CN205179563U - Four shaft air vehicle's well accuse shell structure - Google Patents
Four shaft air vehicle's well accuse shell structure Download PDFInfo
- Publication number
- CN205179563U CN205179563U CN201520876851.2U CN201520876851U CN205179563U CN 205179563 U CN205179563 U CN 205179563U CN 201520876851 U CN201520876851 U CN 201520876851U CN 205179563 U CN205179563 U CN 205179563U
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- CN
- China
- Prior art keywords
- supporting component
- middle control
- supporting
- shell structure
- module
- 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.)
- Expired - Fee Related
Links
- 238000009434 installation Methods 0.000 abstract description 6
- 239000006185 dispersion Substances 0.000 description 5
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
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- Cooling Or The Like Of Electrical Apparatus (AREA)
Abstract
The utility model discloses a four shaft air vehicle's well accuse shell structure, including well accuse casing, the inside power that is provided with of well accuse casing, the bottom of well accuse casing is provided with the thermovent, the inside fan that is provided with of well accuse casing, the fan air outlet is towards the thermovent setting, the inside support that is fixed with of well accuse casing, the support includes first supporting component and second supporting component, first supporting component and second supporting component mutually perpendicular and the setting of pegging graft, still include dock Panel, dock Panel is provided with a plurality of spliced eyes, first supporting component and second supporting component all are provided with pegs graft protrudingly with the spliced eye complex, dock Panel, first supporting component and second supporting component form the mounting groove of power supply source installation.
Description
Technical field
The utility model relates to a kind of flight instruments, and more particularly, it relates to a kind of middle control shell structure of four-axle aircraft.
Background technology
Aircraft is a kind of a kind of device automatically flown by remote control or pre-set programs, be widely used in monitoring field, in multiple field such as space industry, it comprises a control device, be arranged in control housing, middle control housing is centrally symmetrically arranged with at least four connecting portions, connecting portion is removably connected with connecting axle, the connecting axle other end is provided with motor, motor linkage is provided with blade, some motors are work strip aircraft flight simultaneously, one end and the connecting portion of connecting axle removably connect, its other end is fixed with motor valve jacket, motor valve jacket inside is provided with motor and is fixedly installed blade, the direction of described blade is vertical with the direction of corresponding connection parts, existing aircraft carries out cabling by the inner chamber of control device connecting portion, all driver modules and power supply are all arranged on middle control enclosure interior, but time at present due to work, the heat that power supply produces is larger, if heat cannot be derived in time, the job stability of electronic component in aircraft can be affected, thus affect the useful life of aircraft.
Utility model content
For the deficiency that prior art exists, the purpose of this utility model is to provide the middle control shell structure of the four-axle aircraft that a kind of heat dispersion is high.
For achieving the above object, the utility model provides following technical scheme: a kind of middle control shell structure of four-axle aircraft, comprise middle control housing, described middle control enclosure interior is provided with power supply, the bottom of described middle control housing is provided with thermovent, middle control enclosure interior is provided with blower fan, described fan outlet is arranged towards thermovent, described middle control enclosure interior is fixed with support, described support comprises the first supporting component and the second supporting component, the mutually vertical and grafting setting of described first supporting component and the second supporting component; Also comprise fixed panel, described fixed panel is provided with some spliced eyes, it is protruding that described first supporting component and the second supporting component are provided with the grafting coordinated with spliced eye, and described fixed panel, the first supporting component and the second supporting component form the mounting groove that power supply source is installed.
Such setting, by arranging blower fan and thermovent in middle control housing, correspondence forms a mounting groove on support, power supply source is placed, to ensure to there will not be larger installation question when installing, and be supplied to the larger memory space of power supply one, ensure that the design requirement of power supply is to ensure the heat-sinking capability of four-axle aircraft, pass through the setting of the first supporting component and the second supporting component simultaneously, ensure that fixing stability and the steadiness of installation.
The utility model can be set to further: described first supporting component is provided with two piece of first supporting bracket be arranged in parallel, described second supporting component is provided with two pieces of second supporting brackets be arranged in parallel, and described first supporting bracket, the second supporting bracket are around forming the standing groove placed for blower fan; Described standing groove is communicated with setting with described mounting groove.
Such setting, by the supporting bracket be arranged in parallel, form the standing groove placed for blower fan, the several end face of standing groove is fixed with blower fan respectively, so, ensure that steadiness during placement, and the standing groove at blower fan place is communicated with the mounting groove at power supply place, and the power supply module that to be requirement higher compared with high heat dispersion, so arrange like this, can radiating efficiency be improved, ensure heat dispersion.
The utility model can be set to further: described first supporting bracket and the second supporting bracket are provided with some louvres.By the setting of the louvre of supporting bracket, ensure that the exchange area of air, improve the efficiency of fan radiating.
The utility model can be set to further: be fixed with some first brace summers between two pieces of described first supporting brackets.By the setting of the first brace summer, improve the stability of two supporting constructions further.
The utility model can be set to further: be fixed with some second brace summers between two pieces of described second supporting brackets.Relative equally the first brace summer of second brace summer plays the effect of stable support and balance.
The utility model can be set to further: described first brace summer is provided with some air holes.By the setting of air holes, its radiating efficiency can be ensured, be conducive to middle control enclosure interior and form air-flow.
The utility model can be set to further: also include the radio station module of separate setting, main control module, receiver module and IMU module, and described radio station module, main control module, receiver module and IMU module are all arranged at the end face of installation panel.By such setting, facilitate each module change and repair, ensure radiating effect.
By adopting technique scheme, compared to existing technology, serve following effect, improve heat dispersion, and each module is independently arranged, convenient for maintaining is changed, the setting of support simultaneously ensure that the stability of installation, simultaneously for the installation of power supply provides enough spaces, ensure that the design requirement of power supply, improve small product size constant when, cruising time and heat dispersion can be improved as much as possible.
Accompanying drawing explanation
Fig. 1 controls shell structure schematic diagram in the utility model;
Fig. 2 controls housing upward view in the utility model;
Fig. 3 controls housing vertical view in the utility model;
Fig. 4 is the utility model supporting structure schematic diagram;
Fig. 5 is the utility model supporting structure front view;
Fig. 6 is the utility model support second structural representation;
Fig. 7 is the utility model supporting component structural representation;
Fig. 8 is the utility model supporting component front view;
Fig. 9 is the utility model first supporting bracket and the second supporting plate structure schematic diagram.
Reference numeral: 100, middle control housing; 110, thermovent; 120, blower fan; 200, support; 210, the first supporting component; 211, the first supporting bracket; 212, the first brace summer; 220, the second supporting component; 221, the second supporting bracket; 222, the second brace summer; 230, standing groove; 201, grafting is protruding; 202, louvre; 203, air holes; 230, fixed panel; 231, spliced eye; 300, mounting groove; 410, radio station module; 420, main control module; 430, receiver module; 440, IMU module.
Embodiment
Referring to figs. 1 through Fig. 9, the utility model embodiment is described further.
Shown in seeing figures.1.and.2, a kind of middle control housing 100 structure of four-axle aircraft, comprise middle control housing 100, middle control housing 100 inside is provided with power supply, with reference to shown in Fig. 3, the bottom of middle control housing 100 is provided with thermovent 110, be arranged on the middle position of middle control housing 100, thermovent 110 is arranged to netted, prevent blower fan 120 from coming off and damaging, middle control housing 100 inside is provided with blower fan 120, blower fan 120 air outlet is arranged towards thermovent 110, middle control housing 100 inside is fixed with support 200, with reference to shown in Fig. 4 and Fig. 5, support 200 comprises the first supporting component 210 and the second supporting component 220, the mutually vertical and grafting setting of first supporting component 210 and the second supporting component 220, also comprise fixed panel 230, fixed panel 230 is provided with some spliced eyes 231, first supporting component 210 and the second supporting component 220 are provided with the grafting projection 201 coordinated with spliced eye 231, fixed panel 230, first supporting component 210 and the second supporting component 220 form the mounting groove 300 that power supply source is installed, with reference to shown in Fig. 5, fixed panel 230 is provided with some braces, and brace splices and is fixed on different supporting components.
First supporting component 210 is provided with two piece of first supporting bracket 211 be arranged in parallel, second supporting component 220 is provided with two pieces of second supporting bracket 221, first supporting bracket 211, second supporting brackets 221 be arranged in parallel around forming the standing groove 230 placed for blower fan 120; Standing groove 230 is communicated with setting with mounting groove 300, and standing groove 230 and mounting groove 300 are separated by a heat-dissipation spacer, dispels the heat mechanically to be provided with some through holes, for ensureing the connectedness of two grooves.
First supporting bracket 211 and the second supporting bracket 221 are provided with some louvres 202, louvre 202 spaced set, ensure that stability and the radiating efficiency of structure.
With reference to shown in Fig. 7, between two piece of first supporting bracket 211, be fixed with some first brace summers 212.Some second brace summers 222 are fixed with between two piece of second supporting bracket 221.
First brace summer 212 is provided with some air holes 203.Wind space is apart from arranging.
With reference to shown in Fig. 6, also include the radio station module 440IMU410 of separate setting, main control module 440IMU420, receiver module 440IMU430 and IMU module 440IMU, radio station module 440IMU410, main control module 440IMU420, receiver module 440IMU430 and IMU module 440IMU are all arranged at the end face of fixed panel 230;
With reference to described in Fig. 9, the first supporting bracket 211 and the second supporting bracket 221 such as under type fix clamping, can ensure its stability of installing like this.
The above is only preferred implementation of the present utility model, protection range of the present utility model be not only confined to above-described embodiment, and all technical schemes belonged under the utility model thinking all belong to protection range of the present utility model.It should be pointed out that for those skilled in the art, do not departing from the some improvements and modifications under the utility model principle prerequisite, these improvements and modifications also should be considered as protection range of the present utility model.
Claims (7)
1. the middle control shell structure of a four-axle aircraft, comprise middle control housing, described middle control enclosure interior is provided with power supply, it is characterized in that: the bottom of described middle control housing is provided with thermovent, middle control enclosure interior is provided with blower fan, and described fan outlet is arranged towards thermovent, and described middle control enclosure interior is fixed with support, described support comprises the first supporting component and the second supporting component, the mutually vertical and grafting setting of described first supporting component and the second supporting component;
Also comprise fixed panel, described fixed panel is provided with some spliced eyes, it is protruding that described first supporting component and the second supporting component are provided with the grafting coordinated with spliced eye, and described fixed panel, the first supporting component and the second supporting component form the mounting groove that power supply source is installed.
2. the middle control shell structure of a kind of four-axle aircraft as claimed in claim 1, it is characterized in that: described first supporting component is provided with two piece of first supporting bracket be arranged in parallel, described second supporting component is provided with two pieces of second supporting brackets be arranged in parallel, and described first supporting bracket, the second supporting bracket are around forming the standing groove placed for blower fan; Described standing groove is communicated with setting with described mounting groove.
3. the middle control shell structure of a kind of four-axle aircraft as claimed in claim 2, is characterized in that: described first supporting bracket and the second supporting bracket are provided with some louvres.
4. the middle control shell structure of a kind of four-axle aircraft as claimed in claim 3, is characterized in that: be fixed with some first brace summers between two pieces of described first supporting brackets.
5. the middle control shell structure of a kind of four-axle aircraft as claimed in claim 3, is characterized in that: be fixed with some second brace summers between two pieces of described second supporting brackets.
6. the middle control shell structure of a kind of four-axle aircraft as claimed in claim 4, is characterized in that: described first brace summer is provided with some air holes.
7. in a kind of four-axle aircraft as described in claim 1 or 2 or 3 or 4 or 5 or 6, control shell structure, it is characterized in that: also include the radio station module of separate setting, main control module, receiver module and IMU module, described radio station module, main control module, receiver module and IMU module are all arranged at the end face of fixed panel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520876851.2U CN205179563U (en) | 2015-11-05 | 2015-11-05 | Four shaft air vehicle's well accuse shell structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520876851.2U CN205179563U (en) | 2015-11-05 | 2015-11-05 | Four shaft air vehicle's well accuse shell structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205179563U true CN205179563U (en) | 2016-04-20 |
Family
ID=55743488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520876851.2U Expired - Fee Related CN205179563U (en) | 2015-11-05 | 2015-11-05 | Four shaft air vehicle's well accuse shell structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205179563U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107113997A (en) * | 2016-09-26 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Cooling mechanism and the unmanned vehicle with the cooling mechanism |
-
2015
- 2015-11-05 CN CN201520876851.2U patent/CN205179563U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107113997A (en) * | 2016-09-26 | 2017-08-29 | 深圳市大疆创新科技有限公司 | Cooling mechanism and the unmanned vehicle with the cooling mechanism |
| WO2018053872A1 (en) * | 2016-09-26 | 2018-03-29 | 深圳市大疆创新科技有限公司 | Heat dissipation mechanism, and unmanned aerial vehicle provided with heat dissipation mechanism |
| CN107113997B (en) * | 2016-09-26 | 2019-07-16 | 深圳市大疆创新科技有限公司 | Cooling mechanism and unmanned vehicle with the cooling mechanism |
| CN110139544A (en) * | 2016-09-26 | 2019-08-16 | 深圳市大疆创新科技有限公司 | Cooling mechanism and unmanned vehicle with the cooling mechanism |
| CN110139544B (en) * | 2016-09-26 | 2020-07-07 | 深圳市大疆创新科技有限公司 | Heat dissipation mechanism and have this heat dissipation mechanism's unmanned vehicles |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160420 |