CN204802091U - Filtration and portable object - Google Patents
Filtration and portable object Download PDFInfo
- Publication number
- CN204802091U CN204802091U CN201520366689.XU CN201520366689U CN204802091U CN 204802091 U CN204802091 U CN 204802091U CN 201520366689 U CN201520366689 U CN 201520366689U CN 204802091 U CN204802091 U CN 204802091U
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- Prior art keywords
- filtration
- air
- filtration members
- fuselage
- members
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Abstract
The utility model provides a filtration and portable object, this portable object includes the fuselage. The air inlet has been seted up to this fuselage, and this portable object includes the filtration, and this filtration is acceptd at this air inlet, and the air gets into this fuselage via this filtration and this air inlet, and this air current is when this filtration, and this filtration cleans this air. This filtration will get into filterings such as granule and steam in the air of this fuselage, guarantee the cleanness that gets into the air of this fuselage, and then guarantee the inside cleanness of this fuselage, reduce electron device's fault rate, improve life.
Description
Technical field
The utility model relates to a kind of loose impediment with filtration.
Background technology
At present, the electronics package of most unmanned vehicle is all out exposed, a little unmanned vehicle has the shell for accommodating electronics package, but this shell is simple shell structure up and down and does not have unified admission port, more not to the filtration that the air that will enter this admission port filters, this just causes the heat radiation of unmanned vehicle bad, and unmanned vehicle cleaning inside can not be guaranteed, and then causes that this electronics package fault rate is high, service life is low.
Utility model content
In view of this, be necessary to provide a kind of dispel the heat better and filtration and the loose impediment of cleaning inside can be ensured.
A kind of filtration, it comprises:
First filtration members, for filtering solids;
Second filtration members, for filter liquide; And
3rd filtration members, for filtering steam and solid, the size of the solid that this first filtration members is filtered is different from the size of the solid that the 3rd filtration members is filtered.
Further, this second filtration members and the 3rd filtration members are arranged in this first filtration members.
Further, this second filtration members comprises by the screen plate having the breathing material of adsorbability effect to make liquid;
Or this second filtration members comprises the screen plate be made up of air-impermeable material.
Further, this first filtration members comprises meshed first filter screen of tool.
Further, this first filtration members offers the first groove, and this first filter screen covers this first groove.
Further, this first filtration members also offers groove, and this groove is connected with this first groove, and it is for accommodating this first filter screen and this second filtration members.
Further, the dust in the 3rd filtration members filtered air.
Further, the 3rd filtration members comprises the second filter screen be made up of permeability to air sorbing material.
Further, the 3rd filtration members offers the second groove, and this second filter screen covers this second groove.
Further, this filtration also comprises fan, and this fan is for accelerating the air-flow velocity through this filtration.
Further, this fan comprises following at least one: tube axial fan, radial fan.
Further, this filtration also comprises temperature regulating part, and this temperature regulating part is used for the air after filtering this filtration, and/or the air before the filtration of this filtration carries out temperature adjustment.
Further, this temperature regulating part comprises following at least one: heater element, cooling device.
A kind of loose impediment, it comprises fuselage and filtration as above, this fuselage offers admission port, this filtration is arranged on this admission port, air enters this fuselage via this filtration and this admission port, when this air flows through this filtration, this filtration cleans this air.
Further, this loose impediment is unmanned vehicle.
Further, also comprise the horn be communicated with this fuselage, this air flows in this horn via after this fuselage.
Further, also comprise the Power Component be arranged on horn, the inner space of this horn and this Power Component, the air-flow in this horn is dispelled the heat to this Power Component.
Adopt filtration of the present utility model and loose impediment, this fuselage offers admission port, contain filtration in this admission port, air unification enters this fuselage after this filtration filters, and is conducive to the heat radiation of the electronics package be housed in this fuselage; This filtration will enter the filterings such as particle in the air of this fuselage and steam, ensure that the clean of the air entering this fuselage, and then ensure that the clean of this unmanned vehicle inside, reduce the fault rate of electronics package, improve service life.
Accompanying drawing explanation
Fig. 1 is the sectional perspective schematic diagram of the unmanned vehicle of the utility model first embodiment.
Fig. 2 is another sectional perspective schematic diagram of the unmanned vehicle in Fig. 1.
Fig. 3 is the decomposing schematic representation of the unmanned vehicle in Fig. 2.
Fig. 4 is another decomposing schematic representation of the unmanned vehicle in Fig. 3.
Fig. 5 is the structural representation of the 3rd filtration members of unmanned vehicle in Fig. 3.
Fig. 6 is the sectional perspective schematic diagram of the unmanned vehicle of the utility model second embodiment.
Fig. 7 is the sectional perspective schematic diagram of the unmanned vehicle of the utility model the 3rd embodiment.
Main element nomenclature
| Unmanned vehicle | 100，200，300 |
| Fuselage | 10 |
| Host cavity | 11 |
| Outside face | 12 |
| Admission port | 13 |
| Medial surface | 131 |
| First draw-in groove | 14 |
| Draw-in groove | 15 |
| Mounting hole | 16 |
| Filtration | 20 |
| Baffle plate | 17 |
| Air inlet duct | 171 |
| First filtration members | 21 |
| First side | 211 |
| First groove | 2111 |
| Second side | 212 |
| Groove | 2121 |
| Contiguous block | 2122 |
| Tapped bore | 2123 |
| End face | 213 |
| First projection | 214 |
| Second draw-in groove | 2141 |
| First boss | 215 |
| First filter screen | 216 |
| 3rd side | 217 |
| Rotating shaft | 218 |
| Second filtration members | 22 |
| Through hole | 221 |
| 3rd filtration members | 23 |
| First surface | 231 |
| Second surface | 232 |
| Second groove | 233 |
| Second filter screen | 234 |
| 3rd surface | 235 |
| Second projection | 236 |
| Second boss | 237 |
| Horn | 30 |
| Foot rest | 40 |
| Fan | 201 |
| Temperature regulating part | 301 |
Following detailed description of the invention will further illustrate the utility model in conjunction with above-mentioned accompanying drawing.
Detailed description of the invention
Below in conjunction with accompanying drawing, embodiments more of the present utility model are elaborated.When not conflicting, the feature in following embodiment and embodiment can combine mutually.
Refer to Fig. 1, the unmanned vehicle 100 of the utility model first embodiment, it comprises fuselage 10, filtration 20, horn 30 and foot rest 40.
Refer to Fig. 2 to Fig. 5, this fuselage 10 offers host cavity 11, and this host cavity 11 is for accommodating the electronics package (not shown) of this unmanned vehicle 100.This fuselage 10 also includes outside face 12.In present embodiment, the outside face 12 of this fuselage 10 offers the admission port 13 be connected with this host cavity 11.This admission port 13 allows outside air to enter in the host cavity 11 of this fuselage 10, and contains this filtration 20 in this admission port 13.This fuselage 10 comprises the medial surface 131 surrounding this admission port 13, and this medial surface 131 connects this outside face 12.Outside air enters this fuselage 10 by this admission port 13, to dispel the heat to the control system be housed in this host cavity 11 and other parts.
This fuselage 10 also offers the first draw-in groove 14.This first draw-in groove 14 runs through this outside face 12 and this medial surface 131, and it is connected with this admission port 13.In present embodiment, the quantity of this first draw-in groove 14 is two, and two these the first draw-in groove 14 intervals are arranged.Be appreciated that in other embodiments, the quantity of this first draw-in groove 14 can increase according to actual needs or reduce.This fuselage 10 offers draw-in groove 15.In present embodiment, the quantity of this draw-in groove 15 is two, and two these draw-in grooves 15 lay respectively at the both sides of this admission port 13, and separately, the center shaft of two these draw-in grooves 15 is parallel to each other; Be appreciated that in other embodiments, the quantity of this draw-in groove 15 can increase according to actual needs or reduce.
Baffle plate 17 is provided with, for keeping off this filtration 20 in this admission port 13.This baffle plate 17 offers air inlet duct 171, and this air inlet duct 171 is connected with this host cavity 11, and outside air enters this host cavity 11 through this air inlet duct 171.
This fuselage 10 also offers mounting hole 16, and this mounting hole 16 is for passing for this horn 30.In present embodiment, the quantity of this mounting hole 16 is four, and four these mounting hole 16 intervals are arranged; Be appreciated that in other embodiments, according to the difference of the quantity of this horn 30, the quantity of this mounting hole 16 can suitably increase or reduce.
This filtration 20 will enter particle and steam etc. in the air of this fuselage 10 from this admission port 13 for filtering, it comprises the first filtration members 21, second filtration members 22 and the 3rd filtration members 23.This first filtration members 21 is for filtering solid, and such as, the first filtration members 21 will enter particle larger in the air of this fuselage 10 from the admission port 13 of this fuselage 10 for filtering.The end face 213 that first filtration members 21 comprises the first side 211, the second side 212 be connected with this first side 211 and is connected with this second side 212.This first filtration members 21 offers the first groove 2111, and this first groove 2111 runs through this first side 211 and this second side 212.In present embodiment, the quantity of this first groove 2111 is six, and six these the first grooves 2111 set in a row; Be appreciated that in other embodiments, the quantity of this first groove 2111 can increase as required or reduce.
In present embodiment, six these the first grooves 2111 are not interconnected, and are appreciated that in other embodiments, and six these the first grooves 2111 can be interconnected.This first filtration members 21 also offers groove 2121.This groove 2121 caves in this first side 211 from this second side 212, and it is for accommodating meshed first filter screen 216 of tool and this second filtration members 22.This first filter screen 216 covers six these the first grooves 2111, and it will enter particle larger in the air of this fuselage 10 from the admission port 13 of this fuselage 10 for filtering.The bottom surface of this groove 2121 is fixed with contiguous block 2122.This contiguous block 2122 is for connecting this second filtration members 22, and it offers tapped bore 2123.This tapped bore 2123 is for accommodating screw (not shown).In present embodiment, the quantity of this contiguous block 2122 is four, and wherein two sides being positioned at six these the first grooves 2111 of four these contiguous blocks 2122, two other this contiguous block 2122 is positioned at the opposite side of six these the first grooves 2111.This first side 211 is formed with the first projection 214, this first projection 214 is positioned at the side of this first groove 2111 away from this end face 213.In present embodiment, this first side 211 is curved surface away from the part of this end face 213.This first projection 214 offers the second draw-in groove 2141.In present embodiment, the quantity of this second draw-in groove 2141 is one, is appreciated that in other embodiments, and the quantity of this second draw-in groove 2141 can increase according to actual needs or reduce.
This end face 213 is fixed with the first boss 215 corresponding to this first draw-in groove 14, this first boss 215 is by being connected to this first filtration members 21 on this fuselage 10 with coordinating of this first draw-in groove 14.In present embodiment, the quantity of this first boss 215 is two, and two these the first boss 215 intervals are arranged; Be appreciated that in other embodiments, the quantity of this first boss 215 can increase according to actual needs or reduce.
This first filtration members 21 also comprises two relative the 3rd sides 217,217, two, the 3rd side and is all connected with this end face 213 and this second side 212.Each 3rd side 217 is fixed with rotating shaft 218, and one end of this rotating shaft 218 is contained in this draw-in groove 15 makes this first filtration members 21 be rotationally connected with this fuselage 10.In present embodiment, this rotating shaft 218 closes on the intersection of this first side 211 and this second side 212; Be appreciated that in other embodiments, the quantity of this rotating shaft 218 can increase according to actual needs or reduce.
This second filtration members 22 is substantially rectangular, and it is for filtering the liquid (as steam etc.) entered by this first filtration members 21 in the air of this second filtration members 22.Wherein in an embodiment, this second filtration members 22 has the gas permeable material of adsorbability effect to make by liquid such as steam, such as superfine fibre, bamboo charcoal material.This second filtration members 22 offers through hole 221.The quantity of this through hole 221 is two, and two these through holes 221 are arranged at the two ends of this second filtration members respectively.In present embodiment, the quantity of this second filtration members 22 is two; Be appreciated that in other embodiments, the quantity of this second filtration members 22 can increase according to actual needs or reduce.In present embodiment, this second filtration members 22 is screen plate; Be appreciated that in other embodiments, two these the second filtration members 22 can be replaced by a screen plate.Be appreciated that in other embodiments, this second filtration members 22 also can be made up of air-impermeable material, now the second filtration members 22 is for barrier air, air-flow is walked around the second filtration members 22 and is flowed, thus is blocked by the liquid in air-flow, and can not enter this admission port 13.
3rd filtration members 23 is for filtering steam and solid, and such as dust, solid suspended particle, for filtering the koniology and the steam that are entered the 3rd filtration members 23 by this second filtration members 22 further.3rd filtration members 23 comprises first surface 231 and the second surface 232 opposing with this first surface 231.3rd filtration members 23 offers the second groove 233, and this second groove 233 runs through this first surface 231 and this second surface 232.3rd filtration members 23 includes the second filter screen 234.This second filter screen 234 covers this second groove 233, and it enters koniology and the steam of the 3rd filtration members 23 through this second filtration members 22 for filtering.The mesh density of this second filter screen 234 is greater than the mesh density of this first filter screen 216.In present embodiment, the second filter screen 234 is made up of permeability to air sorbing material.The upperlimit of the solid that this first filtration members 21 is filtered is greater than the upperlimit of the solid that the 3rd filtration members 23 is filtered.
3rd filtration members 23 also comprises and this first surface 231 and this second surface 232 the 3rd surface 235 connected vertically.3rd surface 235 is fixed with the second projection 236, this second projection 236 is fixedly installed should the second boss 237 of the second draw-in groove 2141 on the surface towards the side of this first filtration members 21.This second boss 237 by with the cooperatively interacting of this second draw-in groove 2141, the 3rd filtration members 23 is connected in this first filtration members 21.In present embodiment, the quantity of this second boss 237 is one, is appreciated that in other embodiments, and the quantity of this second boss 237 can increase according to actual needs or reduce.
This horn 30 is for connecting and supporting the Power Component of this unmanned vehicle 100, and such as, screw propeller and for driving the motor (not shown) etc. of this propeller rotational, this Power Component is in the propulsive effort providing this unmanned vehicle 100 to fly.This horn 30 is communicated with this fuselage 10, and this air flows in this horn 30 via after this fuselage 10, so that give the electronic element radiating in this horn 30, such as, dispels the heat to electronic governor.
Further, this horn 30 and the inner space of this Power Component, make the air-flow in this horn 30 dispel the heat to this Power Component.Such as, this horn 30 is communicated with the motor cavity of Power Component away from one end of fuselage 10, so that give motor radiating.
This foot rest 40 is the supporting construction of this unmanned vehicle 100 when landing, and for preventing the fuselage 10 of this unmanned vehicle 100, is housed in spare part in this fuselage 10 and miscellaneous part because of landing and causes damage.In addition, other function blockes of all right this unmanned vehicle 100 of carry on this foot rest 40, such as, camera, pick up camera, rang sensor etc.
Refer to Fig. 1 and Fig. 2, during assembling, four through holes 221 that four screw (not shown) can be adopted to be each passed through two these the second filtration members 22 screw in four tapped bore 2123 of this first filtration members 21, and this second filtration members 22 is fixed in the groove 2121 of this first filtration members 21.Second boss 237 of the 3rd filtration members 23 cooperatively interacts with the second draw-in groove 2141 of this first filtration members 21 and the 3rd filtration members 23 is connected in this first filtration members 21.One end of two rotating shafts 218 of the first filtration members 21 of this filtration 20 is separately positioned in two draw-in grooves 15 of this fuselage 10, and this first filtration members 21 and this second filtration members 22 are formed with this fuselage 10 and be rotationally connected.Two the first boss 215 of this first filtration members 21 snap in two the first draw-in grooves 14 of this fuselage 10 respectively, make this first filtration members 21 be connected to this fuselage 10.3rd filtration members 23 is between this second filtration members 22 and this fuselage 10, this second filtration members 22 and this admission port 13, just to setting, through three filtration members 23 enter this host cavity 11 after walking around this second filtration members 22 after the air-flow entered from this admission port 13 is stopped by this second filtration members 22.This fuselage 10 is connected to this foot rest 40.Each this horn 30 is connected with this fuselage 10 through this corresponding mounting hole 16.
Be appreciated that this first filtration members 21 is not limited to present embodiment with the connection mode of this fuselage 10, in other embodiments, this first filtration members 21 can be connected on this fuselage 10 by other means, and such as screw connects.
During work, when air passes through the first filter screen 216 of this first filtration members 21, the larger particles in this first filter screen 216 absorbed air.Air through this first filter screen 216 enters this second filtration members 22, and this second filtration members 22 adsorbs the liquid in the air entered by this first filtration members 21.The air passing through this second filtration members 22 enters the second filter screen 234 of the 3rd filtration members 23, and this second filter screen 234 adsorbs the koniology and steam that enter through this second filtration members 22.The air passing through the 3rd filtration members 23 enters the host cavity 11 of this fuselage 10.
Refer to Fig. 6, the unmanned vehicle 200 of the utility model second embodiment is substantially identical with the unmanned vehicle 100 of the utility model first embodiment, and difference is that this unmanned vehicle 200 also comprises fan 201.This fan 201 is arranged on this fuselage 10, and it is positioned at the side of this filtration 20 away from this fuselage 10.This fan 201 will enter the air of this fuselage 10 from this filtration 20 for accelerating when this unmanned vehicle 200 works or flow out the flowing velocity of air of this fuselage 10, and then accelerate the heat radiation of the electronics package be housed in this fuselage 10.This fan comprises following at least one: tube axial fan, radial fan.
Refer to Fig. 7, the unmanned vehicle 300 of the utility model the 3rd embodiment is substantially identical with the unmanned vehicle 100 of the utility model first embodiment, and difference is that this unmanned vehicle 300 also comprises temperature regulating part 301.This temperature regulating part 301 is arranged on this fuselage 10, and it is positioned at the side of this filtration 20 away from this fuselage 10.When this unmanned vehicle 300 works in colder environment, this temperature regulating part 301 heats the air before the filtration of this filtration 20, and then guarantee is housed in the operating temperature of the electronics package in this fuselage 10 in allowed limits.When this unmanned vehicle 300 works in hotter environment, this temperature regulating part 301 freeze this filtration 20 filter before air, and then the operating temperature ensureing to be housed in electronics package in this fuselage 10 is in allowed limits.This temperature regulating part 301 comprises following at least one: heater element, cooling device.This heater element is that electricity heats device; This cooling device is electric refrigeration device.In present embodiment, this temperature regulating part 301 is semiconductor chilling plate; Be appreciated that in other embodiments, this temperature regulating part 301 can carry out for other the element that freezes and heat.
Be appreciated that in other embodiments, this temperature regulating part can be arranged at the side of this filtration 20 this fuselage 10 contiguous, heats the air after this filtration 20 filters or freezes.
Adopt filtration of the present utility model, unmanned vehicle and loose impediment, this fuselage offers admission port, contain filtration in this admission port, air unification enters this fuselage after this filtration filters, and is conducive to the heat radiation of the electronics package be housed in this fuselage; This filtration will enter the filterings such as particle in the air of this fuselage and steam, ensure that the clean of the air entering this fuselage, and then ensure that the clean of this unmanned vehicle inside, reduce the fault rate of electronics package, improve service life.
Be appreciated that described filtration 20 also can be applied in other suitable loose impediments, such as UAV, mobile battlebus, The Cloud Terrace, automobile, bicycle, Electrical Bicycle, ship are first-class.
In addition; those skilled in the art will be appreciated that; above embodiment is only used to illustrate that the utility model and being not used as limits the utility model; as long as within the utility model spirit, the appropriate change do above embodiment and change all drop within the claimed scope of the utility model.
Claims (17)
1. a filtration, is characterized in that: this filtration comprises:
First filtration members, for filtering solids;
Second filtration members, for filter liquide; And
3rd filtration members, for filtering steam and solid, the size of the solid that this first filtration members is filtered is different from the size of the solid that the 3rd filtration members is filtered.
2. filtration as claimed in claim 1, is characterized in that: this second filtration members and the 3rd filtration members are arranged in this first filtration members.
3. filtration as claimed in claim 1, is characterized in that: this second filtration members comprises by the screen plate having the breathing material of adsorbability effect to make liquid;
Or this second filtration members comprises the screen plate be made up of air-impermeable material.
4. filtration as claimed in claim 1, is characterized in that: this first filtration members comprises meshed first filter screen of tool.
5. filtration as claimed in claim 4, it is characterized in that: this first filtration members offers the first groove, this first filter screen covers this first groove.
6. filtration as claimed in claim 5, it is characterized in that: this first filtration members also offers groove, this groove is connected with this first groove, and it is for accommodating this first filter screen and this second filtration members.
7. filtration as claimed in claim 1, is characterized in that: the dust in the 3rd filtration members filtered air.
8. filtration as claimed in claim 1, is characterized in that: the 3rd filtration members comprises the second filter screen be made up of permeability to air sorbing material.
9. filtration as claimed in claim 8, it is characterized in that: the 3rd filtration members offers the second groove, this second filter screen covers this second groove.
10. filtration as claimed in claim 1, it is characterized in that: this filtration also comprises fan, this fan is for accelerating the air-flow velocity through this filtration.
11. filtrations as claimed in claim 10, is characterized in that: this fan comprises following at least one: tube axial fan, radial fan.
12. filtrations as claimed in claim 1, is characterized in that: this filtration also comprises temperature regulating part, and this temperature regulating part is used for the air after filtering this filtration, and/or the air before the filtration of this filtration carries out temperature adjustment.
13. filtrations as claimed in claim 12, is characterized in that: this temperature regulating part comprises following at least one: heater element, cooling device.
14. 1 kinds of loose impediments, it is characterized in that: this loose impediment comprises fuselage and the filtration described in any one of claim 1-13, this fuselage offers admission port, this filtration is arranged on this admission port, air enters this fuselage via this filtration and this admission port, when this air flows through this filtration, this filtration cleans this air.
15. loose impediments as claimed in claim 14, is characterized in that: this loose impediment is unmanned vehicle.
16. loose impediments as claimed in claim 14, it is characterized in that: also comprise the horn be communicated with this fuselage, this air flows in this horn via after this fuselage.
17. loose impediments as claimed in claim 16, is characterized in that: also comprise the Power Component be arranged on horn, the inner space of this horn and this Power Component, and the air-flow in this horn is dispelled the heat to this Power Component.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520366689.XU CN204802091U (en) | 2015-06-01 | 2015-06-01 | Filtration and portable object |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520366689.XU CN204802091U (en) | 2015-06-01 | 2015-06-01 | Filtration and portable object |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204802091U true CN204802091U (en) | 2015-11-25 |
Family
ID=54586951
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520366689.XU Expired - Fee Related CN204802091U (en) | 2015-06-01 | 2015-06-01 | Filtration and portable object |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204802091U (en) |
-
2015
- 2015-06-01 CN CN201520366689.XU patent/CN204802091U/en not_active Expired - Fee Related
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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: 20151125 |
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| CF01 | Termination of patent right due to non-payment of annual fee |