CN216697173U - Ground station compact space heat radiation structure - Google Patents

Ground station compact space heat radiation structure Download PDF

Info

Publication number
CN216697173U
CN216697173U CN202220134497.6U CN202220134497U CN216697173U CN 216697173 U CN216697173 U CN 216697173U CN 202220134497 U CN202220134497 U CN 202220134497U CN 216697173 U CN216697173 U CN 216697173U
Authority
CN
China
Prior art keywords
computer
radiator
module
bottom cover
ground station
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN202220134497.6U
Other languages
Chinese (zh)
Inventor
胡延斌
张应通
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenzhen Huazhiyi Technology Co ltd
Original Assignee
Shenzhen Huazhiyi Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Shenzhen Huazhiyi Technology Co ltd filed Critical Shenzhen Huazhiyi Technology Co ltd
Priority to CN202220134497.6U priority Critical patent/CN216697173U/en
Application granted granted Critical
Publication of CN216697173U publication Critical patent/CN216697173U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02DCLIMATE CHANGE MITIGATION TECHNOLOGIES IN INFORMATION AND COMMUNICATION TECHNOLOGIES [ICT], I.E. INFORMATION AND COMMUNICATION TECHNOLOGIES AIMING AT THE REDUCTION OF THEIR OWN ENERGY USE
    • Y02D10/00Energy efficient computing, e.g. low power processors, power management or thermal management

Landscapes

  • Cooling Or The Like Of Electrical Apparatus (AREA)

Abstract

The utility model discloses a compact space heat radiation structure of a ground station, which comprises: the computer comprises a main box body, a bottom cover arranged at the bottom of the main box body, a computer mainboard arranged on the bottom cover, an air blower fan arranged on the computer mainboard, a computer radiator arranged at the side of the air blower fan, a module radiator arranged at the side of the computer radiator and a battery arranged at the side of the computer mainboard, wherein an air inlet is arranged at the position of the bottom cover corresponding to the computer mainboard, an air outlet is arranged at the position of the bottom cover corresponding to the module radiator, and heat generated by the computer mainboard is discharged to the outside from the air outlet after sequentially passing through the air blower fan, the computer radiator and the module radiator. Through this heat radiation structure outside the quick inside heat outflow equipment of acceleration equipment, can help reducing the temperature of ground station, improve equipment availability factor and operation experience sense, strengthened the stability of product use. In a limited space, the heat dissipation structure is utilized to quickly dissipate heat for the computer mainboard and the image module at the same time, so that the space is reasonably utilized.

Description

Compact space heat radiation structure of ground station
Technical Field
The utility model relates to the field of ground stations, in particular to a compact space heat dissipation structure of a ground station.
Background
The box ground station has been widely popularized in the fields of unmanned aerial vehicles, unmanned ships, robots and the like. Operating personnel need be long-time at outdoor operations, and when summer, because outdoor weather is hotter, the ground station is not good at the inside heat dissipation of box in the use, leads to the heat not to go out the outside to make product surface temperature very high, inside electronic component also can influence reaction efficiency because of the high temperature, reduces the operation and experiences the sense, risk such as equipment crash can appear even.
Accordingly, the prior art is deficient and needs improvement.
SUMMERY OF THE UTILITY MODEL
The utility model aims to overcome the defects of the prior art and provide a compact space heat dissipation structure of a ground station.
The technical scheme of the utility model is as follows: a ground station compact space heat dissipation structure, comprising: the computer comprises a main box body, a bottom cover arranged at the bottom of the main box body, a computer mainboard arranged on the bottom cover, an air blower fan arranged on the computer mainboard, a computer radiator arranged beside the air blower fan, a module radiator arranged beside the computer radiator and a battery arranged beside the computer mainboard, wherein the bottom cover corresponds to the computer mainboard, an air inlet is arranged at the position of the computer mainboard, an air outlet is arranged at the position of the module radiator corresponding to the bottom cover, and heat generated by the computer mainboard is discharged to the outside from the air outlet after passing through the air blower fan, the computer radiator and the module radiator in sequence.
Further, the local station compact space heat dissipation mechanism further comprises an image module, and the image module is attached to the module radiator.
Furthermore, the computer radiator is provided with radiating fins.
Furthermore, a computer radiator air outlet is formed in one side, facing the module radiator, of the computer radiator, a module radiator air inlet is formed in one side, facing the computer radiator, of the module radiator, and a module radiator air outlet is formed in the bottom of the module radiator.
Furthermore, a plurality of strip-shaped grooves are formed in the bottom cover.
By adopting the scheme, the utility model has the following beneficial effects:
1. the heat dissipation structure can quickly accelerate the heat in the equipment to flow out of the equipment, help to reduce the temperature of a ground station, improve the use efficiency and the operation experience of the equipment and enhance the use stability of products;
2. the utility model utilizes the heat dissipation structure to quickly dissipate heat for the computer mainboard and the image module simultaneously in a limited space, thereby reasonably utilizing the space.
Drawings
Fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is an exploded view of the present invention.
Fig. 3 is a schematic structural diagram of the bottom cover of the present invention.
Detailed Description
The utility model is described in detail below with reference to the figures and the specific embodiments.
Referring to fig. 1 to 3, the present invention provides a heat dissipation structure for a compact space of a ground station, including: the computer case comprises a main case body 1, a bottom cover 2 arranged at the bottom of the main case body 1, a computer mainboard 3 arranged on the bottom cover 2, an air blower fan 4 arranged on the computer mainboard 3, a computer radiator 5 arranged at the side of the air blower fan 4, a module radiator 6 arranged at the side of the computer radiator 5 and a battery 7 arranged at the side of the computer mainboard 1. An air inlet 21 is formed in the position, corresponding to the computer mainboard 1, of the bottom cover 2, and an air outlet 22 is formed in the position, corresponding to the module radiator 6, of the bottom cover 2. When the ground station works, a large amount of heat is generated by the computer motherboard 31, and the heat generated by the computer motherboard 3 is exhausted to the outside from the air outlet 22 on the bottom cover 2 after passing through the blower fan 4, the computer radiator 5 and the module radiator 6 in sequence. The noise of the blower fan 4 is low, and noise pollution is reduced.
Specifically, a computer radiator air outlet is arranged on one side, facing the module radiator 6, of the computer radiator 5, a module radiator air inlet is arranged on one side, facing the computer radiator 5, of the module radiator 6, the computer radiator 5 air outlet is in butt joint with the module radiator 6 air inlet, and a module radiator air outlet is arranged at the bottom of the module radiator 6. The heat generated by the computer motherboard 3 is directly blown to the computer radiator 5 by the wind generated by the blower fan 4, then is conducted to the module radiator 6 through the air outlet of the computer radiator 5 and the air inlet of the module radiator 6, and finally is exhausted to the outside through the air outlet of the module radiator 6 and the air outlet 22 on the bottom cover 2. So, can accelerate the inside heat circulation of equipment, reduce the inside temperature of equipment fast.
The computer radiator 5 is provided with radiating fins, so that the radiating effect can be enhanced and the temperature reduction speed can be increased.
This ground station compact space heat dissipation mechanism still includes image module 8, and image module 8 generates heat the amount great, and image module 8 and module radiator 6 laminating, the heat that image module 8 produced directly conducts to module radiator 6 on, conducts to the external world via module radiator 6.
The bottom cover 2 is provided with a plurality of strip-shaped grooves 23, a space for heat circulation is reserved for the electronic components on the bottom cover 2 by arranging the grooves 23, and the air inlet 21 and the air outlet 22 are arranged in the strip-shaped grooves 23.
In conclusion, the utility model has the following beneficial effects:
1. the heat dissipation structure can quickly accelerate the heat in the equipment to flow out of the equipment, help to reduce the temperature of a ground station, improve the use efficiency and the operation experience of the equipment and enhance the use stability of a product;
2. the utility model utilizes the heat dissipation structure to quickly dissipate heat for the computer mainboard and the image module simultaneously in a limited space, thereby reasonably utilizing the space.
The present invention is not limited to the above preferred embodiments, and any modifications, equivalent substitutions and improvements made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims (5)

1. A ground station compact space heat dissipation structure, comprising: the computer comprises a main box body, a bottom cover arranged at the bottom of the main box body, a computer mainboard arranged on the bottom cover, an air blower fan arranged on the computer mainboard, a computer radiator arranged beside the air blower fan, a module radiator arranged beside the computer radiator and a battery arranged beside the computer mainboard, wherein the bottom cover corresponds to the computer mainboard, an air inlet is arranged at the position of the computer mainboard, an air outlet is arranged at the position of the module radiator corresponding to the bottom cover, and heat generated by the computer mainboard is discharged to the outside from the air outlet after passing through the air blower fan, the computer radiator and the module radiator in sequence.
2. The ground station compact space heat dissipation structure of claim 1, further comprising an image module, the image module being attached to the module heat sink.
3. The ground station compact space heat dissipation structure of claim 1, wherein the computer heat sink is provided with heat dissipation fins.
4. The ground station compact space heat dissipation structure of claim 1, wherein a computer heat sink air outlet is disposed at a side of the computer heat sink facing the module heat sink, a module heat sink air inlet is disposed at a side of the module heat sink facing the computer heat sink, and a module heat sink air outlet is disposed at a bottom of the module heat sink.
5. The ground station compact space heat dissipation structure of claim 1, wherein the bottom cover is provided with a plurality of strip-shaped grooves.
CN202220134497.6U 2022-01-18 2022-01-18 Ground station compact space heat radiation structure Active CN216697173U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202220134497.6U CN216697173U (en) 2022-01-18 2022-01-18 Ground station compact space heat radiation structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202220134497.6U CN216697173U (en) 2022-01-18 2022-01-18 Ground station compact space heat radiation structure

Publications (1)

Publication Number Publication Date
CN216697173U true CN216697173U (en) 2022-06-07

Family

ID=81825914

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202220134497.6U Active CN216697173U (en) 2022-01-18 2022-01-18 Ground station compact space heat radiation structure

Country Status (1)

Country Link
CN (1) CN216697173U (en)

Similar Documents

Publication Publication Date Title
CN101859168A (en) Computer case
CN114384979A (en) PC host case capable of realizing efficient heat dissipation
CN202050634U (en) Sealing water cooling device for cooling electronic equipment
US8248799B2 (en) Data center
CN205944337U (en) Battery package heat abstractor and battery package
CN216697173U (en) Ground station compact space heat radiation structure
CN106774751B (en) External surface heat abstractor
CN208572646U (en) A kind of radiator and the hand-held unmanned plane with the radiator break through equipment
CN218337008U (en) Laser galvanometer device with heat radiation structure
CN108448732B (en) Wireless power supply system
CN216700759U (en) Unmanned aerial vehicle
CN203608314U (en) Switch chassis
CN101137281A (en) Double-tooth radiation fin, outdoor cabinet therewith as heat radiator and heat radiating method
CN114667038B (en) Miniaturized piezoelectric air-cooled closed-loop control heat dissipation framework
CN212302406U (en) PC host case capable of realizing efficient heat dissipation
CN203930674U (en) A kind of ruggedized computer cooling cabinet
CN210283963U (en) Charging station
CN207773505U (en) A kind of unmanned plane radiator
CN212515695U (en) Dual heat dissipation device for computer mainframe
CN220755360U (en) Main frame type chassis radiating structure based on transformer and module radiator
US20220312648A1 (en) Chassis and power supply system
CN219999400U (en) Gateway device
CN111077958A (en) Computer case air exhaust system and air exhaust method
CN211979570U (en) Smart city is with high heat dissipation storage device of cloud computing host computer
CN219834787U (en) Layered combined air-cooling heat dissipation mechanism

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant