CN217761324U - Screw machine main machine head for hollow glass autoclave - Google Patents
Screw machine main machine head for hollow glass autoclave Download PDFInfo
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- CN217761324U CN217761324U CN202221041646.0U CN202221041646U CN217761324U CN 217761324 U CN217761324 U CN 217761324U CN 202221041646 U CN202221041646 U CN 202221041646U CN 217761324 U CN217761324 U CN 217761324U
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- autoclave
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Abstract
The utility model relates to a technical field of screw rod machine especially relates to a screw rod machine host computer head that cavity glass autoclave was used. Its technical scheme includes aircraft nose body, cooling chamber, shell and outlet pipe, the shell has been cup jointed to the surface of aircraft nose body, and the inside of aircraft nose body and shell forms the cooling chamber, the outer end face welding in one side of shell has the link, and the outer end face welding in one side of link has the connecting axle, the induction port has been seted up to the outer end face in one side of aircraft nose body, the upper surface intercommunication in cooling chamber has the inlet tube, and the surface threaded connection of inlet tube has the water intaking valve, the lower surface intercommunication in cooling chamber has the outlet pipe that runs through the shell, and the inner wall embedding of outlet pipe is fixed with the fixed net, the inner wall of outlet pipe is located the below embedding of fixed net and is fixed with the connecting net, and the inner wall of outlet pipe is located the below embedding of connecting net and is fixed with the filter screen, the surface threaded connection of outlet pipe has the outlet valve. The utility model discloses be convenient for cool off aircraft nose body.
Description
Technical Field
The utility model relates to a technical field of screw rod machine specifically is a screw rod machine host computer head that cavity glass autoclave was used.
Background
In the 20 th 30 s, swedish engineers studied gas turbines and wanted to find a rotary compressor that would require much higher speeds than a piston compressor in order to be directly driven by the gas turbine and not surge. In order to achieve the above object, he invented a screw compressor. In theory, screw compressors have the characteristics they require, but they have not found application in this field because of the very large displacement necessary to meet the gas turbine operating requirements. Nevertheless, the swedish engineers and the swedish SRM company, in which they are located, continue to study the use of screw compressors in other fields.
At present, when a main machine head of a screw machine for a hollow glass autoclave is used, large heat can be generated, the main machine head is used in the autoclave, and under the conditions of high pressure and high temperature, a shell of the screw machine can deform to cause damage, even large accidents are caused.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a screw rod machine host computer head that cavity glass autoclave was used to solve the problem that proposes among the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a screw machine host computer head that cavity glass autoclave was used, includes aircraft nose body, cooling chamber, shell and outlet pipe, the shell has been cup jointed to the surface of aircraft nose body, and the inside of aircraft nose body and shell forms the cooling chamber, the lower surface intercommunication in cooling chamber has the outlet pipe that runs through the shell, and the inner wall embedding of outlet pipe is fixed with the fixed network, the below embedding that the inner wall of outlet pipe is located the fixed network is fixed with the connecting network, and the below embedding that the inner wall of outlet pipe is located the connecting network is fixed with the filter screen, the surface threaded connection of outlet pipe has the outlet valve.
Preferably, the outer end face of one side of the machine head body is provided with an air suction port penetrating through the shell, and the lower surface of the machine head body is provided with an air exhaust port penetrating through the shell. The screw machine is convenient to use by arranging the air suction port and the air exhaust port in the machine head body.
Preferably, the upper surface of the cooling cavity is communicated with a water inlet pipe, and the outer surface of the water inlet pipe is in threaded connection with a water inlet valve. The water inlet pipe is arranged on the upper surface of the cooling cavity, so that water can conveniently enter the cooling cavity.
Preferably, the inner wall of the handpiece body is welded with a fixing rod, and the outer surface of the fixing rod is rotatably connected with a male rotor. The fixing rod is arranged on the inner wall of the machine head body, so that the male rotor is convenient to install.
Preferably, the inner wall of the handpiece body is welded with a connecting rod, and the outer surface of the connecting rod is rotatably connected with a female rotor. The connecting rod is arranged on the inner wall of the machine head body, so that the female rotor is convenient to install.
Preferably, a connecting frame is welded on the outer end face of one side of the shell, and a connecting shaft is welded on the outer end face of one side of the connecting frame. The connecting frame and the connecting shaft are arranged on one side of the shell, so that the shell is convenient to mount.
Preferably, the aperture of the fixed net, the aperture of the connecting net and the aperture of the filter screen are sequentially reduced. The aperture is reduced in sequence, so that the water is convenient to filter.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses a set up the cooling chamber, inlet tube and outlet pipe, the effect of being convenient for cool off the aircraft nose body has been reached, be connected inlet tube and outlet pipe and water tank, open the water intaking valve, low temperature water gets into the cooling chamber through the inlet tube, flow in the cooling chamber and heat transfer, then open the outlet valve, water after the heat transfer passes through outlet pipe flow return water tank, refrigerate once more, circulative cooling aircraft nose body carries out, the fixed network, connecting network and filter screen can filter aquatic impurity, water can recycle, a large amount of energy is saved.
2. The utility model discloses a set up cloudy rotor, positive rotor and dead lever, reached the effect of the screw rod machine's of being convenient for use, cloudy rotor and positive rotor rotate under power device's effect, can inhale gas through the induction port, and the rethread gas vent is with gas outgoing, the screw rod machine's of being convenient for use.
Drawings
FIG. 1 is a schematic view of the main sectional structure of the present invention;
FIG. 2 is an enlarged schematic view of the water outlet pipe of the present invention;
fig. 3 is a schematic view of the structure of the present invention.
In the figure: 1. an air suction port; 2. a male rotor; 3. a handpiece body; 4. a cooling chamber; 5. a water inlet valve; 6. a water inlet pipe; 7. a connecting frame; 8. fixing the rod; 9. a connecting shaft; 10. a connecting rod; 11. a female rotor; 12. a housing; 13. an exhaust port; 14. a water outlet pipe; 15. fixing the net; 16. connecting a net; 17. filtering with a screen; 18. and (4) a water outlet valve.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", 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 simplification of the description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "provided," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Example one
Referring to fig. 1 to fig. 3, the present invention provides an embodiment: the utility model provides a screw machine host computer head that cavity glass autoclave was used, including aircraft nose body 3, cooling chamber 4, shell 12 and outlet pipe 14, the upper surface intercommunication of cooling chamber 4 has inlet tube 6, and the surface threaded connection of inlet tube 6 has water intaking valve 5, the lower surface intercommunication of cooling chamber 4 has outlet pipe 14 that runs through shell 12, and the inner wall embedding of outlet pipe 14 is fixed with fixed network 15, the inner wall of outlet pipe 14 is located the below embedding of fixed network 15 and is fixed with connecting net 16, and the inner wall of outlet pipe 14 is located the below embedding of connecting net 16 and is fixed with filter screen 17, the surface threaded connection of outlet pipe 14 has outlet valve 18, the aperture of fixed network 15, connecting net 16 and filter screen 17 reduces in proper order.
Of course, as is well known to those skilled in the art, the male rotor 2, the handpiece body 3, the water inlet pipe 6, the female rotor 11 and the water outlet pipe 14 of the present invention also need to provide a power device to enable the normal operation thereof, and as is well known to those skilled in the art, the provision of the power is common to those skilled in the art, and is in the conventional manner or common knowledge, and will not be described herein again, and those skilled in the art can make any choice according to their needs or convenience.
The working principle of the main machine head of the screw machine for the hollow glass autoclave based on the embodiment 1 is as follows: the water inlet pipe 6 and the water outlet pipe 14 are connected with the water tank, the water inlet valve 5 is opened, low-temperature water enters the cooling cavity 4 through the water inlet pipe 6, the low-temperature water flows in the cooling cavity 4 for heat exchange, then the water outlet valve 18 is opened, the water after heat exchange flows back to the water tank through the water outlet pipe 14 for refrigerating again, the machine head body 3 is cooled in a circulating mode, impurities in the water can be filtered through the fixing net 15, the connecting net 16 and the filter screen 17, the water can be recycled, and a large amount of energy is saved.
Example two
As shown in fig. 1-3, the utility model provides a screw machine main head that cavity glass autoclave was used, compare in embodiment one, this embodiment still includes aircraft nose body 3, cooling chamber 4, shell 12 and outlet pipe 14, the inner wall welding of aircraft nose body 3 has dead lever 8, and the surface rotation of dead lever 8 is connected with male rotor 2, the inner wall welding of aircraft nose body 3 has connecting rod 10, and the surface rotation of connecting rod 10 is connected with female rotor 11, shell 12 has been cup jointed to the surface of aircraft nose body 3, and aircraft nose body 3 forms cooling chamber 4 with the inside of shell 12, the outer end face welding of one side of shell 12 has link 7, and the outer end face welding of one side of link 7 has connecting axle 9, the induction port 1 that runs through shell 12 has been seted up to the outer end face of one side of aircraft nose body 3, and the gas vent 13 that runs through shell 12 has been seted up to the lower surface of aircraft nose body 3.
In this embodiment, the female rotor 11 and the male rotor 2 rotate under the action of the power device, so that air can be sucked in through the air suction port 1 and then discharged through the air discharge port 13, thereby facilitating the use of the screw machine.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (7)
1. The utility model provides a screw machine host computer head that cavity glass autoclave was used, includes aircraft nose body (3), cooling chamber (4), shell (12) and outlet pipe (14), its characterized in that: shell (12) have been cup jointed to the surface of aircraft nose body (3), and aircraft nose body (3) and inside formation cooling chamber (4) of shell (12), the lower surface intercommunication in cooling chamber (4) has outlet pipe (14) of running through shell (12), and the inner wall embedding of outlet pipe (14) is fixed with fixed network (15), the below embedding that the inner wall of outlet pipe (14) is located fixed network (15) is fixed with connecting network (16), and the below embedding that the inner wall of outlet pipe (14) is located connecting network (16) is fixed with filter screen (17), the surface threaded connection of outlet pipe (14) has outlet valve (18).
2. The screw machine main head for the autoclave for hollow glass according to claim 1, wherein: the outer end face of one side of the machine head body (3) is provided with an air suction port (1) penetrating through the shell (12), and the lower surface of the machine head body (3) is provided with an air exhaust port (13) penetrating through the shell (12).
3. The screw machine main head for the autoclave for hollow glass according to claim 1, wherein: the upper surface of the cooling cavity (4) is communicated with a water inlet pipe (6), and the outer surface of the water inlet pipe (6) is in threaded connection with a water inlet valve (5).
4. The screw machine main head for the autoclave for hollow glass according to claim 1, wherein: the inner wall welding of aircraft nose body (3) has dead lever (8), and the surface rotation of dead lever (8) is connected with male rotor (2).
5. The screw machine main head for the autoclave for hollow glass according to claim 1, wherein: the inner wall of the machine head body (3) is welded with a connecting rod (10), and the outer surface of the connecting rod (10) is rotatably connected with a female rotor (11).
6. The screw machine main head for the autoclave for hollow glass according to claim 1, wherein: the outer end face of one side of the shell (12) is welded with the connecting frame (7), and the outer end face of one side of the connecting frame (7) is welded with the connecting shaft (9).
7. The screw machine main head for the autoclave for hollow glass according to claim 1, wherein: the aperture of the fixed net (15), the connecting net (16) and the filter screen (17) is reduced in sequence.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202221041646.0U CN217761324U (en) | 2022-05-05 | 2022-05-05 | Screw machine main machine head for hollow glass autoclave |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN202221041646.0U CN217761324U (en) | 2022-05-05 | 2022-05-05 | Screw machine main machine head for hollow glass autoclave |
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CN217761324U true CN217761324U (en) | 2022-11-08 |
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CN202221041646.0U Active CN217761324U (en) | 2022-05-05 | 2022-05-05 | Screw machine main machine head for hollow glass autoclave |
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2022
- 2022-05-05 CN CN202221041646.0U patent/CN217761324U/en active Active
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