CN207826578U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
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- CN207826578U CN207826578U CN201721928047.XU CN201721928047U CN207826578U CN 207826578 U CN207826578 U CN 207826578U CN 201721928047 U CN201721928047 U CN 201721928047U CN 207826578 U CN207826578 U CN 207826578U
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- carry part
- unmanned plane
- power supply
- plug
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- 238000009434 installation Methods 0.000 claims description 12
- 230000007246 mechanism Effects 0.000 claims description 12
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 12
- 210000002421 cell wall Anatomy 0.000 claims description 6
- 230000005611 electricity Effects 0.000 claims description 5
- 230000004580 weight loss Effects 0.000 claims description 4
- 230000005484 gravity Effects 0.000 abstract description 10
- 230000000694 effects Effects 0.000 description 9
- 238000000034 method Methods 0.000 description 6
- 238000005516 engineering process Methods 0.000 description 5
- 208000016261 weight loss Diseases 0.000 description 3
- 230000009471 action Effects 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000005265 energy consumption Methods 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 210000004027 cell Anatomy 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000000428 dust Substances 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 238000004880 explosion Methods 0.000 description 1
- 229910001095 light aluminium alloy Inorganic materials 0.000 description 1
- 229910052744 lithium Inorganic materials 0.000 description 1
- 208000020442 loss of weight Diseases 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000012528 membrane Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The utility model is related to a kind of unmanned plane, including host apparatus, host apparatus is equipped with chassis backplane, and chassis backplane is equipped with power input port；Supply unit, supply unit include power supply box, and at least one battery holding tank is equipped in power supply box, and the inner wall of power supply box is equipped with waterproof layer, and power supply box is additionally provided with output port of power source；Carry device, carry device include the first carry part and the second carry part, and the first carry part is fixedly arranged on chassis backplane, and the second carry part is fixedly arranged on power supply box.Pass through the setting of carry device, first carry part is fixedly arranged on unmanned plane, and the second carry part is fixedly arranged on supply unit, after the second carry part and fixed the first carry part cooperation, namely supply unit carry is in unmanned plane, the convenient carry for realizing battery, since supply unit carry is in uav bottom, center of gravity declines, improve flight stability, multiple battery holding tanks are convenient for battery extension, improve battery supplied ability, and waterproof layer realizes power supply reliability when moist or rainy day flight.
Description
Technical field
The utility model is related to air vehicle technique fields, more particularly to a kind of unmanned plane.
Background technology
Power battery module is one of main module of multi-rotor unmanned aerial vehicle flying platform, is flown for multi-rotor unmanned aerial vehicle
Control system provides electric energy and provides flying power for dynamical system.It is always multi-rotor unmanned aerial vehicle system that the installation of power battery, which is fixed,
One problem of design of uniting.
Common power battery mounting means has：On set the installation of (underlying) bundling type, totally-enclosed battery compartment installation and half is sealed
Close the installation of plug-in type battery compartment.These types of battery carry mode exists
Invention content
Based on this, it is necessary to for unmanned plane battery carry system mounting stability is poor, problem that disassembly efficiency is low, carry
For a kind of unmanned plane.
Its technical solution is as follows：
A kind of unmanned plane, including host apparatus, host apparatus are equipped with chassis backplane, and chassis backplane is equipped with power input
Mouthful；Supply unit, supply unit include the power supply box for loading battery, and at least one battery holding tank is equipped in power supply box,
The inner wall of power supply box is equipped with waterproof layer, and power supply box is additionally provided with the output port of power source for connecting with power input port；Carry
Device, carry device include the first carry part and the second carry part, and the first carry part is fixedly arranged on chassis backplane, and the second carry part is solid
Set on power supply box, the second carry part and the first carry part are detachably fixed and supply unit are made to be fixedly arranged on host apparatus.
Above-mentioned unmanned plane, by the setting of carry device, the first carry part is fixedly arranged on chassis backplane, namely is fixedly arranged on nobody
Machine, the second carry part are fixedly arranged on supply unit, and after the second carry part and fixed the first carry part cooperation namely supply unit is hung
It is loaded in unmanned plane, realizes the convenient carry of battery, since supply unit carry is in uav bottom, center of gravity declines, improves winged
Row stability, at the same it is detachable easy to operation, in addition, multiple battery holding tanks are installed convenient for battery extension, improve battery supplied
Ability, waterproof layer realize power supply reliability when moist or rainy day flight.
Technical solution is illustrated further below：
The first carry part is equipped with the first sliding groove in one of the embodiments, and the second carry part is equipped with matches with the first sliding groove
Close the first mobile sliding rail；Or first carry part be equipped with the second sliding rail, the second carry part is equipped with and the cooperation of the second sliding rail is mobile
Second sliding slot.The cooperation of sliding slot and sliding rail keeps the operation of the carry between supply unit and host apparatus simpler quick, improves
The cooperation of installation effectiveness, sliding slot and sliding rail also functions to the effect of limit, improves the steady of supply unit during unmanned plane during flying
It is qualitative, it is not susceptible to shake, improves the stability of power supply.
The cell wall of the first sliding groove is equipped with the first limit fallen for limiting the second carry part in one of the embodiments,
Portion, the first sliding rail are equipped with the second limiting section coordinated with the first limiting section；Or second sliding rail be equipped with for limiting the second carry part
The third limiting section fallen, the cell wall of second sliding slot are equipped with the 4th limiting section coordinated with third limiting section.Supply unit is located at
The lower section of host apparatus, supply unit and host apparatus realize cooperation and fixed by sliding rail and sliding slot, but due to gravity,
Supply unit may fall from host apparatus and lead to not power, and therefore, setting limiting section is asked with further avoiding this
The generation of topic limits supply unit with host apparatus in the one-movement-freedom-degree of gravity direction by limiting section, avoids supply unit
By falling or detaching on host apparatus, electrical stability is improved.
The first limiting section includes the first limit convex being arranged along the first sliding groove length direction in one of the embodiments,
Edge, the second limiting section include the first limiting groove coordinated with the first defining flange；Or third limiting section includes along the second sliding rail
Second defining flange of length direction setting, the 4th limiting section includes the second limiting groove coordinated with the second defining flange.Limit
The setting of position flange and limiting groove loses the degree of freedom of gravity direction after so that the second carry part and the first carry part is coordinated, real
The technique effect that existing supply unit can not be fallen, obtains better carry technique effect, improves the carry stability of power supply box.
The end of the first sliding rail is equipped in one of the embodiments, enters the first inclined-plane of the first sliding groove or the convenient for it
One chamfering；Or second sliding rail end be equipped with convenient for its enter second sliding slot the second inclined-plane or the second chamfering.First carry part
When carrying out carry operation with the second carry part, since the cooperation of sliding rail and sliding slot needs to be inserted into, in the end set of sliding rail
Inclined-plane or chamfering form the structure with guiding role, so that sliding rail is more easy to enter in sliding slot, realize that more easily carry is grasped
Make, improves carry installation effectiveness.
Carry device further includes clamping mechanism in one of the embodiments, and clamping mechanism is for limiting the first carry part
And the second movement between carry part.Due to that may will produce inclination during unmanned plane during flying and cause supply unit along main
The chassis backplane of machine device moves, namely leads to that phase occurs along sliding slot or slide direction between the second carry part and the first carry part
To movement, the electrical stability of supply unit is influenced, such as leads to contact between output port of power source and power input port not
The setting of the problems such as good, clamping mechanism avoid the problem, and limit the movement between the first carry part and the second carry part certainly
By spending, ensure electrical stability.
Clamping mechanism includes spring catch and the screens mounting base coordinated with spring catch, screens in one of the embodiments,
Mounting base is fixedly arranged on chassis backplane, and the first carry part is equipped with the first card hole, and the second carry part is equipped with the second card hole, spring catch
Coordinate with the first card hole and/or the second card hole and limits the movement between the first carry part and the second carry part.Spring catch
It is easy to operate, and the sliding of the first carry part and the second carry part in sliding rail or sliding slot direction is limited, and then avoid supply unit
It shifts between host apparatus, improves the electrical stability of supply unit.
Further include in one of the embodiments, the first plug and coordinates the first connector of grafting with the first plug, first
Plug is set to chassis backplane, and the other end of the first plug connects with power input port, and the first connector is set to power supply box, and first connects
The other end of head connects with output port of power source；Or further include the second plug and coordinate the second connector of grafting with the second plug,
Second plug is set to power supply box, and the other end of the second plug connects with output port of power source, and the second connector is set to chassis backplane, the
The other end of two connectors connects with power input port.The setting of plug and connector improves output port of power source and power input
Connection convenience between port, improves installation effectiveness, in addition, due to the cooperation between connector and plug be also equipped with it is certain
Fixing acts on, and improves the connective stability between interface, improves electrical stability.
It is additionally provided with port pedestal in one of the embodiments, port pedestal is fixedly arranged on chassis backplane, and port pedestal is equipped with
Mounting groove, the first plug or the second connector are fixedly arranged in mounting groove.Plug or connector are fixedly arranged in mounting groove, improve plug or
Stability of connector during unmanned plane during flying avoids being in contact bad problem, improves electrical stability.
In one of the embodiments, the first carry part along its length it is parallel set there are two, the second carry part and
One carry part is correspondingly provided with two, and the first carry part and the second carry part are additionally provided with weight loss groove.The first carry part being arranged in pairs
Keep power supply box more stable after mounting with the second carry part, while being also that unmanned plane is more equal to the load-bearing stress of power supply box
Even, the setting of weight loss groove further decreases the load during unmanned plane during flying, reduces flight energy consumption, meets the need of distance flight
It asks.
Description of the drawings
Fig. 1 is the supply unit and carry device explosion figure of unmanned plane；
Fig. 2 is the supply unit and carry device-added structure schematic diagram of unmanned plane.
100, power supply box, the 210, first carry part, 211, the first sliding groove, the 212, first card hole, the 220, second carry part,
221, the first sliding rail, the 222, first inclined-plane, the 223, second card hole, 310, spring catch, 320, screens mounting base, 410, first inserts
Head, the 420, first connector, 431, port pedestal, 432, mounting groove, 433, reserved inserting groove.
Specific implementation mode
The embodiments of the present invention are described in detail below in conjunction with the accompanying drawings：
It should be noted that when alleged element is with another element " fixation " in text, it can be directly in another element
Above or there may also be elements placed in the middle.When an element is considered as with another element " connection ", it can be straight
It is connected to another element in succession or may be simultaneously present centering elements.On the contrary, when element is referred to as " directly existing " another element
When "upper", intermediary element is not present.Term as used herein " vertically ", " horizontal ", "left", "right" and similar table
It states for illustrative purposes only, is not offered as being unique embodiment.
Unless otherwise defined, all of technologies and scientific terms used here by the article is led with the technology for belonging to the utility model
The normally understood meaning of technical staff in domain is identical.Terminology used in the description of the utility model herein only be
The purpose of description specific embodiment, it is not intended that in limitation the utility model.Term " and or " used herein packet
Include any and all combinations of one or more relevant Listed Items.
Embodiment as depicted in figs. 1 and 2, a kind of unmanned plane, including host apparatus, host apparatus are equipped with chassis backplane,
Chassis backplane is equipped with power input port；Supply unit, supply unit include the power supply box 100 for loading battery, power supply box
Be equipped at least one battery holding tank in 100, the inner wall of power supply box 100 is equipped with waterproof layer, power supply box 100 be additionally provided with for electricity
The output port of power source that source input port connects；Carry device, carry device include the first carry part 210 and the second carry part
220, the first carry part 210 is fixedly arranged on chassis backplane, and the second carry part 220 is fixedly arranged on power supply box 100, the second carry part 220 with
First carry part 210 is detachably fixed and supply unit is made to be fixedly arranged on host apparatus.
By the setting of carry device, the first carry part 210 is fixedly arranged on chassis backplane, namely is fixedly arranged on unmanned plane, and second
Carry part 220 is fixedly arranged on supply unit, after the second carry part 220 and the first carry part 210 cooperation fixed namely supply unit
Carry realizes the convenient carry of battery in unmanned plane, and since supply unit carry is in uav bottom, center of gravity declines, improves
Flight stability, at the same it is detachable easy to operation, in addition, multiple battery holding tanks are installed convenient for battery extension, improves battery and supply
Should be able to power, waterproof layer realizes power supply reliability when moist or rainy day flight.
In addition, since supply unit and carry device are set to chassis backplane, improving to set on traditional power battery causes
The higher problem in center make the flight of unmanned plane since supply unit and carry device center of gravity are low in the technical solution of the application
It is more steady, the situation of unmanned plane kinetic stability difference caused by existing power battery carry is improved, and fly convenient for unmanned plane
Motion control during row.
Further, power supply box 100 is arranged in sealing structure.Cell package is set in the battery holding tank of power supply box 100,
Due to hermetically sealed structure, to ensure good dust control technology effect.
Further, waterproof layer is waterproof coating or the waterproof membrane for being attached at 100 inner wall of power supply box.Due to power supply box
100 are arranged in sealing structure, and detachably change battery operation, itself just has certain waterproof action.But nobody
For machine in rainy day or wet environment middle and long distance or flying for long time, local environment is increasingly complex, needs better seal, waterproof
The setting of layer avoids water body and enters the problem of power supply box 100 influences battery powered circuit, plays better seal technique effect.
Specifically, as depicted in figs. 1 and 2,100 setting in rectangular configuration of power supply box, power supply box 100 includes polylith rectangle
Plate, the fixed power supply box 100 for being integrated and forming rectangular configuration of polylith rectangular slab.Power supply box 100 is internally provided with battery
Power supply is exported to the line construction of output port of power source.The external interface of power supply box 100 also provides support of supplying power with double circuit, and is respectively
Power communications are supported and power power supply is supported, power supply efficiency higher, while two batteries that are internally provided with of power supply box 100 accommodate
Slot can accommodate the lithium battery of two pieces of 2200mAh, meet the power supply demand of unmanned plane during flying.
On the basis of any of the above-described a embodiment, in embodiment as depicted in figs. 1 and 2, the first carry part 210 is equipped with
The first sliding groove 211, the second carry part 220 is equipped with coordinates the first mobile sliding rail 221 with the first sliding groove 211；Or the first carry part
210 are equipped with the second sliding rail, and the second carry part 220 is equipped with the second sliding slot mobile with the cooperation of the second sliding rail.Sliding slot and sliding rail are matched
It closes that so that carry between supply unit and host apparatus is operated simpler quick, improves installation effectiveness, sliding slot and sliding rail are matched
The effect for also functioning to limit is closed, the stability of supply unit during unmanned plane during flying is improved, is not susceptible to shake, improves and supplies
The stability of electricity.
Further, the first carry part 210 and the second carry part 220 are in that strip structure is arranged, and chassis backplane is also pre-
Equipped with the first mounting hole for fixing the first carry part 210.
In addition, the setting of sliding slot and sliding rail is fixed with carry to preferably dismantle, the case where meeting carry demand
Under, other structures, such as latch structure can also be used.
On the basis of any of the above-described a embodiment, the cell wall of the first sliding groove 211 is equipped with for limiting the second carry part 220
The first limiting section fallen, the first sliding rail 221 are equipped with the second limiting section coordinated with the first limiting section；Or second sliding rail be equipped with use
In the third limiting section that the second carry part 220 of limitation is fallen, the cell wall of second sliding slot is equipped with the coordinate with third limiting section the 4th
Limiting section.Supply unit is located at the lower section of host apparatus, supply unit and host apparatus by sliding rail and sliding slot realize cooperation and
It is fixed, but due to gravity, supply unit may fall from host apparatus and lead to not power, therefore, setting limit
Position portion limits the movement of supply unit and host apparatus in gravity direction to further avoid the generation of the problem, by limiting section
Degree of freedom avoids supply unit by falling or detaching on host apparatus, improves electrical stability.
On the basis of any of the above-described a embodiment, the first limiting section includes being arranged along 211 length direction of the first sliding groove
First defining flange, the second limiting section include the first limiting groove coordinated with the first defining flange；Or third limiting section includes
Along the second defining flange of the second sliding rail length direction setting, the 4th limiting section includes the second limit coordinated with the second defining flange
Position groove.The setting of defining flange and limiting groove loses gravity after so that the second carry part 220 and the first carry part 210 is coordinated
The degree of freedom in direction realizes the technique effect that supply unit can not be fallen, obtains better carry technique effect, improves power supply box
100 carry stability.
Further, the setting of the first limiting section makes the 210 T-shaped slot structure setting of the first carry part, the second limiting section
Being arranged makes the second carry part 220 be in the T-type rail structure setting coordinated with the first carry part 210.
In addition, the first carry part 210 and the second carry part 220 are all made of aluminium product and form, to reduce flying for unmanned plane
Row load, in the case where meeting structural requirement, other light materials can also be used, and further, aircraft aluminum can be used,
Each construction weight is reduced under the premise of ensureing rigidity hardness.
On the basis of any of the above-described a embodiment, the end of the first sliding rail 221 is equipped with enters the first sliding groove 211 convenient for it
The first inclined-plane 222 or the first chamfering；Or second the end of sliding rail be equipped with and enter the second inclined-plane of second sliding slot or the convenient for it
Two chamferings.When first carry part 210 and the second carry part 220 carry out carry operation, since the cooperation of sliding rail and sliding slot needs to insert
Enter, therefore, on the end set inclined-plane or chamfering of sliding rail, forms the structure with guiding role, slided so that sliding rail is more easy to enter
In slot, realize that more easily carry operates, and improves carry installation effectiveness.
On the basis of any of the above-described a embodiment, carry device further includes clamping mechanism, and clamping mechanism is for limiting the
Movement between one carry part 210 and the second carry part 220.It tilts and leads due to that may will produce during unmanned plane during flying
The chassis backplane that source device is sent a telegraph along host apparatus moves, namely leads to edge between the second carry part 220 and the first carry part 210
Sliding slot or slide direction relatively move, and influence the electrical stability of supply unit, such as lead to output port of power source and power supply
The setting of the problems such as poor contact between input port, clamping mechanism avoid the problem, and limit 210 He of the first carry part
One-movement-freedom-degree between second carry part 220 ensures electrical stability.
Clamping mechanism improves the peace of supply unit for limiting the second moving along 211 direction of the first sliding groove of carry part 220
Stability is filled, the stability for the host apparatus power supply capacity that supply unit is unmanned plane is improved.
On the basis of any of the above-described a embodiment, clamping mechanism includes spring catch 310 and the card that coordinates with spring catch 310
Position mounting base 320, screens mounting base 320 are fixedly arranged on chassis backplane, and the first carry part 210 is equipped with the first card hole 212, and second hangs
Holder 220 is equipped with the second card hole 223, and spring catch 310 coordinates and limits with the first card hole 212 and/or the second card hole 223
Make the movement between the first carry part 210 and the second carry part 220.Spring catch 310 is easy to operate, and limits the first carry part
210 and second carry part 220 in the sliding in sliding rail or sliding slot direction, and then avoid occurring between supply unit and host apparatus inclined
It moves, improves the electrical stability of supply unit.
Further, screens mounting base 320 is equipped with the third card hole being used cooperatively with spring catch 310, third card hole
It is correspondingly arranged with the first card hole 212, the second card hole 223.The structure setting reference of spring catch 310 and screens mounting base 320
Existing structure setting is played by the setting of spring catch 310 to the first carry part 210 and the second carry part 220 here
Position-limiting action, avoid during unmanned plane during flying the second carry part 220 that from sliding and then slide along the first sliding groove 211 or
The connective stability between output port of power source and power input port is tilted and influenced, power supply performance is influenced.
Spring catch 310 can set one, also can be equipped with it is multiple, as depicted in figs. 1 and 2, two the first carry parts 210 and second
The corresponding position of carry part 220 is equipped with card hole and the second card hole 223, in order to which spring catch 310 can be arranged in both sides
It is limited, further increases the carry stability of supply unit.
It should be noted that the first card hole 212, the second card hole 223 and third card hole are can be with spring catch 310
Coordinate the pin hole of limit.
On the basis of any of the above-described a embodiment, as depicted in figs. 1 and 2, further includes the first plug 410 and inserted with first
First connector 420 of first 410 cooperation grafting, the first plug 410 are set to chassis backplane, the other end and power supply of the first plug 410
Input port connects, and the first connector 420 is set to power supply box 100, and the other end of the first connector 420 connects with output port of power source；
Or further includes the second plug and the second connector of grafting, the second plug is coordinated to be set to power supply box 100, the second plug with the second plug
The other end connect with output port of power source, the second connector be set to chassis backplane, the other end and power input of the second connector
Mouth connects.The setting of plug and connector improves the connection convenience between output port of power source and power input port, improves
Installation effectiveness improves between interface in addition, since cooperation between connector and plug is also equipped with certain fixing effect
Connective stability improves electrical stability.
Further, the first plug 410 is DB plug male connectors, and the first connector 420 is DB plug females.Using copper DB
Modular plug is to use and be used for the electricity between supply unit and the host apparatus of multi-rotor unmanned aerial vehicle as high current connector
Power connection provides electric power for host apparatus.DB plugs are conventional call of the those skilled in the art to D connector, are inserted
The shape of head similar alphabetical " D " is got, and which is not described herein again.
In addition, the control system of unmanned plane is equipped with independent power management module, each sensor of respectively unmanned plane carries
(DC12V/24V) is provided for (DC3V/5V), mission payload equipment and power motor provides (DC12V-56V) power supply；DB plugs
Port include communication port and supply port, DB plug females connect with output port of power source, and DB plugs male connector and power supply are defeated
Inbound port connects, and power input port is connected with power management module.
Further, as depicted in figs. 1 and 2, there are two the first plug 410 and the first connector 420 are all provided with.
Specifically, the setting of DB plugs male connector and DB plug females, also solves the skimble-scamble technology of existing battery interface
Problem, in conjunction with the setting of power supply box 100, can built-in polylith battery, also solve the technical problem of battery dilatation hardly possible.
On the basis of any of the above-described a embodiment, it is additionally provided with port pedestal 431, port pedestal 431 is fixedly arranged on cabinet bottom
Plate, port pedestal 431 are equipped with mounting groove 432, and the first plug 410 or the second connector are fixedly arranged in mounting groove 432.Plug or connector
It is fixedly arranged in mounting groove 432, improves the stability of plug or connector during unmanned plane during flying, avoid being in contact bad
The problem of, improve electrical stability.
Further, embodiment as depicted in figs. 1 and 2, the first plug 410 pass through the mounting plate being provided thereon and port
Pedestal 431 is fixed, and 432 cell wall of mounting groove of port pedestal 431 also has limited step, and limited step is for limiting the first plug
410 fitting depth in mounting groove 432.As shown in Fig. 2, due to the setting of limited step, the other end of the first plug 410 with
There are gap, which is reserved inserting groove 433 for the slot bottom position of mounting groove 432, reserves inserting groove 433 and is used for power input
Mouthful and the other end of the first plug 410 connect, can direct grafting, the connection that circuit both carries out can also be passed through.
Unmanned plane makes the power battery installation reliability of multi-rotor unmanned aerial vehicle by the setting of supply unit and carry device
Higher, easy for assemble or unload, due to simple in structure, production cost is lower.
On the basis of any of the above-described a embodiment, the first carry part 210 along its length it is parallel set there are two, second
Carry part 220 and the first carry part 210 are correspondingly provided with two, and the first carry part 210 and the second carry part 220 are additionally provided with loss of weight
Slot.The the first carry part 210 and the second carry part 220 being arranged in pairs keep power supply box 100 more stable after mounting, are also simultaneously
Unmanned plane is more uniformly distributed the load-bearing stress of power supply box 100, and the setting of weight loss groove further decreases during unmanned plane during flying
Load reduces flight energy consumption, meets the needs of distance flight.
Each technical characteristic of embodiment described above can be combined arbitrarily, to keep description succinct, not to above-mentioned reality
It applies all possible combination of each technical characteristic in example to be all described, as long as however, the combination of these technical characteristics is not deposited
In contradiction, it is all considered to be the range of this specification record.
Above-described embodiments merely represent several embodiments of the utility model, the description thereof is more specific and detailed,
But therefore it can not be interpreted as the limitation to utility model patent range.It should be pointed out that for the common skill of this field
For art personnel, without departing from the concept of the premise utility, various modifications and improvements can be made, these are belonged to
The scope of protection of the utility model.Therefore, the protection domain of the utility model patent should be determined by the appended claims.
Claims (10)
1. a kind of unmanned plane, which is characterized in that including：
Host apparatus, the host apparatus are equipped with chassis backplane, and the chassis backplane is equipped with power input port；
Supply unit, the supply unit include the power supply box for loading battery, and at least one electricity is equipped in the power supply box
Pond holding tank, the inner wall of the power supply box are equipped with waterproof layer, the power supply box be additionally provided with for the power input port phase
The output port of power source connect；
Carry device, the carry device include the first carry part and the second carry part, and the first carry part is fixedly arranged on described
Chassis backplane, the second carry part are fixedly arranged on the power supply box, and the second carry part and the first carry part are detachable
It fixes and the supply unit is made to be fixedly arranged on the host apparatus.
2. unmanned plane according to claim 1, which is characterized in that the first carry part is equipped with the first sliding groove, and described the
Two carry parts are equipped with first sliding rail mobile with the first sliding groove cooperation；
Or the first carry part is equipped with the second sliding rail, the second carry part is equipped with the mobile with second sliding rail cooperation
Two sliding slots.
3. unmanned plane according to claim 2, which is characterized in that the cell wall of the first sliding groove is equipped with described for limiting
The first limiting section that second carry part is fallen, first sliding rail are equipped with the second limiting section coordinated with first limiting section；
Or second sliding rail is equipped with the third limiting section fallen for limiting the second carry part, the slot of the second sliding slot
Wall is equipped with the 4th limiting section coordinated with the third limiting section.
4. unmanned plane according to claim 3, which is characterized in that first limiting section includes long along the first sliding groove
Spend direction setting the first defining flange, second limiting section include with first defining flange coordinate first limit it is recessed
Slot；
Or the third limiting section includes the second defining flange being arranged along the second sliding rail length direction, the 4th limit
Portion includes the second limiting groove coordinated with second defining flange.
5. unmanned plane according to claim 2, which is characterized in that the end of first sliding rail is equipped with enters institute convenient for it
State the first inclined-plane or the first chamfering of the first sliding groove；Or the end of second sliding rail is equipped with and enters the second sliding slot convenient for it
The second inclined-plane or the second chamfering.
6. unmanned plane according to claim 1, which is characterized in that the carry device further includes clamping mechanism, the card
Position mechanism is used to limit the movement between the first carry part and the second carry part.
7. unmanned plane according to claim 6, which is characterized in that the clamping mechanism include spring catch and with the spring
The screens mounting base of cooperation is sold, the screens mounting base is fixedly arranged on the chassis backplane, and the first carry part is equipped with the first card
Position hole, the second carry part are equipped with the second card hole, the spring catch and first card hole and/or second screens
Hole coordinates and limits the movement between the first carry part and the second carry part.
8. unmanned plane according to claim 1, which is characterized in that further include the first plug and coordinate with first plug
First connector of grafting, first plug are set to the chassis backplane, and the other end and the power supply of first plug are defeated
Inbound port connects, and first connector is set to the power supply box, the other end and the output port of power source of first connector
Connect；
Or further includes the second plug and the second connector of grafting, second plug is coordinated to be set to the electricity with second plug
The other end of source case, second plug connects with the output port of power source, and second connector is set to the chassis backplane,
The other end of second connector connects with the power input port.
9. unmanned plane according to claim 8, which is characterized in that be additionally provided with port pedestal, the port pedestal is fixedly arranged on
The chassis backplane, the port pedestal are equipped with mounting groove, and first plug or second connector are fixedly arranged on the installation
In slot.
10. unmanned plane according to claim 1, which is characterized in that the first carry part is parallel along its length to be set
There are two, the second carry part is correspondingly provided with two with the first carry part, and the first carry part and described second are hung
Holder is additionally provided with weight loss groove.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721928047.XU CN207826578U (en) | 2017-12-29 | 2017-12-29 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721928047.XU CN207826578U (en) | 2017-12-29 | 2017-12-29 | Unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN207826578U true CN207826578U (en) | 2018-09-07 |
Family
ID=63391378
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| CN201721928047.XU Active CN207826578U (en) | 2017-12-29 | 2017-12-29 | Unmanned plane |
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| CN (1) | CN207826578U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111776235A (en) * | 2020-07-29 | 2020-10-16 | 北京云圣智能科技有限责任公司 | Airborne equipment, aircraft and method of plugging and unplugging airborne equipment |
| CN112298524A (en) * | 2020-11-26 | 2021-02-02 | 尚良仲毅(沈阳)高新科技有限公司 | Lower fuselage and unmanned aerial vehicle |
| CN112373695A (en) * | 2020-11-26 | 2021-02-19 | 尚良仲毅(沈阳)高新科技有限公司 | Carry cabin and unmanned aerial vehicle |
-
2017
- 2017-12-29 CN CN201721928047.XU patent/CN207826578U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111776235A (en) * | 2020-07-29 | 2020-10-16 | 北京云圣智能科技有限责任公司 | Airborne equipment, aircraft and method of plugging and unplugging airborne equipment |
| CN112298524A (en) * | 2020-11-26 | 2021-02-02 | 尚良仲毅(沈阳)高新科技有限公司 | Lower fuselage and unmanned aerial vehicle |
| CN112373695A (en) * | 2020-11-26 | 2021-02-19 | 尚良仲毅(沈阳)高新科技有限公司 | Carry cabin and unmanned aerial vehicle |
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Effective date of registration: 20200929 Address after: 510620 Tianhe District, Guangzhou, Tianhe South Road, No. two, No. 2, No. Patentee after: Guangzhou Power Supply Bureau of Guangdong Power Grid Co.,Ltd. Address before: 510620 Tianhe District, Guangzhou, Tianhe South Road, No. two, No. 2, No. Patentee before: GUANGZHOU POWER SUPPLY Co.,Ltd. |
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