CN206265328U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
- Publication number
- CN206265328U CN206265328U CN201621262557.3U CN201621262557U CN206265328U CN 206265328 U CN206265328 U CN 206265328U CN 201621262557 U CN201621262557 U CN 201621262557U CN 206265328 U CN206265328 U CN 206265328U
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- unmanned plane
- accommodating cavity
- pcb board
- fuselage
- shock
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Abstract
The utility model discloses a kind of unmanned plane, including：Fuselage, is provided with accommodating cavity, and the accommodating cavity includes the first accommodating cavity and the second accommodating cavity, and the second accommodating cavity bottom is provided with cover plate；Battery, in first accommodating cavity；And light stream positioner, in second accommodating cavity, and fixation being covered by the cover plate, the light stream positioner includes parallel and spaced first pcb board and the second pcb board, and the shock-absorbing ball for connecting first pcb board and the second pcb board.First pcb board and the second pcb board of the utility model light stream positioner are fixedly connected by shock-absorbing ball, the two ends of the shock-absorbing ball are connected to the bottom wall of the accommodating cavity and the roof of cover plate respectively, so, the shock-absorbing ball can consolidate support the first pcb board and the second pcb board, the light stream positioner is obtained in that good damping effect, and it is simple, convenient to install the process of light stream positioner.
Description
Technical field
The utility model is related to unmanned plane field, particularly a kind of unmanned plane.
Background technology
Aerial photography aircraft is developed rapidly in recent years, wherein based on rotor wing unmanned aerial vehicle, rotor wing unmanned aerial vehicle
Operation principle is to drive propeller to provide lift by motor, is suspended in aerial realization and takes pictures.
In order to realize outdoor gps signal is bad and interior without gps signal in the environment of unmanned plane remain able to perceive ground
Face texture and relative altitude, realize accurate positioning hovering and smooth flight, and light stream positioner is provided with inside unmanned plane.So
And, light stream positioner is very sensitive to vibrations could to be realized being accurately positioned, it is necessary to avoid shaking, in the prior art in order to solve
The vibration problems of light stream positioner, by the mounting structure of light stream positioner design it is sufficiently complex, cause unmanned plane into
This is very high.
Utility model content
Main purpose of the present utility model is to propose a kind of unmanned plane, it is intended to simplify the installation of unmanned plane light stream positioner
Structure, reduces the production cost of unmanned plane on the premise of damping requirement is met.
To achieve the above object, the utility model proposes unmanned plane, including：Fuselage, is provided with accommodating cavity, the accommodating cavity
Including the first accommodating cavity and the second accommodating cavity, the second accommodating cavity bottom is provided with a cover plate；Battery, it is accommodating located at described first
In chamber；And light stream positioner, in second accommodating cavity, and fixation, the light stream positioning are covered by the cover plate
Device includes parallel and spaced first pcb board and the second pcb board, and connects first pcb board and the second pcb board
The first shock-absorbing ball.
Preferably, the accommodating cavity is separated into first accommodating cavity and the second accommodating cavity by the median septum.
Preferably, first shock-absorbing ball includes shock-absorbing ball body, two stopper sections and two elongated ends, stopper section described in two
The both sides up and down of the shock-absorbing ball body are respectively arranged on, are pacified for first pcb board with being formed between the shock-absorbing ball body
First screens of dress and the second screens installed for second pcb board, elongated end described in two connect stopper section described in respectively
And extend to away from the direction of the shock-absorbing ball body.
Preferably, elongated end described in wears first pcb board and is connected to the median septum；Another elongated end
Wear second pcb board and be connected to the cover plate.
Preferably, the unmanned plane also includes rotor power component, and the fuselage is hollow rectangular-shape, and the machine
The upper and lower surface of body is hollow out, and the rotor power component is arranged at the fuselage interior.
Preferably, the ratio that the fretwork area of the fuselage accounts for the fuselage gross area is 80%-93%.
Preferably, four of the fuselage all sides are respectively provided with least one obstacle avoidance apparatus.
Preferably, the unmanned plane also includes upper mounted plate and bottom plate, and fixed plate is consolidated with fuselage upper surface
Fixed connection, the bottom plate is fixedly connected with fuselage lower surface, and fixed plate and bottom plate are connected by a column,
The obstacle avoidance apparatus are located at fixed plate.
Preferably, the unmanned plane also includes a camera installing plate, and the camera installing plate is mounted by the second shock-absorbing ball
In fixed plate lower section, a filming apparatus are installed with the camera installing plate.
Preferably, the fuselage bottom is provided with holding tank, be provided with the holding tank can folding and unfolding leg, it is described can folding and unfolding branch
Pin includes the rotation section and the foot section for supporting the fuselage, the foot section and the receiving that are hinged with the holding tank
Groove clamping is being contained in the holding tank.
The utility model is provided with accommodating cavity in the fuselage of unmanned plane, by light stream positioner in the accommodating cavity
Afterwards, the accommodating cavity is covered by cover plate, so as to the light stream positioner is fixed in the accommodating cavity.Wherein, it is described
Light stream positioner includes the first pcb board and the second pcb board, and the first pcb board and the second pcb board are fixedly connected by shock-absorbing ball,
The two ends of the shock-absorbing ball are connected to the bottom wall of the accommodating cavity and the roof of cover plate respectively, in this way, the light stream positioner
Good damping effect is obtained in that, and it is more simple and convenient to install the process of light stream positioner.
Brief description of the drawings
In order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to the structure shown in these accompanying drawings.
Fig. 1 is the structural representation of the embodiment unmanned aerial vehicle body of the utility model one；
Fig. 2 is the dorsal view of the embodiment unmanned plane of the utility model one；
Fig. 3 is the sectional view in A-A directions in Fig. 2；
Fig. 4 is the dimensional structure diagram of light stream positioner in Fig. 3；
Fig. 5 is the dimensional structure diagram of shock-absorbing ball；
Fig. 6 is the dimensional structure diagram of fixation kit.
Drawing reference numeral explanation：
| Label | Title | Label | Title |
| 100 | Fuselage | 320 | Second pcb board |
| 200 | Battery | 330 | First shock-absorbing ball |
| 300 | Light stream positioner | 510 | Upper mounted plate |
| 400 | Obstacle avoidance apparatus | 520 | Bottom plate |
| 500 | Fixation kit | 530 | Camera installing plate |
| 110 | Accommodating cavity | 540 | Second shock-absorbing ball |
| 120 | Mounting groove | 331 | Shock-absorbing ball body |
| 130 | Holding tank | 332 | Stopper section |
| 140 | Mounting hole site | 333 | Elongated end |
| 310 | First pcb board |
The realization of the utility model purpose, functional characteristics and advantage will be described further referring to the drawings in conjunction with the embodiments.
Specific embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the present utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making creative work premise
Lower obtained every other embodiment, belongs to the scope of the utility model protection.
If it is to be appreciated that related in the utility model embodiment directionality indicate (such as upper and lower, left and right, it is preceding,
Afterwards ...), then directionality indicates to be only used for explaining relative between each part under a certain particular pose (as shown in drawings)
Position relationship, motion conditions etc., if the particular pose changes, directionality indicates also correspondingly to change therewith.
If in addition, relate to the description of " first ", " second " etc. in the utility model embodiment, should " first ", " the
Two " description etc. is only used for describing purpose, and it is not intended that indicating or implying its relative importance or implicit indicate meaning
The quantity of the technical characteristic for showing.Thus, " first " is defined, the feature of " second " can express or implicitly include at least one
Individual this feature.In addition, the technical scheme between each embodiment can be combined with each other, but must be with ordinary skill
Personnel can be implemented as basis, when the combination appearance of technical scheme is conflicting or cannot realize it will be understood that this technical side
The combination of case does not exist, not within the protection domain of the utility model requirement yet.
The utility model proposes a kind of unmanned plane, the fuselage of the unmanned plane is provided with accommodating cavity, and light is provided with the accommodating cavity
Stream positioner, the mounting structure of the light stream positioner is simple, with low cost.
The unmanned plane proposed in the embodiment of the utility model one, as shown in Figure 1 to Figure 3, including：Fuselage 100, battery 200
And light stream positioner 300, the fuselage 100 is provided with accommodating cavity 110, and the accommodating cavity 110 includes the first accommodating cavity and the
Two accommodating cavities (accompanying drawing is not shown), the bottom of second accommodating cavity is provided with cover plate, and the battery 200 is housed located at described first
In chamber, for being powered for the unmanned plane；The light stream positioner 300 is located in second accommodating cavity, and by the lid
Plate covers fixation.Wherein, the light stream positioner 300 includes the parallel and spaced PCB of first pcb board 310 and the 2nd
Plate 320, the first pcb board 310 and the second pcb board 320 are the master control borad of the unmanned plane, perform control unmanned plane during flying, positioning
Etc. function.It is fixedly connected by the first shock-absorbing ball 330 between the pcb board 320 of first pcb board 310 and second, and then, in peace
Also the damping requirement of light stream positioner 300 is disclosure satisfy that in the case that dress process is very easy so that light stream positioner 300
Realize accurate positioning hovering and smooth flight.
Specifically, Fig. 2 is continued referring to, it is contemplated that avoid being needed while dismantling nobody during dismounting light stream positioner 300
The battery 200 of machine, the light stream positioner 300 is isolated with the battery 200 by median septum, and the median septum is by the appearance
Put chamber 110 and be separated into first accommodating cavity and the second accommodating cavity, the battery 200 is described in first accommodating cavity
Light stream positioner 300 is located in the second accommodating cavity of the lower section of the battery 200, in this way, during dismounting light stream positioner 300,
Only open the second installation cavity, it is not necessary to while dismantling the battery 200 in the first installation cavity.Additionally, the first shock-absorbing ball 330
After top wears first pcb board 310, the bottom wall of median septum is connected to, the bottom of the first shock-absorbing ball 330 wears described second
After pcb board 320, the roof of cover plate is connected to, in this way, light stream positioner 300 can be by the first shock-absorbing ball 330 and top
The cover plate of median septum and bottom is realized being in close contact, therefore, the utility model proposes the not only dismounting side of light stream positioner 300
Just, and mounting structure is very firm, the sharp pounding of light stream positioner 300 can be effectively prevented from.
Refer to Fig. 3 and Fig. 4, it is contemplated that when the first shock-absorbing ball 330 and the first pcb board 310 and the second pcb board 320 are installed,
First shock-absorbing ball 330 needs to insert the installation through-hole on the first pcb board 310 and the second pcb board 320, in the present embodiment, described
The both sides of the stopper section 332 of the first shock-absorbing ball 330, are respectively equipped with as the insertion installation through-hole of the stopper section 332 provides guide-localization
The elongated end 333 of effect.
Fig. 5 is refer to, first shock-absorbing ball 330 includes shock-absorbing ball body 331, two stopper sections 332 and two elongated ends
333, stopper section 332 described in two is respectively arranged on the both sides of the shock-absorbing ball body 331, and between the shock-absorbing ball body 331
The screens installed for 310 and second pcb board of the first pcb board 320 is formed, elongated end 333 described in two is connected described in one respectively
Stopper section 332 simultaneously extends, the cylindrical setting of the elongated end 333, its diameter to away from the direction of the shock-absorbing ball body 331
Diameter with the installation through-hole is adapted to, so as to conveniently insert installation through-hole.As a kind of preferred embodiment, the elongated end
333 is being in tapered setting on the direction of the shock-absorbing ball body 331, in this way, can more facilitate the elongated end 333 to enter institute
State installation through-hole.
The assembling process of light stream positioner 300 is illustrated in conjunction with Fig. 3 and Fig. 4, first, by the first shock-absorbing ball
The elongated end 333 at 330 tops is directed at the installation through-hole on the first pcb board 310, the elongated end of the bottom of the first shock-absorbing ball 330 333 pairs
Installation through-hole on accurate second pcb board 320；Then, the first pcb board 310 and the second pcb board 320 are pressed opposite to each other so that first
The installation through-hole of the pcb board 320 of pcb board 310 and second snap in correspondingly respectively shock-absorbing ball body 331 and stopper section 332 it
Between the first screens and the second screens in, so as to complete the first shock-absorbing ball 330 and the first pcb board 310 and the second pcb board 320
Assembling is fixed.
In the another embodiment of the utility model, four all sides of the unmanned aerial vehicle body are provided with least one obstacle avoidance apparatus
400, so as to realize the barrier avoiding function of unmanned plane, the obstacle avoidance apparatus 400 can be infrared obstacle avoidance apparatus, avoiding obstacles by supersonic wave device
Or visual token obstacle avoidance apparatus etc., in the present embodiment, the obstacle avoidance apparatus 400 are provided with four, and interval is set up separately in the fuselage
All sides, and the obstacle avoidance apparatus are infrared obstacle avoidance apparatus.Specifically, Fig. 1 and Fig. 5, the unmanned aerial vehicle body 100 be refer to
Four all sides be respectively provided with a mounting hole site 140, the infrared emitting probe and receiving transducer of the obstacle avoidance apparatus 400 in
The mounting hole site 140 is passed, on the one hand, 140 pairs of obstacle avoidance apparatus 400 of mounting hole site have in position-limiting action；The opposing party
Face, mounting hole site 140 is passed for infrared probe so that infrared probe can successfully carry out ultrared transmitting and collection, enter
And determine whether there is the position of barrier and barrier.Wherein, an obstacle avoidance apparatus for side 400 pass through a fixation kit
500 install fixation with the fuselage of unmanned plane, specifically, continue referring to Fig. 1, and a side of the fuselage offers an installation
Groove 120, the obstacle avoidance apparatus 400 are installed in the mounting groove 120 by a fixation kit 500, and the fixation kit 500 is wrapped
Upper mounted plate 510 and bottom plate 520 are included, fixed plate 520 is fixed on the upper of bottom plate 520 by a column
Side, the obstacle avoidance apparatus 400 are fixed on fixed plate 510.
In the utility model above-described embodiment, Fig. 6 is refer to, the unmanned plane (does not show also including a filming apparatus in figure
Go out), such as high definition camera, high-definition camera.Specifically, the upper mounted plate 510 of the fixation kit 500 and bottom plate 520
Between be provided with for the filming apparatus install camera installing plate 530, the camera installing plate 530 pass through the second shock-absorbing ball 540
The lower section of fixed plate 510 is mounted on, in this way, the vibrations produced in unmanned plane running will not cause described shooting to fill
Vibrations are put, so that the filming apparatus can shoot the photo of high definition or record the video of high definition.Preferably, described
Two shock-absorbing balls 540 are identical with the structure of the first shock-absorbing ball 330 in above-described embodiment, i.e.,：The two of the stopper section of the second shock-absorbing ball 540
Side also is provided with elongated end, so, it is possible to facilitate the installation of the second shock-absorbing ball 540 and camera installing plate 530.Certainly, the second damping
Ball 540 can also use vibration damping spherical structure of the prior art.
In the utility model above-described embodiment, Fig. 1 is refer to, in order to reduce the weight of unmanned plane, extend the continuous of unmanned plane
Boat ability, the fuselage 100 of unmanned plane is hollow rectangular-shape, and the upper and lower surface of the fuselage 100 is hollow out,
The rotor power component of the unmanned plane is arranged at the fuselage interior.Specifically, the fuselage 100 is in flat rectangular body, machine
The upper and lower surface of body 100 is correspondingly arranged into engraved structure, and the edge of fuselage upper surface and fuselage lower surface is by interval
The reinforcing plate of setting is connected, and the accommodating cavity 110 of the light stream positioner is located at the center of the fuselage 100, the nothing
Man-machine rotor power component is inside fuselage 100, and uniform ring is located at the surrounding of the accommodating cavity 110.On the one hand, it is described
The fuselage 100 of engraved structure can mitigate unmanned plane weight；On the other hand, the nothing of multiple rotors is set for the inside of fuselage 100
Man-machine, fuselage 100 needs to meet the requirement of air circulation, therefore, the surface of fuselage 100 of unmanned plane is set in hollow out.Through engineering
The repetition test of technical staff, when the fretwork area on the surface of the fuselage 100 is with the area ratio of fuselage 100 of whole unmanned plane
During 80%-93%, the endurance of the unmanned plane, air circulation best results.
In the utility model above-described embodiment, please referring now still to Fig. 1, it is contemplated that unmanned plane landing after, fuselage 100 directly with ground
Face contact can cause abrasion to fuselage 100, therefore in this implementation, the bottom of fuselage 100 of the unmanned plane is provided with retractable branch
Pin.Specifically, the bottom of the fuselage 100 is provided with holding tank 130, be provided with the holding tank 130 it is described can folding and unfolding leg, it is described
Can folding and unfolding leg include the rotation section that is hinged with the holding tank 130 and the foot section for supporting the fuselage 100, the branch
Foot and the clamping of the holding tank 130 are being contained in the holding tank 130.When the unmanned plane during flying, the foot section
It is contained in the holding tank 130, and is connected and fixed with the holding tank 130；When the unmanned plane lands, the foot section
The holding tank 130 is stretched out, so as to avoid fuselage 100 from being contacted with ground, the bottom of fuselage 100 is efficiently avoid and is worn.
In the present embodiment, the foot section realizes clamping with the holding tank 130 by interference fit, in other embodiment
In, can also realize connecting and fixing by buckle between the foot section and the holding tank, for example, the foot section convex
If fixture block, the inwall correspondence fixture block of the holding tank sets draw-in groove, in this way, the foot section can be with the holding tank reality
Existing clamping.
Preferred embodiment of the present utility model is the foregoing is only, the scope of the claims of the present utility model is not thereby limited,
It is every under inventive concept of the present utility model, the equivalent structure made using the utility model specification and accompanying drawing content is become
Change, or directly/be used in other related technical fields indirectly and be included in scope of patent protection of the present utility model.
Claims (10)
1. a kind of unmanned plane, it is characterised in that including：
Fuselage, is provided with accommodating cavity, and the accommodating cavity includes the first accommodating cavity and the second accommodating cavity, and the second accommodating cavity bottom sets
There is a cover plate；
Battery, in first accommodating cavity；And
Light stream positioner, in second accommodating cavity, and covers fixation, the light stream positioner bag by the cover plate
Include parallel and spaced first pcb board and the second pcb board, and connect first pcb board and the second pcb board first
Shock-absorbing ball.
2. unmanned plane as claimed in claim 1, it is characterised in that the accommodating cavity is provided with median septum, the median septum will
The accommodating cavity is separated into first accommodating cavity and the second accommodating cavity.
3. unmanned plane as claimed in claim 2, it is characterised in that first shock-absorbing ball includes shock-absorbing ball body, two backstops
Portion and two elongated ends, stopper section described in two are respectively arranged on the both sides up and down of the shock-absorbing ball body, with the shock-absorbing ball sheet
The first screens installed for first pcb board and the second screens installed for second pcb board are formed between body, described in two
Elongated end connects stopper section described in one and extends to away from the direction of the shock-absorbing ball body respectively.
4. unmanned plane as claimed in claim 3, it is characterised in that elongated end described in wears first pcb board and abuts
In the median septum；Another elongated end wears second pcb board and is connected to the cover plate.
5. unmanned plane as claimed in claim 1, it is characterised in that the unmanned plane also includes rotor power component, the machine
As hollow rectangular-shape, and the upper and lower surface of the fuselage is hollow out, and the rotor power component is arranged at
The fuselage interior.
6. unmanned plane as claimed in claim 5, it is characterised in that the fretwork area of the fuselage accounts for the ratio of the fuselage gross area
It is 80%-93%.
7. unmanned plane as claimed in claim 5, it is characterised in that all sides of four of the fuselage are respectively provided with least one and keep away
Fault device.
8. unmanned plane as claimed in claim 7, it is characterised in that the unmanned plane also includes upper mounted plate and bottom plate,
Fixed plate is fixedly connected with fuselage upper surface, and the bottom plate is fixedly connected with fuselage lower surface, fixed
Plate and bottom plate are connected by a column, and the obstacle avoidance apparatus are located at fixed plate.
9. unmanned plane as claimed in claim 8, it is characterised in that the unmanned plane also includes a camera installing plate, the phase
Machine installing plate is mounted on fixed plate lower section by the second shock-absorbing ball, and shooting dress is installed with the camera installing plate
Put.
10. unmanned plane as claimed in claim 1, it is characterised in that the fuselage bottom is provided with holding tank, in the holding tank
Be provided with can folding and unfolding leg, it is described can folding and unfolding leg include the rotation section that is hinged with the holding tank and for supporting the fuselage
Foot section, the foot section and the holding tank clamping are being contained in the holding tank.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621262557.3U CN206265328U (en) | 2016-11-22 | 2016-11-22 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621262557.3U CN206265328U (en) | 2016-11-22 | 2016-11-22 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206265328U true CN206265328U (en) | 2017-06-20 |
Family
ID=59039779
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621262557.3U Active CN206265328U (en) | 2016-11-22 | 2016-11-22 | Unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206265328U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444666A (en) * | 2017-07-25 | 2017-12-08 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of taking photo by plane with camera damping device |
| CN107640310A (en) * | 2017-10-09 | 2018-01-30 | 北京沃氏航空科技有限公司 | Unmanned plane damping push and pull system and unmanned plane |
-
2016
- 2016-11-22 CN CN201621262557.3U patent/CN206265328U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444666A (en) * | 2017-07-25 | 2017-12-08 | 芜湖超源力工业设计有限公司 | A kind of unmanned plane of taking photo by plane with camera damping device |
| CN107640310A (en) * | 2017-10-09 | 2018-01-30 | 北京沃氏航空科技有限公司 | Unmanned plane damping push and pull system and unmanned plane |
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|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20191211 Address after: Room 812, enterprise service center, No. 17, section 3, west section of Changjiang North Road, Lingang Economic Development Zone, Yibin City, Sichuan Province Patentee after: Sichuan Yidian Aviation Technology Co., Ltd Address before: Baoan District Shiyan street Shenzhen city Guangdong province 518108 Songbai road Tangtou junctions electric science and Technology Park Co-patentee before: Shenzhen AEE Technology Co., Ltd. Patentee before: Shenzhen Yidian Aviation Technology Co., Ltd. |