CN215942988U - Fuselage structure and have its robot - Google Patents
Fuselage structure and have its robot Download PDFInfo
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- CN215942988U CN215942988U CN202120654989.3U CN202120654989U CN215942988U CN 215942988 U CN215942988 U CN 215942988U CN 202120654989 U CN202120654989 U CN 202120654989U CN 215942988 U CN215942988 U CN 215942988U
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- 230000017525 heat dissipation Effects 0.000 claims abstract description 43
- 239000012528 membrane Substances 0.000 claims description 10
- 238000005034 decoration Methods 0.000 claims description 9
- 230000008901 benefit Effects 0.000 abstract description 14
- 230000000694 effects Effects 0.000 abstract description 12
- 238000009434 installation Methods 0.000 description 9
- 238000007789 sealing Methods 0.000 description 8
- 238000001816 cooling Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 3
- 238000005192 partition Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 241000282414 Homo sapiens Species 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 238000003491 array Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 235000001968 nicotinic acid Nutrition 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
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Abstract
The utility model relates to a fuselage structure and a robot with the fuselage structure, wherein the fuselage structure comprises: a housing; the core control assembly is accommodated in the shell and used for controlling the whole machine; the heat dissipation part is arranged in the shell, is distributed close to the core control assembly and is used for forming a flow airflow in the shell; wherein, be equipped with air inlet district and air-out district on the casing, be following the air inlet district extremely be equipped with in proper order in the direction in air-out district the radiating piece with the core control subassembly. Through the mode, the utility model can prevent the temperature rise in the machine body structure from being too high, and has the advantage of good heat dissipation effect.
Description
[ technical field ] A method for producing a semiconductor device
The utility model relates to the technical field of robots, in particular to a robot body structure and a robot with the same.
[ background of the utility model ]
The robot, as a product of advanced integrated control theory, mechano-electronics, computers, materials and bionics, can automatically execute various operations, is suitable for various severe working environments, and brings great effects for releasing the workload of human beings and improving the production efficiency, so that the robot is widely applied to various fields of production and life.
With the continuous development of the robot technology, the robot has increasingly powerful functions and meets various complex application requirements. The problem that follows is that the core control components of the robot are increasingly complex and the number of heat generating components is increasing. The excessive heating value causes the environment temperature in the robot to be high, and the normal work of the robot is seriously influenced. Accordingly, there is a need for improvements in the art that overcome the deficiencies in the prior art.
[ Utility model ] content
The utility model aims to provide a machine body structure and a robot with the same, which can prevent the temperature rise in the machine body structure from being too high and have the advantage of good heat dissipation effect.
The purpose of the utility model is realized by the following technical scheme:
a fuselage structure comprising: a housing; the core control assembly is accommodated in the shell and used for controlling the whole machine; the heat dissipation part is arranged in the shell, is distributed close to the core control assembly and is used for forming a flow airflow in the shell; wherein, be equipped with air inlet district and air-out district on the casing, be following the air inlet district extremely be equipped with in proper order in the direction in air-out district the radiating piece with the core control subassembly.
In one embodiment, the core control assembly comprises at least two PCB control panels, and the PCB control panels are arranged along the direction from the air inlet area to the air outlet area.
In one embodiment, the air inlet area is provided with a first waterproof breathable membrane, and the air outlet area is provided with a second waterproof breathable membrane.
In one embodiment, the heat dissipation member is a heat dissipation fan, and the heat dissipation fan is disposed at the air inlet area.
In one embodiment, the casing is divided into an upper part and a lower part, and comprises a lower casing and an upper casing, wherein the lower casing is provided with the air inlet area, and the upper casing is provided with the air outlet area.
In one embodiment, the lower casing is hollow inside and is provided with an opening at the top, so as to form a main chamber, and the core control assembly and the heat dissipation member are arranged in the main chamber.
In one embodiment, the air intake area, the heat sink, and the core control assembly at least partially overlap in an up-down direction.
In one embodiment, the air outlet area is further provided with an upper shell decoration, and a third waterproof breathable membrane is arranged between the air outlet area and the upper shell decoration; and the upper shell decorating part is provided with a hollow hole for air outlet and heat dissipation.
In one embodiment, the core control assembly further comprises a mounting frame, and the PCB control board is detachably arranged on the mounting frame to form a whole with the mounting frame.
The utility model adopts another technical scheme that:
a robot comprising a fuselage structure as described above.
Compared with the prior art, the utility model has the following beneficial effects:
according to the machine body structure and the robot with the same, the core control assembly can be fully cooled through the cooling piece, so that the internal temperature rise of the machine body structure is prevented from being too high, and the machine body structure and the robot with the same have the advantage of good cooling effect.
[ description of the drawings ]
Fig. 1 is a schematic view in plan view of the fuselage structure proposed by the utility model.
Fig. 2 is an exploded view of fig. 1.
Fig. 3 is a schematic view of the fuselage structure proposed by the utility model in the bottom view.
Fig. 4 is a schematic cross-sectional structure of fig. 1.
Fig. 5 is an enlarged schematic view of a region B in fig. 4.
Fig. 6 is an enlarged schematic view of the region C in fig. 4.
Fig. 7 is an exploded view of the upper housing and the upper housing trim of fig. 2.
Fig. 8 is an exploded view of the upper housing and the second waterproof, breathable membrane of fig. 6.
Fig. 9 is a schematic structural diagram of the core control assembly of fig. 4.
[ detailed description ] embodiments
In order to make the aforementioned objects, features and advantages of the present invention comprehensible, embodiments accompanied with figures are described in detail below. It is to be understood that the specific embodiments described herein are merely illustrative of the utility model and are not limiting of the utility model. It should be further noted that, for the convenience of description, only some of the structures related to the present invention are shown in the drawings, not all of the structures. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
The terms "comprising" and "having," as well as any variations thereof, in the present invention are intended to cover non-exclusive inclusions. For example, a process, method, system, article, or apparatus that comprises a list of steps or elements is not limited to only those steps or elements listed, but may alternatively include other steps or elements not listed, or inherent to such process, method, article, or apparatus.
Reference herein to "an embodiment" means that a particular feature, structure, or characteristic described in connection with the embodiment can be included in at least one embodiment of the utility model. The appearances of the phrase in various places in the specification are not necessarily all referring to the same embodiment, nor are separate or alternative embodiments mutually exclusive of other embodiments. It is explicitly and implicitly understood by one skilled in the art that the embodiments described herein can be combined with other embodiments.
Referring to fig. 1 to 6, the present invention provides a fuselage structure, including: a housing 210; a core control component 220 accommodated in the casing 210 for overall control; and a heat sink 277 disposed within the casing 210 and distributed proximate to the core control assembly 220 for creating a flow of air within the casing 210; the casing 210 is provided with an air inlet region 2128 and an air outlet region 2119, and the heat sink 277 and the core control module 220 are sequentially arranged along the direction from the air inlet region 2128 to the air outlet region 2119. In this way, the core control assembly 220 can be fully cooled by the cooling element 277, so that the internal temperature rise of the machine body structure is prevented from being too high, and the heat dissipation device has the advantage of good heat dissipation effect.
In the present invention, the heat sink 277 is a heat dissipation fan, and the heat dissipation fan is disposed at the air inlet area 2128, so that the external air can be quickly sucked into the casing 210, and effective heat dissipation of the core control component 220 is realized. The external air, which is relatively cool, finally flows out of the air outlet region 2119 after entering the housing 210 through the air inlet region 2128, so that a heat dissipating air flow is formed in the housing 210 along the direction from the air inlet region 2128 to the air outlet region 2119, and the hollow arrows in fig. 5 and 6 indicate the flow direction of the heat dissipating air flow. In order to improve the heat dissipation efficiency of the core control module 220, the air inlet region 2128, the heat dissipation member 277 and the core control module 220 are at least partially overlapped in the vertical direction, so that the air flow entering the casing 210 through the air inlet region 2128 can be intensively blown to the core control module 220, and the core control module has the advantages of good heat dissipation effect and high heat dissipation efficiency. In order to further improve the heat dissipation efficiency of the core control module 220 and improve the heat dissipation effect, the projections of the air inlet region 2128, the heat dissipation member 277, the core control module 220, and the air outlet region 2119 in the vertical direction are overlapped with each other, so that the flow path of the heat dissipation airflow is short, the heat in the casing 210 can be taken away to the greatest extent, and the core control module has the advantages of high heat dissipation efficiency and good heat dissipation effect.
In the present invention, the casing 210 is substantially ship-shaped, and the casing 210 is divided into an upper part and a lower part, where the upper part and the lower part are consistent with the upper part and the lower part in the drawings, and the casing 210 includes the lower casing 212 and the upper casing 211 detachably installed on the lower casing 212, so that the core control assembly 220 and the heat sink 277 can be conveniently installed in the casing 210, and the appearance is elegant. The lower housing 212 is hollow inside and is provided with an open top to form a main chamber 215, and the upper housing 211 is used for closing the opening of the main chamber 215 to form a closed space isolated from the outside. An air inlet area 2128 is arranged on the lower shell 212, an air outlet area 2119 is arranged on the upper shell 211, the core control module 220 and the heat dissipation member 277 are arranged in the main chamber 215, and the heat dissipation member 277 is connected with the core control module 220 through a circuit.
Referring to fig. 9, the core control assembly 220 includes a mounting frame 224 and at least two PCB control boards detachably mounted on the mounting frame 224 to form a single body with the mounting frame 224. The PCB control board generates a large amount of heat during operation, and the heat sink 277 is provided to dissipate heat of the PCB control board. In the utility model, the PCB control board is arranged along the direction from the air inlet area 2128 to the air outlet area 2119, namely the PCB control board is distributed along the up-down direction, under the condition, the arrangement direction of the PCB control board is consistent with the flowing direction of the heat dissipation airflow, the heat on the PCB control board can be taken away by the heat dissipation airflow to the greatest extent, and the utility model has the advantages of good heat dissipation effect and high heat dissipation efficiency.
Further, the mounting rack 224 is provided with three PCB control boards, and the three PCB control boards are fastened on the mounting rack 224 through screws respectively. The three PCB control boards are a power PCB control board 221, a motion PCB control board 222, and an application PCB control board 223, respectively. The mounting bracket 224 includes first and second plate portions 2241 and 2242, the first and second plate portions 2241 and 2242 are distributed in the up-down direction, and the first and second plate portions 2241 and 2242 have a space in a direction perpendicular to the up-down direction for accommodating the PCB control board. Wherein, power PCB control panel 221 and motion PCB control panel 222 are located on first board portion 2241 dorsad, use PCB control panel 223 to locate on second board portion 2242, distribute side by side between power PCB control panel 221, motion PCB control panel 222 and the use PCB control panel 223, have compact structure, advantage that occupation space is little.
In order to prevent moisture and dirt in the external environment from entering the casing 210, the air inlet section 2128 is provided with a first waterproof air-permeable membrane 2129, and the air outlet section 2119 is provided with a second waterproof air-permeable membrane 2118, as shown in fig. 5 and 8, so that moisture and dirt in the external environment can be effectively prevented from entering the casing 210 to affect the normal operation of the electronic components inside the casing 210. In the present invention, the air inlet region 2128 comprises a plurality of small air inlet holes, and the air inlet region 2128 is formed by a plurality of small air inlet holes in an array; the air outlet region 2119 comprises a plurality of small air outlet holes, and the air outlet region 2119 is formed by a plurality of small air outlet hole arrays; the air inlet small holes and the air outlet small holes have the air inlet function and the air homogenizing function. It is understood that the air inlet 2128 and the air outlet 2119 may be through holes with larger apertures, or a fence structure, etc., according to the actual requirement.
Further, as shown in fig. 7, an upper housing decoration 2117 is further disposed on the upper housing 211, the upper housing decoration 2117 is located outside the upper housing 211, and the upper housing decoration 2117 covers the air outlet zone 2119 for decoration. The upper casing decorating part 2117 is provided with a hollow hole for air outlet and heat dissipation, and heat dissipation airflow flowing out of the air outlet area 2119 can be discharged to the external environment through the hollow hole of the upper casing decorating part 2117. In order to prevent moisture and dirt in the external environment from entering the air outlet region 2119 through the hollow holes, a third moisture-proof and breathable membrane 2116 is arranged between the air outlet region 2119 and the upper casing decorating part 2117.
In the present invention, the top opening of the lower housing 212 is annular, a sealing ring 283 is disposed on the opening, and the sealing ring 283 is adhered to the opening by gluing, but it should be understood that the sealing ring 283 is also annular, and the sealing ring 283 may be an integral ring or may be spliced by different parts to form an integral ring. After the upper housing 211 and the lower housing 212 are mounted, the edge of the upper housing 211 abuts against the sealing ring 283, so that the upper housing 211 and the lower housing 212 are sealed. In order to facilitate the installation of the core control unit 220 and the heat sink 277 in the main chamber 215, the portions of the openings do not lie on the same horizontal plane, and specifically, the portion of the opening in the length direction of the lower housing 212 sinks, that is, there is a height difference in the up-down direction between the portion of the opening in the length direction of the lower housing 212 and the portion of the opening in the width direction of the lower housing 212, which is provided to: for enlarging the opening to better expose the main chamber 215 for ease of installation. In the present invention, the opening at the top of the lower housing 212 is required to satisfy the following requirements: the projection of the opening on the bottom of the lower housing 212 is equal to or larger than the bottom area of the main chamber 215, and the projection is obtained by a parallel projection method. Therefore, the device has the advantage of convenience in disassembly and assembly.
The lower case 212 has a front mounting cavity S and a rear mounting cavity R formed at both ends in the longitudinal direction. The two longitudinal ends are defined as a front end of the lower case 212 and a rear end of the lower case 212, respectively, and it is understood that the front end of the lower case 212 is provided with the front mounting cavity S and the rear end of the lower case 212 is provided with the rear mounting cavity R. The front mounting cavity S and the rear mounting cavity R are respectively independent from the main cavity 215, where the independent means: the front installation cavity S is separated from the main cavity 215 by a partition plate, and the rear installation cavity R is separated from the main cavity 215 by a partition plate. The front end of the front installation cavity S is opened so as to be convenient for installing a front limb (not shown); the rear mounting chamber R is open at its rear end to facilitate mounting of a rear limb (not shown). The opening part of the front installation cavity S is provided with a front end cover component 213, and the opening part of the rear installation cavity R is provided with a rear end cover component 214.
To facilitate mounting of the front and rear limbs to the cabinet 210, the front and rear head assemblies 213 and 214 are separately provided. Specifically, the front end cover assembly 213 is arranged in an upper and lower split manner, or in a left and right split manner; the rear end cap assembly 214 is disposed in a vertically split manner, or in a horizontally split manner. In the utility model, the front end cover assembly 213 and the rear end cover assembly 214 are arranged in an up-down split manner, the front end cover assembly 213 comprises a front upper end cover 2131 and a front lower end cover 2132, and the front upper end cover 2131 and the front lower end cover 2132 are detachably arranged at the front end opening of the front installation cavity S; the rear end cap assembly 214 includes a rear upper end cap 2141 and a rear lower end cap 2142, and the rear upper end cap 2141 and the rear lower end cap 2142 are detachably disposed at the rear end opening of the rear mounting cavity R.
It is understood that the fuselage structure of the present invention can be applied to different usage scenarios, as exemplified below.
The body structure of the present invention can be applied to a robot. Wherein the robot comprises a fuselage structure as described above.
In summary, the core control assembly 220 can be fully cooled by the cooling element 277, so that the temperature rise inside the machine body structure is prevented from being too high, and the advantage of good cooling effect is achieved; furthermore, the PCB control board is distributed along the up-down direction, heat on the PCB control board can be taken away to the maximum extent by the heat dissipation airflow, and the heat dissipation device has the advantages of good heat dissipation effect and high heat dissipation efficiency; furthermore, the PCB control board is stacked on the mounting frame 224, which has the advantages of compact structure and small occupied space; furthermore, a sealing ring 283 is arranged at the opening of the lower shell 212, and after the upper shell 211 and the lower shell 212 are installed, the edge of the upper shell 211 abuts against the sealing ring 283, so that the sealing effect is good; further, the parts of the opening of the lower housing 212 are not located on the same horizontal plane, so as to enlarge the opening, better expose the main chamber 215, and provide the advantage of convenient installation.
The above is only one embodiment of the present invention, and any other modifications based on the concept of the present invention are considered as the protection scope of the present invention.
Claims (10)
1. A fuselage structure, comprising:
a housing (210);
the core control assembly (220) is accommodated in the shell (210) and is used for controlling the whole machine; and
-a heat sink (277) arranged within the casing (210) and distributed close to the core control assembly (220) for creating a flow of air within the casing (210);
wherein, be equipped with air inlet district (2128) and air-out district (2119) on casing (210), be in the edge air inlet district (2128) extremely be equipped with in proper order in the direction of air-out district (2119) heat dissipation piece (277) with core control subassembly (220).
2. The fuselage structure as defined in claim 1,
the core control assembly (220) comprises at least two PCB control panels, and the PCB control panels are arranged along the direction from the air inlet area (2128) to the air outlet area (2119).
3. The fuselage structure as defined in claim 1,
the air inlet area (2128) is provided with a first waterproof breathable membrane (2129), and the air outlet area (2119) is provided with a second waterproof breathable membrane (2118).
4. The fuselage structure as defined in claim 1,
the heat dissipation piece (277) is a heat dissipation fan, and the heat dissipation fan is arranged at the air inlet area (2128).
5. The fuselage structure as defined in claim 1,
the upper and lower components of a whole that can function independently setting of casing (210) is including casing (212) and last casing (211) down, be equipped with down on casing (212) air inlet district (2128), be equipped with on last casing (211) air-out district (2119).
6. The fuselage structure as defined in claim 5,
the lower shell (212) is hollow inside and is arranged with an opening at the top, so as to form a main chamber (215), and the core control assembly (220) and the heat dissipation member (277) are arranged in the main chamber (215).
7. The fuselage structure as defined in claim 1,
the air inlet area (2128), the heat dissipation member (277) and the core control component (220) are at least partially overlapped in the vertical direction.
8. The fuselage structure as defined in claim 1,
the air outlet area (2119) is further provided with an upper shell decoration (2117), and a third waterproof breathable membrane (2116) is arranged between the air outlet area (2119) and the upper shell decoration (2117);
wherein, go up casing decoration (2117) and be equipped with the fretwork hole for the air-out heat dissipation.
9. The fuselage structure as defined in claim 2,
the core control assembly (220) further comprises a mounting rack (224), and the PCB control board is detachably arranged on the mounting rack (224) to form a whole with the mounting rack (224).
10. A robot, characterized by comprising a fuselage structure according to any one of claims 1 to 9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120654989.3U CN215942988U (en) | 2021-03-31 | 2021-03-31 | Fuselage structure and have its robot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120654989.3U CN215942988U (en) | 2021-03-31 | 2021-03-31 | Fuselage structure and have its robot |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215942988U true CN215942988U (en) | 2022-03-04 |
Family
ID=80506072
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120654989.3U Active CN215942988U (en) | 2021-03-31 | 2021-03-31 | Fuselage structure and have its robot |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215942988U (en) |
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2021
- 2021-03-31 CN CN202120654989.3U patent/CN215942988U/en active Active
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| GR01 | Patent grant | ||
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| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221109 Address after: No.018, 8th floor, building 6, No.33 yard, middle Xierqi Road, Haidian District, Beijing 100085 Patentee after: BEIJING XIAOMI MOBILE SOFTWARE Co.,Ltd. Patentee after: Dreame technology (Suzhou) Co.,Ltd. Address before: 215000 E3, building 16, No. 2288, Wuzhong Avenue, Yuexi, Wuzhong District, Suzhou City, Jiangsu Province Patentee before: Dreame technology (Suzhou) Co.,Ltd. |