharging funnel 5 is used for receiving cooling liquid flowing down from the screw, the cooling liquid is mixed with debris and enters the discharging funnel 5 and enters the filtering box 4 from the discharging funnel 5, the valve 6 is an electric gate valve, the electric gate valve is more convenient to use compared with a manual valve 6,
a plurality of groups of filtering units are horizontally arranged in the filtering box 4, each filtering unit comprises an installation frame 7, a rotating shaft 8 extending along the front-back direction is rotatably arranged at the right end of the installation frame 7, a filtering net 9 is connected at the left side of the rotating shaft 8, the rotating shaft 8 rotates to drive the filtering net 9 to rotate, a rubber sealing ring is arranged at the upper end of the filtering net 9, the sealing between the side surface of the filtering net 9 and the installation frame 7 is realized, the fragments are prevented from falling from the interval between the installation frame 7 and the filtering net 9,
the outer side of the filter box 4 is provided with a rotating mechanism connected with each rotating shaft 8, the rotating mechanism comprises a rack 11 and a plurality of gears 10, the gears 10 are respectively installed at the end parts of the rotating shafts 8, the rack 11 is horizontally arranged below the gears 10 in a sliding manner and is meshed with each gear 10, the outer side of the filter box 4 is horizontally provided with an electric telescopic rod 12 connected with the rack 11, the electric telescopic rod 12 controls the rack 11 to horizontally slide so as to enable the gears 10 meshed with the rack 11 to rotate and enable each filter screen 9 to rotate, electromagnets 16 are installed on the filter screens 9, the electromagnets 16 are convenient for adsorbing iron scraps, the filter screens 9 rotate to a vertical state, the electromagnets 16 are closed to enable the scraps on the filter screens 9 to fall under the action of gravity,
4 lateral walls of filter tank of filter unit below rotate and are provided with deflector 13, 4 side hinges of filter tank of keeping away from deflector 13 have discharge door 14, 13 free ends of deflector are connected with and connect rope 15, the one end that keeps away from deflector 13 of connecting rope 15 is connected with discharge door 14, open discharge door 14, it is rotating to connect rope 15 to pull deflector 13, extend 13 free ends of deflector outside filter tank 4, be convenient for derive the piece that falls from filter screen 9 outside filter tank 4.
The specific working conditions are as follows: starting the circulating mechanism, conveying the cooling liquid to the water spray head 3 by the circulating mechanism to cool the screw rod, enabling the flowing-down cooling liquid and the fragments to fall into the blanking funnel 5 and enter the filter box 4, filtering the fragments by the filter screen 9 in a horizontal state, enabling the filtered cooling liquid to enter the circulating mechanism,
when the piece on the filter screen 9 is more, close valve 6, open discharge door 14, connect rope 15 and pull deflector 13 and rotate, extend deflector 13 free end outside rose box 4, control slewing mechanism rotates filter screen 9 to vertical state and closes electro-magnet 16, and the piece is outside discharge door 14 from deflector 13 roll-off, can be timely discharge the piece, and rose box 4 need not very greatly, practices thrift the space.
The above embodiments are only preferred embodiments of the present invention, and the protection scope of the present invention cannot be limited thereby, and any insubstantial changes and substitutions made by those skilled in the art based on the present invention are all within the protection scope of the present invention.

Claims (6)

1. The utility model provides an aviation screw tapping machine cooling system, sets up on the tapping machine, its characterized in that: including spraying the mechanism, circulation mechanism and filtering mechanism, circulation mechanism includes water tank and circulating pump, it includes the sprinkler bead to spray the mechanism, the sprinkler bead adopts the pipe connection with circulation mechanism, filtering mechanism includes the rose box, the rose box top is provided with inserts the unloading funnel of establishing in the rose box, unloading funnel lower extreme installation valve, the rose box lower extreme is provided with the fluid-discharge tube with the water tank intercommunication, the level is provided with multiunit filter unit in the rose box, filter unit includes the installing frame, the installing frame right-hand member rotates and sets up the pivot of extending along the fore-and-aft direction, the pivot left side is connected with the filter screen, the rose box outside is provided with the slewing mechanism that each pivot is connected, the rose box lateral wall of filter unit below rotates and is provided with the deflector, the rose box side of keeping away from the deflector articulates there is the discharge door.
2. The aviation screw tapping machine cooling system of claim 1, wherein: the rotating mechanism comprises a rack and a plurality of gears, the gears are respectively installed at the end parts of the rotating shafts, the rack is horizontally arranged below the gears in a sliding mode and is meshed with the gears, and an electric telescopic rod connected with the rack is horizontally arranged on the outer side of the filter box.
3. The cooling system for an aviation screw tapping machine as claimed in claim 1, wherein: the guide plate free end be connected with the connection rope, the one end of connecting the rope and keeping away from the guide plate is connected with the discharge door.
4. The aviation screw tapping machine cooling system of claim 1, wherein: the valve is an electric gate valve.
5. The cooling system for an aviation screw tapping machine as claimed in claim 1, wherein: the lower ends of the filter screens are provided with electromagnets.
6. The aviation screw tapping machine cooling system of claim 1, wherein: the upper end of the filter screen is provided with a rubber sealing ring.
CN202220893352.4U 2022-04-18 2022-04-18 Cooling system of aviation screw tapping machine Active CN217991854U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220893352.4U CN217991854U (en) 2022-04-18 2022-04-18 Cooling system of aviation screw tapping machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220893352.4U CN217991854U (en) 2022-04-18 2022-04-18 Cooling system of aviation screw tapping machine

Publications (1)

Publication Number Publication Date
CN217991854U true CN217991854U (en) 2022-12-09

Family

ID=84287891

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220893352.4U Active CN217991854U (en) 2022-04-18 2022-04-18 Cooling system of aviation screw tapping machine

Country Status (1)

Country Link
CN (1) CN217991854U (en)

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