Integrated heat dissipation type micro-pressure oxygen cabin pneumatic control host

Abstract

The utility model relates to an integrated heat dissipation type micro-pressure oxygen cabin pneumatic control host which comprises a shell, a first air duct structure and a second air duct structure, an air inlet is formed in the top side of the shell, a first air outlet is formed in the bottom end of the shell, and a second air outlet is formed in the side face, close to the bottom end, of the shell. The first air duct structure is communicated with the air inlet, the first air duct structure is communicated with one of the first air outlet and the second air outlet, and the second air duct structure is communicated with the other one of the first air outlet and the second air outlet. The air inlet and the second air outlet are formed in the two non-adjacent positions of the shell, so that the transmitted hot air flow is prevented from being sucked back into the system, the heat accumulation condition is avoided, the cruising ability of the product is improved, and the service life of the product is prolonged.

Description

TECHNICAL FIELD

[0001] The present application relates to the technical field of micro-pressure oxygen cabin, and particularly relates to a micro-pressure oxygen cabin air control host integrated with a heat dissipation function. BACKGROUND

[0002] Some micro-pressure oxygen cabins on the market have an air inlet and an air outlet in close positions, so that the hot air flow emitted is sucked back to the air control host system, heat is accumulated, the temperature of the cabin exceeds the limit after a period of operation, the normal operation of the compressor is affected, and the long-time operation and service life of the product are not conducive.

[0003] Therefore, the prior art has defects and needs to be improved. SUMMARY

[0004] The present application provides a micro-pressure oxygen cabin air control host integrated with a heat dissipation function to solve the problem that the air inlet and the air outlet of some micro-pressure oxygen cabins are in close positions, so that the hot air flow emitted is sucked back to the air control host system, heat is accumulated, the temperature of the cabin exceeds the limit after a period of operation, the normal operation of the compressor is affected, and the long-time operation and service life of the product are not conducive.

[0005] In a first aspect, the present application provides a micro-pressure oxygen cabin air control host integrated with a heat dissipation function, which comprises an outer shell, a first air duct structure and a second air duct structure, an air inlet is formed on the top side of the outer shell, a first air outlet is formed at the bottom end of the outer shell, and a second air outlet is formed on the side of the outer shell close to the bottom end, the first air duct structure is in communication with the air inlet, the first air duct structure is in communication with one of the first air outlet and the second air outlet, and the second air duct structure is in communication with the other one of the first air outlet and the second air outlet.

[0006] Optionally, the first air duct structure is in communication with the first air outlet, and the second air duct structure is in communication with the second air outlet.

[0007] Optionally, the first air duct structure is in communication with the second air outlet, and the second air duct structure is in communication with the first air outlet.

[0008] Optionally, the air inlet is formed on the top end or the side close to the top end of the outer shell.

[0009] Optionally, the outer shell is in the shape of a regular prism, a cylinder or an elliptic cylinder.

[0010] Optionally, the first air duct structure comprises an air inlet treatment assembly and a compressor, the air inlet treatment assembly is in communication with the air inlet and the compressor respectively, and the compressor is in communication with one of the first air outlet and the second air outlet.

[0011] Optionally, the first air duct structure and the second air duct structure are arranged in the outer shell.

[0012] Optionally, the air intake processing assembly comprises air intake filter cotton, an air intake filter box and an air intake silencer box, the air intake filter box is in communication with the air inlet, the air intake filter cotton is located at one end of the air intake filter box pipe and covers the air inlet, and the air intake silencer box is in communication with the air intake filter box and the compressor respectively.

[0013] Optionally, the second air duct structure comprises a hood fan and a compressor hood, the compressor hood is arranged outside the compressor, and the hood fan is located directly above the compressor hood and opposite to the compressor hood at the air outlet end.

[0014] Optionally, the air inlet is provided with 1-4 groups.

[0015] Compared with the prior art, the above technical scheme provided by the embodiment of the present application has the following advantages:

[0016] The embodiment of the present application avoids the outflow of hot air in the system and the generation of heat accumulation, which is beneficial to improve the endurance and service life of the product. BRIEF DESCRIPTION OF DRAWINGS

[0017] The accompanying drawings, which are incorporated into and form part of the specification, illustrate embodiments consistent with the present application and, together with the specification, serve to explain the principles of the application.

[0018] In order to more clearly illustrate the technical scheme in the embodiments of the present application or the prior art, the drawings needed to be used in the embodiment or the prior art description will be briefly introduced below, and obviously, other drawings can also be obtained by those skilled in the art without creative labor.

[0019] One or more embodiments are exemplarily illustrated by the pictures in the corresponding drawings, which do not constitute a limitation on the embodiments, and elements with the same reference numerals in the drawings represent similar elements, unless otherwise specified, and the drawings in the drawings do not constitute a proportional limitation.

[0020] Figure 1 A perspective view of an integrated heat dissipation type micro-pressure oxygen cabin gas control host provided by the embodiment of the present application is shown.

[0021] Figure 2 A perspective view of another integrated heat dissipation type micro-pressure oxygen cabin gas control host provided by the embodiment of the present application is shown.

[0022] Figure 3 A perspective view of a partial structure of an integrated heat dissipation type micro-pressure oxygen cabin gas control host provided by the embodiment of the present application is shown.

[0023] Figure 4 For Figure 3 Enlarged view at A in Figure 1.

[0024] BRIEF DESCRIPTION OF DRAWINGS

[0025] 1. housing; 2. first air duct structure; 3. second air duct structure; 4. control unit; 5. air inlet; 6. first air outlet; 7. second air outlet; 8. air inlet treatment assembly; 10. air inlet filter cotton; 11. air inlet filter box; 12. air inlet silencer box; 13. shroud fan; 14. compressor shroud. DETAILED DESCRIPTION

[0026] In order to make the objects, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be described clearly and completely below in connection with the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments of the present application. Based on the embodiments in the present application, all other embodiments obtained by a person of ordinary skill in the art without creative effort belong to the scope of protection of the present application.

[0027] The following disclosure provides many different embodiments, or examples, for implementing different structures of the present application. For the purpose of simplicity, the elements and settings of particular examples in the following description will be described with reference to specific arrangements and examples. These are, of course, merely examples and are in no way limiting to the present application. Furthermore, the present application can be practiced with the exact arrangement of elements and / or settings used in different examples. Such variations are considered to be within the scope of the present application as defined by the appended claims.

[0028] For the purpose of description, spatial relative terms, such as "internal", "external", "lateral", "medial", "under", "below", "above", "on", "front", "back", etc., can be used to describe the relative position relationship or movement of one element or feature with respect to another element or feature as shown in the drawings. Such spatial relative terms are intended to include different orientations of the device in use or operation in addition to the orientation depicted in the drawings. For example, if the device in the drawings is turned over or reversed, or the orientation of the device is changed, the indication of the direction will also change accordingly, for example, the element described as "under" or "below" another element or feature will be subsequently oriented as "above" or "over" the other element or feature. Therefore, the example term "below" can include both upward and downward positions. The device can be additionally oriented (rotated 90 degrees or in other directions) and the spatial relative relationship descriptors used in the text are interpreted accordingly.

[0029] In order to solve the technical problems in the prior art, the application provides an integrated heat dissipation type micro-pressure oxygen cabin air control host computer, which can realize the following effects: the air inlet and the second air outlet are arranged at two non-adjacent positions of the shell, the outgoing hot air flow is avoided from being sucked back into the system, the generation of heat accumulation is avoided, and the endurance and service life of the product are improved.

[0030] Figures 1-4 The integrated heat dissipation type micro-pressure oxygen cabin air control host computer provided by the application comprises a shell 1, a first air duct structure 2, a second air duct structure 3 and a control part 4. The first air duct structure 2 and the second air duct structure 3 are arranged in the shell 1. The control part 4 is partially arranged in the shell 1 and partially extends out of the shell 1 and is exposed on the surface of the shell 1. The control part 4 is electrically connected with the first air duct structure 2 and the second air duct structure 3. The first air duct structure 2 is used for air purification, the second air duct structure 3 is used for air blowing and heat dissipation in the shell 1, and the user can control the working states of the first air duct structure 2 and the second air duct structure 3 through the control part 4.

[0031] Further, please continue to refer to Figures 1-2 An air inlet 5 is formed on the top side of the shell 1, a first air outlet 6 is formed at the bottom end of the shell 1, and a second air outlet 7 is formed on the side surface of the shell 1 close to the bottom end. The first air duct structure 2 is in communication with the air inlet 5, the first air duct structure 2 is in communication with the first air outlet 6, and the second air duct structure 3 is in communication with the second air outlet 7. The air outlets are arranged non-adjacently through the first air outlet 6 and the second air outlet 7, so that the heat accumulation of the two air outlets is avoided, the heat dissipation effect of the whole machine is affected, the outgoing hot air flow is avoided from being sucked back into the system, the generation of heat accumulation is avoided, the endurance and service life of the product are improved. It can be understood that the first air duct structure 2 can also be in communication with the second air outlet 7. At this time, the second air duct structure 3 is in communication with the first air outlet 6, and the specific arrangement can be made according to the actual structure needs.

[0032] Please continue to refer to Figures 1-2 The air inlet 5 is formed on the top end or the side surface close to the top end of the shell 1, so that the air inlet 5, the first air outlet 6 and the second air outlet 7 are not arranged adjacently. In the application, the shell 1 is in the shape of a prism, specifically a quadrangular prism. The air inlet 5 is arranged at the upper end position of the side surface, the first air outlet 6 is arranged at the bottom surface, and the second air outlet 7 is arranged at the lower end position of the side surface. However, the shell 1 can also be in the shape of a cylinder or an elliptical cylinder, and the specific arrangement can be made according to the actual needs. The air inlet 5 of the application is not arranged on the top surface, which can prevent some large debris from easily entering the inside of the machine body, improve the cleaning degree of the inside of the machine body, and the air inlet 5 can also be arranged on the top surface.

[0033] Please refer toFigures 3-4 The first air duct structure 2 comprises an air intake treatment assembly 8 and a compressor, the air intake treatment assembly 8 is communicated with the air inlet 5 and the compressor (not shown in the figure) respectively, and the compressor is communicated with the first air outlet 6, wherein the air intake treatment assembly 8 comprises air intake filter cotton 10, an air intake filter box 11 and an air intake silencer box 12, the air intake filter box 11 is communicated with the air inlet 5, the air intake filter cotton 10 is located at one end of a pipe opening of the air intake filter box 11 and covers the air inlet 5, and the air intake silencer box 12 is communicated with the air intake filter box 11 and the compressor respectively. The air intake filter cotton 10 is arranged to filter out dust, dust and other micro-particles in the air, so as to output relatively clean air, and activated carbon is arranged in the air intake filter box 11 to adsorb peculiar smell and remove formaldehyde.

[0034] In the utility model, the air inlet 5 is arranged as two groups, therefore, the air intake treatment assembly 8 is also arranged as two groups, each air intake treatment assembly 8 is communicated with one air inlet 5 and the compressor respectively, and arranging multiple air inlets 5 is also beneficial to solve the problem that one air inlet 5 is blocked by the outside and cannot intake air, thereby affecting the working efficiency.

[0035] Please continue to refer to Figure 4 The second air duct structure 3 comprises a machine cover fan 13 and a compressor machine cover 14, the compressor machine cover 14 covers the outside of the compressor, the machine cover fan 13 is located directly above the compressor machine cover 14 and the air outlet end thereof is opposite to the compressor machine cover 14. The compressor machine cover 14 is arranged to protect the compressor, so as to avoid the internal structure of the shell 1 from being easily scratched by the compressor and damaging the compressor, thereby being beneficial to prolonging the service life of the compressor; the machine cover fan 13 is arranged, so that the heat generated by the compressor is transmitted to the compressor machine cover 14, the machine cover fan 13 accelerates the flow of the air speed at the compressor machine cover 14, the heat is quickly taken away and blown out through the second air outlet 7, so that the temperature of the compressor does not rise too high after working for a period of time, thereby being beneficial to prolonging the endurance and the service life of the compressor.

[0036] In the above embodiments, the description of each embodiment has its own emphasis, and the parts not described in detail in a certain embodiment can be referred to the related description of other embodiments.

[0037] In the description of the present application, it should be understood that the orientation or positional relationship indicated by the terms "center", "longitudinal", "transverse", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise" and the like are based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present application and simplifying the description, and therefore cannot be understood as indicating or implying that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore cannot be understood as limiting the present application.

[0038] In addition, the terms "first", "second", etc. are used herein only to describe different instances, and do not imply or suggest relative importance or a number of the technical features indicated. Thus, the features defined with "first", "second" can include one or more of the features explicitly or implicitly. In the description of the present application, the meaning of "a plurality of" is two or more, unless otherwise explicitly specified and limited.

[0039] In the present application, unless otherwise explicitly specified and limited, the terms "mounting", "connecting", "connecting", "fixing" and the like should be understood broadly, for example, it can be connected, or detachable, or integrated; it can be mechanical connection, or electrical connection; it can be directly connected, or indirectly connected through an intermediate medium, or the internal communication of two elements or the interaction relationship between two elements. For those skilled in the art, the specific meaning of the above terms in the present application can be understood according to the specific circumstances.

[0040] In the present application, unless otherwise explicitly specified and limited, the first feature "on" or "under" the second feature can include the first and second features in direct contact, or the first and second features not in direct contact but in contact through another feature between them. Moreover, the first feature "on", "above" and "above" the second feature includes the first feature directly above and obliquely above the second feature, or only indicates that the first feature is higher than the second feature in horizontal height. The first feature "below", "below" and "below" the second feature includes the first feature directly below and obliquely below the second feature, or only indicates that the first feature is lower than the second feature in horizontal height.

[0041] In the description of the present application, the description of the terms "one embodiment", "some embodiments", "example", "specific example", or "some examples" and the like means that the specific features, structures, materials or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present application. In the present application, the illustrative description of the above terms should not be understood as necessarily referring to the same embodiment or example. Moreover, the specific features, structures, materials or characteristics described can be combined in any one or more embodiments or examples in a suitable manner. In addition, those skilled in the art can combine and combine different embodiments or examples described in the present application.

[0042] Obviously, those skilled in the art can make various modifications and variations to the present application without departing from the spirit and scope of the present application. Thus, these modifications and variations of the present application are intended to be included within the scope of the claims of the present application and their equivalents.

[0043] The above is merely specific embodiments of the present application, and the protection scope of the present application is not limited thereto, and any modification or replacement within the technical scope disclosed by the present application can be easily thought by those skilled in the art, and these modifications or replacements shall be encompassed in the protection scope of the present application. Therefore, the protection scope of the present application shall be subject to the protection scope of the claims.

Claims

1. An integrated heat-dissipating micro-pressure oxygen chamber air control unit, characterized in that: The air inlet is arranged on the top end or the side close to the top end of the shell.

2. The integrated heat-dissipation micro-pressure oxygen cabin gas control host of claim 1, wherein: The first air duct structure is in communication with the first air outlet, and the second air duct structure is in communication with the second air outlet.

3. The integrated heat-dissipation micro hyperbaric oxygen cabin gas control host computer according to claim 1, characterized in that: The first air duct structure is in communication with the second air outlet, and the second air duct structure is in communication with the first air outlet.

4. The integrated heat-dissipation micro-oxygen cabin air control host computer of claim 1, wherein: The air inlet is arranged on the top end or the side close to the top end of the shell.

5. The integrated heat-dissipation micro-oxygen cabin air control host computer of claim 1, wherein: The shell is in the shape of a regular prism, a cylinder or an elliptic cylinder.

6. The integrated heat-dissipation micro-oxygen cabin air control host computer of claim 1, wherein: The first air duct structure comprises an air inlet treatment assembly and a compressor, the air inlet treatment assembly is in communication with the air inlet and the compressor respectively, and the compressor is in communication with one of the first air outlet and the second air outlet.

7. The integrated heat-dissipation micro-oxygen cabin air control host computer of claim 1, wherein: The first air duct structure and the second air duct structure are arranged in the shell.

8. The integrated heat-dissipation micro-oxygen cabin air control host computer of claim 6, wherein: The air inlet treatment assembly comprises air inlet filter cotton, an air inlet filter box and an air inlet silencer box, the air inlet filter box is in communication with the air inlet, the air inlet filter cotton is arranged at one end of the air inlet filter box and covers the air inlet, and the air inlet silencer box is in communication with the air inlet filter box and the compressor respectively.

9. The integrated heat-dissipation micro-oxygen cabin air control host computer of claim 8, wherein: The second air duct structure comprises a machine cover fan and a compressor machine cover, the compressor machine cover is arranged outside the compressor, the machine cover fan is arranged directly above the compressor machine cover, and the air outlet end of the machine cover fan is opposite to the compressor machine cover.

10. The integrated heat-dissipation micro-oxygen cabin air control host computer of claim 1, wherein: The air inlet is provided with 1-4 groups.

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