Cooling mechanism of disc separator

Abstract

The utility model discloses a cooling mechanism of a disc separator, which is characterized in that the inner walls of a machine body and a machine cover are respectively provided with a cooling interlayer, and the cooling interlayers are matched with a water inlet hose, a metal hose and a water outlet hose to form a cooling passage, so that for some small separators, the limitation of the structural size of the separators can be effectively avoided; the situation that a cooling channel cannot be directly formed in the separator is avoided, so that the cooling requirement of the small separator is met, the temperature of the interior of the separator and the temperature of the surface of the separator body and the surface of the separator cover are reduced, the mechanical performance and use safety of the separator are improved, the service life of the separator is prolonged, and the safety of operators is better protected.

Description

Technical Field

[0001] The utility model belongs to the technical field of separation equipment, relates to the cooling of separation equipment, and specifically relates to a cooling mechanism of a disc-type separator. Background Art

[0002] The disc separator is a high-speed rotating centrifugal separation device. During operation, the device will generate a lot of heat due to energy loss and air friction, which will cause the temperature inside the machine and the surface of the cover to rise. This temperature rise will affect the mechanical performance and service life of the separator. The temperature rise on the surface of the cover will also pose a risk of scalding the operator. Therefore, whether it is to ensure the mechanical performance and safety of the separator, or to protect the operator from being scalded, it is necessary to consider cooling the machine during use.

[0003] The commonly used method of cooling the separator is to directly form a cooling channel inside the machine. However, for some small separators, due to the limitation of their own structural size, it is impossible to directly form a cooling channel inside the machine to effectively cool the separator in operation. Therefore, it is necessary to design a cooling mechanism different from the traditional cooling method for small separators. Utility Model Content

[0004] In view of the above problems, the main purpose of the utility model is to design a disc separator cooling mechanism to solve the temperature reduction and cooling problem of a small separator with limited structural size.

[0005] In order to achieve the above purpose, the utility model adopts the following technical solutions:

[0006] A cooling mechanism for a disc separator comprises a body and a cover, wherein the body and the cover are connected by screws, a body cooling interlayer is arranged on the inner wall of the body, a cover cooling interlayer is arranged on the inner wall of the cover, and the body cooling interlayer is connected with the cover cooling interlayer through a metal hose;

[0007] A water inlet joint is arranged at the outer bottom of the fuselage cooling interlayer, and a water outlet joint is arranged at the outer upper part of the cover cooling interlayer. The water inlet joint is connected to a water inlet hose, and the water outlet joint is connected to a water outlet hose.

[0008] As a further description of the utility model, a first joint is arranged at the upper outer part of the fuselage cooling interlayer, a second joint is arranged at the lower outer part of the cover cooling interlayer, one end of the metal hose is connected to the first joint, and the other end of the metal hose is connected to the second joint.

[0009] As a further description of the present invention, the first joint and the second joint are both arranged horizontally, and the angular positions of the first joint and the second joint are the same.

[0010] As a further description of the present invention, the water inlet joint and the first joint have the same angular position, and the water inlet joint and the water outlet joint have an angular position of 180°±10°.

[0011] As a further description of the utility model, the other ends of the water inlet hose and the water outlet hose are both connected to a converter and a ball valve.

[0012] As a further description of the utility model, the water inlet hose, the fuselage cooling interlayer, the metal hose, the cover cooling interlayer, and the water outlet hose form a cooling passage from bottom to top.

[0013] Compared with the prior art, the technical effects of the utility model are:

[0014] The utility model provides a cooling mechanism for a disc-type separator, in which cooling interlayers are respectively arranged on the inner walls of a body and a cover, and the cooling interlayer cooperates with a water inlet hose, a metal hose and a water outlet hose to form a cooling passage. For some small separators, it can effectively avoid the situation that a cooling passage cannot be directly formed inside the machine due to the limitation of its own structural size, thereby meeting the demand for cooling of the small separator, reducing the temperature inside the separator and the surface of the body and cover of the separator, improving the mechanical performance, safety of use and service life of the separator, and better protecting the safety of the operator. BRIEF DESCRIPTION OF THE DRAWINGS

[0015] Figure 1 This is an overall structural view of the cooling mechanism of the utility model.

[0016] In the figure, 1. fuselage, 11. fuselage cooling interlayer, 12. first joint, 2. machine cover, 21. machine cover cooling interlayer, 22. second joint, 3. metal hose, 4. water inlet joint, 41. water inlet hose, 5. adapter, 6. ball valve, 7. water outlet joint, 71. water outlet hose. DETAILED DESCRIPTION

[0017] The utility model is described in detail below with reference to the accompanying drawings:

[0018] In one embodiment of the utility model, a disc separator cooling mechanism is disclosed, such as Figure 1As shown, it includes a fuselage 1, a fuselage cooling interlayer 11, a machine cover 2, a machine cover cooling interlayer 21, a metal hose 3, a water inlet joint 4, a water inlet hose 41, an adapter 5, a ball valve 6, a water outlet joint 7, and a water outlet hose 71. The adapter and the ball valve are arranged in two groups, respectively matching the water inlet hose 41 and the water outlet hose 71. The water inlet hose 41 and the water outlet hose 71 include but are not limited to the form of metal hoses. Specifically, in this embodiment, the fuselage 1 and the cover 2 are connected by screws, the fuselage cooling interlayer 11 is arranged on the inner wall of the fuselage 1, the cover cooling interlayer 21 is arranged on the inner wall of the cover 2, the metal hose 3 connects the fuselage cooling interlayer 11 and the cover cooling interlayer 21, the water inlet joint 4 is arranged at the outer bottom of the fuselage cooling interlayer 11, one end of the water inlet hose 41 is connected to the water inlet joint 4, and the other end is connected to the adapter 5 and the ball valve 6, the water outlet joint 7 is arranged on the outer upper part of the cover cooling interlayer 21, one end of the water outlet hose 71 is connected to the water outlet joint 7, and the other end is connected to the adapter 5 and the ball valve 6.

[0019] More specifically, in this embodiment, a first joint 12 is provided at the upper outer portion of the fuselage cooling interlayer 11, a second joint 22 is provided at the lower outer portion of the cover cooling interlayer 21, one end of the metal hose 3 is connected to the first joint 12, and the other end of the metal hose 3 is connected to the second joint 22. The first joint 12 and the second joint 22 are both horizontally arranged, and the angular positions of the first joint 12 and the second joint 22 are the same.

[0020] It should also be noted that the above-mentioned water inlet joint 4 has the same angular position as the first joint 12, and the angular position with the water outlet joint 7 is 180°±10°, so that the cooling water can quickly fill and flow through the entire cooling channel after flowing in from the water inlet joint 4, and quickly flow out from the water outlet joint 7.

[0021] The water inlet hose 41, the fuselage cooling interlayer 11, the metal hose 3, the cover cooling interlayer 21, and the water outlet hose 71 described in this embodiment form a cooling water flow passage from bottom to top to ensure that the cooling water can flow quickly and fully through the entire fuselage 1 and the cover 2 after entering the machine, so that the machine can be better cooled.

[0022] During use, cooling water that meets the requirements enters the fuselage cooling interlayer 11 from the water inlet hose 41, flows into the machine cover cooling interlayer 21 through the connected metal hose 3, and then flows out to the outside of the machine from the water outlet hose 71 connected to the machine cover cooling interlayer 21; the adapter 5 and the ball valve 6 are respectively connected to the ends of the cooling water inlet hose 41 and the water outlet hose 71, so that the water inlet and water outlet amounts of the cooling water can be adjusted through the ball valve 6; during the flow of cooling water, the temperature difference is used to take away part of the heat generated during the operation of the machine, thereby achieving the purpose of cooling the machine.

[0023] The above content discloses the technical solution of the utility model, which has the following advantages over the prior art:

[0024] 1. The utility model enters the cooling interlayer of the machine cover from the cooling interlayer of the machine body through the externally connected metal hose, effectively avoiding the adverse effects caused by the limited structural size of machine parts;

[0025] 2. The body and cover of the utility model are respectively provided with closed cooling interlayers, so as to ensure the formation of a flow channel for cooling water and the cooling water will not leak during the flow process;

[0026] 3. The cooling water of the utility model enters the separator from the bottom of the cooling interlayer of the fuselage and flows out of the separator from the upper part of the cooling interlayer of the cover, so that the cooling water circulation process is carried out in a relatively sufficient and closed passage, meeting the cooling needs of small separators, improving the mechanical properties, safety of use and service life of the separator, and better protecting the safety of operators.

[0027] The above embodiments are only used to illustrate the technical solution of the utility model rather than to limit it. Other modifications or equivalent substitutions made to the technical solution of the utility model by ordinary technicians in this field should be included in the scope of the claims of the utility model as long as they do not depart from the spirit and scope of the technical solution of the utility model.

Claims

1. A cooling mechanism for a disc separator, comprising a body and a cover, wherein the body and the cover are connected by screws, and characterized in that: The fuselage inner wall is provided with a fuselage cooling interlayer, the cover inner wall is provided with a cover cooling interlayer, and the fuselage cooling interlayer is connected with the cover cooling interlayer through a metal hose; A water inlet joint is arranged at the outer bottom of the fuselage cooling interlayer, and a water outlet joint is arranged at the outer upper part of the cover cooling interlayer. The water inlet joint is connected to a water inlet hose, and the water outlet joint is connected to a water outlet hose.

2. A disc separator cooling mechanism according to claim 1, characterized in that: A first joint is arranged at the upper outer part of the fuselage cooling interlayer, a second joint is arranged at the lower outer part of the cover cooling interlayer, one end of the metal hose is connected to the first joint, and the other end of the metal hose is connected to the second joint.

3. A cooling mechanism for a disc separator according to claim 2, characterized in that: The first joint and the second joint are both arranged horizontally, and the angular positions of the first joint and the second joint are the same.

4. A disc separator cooling mechanism according to claim 2 or 3, characterized in that: The angular position of the water inlet joint is the same as that of the first joint, and the angular position of the water inlet joint and the water outlet joint is 180°±10°.

5. The cooling mechanism of a disc separator according to claim 1, characterized in that: The other ends of the water inlet hose and the water outlet hose are both connected to a converter and a ball valve.

6. A cooling mechanism for a disc separator according to claim 1, characterized in that: The water inlet hose, the fuselage cooling interlayer, the metal hose, the cover cooling interlayer, and the water outlet hose form a cooling passage from bottom to top.

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