CN207060390U - Unmanned plane and unmanned plane frame - Google Patents
Unmanned plane and unmanned plane frame Download PDFInfo
- Publication number
- CN207060390U CN207060390U CN201720954647.7U CN201720954647U CN207060390U CN 207060390 U CN207060390 U CN 207060390U CN 201720954647 U CN201720954647 U CN 201720954647U CN 207060390 U CN207060390 U CN 207060390U
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- unmanned plane
- electronic installation
- top plate
- bottom plate
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Abstract
The utility model provides a kind of unmanned plane, the bottom plate and electronic installation being be arranged in parallel including top plate, with the top plate, the top plate is fixedly mounted with the bottom plate to form installing space, the electronic installation is installed in the installing space, the top plate opens up the bit-avoiding slot for connecting the installing space, electronic installation described in the bit-avoiding slot face.Unmanned plane of the present utility model, directly electronic installation can be safeguarded by the bit-avoiding slot of top plate, it is very convenient.
Description
Technical field
The utility model belongs to unmanned plane during flying device technical field, more particularly to a kind of unmanned plane and unmanned plane frame.
Background technology
Unmanned plane refers to the not manned vehicle being controlled using wireless remote control device and electronic installation, such as nobody is straight
The machine of liter, unmanned fixed-wing aircraft, unmanned gyroplane etc..In recent years, with Development of UAV, because it has maneuverability, reaction
Quickly, unmanned flight, operation requires low advantage, and unmanned plane has been widely used in agricultural plant protection, photography of taking photo by plane, electric power patrol
Inspection, environmental monitoring, forest fire protection and disaster inspection, effectively overcome the deficiency that manned aircraft carries out aerial work.
The airframe structure design of traditional unmanned plane is unreasonable, and the electronic installation on unmanned plane is not easy to tie up on fuselage
Shield.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane and unmanned plane for being easy to safeguard the electronic installation on fuselage
Frame.
The utility model is achieved in that a kind of unmanned plane, including top plate, the bottom plate that is be arranged in parallel with the top plate and
Electronic installation, the top plate are fixedly mounted to form installing space with the bottom plate, and the electronic installation is installed on the installation
In space, the top plate opens up the bit-avoiding slot for connecting the installing space, electronic installation described in the bit-avoiding slot face.
It should be understood that the bit-avoiding slot runs through the top plate close to one end of the electronic installation.
It should be understood that the electronic installation is fixed on the bottom plate, the bottom plate, which is provided with, to be used to house the electronics
The stopper slot of device is spacing to be carried out to the electronic installation.
It should be understood that the electronic installation is to control electric control gear for flying.
It should be understood that the unmanned plane also includes being covered on based shell on the bottom plate, the based shell with it is described
Bottom plate is collectively forming to accommodate the host cavity of the electronic installation, and the based shell includes the base enclosure being fixedly connected with the bottom plate
Body and the top cover being detachably connected with the base enclosure body, one is opened up on the base enclosure body and is communicated simultaneously with the host cavity
The mounting hole of the host cavity is passed in and out for the electronic installation, the top cover is on the mounting hole.
It should be understood that the base enclosure body includes being used for the upper shell being detachably connected with the top cover, the upper casing
Body is offered with the structure matching of the top cover and for accommodating the mating groove of the top cover, is installed with the mating groove
First magnetic part, the second magnetic part for being connected with the first magnetic part magnetic is correspondingly arranged on the top cover.
It should be understood that the housing unit also includes being used for the installation housing for connecting the top plate and the based shell,
The installation housing includes and the top plate is fixedly connected two be connected shell and be arranged at two and described connect between shells and be used for
The tie-beam of the two connection shells is connected, the two connection shells are fixedly connected with the upper shell.
It should be understood that the unmanned plane also includes the installing frame for storing, the installing frame is set in frame-type and institute
The one end for stating installing frame is inserted in the installing space, and the installing frame is fixedly connected with the bottom plate.
A kind of unmanned plane frame, including the bottom plate that top plate and the top plate be arranged in parallel, the top plate are consolidated with the bottom plate
Dingan County is filled with the installing space to be formed for mounting electronic device, and the top plate opens up the bit-avoiding slot for connecting the installing space,
Electronic installation described in the bit-avoiding slot face.
It should be understood that the bit-avoiding slot runs through the top plate close to one end of the electronic installation.
The utility model has the technical effect that relative to prior art：Unmanned plane and unmanned plane frame of the present utility model,
Directly electronic installation can be safeguarded by the bit-avoiding slot of top plate, it is very convenient.
Brief description of the drawings
In order to illustrate more clearly of the technical scheme of the utility model embodiment, below will to the utility model embodiment or
The required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings described below is only
Some embodiments of the utility model, for those of ordinary skill in the art, on the premise of not paying creative work,
Other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the stereogram for the unmanned plane that the utility model embodiment provides.
Fig. 2 is the exploded view for the unmanned plane that the utility model embodiment provides.
Fig. 3 is the part-structure stereogram for the unmanned plane that the utility model embodiment provides.
Fig. 4 is fuselage, horn, undercarriage, installation housing and the Power Component that the utility model embodiment provides.
Fig. 5 is the solid that undercarriage, horn, the Power Component that the utility model embodiment provides close part airframe structure
Figure.
Fig. 6 is the stereogram for the housing unit that the utility model embodiment provides.
Fig. 7 is the stereogram for the connection shell that the utility model embodiment provides.
Fig. 8 is the stereogram for the base enclosure body that the utility model embodiment provides.
Description of reference numerals：
Embodiment
Embodiment of the present utility model is described below in detail, the example of the embodiment is shown in the drawings, wherein from beginning
Same or similar element is represented to same or similar label eventually or there is the element of same or like function.Below by ginseng
The embodiment for examining accompanying drawing description is exemplary, it is intended to for explaining the utility model, and it is not intended that to the utility model
Limitation.
In order that the purpose of this utility model, technical scheme and advantage are more clearly understood, below in conjunction with accompanying drawing and implementation
Example, the utility model is further elaborated.
As depicted in figs. 1 and 2, the utility model embodiment provides a kind of unmanned plane and includes fuselage 100, consolidates with fuselage 100
Dingan County dress electronic installation 800, be fixedly connected with the fuselage 100 multiple horns 200, be fixedly connected with fuselage 100 two
Undercarriage 300, the housing unit 400 for being covered on fuselage 100, be installed on horn 200 the end of remote fuselage 100 power packages
Part 500, the liquid storage container 600 for being installed on fuselage 100 and being used for storage solutions, it is installed on fuselage 100 and for being power
The battery 700 that component 500 is powered.
Further, as shown in Figures 2 and 3, fuselage 100 includes fuselage body 110 and fixed with fuselage body 110 to connect
The installing frame 120 stored is connect and is used for, fuselage body 110 includes the bottom plate 113 and top plate 111 for be arrangeding in parallel and being fixedly connected,
Top plate 111 is collectively forming an installing space 114 for being used to accommodate electronic installation 800 with bottom plate 113, and electronic installation 800 is in installation
Is fixedly connected with bottom plate 113 in space 114, top plate 111 opens up a bit-avoiding slot 112 and communicated with installing space 114 to be filled with supplied for electronic
Put 800 to be put into installing space 114 or take out out of installing space 114, the face electronic installation 800 of bit-avoiding slot 112 is set；Installing frame
120 set in frame-type and are fixedly connected in the one end of installing frame 120 insertion installing space 114 and with bottom plate 113, installing frame
A dividing plate 123 is provided with 120, installing frame 120 has the first installation cavity 121 and the second installation cavity 122 for storing, dividing plate
123 are spaced apart the first installation cavity 121 and the second installation cavity 122, and battery 700 is installed in the first installation cavity 121, and liquid storage holds
Device 600 is installed in the second installation cavity 122, and the bottom of liquid storage container 600 is fixedly connected with the top of bottom plate 113.
Further, multiple horns 200 are distributed in around fuselage 100 that (unmanned plane in the present embodiment is with four horns
200 illustrate, but are not limited thereto), and horn 200 is fixedly connected with fuselage 100, specifically, as shown in Figure 2 and Figure 5,
The one end of horn 200 is stretched into installing space 114 and is fixedly connected with bottom plate 113, and the sidepiece of horn 200 and installing frame 120
Side wall is fixedly connected, and top plate 111 covers the top connect with horn 200.
Further, four Power Components 500, which correspond, is installed on four ends of the horn 200 away from fuselage 100, and four
Individual Power Component 500 electrically connects the Power Component 500 for providing flying power with battery 700, and four Power Components 500 are equal
It is connected to control the flight stake situation of unmanned plane with the signal of electronic installation 800.
Certainly, in the utility model other embodiment, unmanned plane is right at least provided with a horn 200, Power Component 500
Should be at least provided with one.
Further, as shown in Fig. 2 each Power Component 500 includes propeller 510 and driven with propeller 510 to connect
Connecing and drive propeller 510 to rotate to provide the driver 520 of flying power, driver 520 is fixedly installed on horn 200,
Battery 700 is electrically connected with driver 520 and provides electric energy for driver 520, and electronic installation 800 is connected with the signal of driver 520,
Electronic installation 800 is by controlling driver 520 to control the flight condition of unmanned plane.
Further, two undercarriages 300 are both secured to the lower section of fuselage 100 to ensure the stabilization of unmanned plane takeoff and landing
Property, specifically, as shown in figure 1, undercarriage 300 include be used for contacted with supporting surface and support fuselage 100 supporting part 310 and
Respectively at the first connecting portion 320 and second connecting portion 330 that the both ends of supporting part 310 and supporting part 310 are wholely set, the first connection
Portion 320 is fixedly connected with the one end of fuselage 100, and second connecting portion 330 is fixedly connected with the other end of fuselage 100.Specifically
Ground, first connecting portion 320 are fixedly connected with the side wall of installing frame 120, and the bottom of second connecting portion 330 and bottom plate 113, which is fixed, to be connected
Connect, unmanned plane is positioned on supporting surface by two undercarriages 300, by the bottom surface of fuselage 100 close to supporting surface, two undercarriages 300 it
Between apart from flaring set, supporting surface and two undercarriages 300 collectively form triangular support configurations more stably to support fuselage
100。
Further, as shown in fig. 6, housing unit 400 includes the installation housing 410 and based shell 420 being fixedly connected, such as
Shown in Fig. 4, installation housing 410 includes symmetrically arranged two connection shells 411 and is arranged between two connection shells 411 and is connected with two
The tie-beam 414 that shell 411 is fixedly connected, two connection shells 411 are set in arcuate, as shown in fig. 7, the connection bottom margin of shell 411
Extend and formed the connecting plate 412 to be fitted with the plate face of top plate 111 to side, the connection top edge of shell 411 extends simultaneously to side
Fixed part 413 is formed, installation housing 410 is fixedly connected by connecting plate 412 with top plate 111, and installation housing 410 passes through fixed part
413 are fixedly connected with based shell 420, and the end that two connection shells 411 tilt extended and remote top plate 111 is close to each other,
Two connection shells 411 are provided with antenna mounting groove 414, and antenna mounting groove 414, which also tilts, to be extended, antenna mounting groove 414
Inclined plane and the plate face of top plate 111 are set in angle, and the angular range of the angle is more than or equal to 30 ° and is less than or equal to
70 °, for strengthening the intensity of wireless signal to improve the stability of the transmission of wireless signal, reliability.
Further, as shown in Fig. 2 based shell 420 includes base enclosure body 421 and with detachably connecting on base enclosure body 421
The top cover 429 connect, as shown in figure 8, base enclosure body 421 is included in extended upper shell 425 and procapsid 422, and on
Housing 425 is wholely set with procapsid 422, upper shell 425 and the bearing of trend of bearing of trend and procapsid 422 substantially hang down
Directly.Specifically, the bearing of trend of upper shell 425 is roughly parallel to the plate face of top plate 111, and the bearing of trend of procapsid 422 is substantially
Perpendicular to the plate face of top plate 111.
Based shell 420 is fixedly connected and is covered on top plate 111 and bottom plate 113 with top plate 111 by installing housing 410,
Based shell 420 is collectively forming with bottom plate 113 to accommodate the host cavity of electronic installation 800 (the non-label of figure), specifically, upper shell
425th, procapsid 422 and top cover 429 surround host cavity jointly with bottom plate 113, and the crown center position of upper shell 425 opens up one and matched somebody with somebody
Close groove 427 with accommodate top cover 429 and it is multiple be fixedly connected installation housing 410 screw 427a, screw 427a, which is arranged at, to be matched somebody with somebody
The bottom of groove 427 is closed, the fixed part 413 of shell 411 is connected and is locked with the screw 427a of upper shell 425 by determining part (not shown)
Fastening, the structure of mating groove 427 is set with the structure matching of top cover 429, specifically, shape and the top cover 429 of mating groove 427
Form fit set, the depth of mating groove 427 and the thickness matching of top cover 429 are set, and top cover 429 can with base enclosure body 421
Dismantling connection also opens up one at mating groove 427, on upper shell 425 and the simultaneously disengaging of electronic devices 800 collecting is communicated with host cavity
The mounting hole 426 of chamber, specifically, in the bottom of mating groove 427 open up one installed with electronic devices 800 when the mounting hole that passes through
426, the aperture of mounting hole 426 is less than the size of the bottom land of mating groove 427, and mounting hole 426 runs through the bottom land of mating groove 427, peace
Dress hole 426 connects setting, and mounting hole 426 and bit-avoiding slot 112 and electronics with host cavity, bit-avoiding slot 112 and installing space 114
Device 800 aligns setting, and screw 427a is arranged at the peripheral position of mounting hole 426.
Further, in being installed with multiple first magnetic parts (figure non-label), and first in the bottom land of mating groove 427
Magnetic part is arranged at the peripheral position of mounting hole 427, and the first magnetic part is magnet, and top cover 429 is installed with and the first magnetic
Part corresponds setting and the second magnetic part (the non-label of figure) made of magnetic material, and the second magnetic part is ferrimagnet system
Into, the pole of the second magnetic part and the first magnetic part polarity to anti-, when top cover 429 is installed, multiple second magnetic parts of top cover 429
Correspond and install with multiple first magnetic parts in mating groove 427, the second magnetic part is attracting by magnetic force with the first magnetic part
And be that top cover 429 is fixedly installed in mating groove 427, and be covered on mounting hole 426.
When electronic installation 800 is installed, electronic installation 800 is put into host cavity by mounting hole 426, after bit-avoiding slot 112
It is installed on bottom plate 113, and electronic installation 800 is installed in installing space 114；When electronic installation 800 is dismantled, make the second magnetic
Part separates with the first magnetic part and takes out top cover 429 out of mating groove 427, and being taken on bottom plate 113 electronic installation 800 and passes through
Bit-avoiding slot 112, then electronic installation 800 is taken out at mounting hole 426, the based shell 420 of the utility model embodiment can improve
The convenience of electronic installation dismounting, it is necessary to which complete machine is dismantled when avoiding replacing electronic installation 800, improve unmanned plane replacing
The efficiency of electronic installation 800, and reduce the cost that unmanned plane changes the efficiency of electronic installation 800.
Further, the both sides of procapsid 422 are respectively provided with one and are communicated with host cavity and lead to the ventilation culvert of electronic installation 800
Road 423, during unmanned plane during flying, because the operation of electronic installation 800 can produce substantial amounts of heat, there is two ventilations culvert in extraneous cold space
Road 423 enters in host cavity to be cooled with electronic devices 800.
The unmanned plane of the utility model embodiment can improve electronic installation 800 dismounting convenience, when need change or
When overhauling electronic installation 800, top cover 429 is taken out out of mating groove 427, then electronic installation 800 is removed simultaneously from bottom plate 113
Taken out by mounting hole 426, when electronic installation 800 reinstalls bottom plate 113, electronic installation 800 is put into host cavity simultaneously by mounting hole 426
It is positioned on bottom plate 113 and is fixedly mounted, compared with prior art, avoids when changing electronic installation 800, it is necessary to which complete machine is torn open
Unload, improve unmanned plane change electronic installation 800 efficiency, and reduce unmanned plane change electronic installation 800 efficiency into
This.
When top cover 429 is installed, the second magnetic part can the magnetic part of automatic absorbing second close to the first magnetic part, the first magnetic part
And adsorb top cover 429, only need to adjust top cover 429 makes top cover 429 and mating groove 427 right in the position of mating groove 427 and angle
Positive installation, the efficiency of installation is greatly improved, when top cover 429 is dismantled, the first magnetic part is separated and is moved with the second magnetic part
Top cover 429 is opened, the dismounting of top cover 429 is very convenient, and need not collect the connector for top cover 429 and base enclosure body 421,
Compared with conventional art, the top cover 429 of the utility model embodiment is high with the disassembly efficiency of base enclosure body 421, top cover 429 and base
Shell body 421 is connected by the second magnetic part with the magnetic force of the first magnetic part, can realize repeated disassembled and assembled, and convenient disassembly.
When due to failure air crash occurs for unmanned plane, top plate 111 and bottom plate 113 can fill to the electronics in installing space 114
Put 800 to play a protective role, avoid loading directly impact electronic installation 800 and cause electronic installation 800 to damage, with reduce maintenance into
This.
Installing frame 120 inserts installing space 114 and is fixedly connected with bottom plate 113, can optimize the installing space of unmanned plane
114, and the first installation cavity 121 of the setting of installing frame 120 and the second installation cavity 122 can at least install two kinds of different size objects,
Second installation cavity 122 is arranged between the first installation cavity 121 and electronic installation 800, and further, battery 700 is installed on first
Installation cavity 121, liquid storage container 600 are installed in the second installation cavity 122, and battery 700 and electronic installation 800 produce at work
Heat, after heat caused by the liquid absorption battery 700 and electronic installation 800 in liquid storage container 600, during fluid removal, take away heat
Amount, it can play a part of cooling for battery 700 and electronic installation 800, to extend the service life of unmanned plane.
The utility model also provides a kind of unmanned plane frame, including the bottom that top plate 111 and the top plate 111 be arranged in parallel
Plate 113, the top plate 111 are fixedly mounted to form the installing space 114 for mounting electronic device 800 with the bottom plate 113,
The top plate 111 opens up the bit-avoiding slot 112 for connecting the installing space 114, electronic installation described in the face of bit-avoiding slot 112
800。
The unmanned plane frame of the utility model embodiment, can be directly to electronic installation by the bit-avoiding slot 112 of top plate 111
800 are safeguarded, very convenient.
Further, the bit-avoiding slot 800 runs through the top plate 111 close to one end of the electronic installation 800.
Preferred embodiment of the present utility model is the foregoing is only, it is all at this not to limit the utility model
All any modification, equivalent and improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (10)
- A kind of 1. unmanned plane, it is characterised in that the bottom plate and electronic installation being be arranged in parallel including top plate, with the top plate, it is described Top plate is fixedly mounted to form installing space with the bottom plate, and the electronic installation is installed in the installing space, the top Plate opens up the bit-avoiding slot for connecting the installing space, electronic installation described in the bit-avoiding slot face.
- 2. unmanned plane as claimed in claim 1, it is characterised in that the bit-avoiding slot fills through the top plate close to the electronics The one end put.
- 3. unmanned plane as claimed in claim 1 or 2, it is characterised in that the electronic installation is fixed on the bottom plate, the bottom It is spacing to be carried out to the electronic installation that plate is provided with the stopper slot for being used to house the electronic installation.
- 4. unmanned plane as claimed in claim 1 or 2, it is characterised in that the electronic installation is to control automatically controlled dress for flying Put.
- 5. unmanned plane as claimed in claim 1, it is characterised in that the unmanned plane also includes the base being covered on the bottom plate Housing, the based shell and the bottom plate are collectively forming to accommodate the host cavity of the electronic installation, the based shell include with Base enclosure body that the bottom plate is fixedly connected and the top cover being detachably connected with the base enclosure body, open on the base enclosure body If a mounting hole for being communicated with the host cavity and supplying the electronic installation to pass in and out the host cavity, the top cover are located at the peace Fill on hole.
- 6. unmanned plane as claimed in claim 5, it is characterised in that the base enclosure body is included for detachable with the top cover The upper shell of connection, the upper shell are offered with the structure matching of the top cover and for accommodating the mating groove of the top cover, The first magnetic part is installed with the mating groove, is correspondingly arranged on and is used for and the first magnetic part magnetic on the top cover Second magnetic part of connection.
- 7. unmanned plane as claimed in claim 6, it is characterised in that the housing unit also include be used for connect the top plate with The installation housing of the based shell, the installation housing include and the top plate is fixedly connected two is connected shell and is arranged at two Between the connection shell and for connecting two tie-beams for connecting shells, the two connection shells are fixed with the upper shell to be connected Connect.
- 8. the unmanned plane as described in any one of claim 1 to 2, it is characterised in that the unmanned plane is also included for storage Installing frame, the installing frame is set in frame-type and the one end of the installing frame is inserted in the installing space, the installing frame Be fixedly connected with the bottom plate.
- A kind of 9. unmanned plane frame, it is characterised in that the bottom plate being be arranged in parallel including top plate, with the top plate, the top plate with The bottom plate is fixedly mounted to form the installing space for mounting electronic device, and the top plate opens up the connection installing space Bit-avoiding slot, electronic installation described in the bit-avoiding slot face.
- 10. unmanned plane frame as claimed in claim 9, it is characterised in that the bit-avoiding slot is through the top plate close to described One end of electronic installation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720954647.7U CN207060390U (en) | 2017-08-01 | 2017-08-01 | Unmanned plane and unmanned plane frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720954647.7U CN207060390U (en) | 2017-08-01 | 2017-08-01 | Unmanned plane and unmanned plane frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207060390U true CN207060390U (en) | 2018-03-02 |
Family
ID=61519145
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720954647.7U Active CN207060390U (en) | 2017-08-01 | 2017-08-01 | Unmanned plane and unmanned plane frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207060390U (en) |
-
2017
- 2017-08-01 CN CN201720954647.7U patent/CN207060390U/en active Active
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 510000 Block C, 115 Gaopu Road, Tianhe District, Guangzhou City, Guangdong Province Patentee after: Guangzhou Jifei Technology Co.,Ltd. Address before: 510000, Guangdong, Guangzhou, Gaotang Tianhe District Software Park Road, No. 1, 3A01 Patentee before: Guangzhou Xaircraft Technology Co.,Ltd. |
|
| CP03 | Change of name, title or address |