CN217813607U

CN217813607U - High heat dissipation copper turbine

Info

Publication number: CN217813607U
Application number: CN202221679384.0U
Authority: CN
Inventors: 刘斌
Original assignee: Zhongzhou Technology Jiangxi Transmission Co ltd
Current assignee: Zhongzhou Technology Jiangxi Transmission Co ltd
Priority date: 2022-07-01
Filing date: 2022-07-01
Publication date: 2022-11-15
Anticipated expiration: 2032-07-01

Abstract

The utility model discloses a high heat dissipation copper turbine, which comprises a turbine body and a heat dissipation mechanism, wherein the heat dissipation mechanism is arranged at two ends of the turbine body, first heat dissipation holes in the heat dissipation mechanism are respectively arranged at two ends of the turbine body, and the heat dissipation mechanism also comprises second heat dissipation holes, fins, through holes, connecting plates and a heat conduction net; the utility model discloses a setting of heat dissipation mechanism, can effectually make it possess high radiating effect, so that it realizes the effect that self preservation protected, and the operation of the equipment of assurance, prevent wearing and tearing and damage because of the high temperature appearing simultaneously, at first utilize first louvre, the second louvre, fins, through hole and connecting hole carry out first heat dissipation work, then recycle connecting plate and heat conduction net and carry out heat conduction work, thereby its radiating efficiency increases once more, through installation mechanism's setting, can make it possess the effect of easy to assemble dismouting, can make things convenient for people's operation and use.

Description

High heat dissipation copper turbine

Technical Field

The utility model relates to a copper turbine technical field specifically is a high heat dissipation copper turbine.

Background

The turbine is a fan in an engine of an automobile or an airplane, fuel steam is blown into the engine by utilizing waste gas to improve the performance of the engine, the turbine is a rotary power machine for converting the energy of a flowing working medium into mechanical work by a high-heat-dissipation copper turbine, the turbine is one of main parts of an aeroengine, a gas turbine and a steam turbine, and parts in a turbocharged engine are usually in high-temperature and high-impact environments, so that the engine has special requirements on engine oil, and has the effects of better abrasion resistance, high temperature resistance, high speed for establishing a lubricating oil film, high oil film strength, good stability, low viscosity and the like. Because the turbine can produce higher temperature in long-time high-speed operation to because the material of copper turbine belongs to the metal of heat absorption class, traditional copper turbine thermal diffusivity is lower, not only is unfavorable for high radiating effect, moreover appears wearing and tearing easily and damages.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a high heat dissipation copper turbine possesses high radiating effect, and the operation of the equipment of guaranteeing moreover prevents simultaneously because of wearing and tearing and damage appear in the high temperature to solve the problem of proposing among the above-mentioned background art.

In order to achieve the above object, the utility model provides a following technical scheme: a high-heat-dissipation copper turbine comprises a turbine body and heat dissipation mechanisms, wherein the heat dissipation mechanisms are arranged at two ends of the turbine body, and first heat dissipation holes in the heat dissipation mechanisms are respectively formed at two ends of the turbine body;

the heat dissipation mechanism further comprises second heat dissipation holes, fins, through holes, connecting holes, a connecting plate and a heat conduction net, the second heat dissipation holes are formed in the two ends of the turbine body respectively, the fins are installed inside the second heat dissipation holes, the through holes are formed in the outer side of the turbine body, the connecting holes are formed between the first heat dissipation holes and the second heat dissipation holes, the connecting plate is installed in the upper portion and the lower portion of the two ends of the turbine body respectively, and the heat conduction net is installed at one end of the connecting plate.

Preferably, both ends of the turbine body are provided with mounting mechanisms, and each mounting mechanism comprises a connecting pipe, a sliding block, a groove, a spring, a supporting block, a thread groove and a threaded rod.

Preferably, the connection pipes are respectively installed at both ends of the turbine body, and the sliders are installed at both sides inside the connection pipes.

Preferably, the groove is formed in the inner side of the sliding block, and the spring is installed at one end of the inner cavity of the groove.

Preferably, the abutting block is installed at one end of the spring, a telescopic rod is installed at one end of the inner cavity of the groove, and one end of the telescopic rod and one end of the abutting block are installed.

Preferably, the axis body is all installed to the inside of turbine body and connecting pipe, the spout has all been seted up to the both sides of axis body.

Preferably, the sliding connection of slider is in the inside of spout, the thread groove is seted up respectively in the upper and lower two parts of axis body, the one end of threaded rod and the inside threaded connection of thread groove.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the utility model discloses a setting of heat dissipation mechanism can effectually make it possess high radiating effect to in its effect that realizes the self preservation and protect, the operation of the equipment of assurance prevents simultaneously because of wearing and tearing and damage appear in the high temperature, at first utilizes first louvre, second louvre, fin, through hole and connecting hole to carry out first heat dissipation work, and then recycles connecting plate and heat conduction net and carries out heat conduction work, thereby increases its radiating efficiency once more.

2. The utility model discloses through installation mechanism's setting, can make it possess the effect of easy to assemble dismouting, not only can make things convenient for people's operation and use, shortened the time of dismouting moreover, utilize slider, recess, spring and support the piece convenience to fix a position it and support tight work, then utilize thread groove and threaded rod threaded connection's relation conveniently to play the fixed effect of locking.

Drawings

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

FIG. 2 is a schematic view of a partial enlarged structure at A in FIG. 1 according to the present invention;

fig. 3 is a schematic view of the structure of the fin of the present invention;

fig. 4 is a schematic diagram of the connecting plate structure of the present invention.

In the figure: 1. a turbine body; 2. a heat dissipation mechanism; 21. a first heat dissipation hole; 22. a second heat dissipation hole; 23. a fin; 24. a through hole; 25. connecting holes; 26. a connecting plate; 27. a thermally conductive mesh; 3. an installation mechanism; 31. a connecting pipe; 32. a slider; 33. a groove; 34. a spring; 35. a resisting block; 36. a thread groove; 37. a threaded rod; 4. a shaft body; 5. a chute.

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.

It should be noted that all directional indicators (such as up, down, left, right, front, back \8230;) are provided in embodiments of the present invention. It is only used to explain the relative position relationship, movement, etc. of the components in a particular attitude (as shown in the drawings), and if the particular attitude changes, the directional indication changes accordingly. In addition, descriptions in the present application as to "first", "second", and the like are for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicit to the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory to each other or cannot be realized, such a combination should not be considered to exist, and is not within the protection scope of the present invention.

Referring to fig. 1 to 4, the present invention provides a high heat dissipation copper turbine, which includes a turbine body 1 and a heat dissipation mechanism 2, wherein the heat dissipation mechanism 2 is disposed at two ends of the turbine body 1, first heat dissipation holes 21 in the heat dissipation mechanism 2 are respectively disposed at two ends of the turbine body 1, and the first heat dissipation holes 21 are used to facilitate the rotation of the turbine body and perform the primary heat dissipation work in cooperation with the through holes 24;

it should be noted that, as shown in fig. 1, 3 and 4, the heat dissipation mechanism 2 further includes a second heat dissipation hole 22, fins 23, through holes 24, connection holes 25, connection plates 26 and heat conduction nets 27, the second heat dissipation hole 22 is respectively opened at two ends of the turbine body 1, the fins 23 are installed inside the second heat dissipation hole 22, and the cooperation between the second heat dissipation hole 22 and the fins 23 is convenient to achieve the effect of secondary heat dissipation;

the through hole 24 is seted up in the outside of turbine body 1, the connecting hole 25 is seted up between first louvre 21 and second louvre 22, connecting plate 26 is installed respectively in the upper and lower two of turbine body 1 both ends, heat conduction net 27 is installed in the one end of connecting plate 26, and the through hole 24 of seting up can be used to make and communicate between first louvre 21 and the second louvre 22, thereby play the effect of ventilating, in order to better carry out the work of dispelling the heat, and connecting plate 26 is convenient for install heat conduction net 27, and heat conduction net 27 then is used for playing the effect of absorbed heat, and can directly give off in the air when it rotates, thereby its radiating effect has been improved.

Can effectually make it possess high radiating effect to its effect that realizes the self preservation and protects, the operation of the equipment of guaranteeing moreover prevents wearing and tearing and damage because of the high temperature appearance simultaneously.

Preferably, as shown in fig. 1, 2 and 3, the mounting mechanisms 3 are disposed at two ends of the turbine body 1, and each mounting mechanism 3 includes a connecting pipe 31, a sliding block 32, a groove 33, a spring 34, a resisting block 35, a thread groove 36 and a threaded rod 37, so that the mounting mechanisms can achieve an effect of facilitating mounting and dismounting.

In addition, as shown in fig. 1, 2 and 3, the connecting pipes 31 are respectively installed at both ends of the turbine body 1, the sliders 32 are installed at both sides inside the connecting pipes 31, the components inside the connecting pipes 31 are conveniently connected by using the connecting pipes 31, and the sliders 32 can also play a role in assisting installation and disassembly, and play a role in limiting when being conveniently installed.

In addition, as shown in fig. 1, 2 and 3, the groove 33 is opened on the inner side of the sliding block 32, the spring 34 is installed at one end of the inner cavity of the groove 33, the groove 33 is used for facilitating installation of the spring 34 and retraction of the abutting block 35, and the spring 34 can be used for connecting the abutting block 35 and pushing the abutting block 35 to achieve the abutting effect through the elasticity of the spring.

Further, as shown in fig. 1, 2 and 3, support the piece 35 and install in the one end of spring 34, the telescopic link is installed to the one end of recess 33 inner chamber, the one end of telescopic link with support the one end installation of piece 35, utilize to support the piece 35 and can support tight work to axis body 4 when being promoted it and remove, and the setting of telescopic link can be used for carrying out auxiliary stay to spring 34, axis body 4 then is used for driving it and rotates the work after the installation is accomplished.

In addition, as shown in fig. 1, 2 and 3, the shaft body 4 is installed inside the turbine body 1 and the connecting pipe 31, the sliding grooves 5 are formed in both sides of the shaft body 4, and the sliding grooves 5 are conveniently arranged to be in sliding connection with the sliding blocks 32, so that the limiting operation is assisted.

In addition, as shown in fig. 1, 2 and 3, the sliding connection of slider 32 is in the inside of spout 5, and thread groove 36 is seted up respectively in the upper and lower two parts of axis body 4, the one end of threaded rod 37 and the inside threaded connection of thread groove 36, through seting up of thread groove 36 conveniently with threaded rod 37 carry out threaded connection, so that it carries out locking work, and the top and the bottom of connecting pipe 31 all open and shut threaded hole, and it cooperates threaded rod 37 to carry out the screw rotation, so that it carries out the locking work of screw extension.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a high heat dissipation copper turbine, includes turbine body (1) and heat dissipation mechanism (2), its characterized in that: the heat dissipation mechanisms (2) are arranged at two ends of the turbine body (1), and first heat dissipation holes (21) in the heat dissipation mechanisms (2) are respectively formed at two ends of the turbine body (1);

the heat dissipation mechanism (2) is characterized by further comprising second heat dissipation holes (22), fins (23), through holes (24), connecting holes (25), connecting plates (26) and heat conduction nets (27), the second heat dissipation holes (22) are respectively arranged at two ends of the turbine body (1), the fins (23) are arranged inside the second heat dissipation holes (22), the through holes (24) are arranged on the outer side of the turbine body (1), the connecting holes (25) are arranged between the first heat dissipation holes (21) and the second heat dissipation holes (22), the connecting plates (26) are respectively arranged at the upper portion and the lower portion of two ends of the turbine body (1), and the heat conduction nets (27) are arranged at one ends of the connecting plates (26).

2. The high heat dissipation copper turbine of claim 1, wherein: the turbine comprises a turbine body (1) and is characterized in that mounting mechanisms (3) are arranged at two ends of the turbine body (1), and each mounting mechanism (3) comprises a connecting pipe (31), a sliding block (32), a groove (33), a spring (34), a supporting block (35), a thread groove (36) and a threaded rod (37).

3. The high heat dissipation copper turbine of claim 2, wherein: the connecting pipes (31) are respectively arranged at two ends of the turbine body (1), and the sliding blocks (32) are arranged at two sides inside the connecting pipes (31).

4. The high heat dissipation copper turbine of claim 3, wherein: the groove (33) is arranged on the inner side of the sliding block (32), and the spring (34) is arranged at one end of the inner cavity of the groove (33).

5. The high heat dissipation copper turbine of claim 4, wherein: the supporting block (35) is installed at one end of the spring (34), a telescopic rod is installed at one end of the inner cavity of the groove (33), and one end of the telescopic rod is installed at one end of the supporting block (35).

6. The high heat dissipation copper turbine of claim 5, wherein: the inside of turbine body (1) and connecting pipe (31) all installs axis body (4), spout (5) have all been seted up to the both sides of axis body (4).

7. The high heat dissipation copper turbine of claim 6, wherein: the sliding connection of slider (32) is in the inside of spout (5), thread groove (36) are seted up respectively in the upper and lower two parts of axis body (4), the internal thread connection of one end and thread groove (36) of threaded rod (37).