CN110217399A - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
- Publication number
- CN110217399A CN110217399A CN201910470892.4A CN201910470892A CN110217399A CN 110217399 A CN110217399 A CN 110217399A CN 201910470892 A CN201910470892 A CN 201910470892A CN 110217399 A CN110217399 A CN 110217399A
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- CN
- China
- Prior art keywords
- mounting rack
- locking part
- fixed body
- unmanned plane
- fuselage
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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- 230000009471 action Effects 0.000 claims description 3
- 238000009434 installation Methods 0.000 description 4
- 238000010586 diagram Methods 0.000 description 3
- 238000007689 inspection Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 229910052799 carbon Inorganic materials 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 208000010138 Diastema Diseases 0.000 description 1
- 206010039203 Road traffic accident Diseases 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 210000000475 diastema Anatomy 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 208000020442 loss of weight Diseases 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000007480 spreading Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
- H01M50/00—Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
- H01M50/20—Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02E60/10—Energy storage using batteries
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Electrochemistry (AREA)
- General Chemical & Material Sciences (AREA)
- Battery Mounting, Suspending (AREA)
Abstract
The invention discloses a kind of unmanned plane, it is related to aviation aircraft technical field, main purpose is that the battery of unmanned plane is avoided to fall off or generate vibration, to guarantee the normal operation of unmanned plane.Main technical schemes of the invention are as follows: the unmanned plane includes: fuselage, and mounting rack is provided on the fuselage, the first locking part is provided on the mounting rack；Battery fixing structure, the battery fixing structure include fixed body, and chamfered shape is provided in the fixed body and is adapted with the chamfered shape of battery, and the accommodating chamber for accommodating the battery；Wherein, the fixed physical efficiency slides into the mounting rack, and the fixed body can be locked in the mounting rack by first locking part.Present invention is mainly used for avoid battery from falling off or generate vibration.
Description
Technical field
The present invention relates to aviation aircraft technical fields, in particular to a kind of unmanned plane.
Background technique
Unmanned plane is just increasingly extensive for the application development of various industries, at this stage, unmanned plane have been applied to take photo by plane, agriculture
Woods plant protection, geological prospecting, electric inspection process, oil and gas pipeline inspection, expressway traffic accident management, forest fire protection inspection collection pollution environment
The every field such as prospecting.
Wherein, multi-rotor unmanned aerial vehicle is a kind of inorganic man-machine type for capableing of VTOL, and it is mostly electronic unmanned plane.Mesh
Before, the battery of multi-rotor unmanned aerial vehicle usually passes through magic band and is fixed on the mounting rack of fuselage, since magic band easily damages
It is bad, easily battery is caused to fall off；Or baffle is used on the mounting rack of fuselage, to use battery limiting by the long period
Afterwards, baffle is easy to damage and generate diastema, and battery is caused to fall off, or make unmanned plane generate high-frequency vibration in operation and to control
System impacts.Particularly with current heavy-duty, long endurance larger heavier battery for, above-mentioned battery fixed form pole
For inconvenience.
Summary of the invention
In view of this, the embodiment of the present invention provides a kind of unmanned plane, main purpose be avoid the battery of unmanned plane fall off or
Vibration is generated, to guarantee the normal operation of unmanned plane.
In order to achieve the above objectives, present invention generally provides following technical solutions:
The embodiment of the invention provides a kind of unmanned planes, comprising:
Fuselage is provided with mounting rack on the fuselage, the first locking part is provided on the mounting rack；
Battery fixing structure, the battery fixing structure include fixed body, be provided in the fixed body chamfered shape with
The chamfered shape of battery is adapted, and the accommodating chamber for accommodating the battery；
Wherein, the fixed physical efficiency slides into the mounting rack, and the fixed body can be locked in by first locking part
In the mounting rack.
Further, first locking part has lockup state and unlocked state；
When first locking part is in lockup state, the fixed physical efficiency is locked in the mounting rack；
When first locking part is in the unlocked state, the fixed physical efficiency skids off the mounting rack.
Further, it is respectively arranged on the mounting rack and the fixed body and opposite first through hole and second is led to
Hole；
Connector, the connector are connected to the mounting rack bottom；
Handle, the handle are rotatablely connected by elastic component and the connector；
Positioning pin, one end of the positioning pin and the handle are rotatablely connected, and the other end penetrates the first through hole and institute
State the second through-hole；
Wherein, when the handle is pressed, the positioning pin can be retracted in the first through hole, form described first
The unlocked state of locking part；When the handle is released, the handle capable of being resets under the action of the elastic component, and drives
The positioning pin resets, and forms the lockup state of first locking part.
Further, the end of the mounting rack is provided with limit plate；
When the fixed body slides into the mounting rack, and abuts against with the limit plate, the first locking part energy
The fixed body is locked in the mounting rack.
Further, the first sliding rail is provided on the mounting rack；
The second sliding rail for being slidably connected with first sliding rail is provided on the fixed body, the fixed physical efficiency is logical
It crosses first sliding rail and second sliding rail slides in or out the mounting rack.
Further, charging interface is provided on the fixed body, the charging interface with the battery for being electrically connected.
Further, the battery fixing structure further includes the connecting plate for being set to the fixed body top surface；
Second sliding rail is set on the connecting plate.
Further, the mounting rack, which has, slides in or out its internal open end for the fixed body, and with institute
The connecting pin that open end is away from each other is stated, the connecting pin and the fuselage are rotatablely connected；
The unmanned plane further includes the second locking part, and second locking part has lockup state and unlocked state；
When second locking part is in lockup state, the mounting rack can be locked in the fuselage；
When second locking part is in the unlocked state, the open end of the mounting rack can be rotated relative to the fuselage
And it is lifted.
Further, the mounting rack has bottom plate；
Second locking part includes being rotatablely connected with the fuselage, and the rotating member opposite with the bottom end；
Wherein, the rotating member can the relatively described fuselage turn to first position and the second position, and work as the rotating member
When turning to the first position, the rotating member is pressed in the bottom plate, forms the lockup state of second locking part；When
When the rotating member turns to the second position, the rotating member is detached from the bottom plate, forms the solution of second locking part
Lock status.
Further, the fuselage, which has, protrudes from the bottom plate, and the step opposite with the bottom end；
One end of the rotating member is rotationally connected with the step surface of the step, and the other end protrudes from the step of the step
Face, and it is provided with the convex edge extended to the bottom plate, the convex edge is arc；
When the rotating member rotates between the first position and the second position relative to the fuselage, the convex edge
It can be pressed in the bottom plate around the wedge angle of the step or be detached from the bottom plate.
By above-mentioned technical proposal, the present invention is at least had the advantages that
Unmanned plane provided in an embodiment of the present invention, by the way that the first locking part, and setting are arranged on the mounting rack of fuselage
Battery fixing structure including fixed body, and chamfered shape receiving compatible with the chamfered shape of battery is provided in fixed body
Chamber is contained in the battery of unmanned plane in the accommodating chamber of fixed body, and fixed physical efficiency slides into mounting rack, and the first lock
The fixed body that stop can will slide into mounting rack is locked in mounting rack, and so, the fixed body for accommodating battery can lead to
It crosses the first locking part to be fixed in mounting rack, will not fall off, and vibration will not be generated, simultaneously as the chamfered shape of accommodating chamber
It is adapted with the chamfered shape of battery, therefore battery will not also generate vibration in fixed body and more will not fall off, and ensure that nobody
The normal operation of machine, it is easy to use.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of the unmanned plane provided in an embodiment of the present invention at the first visual angle；
Fig. 2 is the enlarged drawing in Fig. 1 at A；
Fig. 3 is a kind of structural schematic diagram of the unmanned plane provided in an embodiment of the present invention at the second visual angle；
Fig. 4 is the structural schematic diagram of locking relationship between mounting rack and the second locking part in Fig. 3.
Specific embodiment
To make the object, technical solutions and advantages of the present invention clearer, below in conjunction with the preferred embodiment of the present invention
In attached drawing, technical solution in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from beginning to end or
Similar label indicates same or similar element or element with the same or similar functions.Described embodiment is this hair
Bright a part of the embodiment, instead of all the embodiments.The embodiments described below with reference to the accompanying drawings are exemplary, it is intended to
It is used to explain the present invention, and is not considered as limiting the invention.Based on the embodiments of the present invention, ordinary skill
Personnel's every other embodiment obtained without creative efforts, shall fall within the protection scope of the present invention.
The embodiment of the present invention is described in detail with reference to the accompanying drawing.
In the description of the present embodiment, it is to be understood that term " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or positional relationship of the instructions such as "left", "right", "vertical", "horizontal", "top", "bottom" "inner", "outside" is based on attached drawing institute
The orientation or positional relationship shown is merely for convenience of description the present embodiment and simplifies description, rather than indication or suggestion meaning
Device or element must have a particular orientation, be constructed and operated in a specific orientation, therefore should not be understood as to the present embodiment
The limitation of protection scope.
As shown in Figure 1, the unmanned plane can be multi-rotor unmanned aerial vehicle the embodiment of the invention provides a kind of unmanned plane,
Including fuselage 1, it is provided with mounting rack 2 on the fuselage 1, the first locking part 4 can be set on the mounting rack 2；Battery fixed knot
Structure 3 comprising fixed body 31 can be set chamfered shape in the fixed body 31 and be adapted with the chamfered shape of battery, and use
In the accommodating chamber 311 for accommodating battery；Wherein, fixed body 31 can slide into mounting rack 2, and the first locking part 4 can be by fixed body 31
It is locked in mounting rack 2.
In some instances, mounting rack 2 can be the frame being mainly made of bottom plate and two side plates being connected on bottom plate
Body structure can be placed with multiple through-holes on bottom plate and side plate, and the bottom plate and side plate can be made of carbon fibre material,
So as to the heat dissipation of loss of weight and battery.And the fixed body 31 of battery fixing structure 3 can be compatible with cell widths for a width
Rectangular-shape body structure, and the settable demarcation plate in the body structure, multiple and battery can be formed in fixed body 31
The compatible accommodating chamber 311 of profile meets the requirement of unmanned plane to store multiple batteries.Specifically, the fixed body 31
It can be made of aluminum alloy materials, can not only reduce cost, it is easy to process, moreover, it is also possible on the surface of fixed body 31
It is covered with through-hole, can not only plays the heat spreading function to battery, 1 weight of fuselage can also be mitigated, unmanned plane is carried
More load or equipment.
Unmanned plane provided in an embodiment of the present invention, by the way that the first locking part, and setting are arranged on the mounting rack of fuselage
Battery fixing structure including fixed body, and chamfered shape receiving compatible with the chamfered shape of battery is provided in fixed body
Chamber is contained in the battery of unmanned plane in the accommodating chamber of fixed body, and fixed physical efficiency slides into mounting rack, and the first lock
The fixed body that stop 4 can will slide into mounting rack is locked in mounting rack, and so, the fixed body for accommodating battery can lead to
It crosses the first locking part 4 to be fixed in mounting rack, will not fall off, and vibration will not be generated, simultaneously as the chamfered shape of accommodating chamber
It is adapted with the chamfered shape of battery, therefore battery will not also generate vibration in fixed body and more will not fall off, and ensure that nobody
The normal operation of machine, it is easy to use.
In some instances, the first locking part 4 above-mentioned can have lockup state and unlocked state；When the first locking part
4 be in lockup state when, fixed body 31 can be locked in mounting rack 2；When the first locking part 4 is in the unlocked state, fixed body
31 can skid off mounting rack 2.When installing battery, battery can be contained in the fixed body 31 of battery structure, then by fixed body
31 slide into mounting rack 2, the first locking part 4 may make to be in lockup state at this time, are locked at fixed body 31 to realize
In mounting rack 2, and unmanned plane can be kept at work, battery will not fall off and vibrate；When dismantling battery, can make
First locking part 4 is in the unlocked state, then skids off the fixed body 31 of battery fixing structure 3 out of mounting rack 2, can be realized
The disassembly of battery.
Wherein, the structure type of the first locking part 4 can there are many, fixed body 31 is locked at installation as long as can be realized
In frame 2 or fixed body 31 is enabled to skid off mounting rack 2.
In some instances, referring to fig. 2, and Fig. 1 is combined, which may include being respectively arranged at mounting rack 2
With on fixed body 31 and opposite first through hole and the second through-hole；Connector 41, the connector 41 can connect in 2 bottom of mounting rack
Portion；Handle 42, the handle 42 can be rotatablely connected by elastic component 43 and connector 41；Positioning pin 44, the one of the positioning pin 44
End can be rotatablely connected with handle 42, and the other end can penetrate first through hole and the second through-hole.
In some instances, the bottom phase in mounting rack 2 and fixed body 31 can be set in first through hole and the second through-hole
Position is answered, moreover, the second through-hole being arranged on fixed body 31 can also be card slot, as long as positioning pin 44 is passing through mounting rack 2
First through hole after can be plugged in the second through-hole or card slot, with locking fixed body 31.Connector 41 can be to be fixed on
The connecting plate of 2 bottom of mounting rack, and in order to save space, can the aperture on connecting plate so that the aperture of 44 through-hole of positioning pin is worn
Enter first through hole and the second through-hole.And it includes 42 ontology of handle and arc panel connected to it that the structure of handle 42, which can be, two
The junction of person is rotatablely connected by a fixing piece and connector 41, and the end of arc panel and one end of positioning pin 44 rotate and connect
It connects；Elastic component 43 can connect between connector 41 and arc panel, and the elastic component 43 can be spring.
According to above-described embodiment, when handle body is pressed, arc panel can overcome the elastic force of elastic component 43 and drive and determine
Position pin 44 is retracted in first through hole from the second through-hole, allows fixed body 31 to skid off mounting rack 2, so as to form first
The unlocked state of locking part 4；When handle body is released, 42 ontology of handle and arc panel are under the elastic force effect of elastic component 43
It resets, so that positioning pin 44 resets under the drive of arc panel, i.e., is penetrated in the second through-hole herein, by 31 locking of fixed body
In mounting rack 2, so as to form the lockup state of the first locking part 4, structure is simple, realizes reliable.
In order to enable the fixed body 31 of battery fixing structure 3 can be more firmly locked in mounting rack 2, some
In example, referring to Fig. 3, limit plate 21 can be set in the end of mounting rack 2, installed to realize when fixed body 31 slides into
In frame 2, and when abutting against with limit plate 21, fixed body 31 can be locked in mounting rack 2 by the first locking part 4.That is,
When fixed body 31 is locked in mounting rack 2 by the first locking part 4, the end of fixed body 31 can offset with limit plate 21, play
To the double limitation fixed function of fixed body 31, vibration will not be generated or fall off by further ensuring fixed body 31, avoid nothing
It is man-machine to influence the center of gravity of unmanned plane because fixed body shifts in flight course.Moreover, passing through the setting of limit plate 21, also
It can be slid into mounting rack 2 for fixed body 31 and play position-limiting action, i.e., when 31 end of fixed body and limit plate 21 offset, then table
Show that fixed body 31 slides into place, at this time the first locking part 4 can locking fixed body 31, using more convenient.
Mounting rack 2 is slid in or out for the ease of the fixed body 31 of battery fixing structure 3, in some instances, referring to figure
3, the first sliding rail 22 can be provided on mounting rack 2；And setting connects for sliding with the first sliding rail 22 on fixed body 31
The second sliding rail 311 connect enables fixed body 31 to slide in or out in mounting rack 2 by the first sliding rail 22 and the second sliding rail 311,
So that multiple batteries can integrally and be conveniently and efficiently loaded and unloaded on unmanned plane.
Wherein, the structure type of the first sliding rail 22 and the second sliding rail 311 can there are many, as long as fixed body 31 may be implemented
Being slidably connected between mounting rack 2, in order to guarantee Stable sliding and positioning of the fixed body 31 in mounting rack 2, first
The quantity of sliding rail 22 can be four, and the four corners of mounting rack 2 can be distributed in along the length direction of mounting rack 2, similarly, the
The quantity of two sliding rails 311 can be four, and the four corners of fixed body 31 can be distributed in along the length direction of fixed body 31.
In some instances, the second sliding rail 311 can be the sliding slot arranged along 31 length direction of fixed body；And the first sliding rail
22 can be arranged on mounting rack 2 and to roll along multiple bearings of 2 length direction of mounting rack arrangement, multiple bearing and sliding slot
Realization is slidably connected, and structure is simple, realizes reliable.
In some instances, referring to Fig. 1, charging interface 312 can be set on the fixed body 31 of battery fixing structure 3,
The charging interface 312 with battery for being electrically connected, thus realize when needing to charge to battery, it only need to be by the charging interface 312
It is electrically connected with power interface, the charging of battery can be completed, it is easy to use without carrying out other operations.Specifically, the charging
Interface 312 can be set in the end of fixed body 31, in order to its connection between power interface.
In some instances, referring to Fig. 1, handle 313 can also be set in the end of fixed body 31, in order to operator
It can be pulled out by the handle 313 or be pushed into fixed body 31, convenient for installation of the battery fixing structure 3 in mounting rack 2.
In some instances, referring to Fig. 3, battery fixing structure 3 can also include the connection for being set to 31 top surface of fixed body
Plate 32；Second sliding rail 311 is set on the connecting plate 32.By the setting of connecting plate 32, so that the battery fixing structure 3 is installed
To the mounting rack 2 of fuselage 1, fixed body 31 can have certain interval between the other components of fuselage 1, to avoid fuselage
It is interfered between 1 other components and fixed body 31, to guarantee respective work.Wherein, in order to mitigate weight and mention
High intensity, the connecting plate 32 can be figure of eight plate.
Due to being located at the end of mounting rack 2 on fuselage 1 there may be other structures or components, to mounting rack 2
It is interior to slide into or easily sent out with the other structures or components when skidding off the fixed body 31 of battery fixing structure 3 out of mounting rack 2
Raw interference, causes fixed body 31 that can not slide in or out, in order to solve this problem, in some instances, referring to Fig. 3, installation
Frame 2, which has, slides in or out its internal open end 23, and the connecting pin 24 being away from each other with the open end 23 for fixed body 31,
The connecting pin 24 can be rotatablely connected with fuselage 1；The unmanned plane can also include the second locking part, which has lock
Only state and unlocked state；When second locking part is in lockup state, mounting rack 2 can be locked in fuselage 1；When second lock
When stop is in the unlocked state, the open end 23 of mounting rack 2 can rotate relative to fuselage 1 and is lifted.
According to above-described embodiment, since the connecting pin of mounting rack 2 and fuselage 1 are rotation connection, so that the opening of mounting rack 2
The opposite fuselage 1 of 23 energy of end is lifted or puts down, therefore, when the second locking part is in the unlocked state, the open end 23 of mounting rack 2
It can be lifted and cross the other structures being arranged on fuselage 1 or components, at this point, the opening from mounting rack 2 by fixed body 31 again
Mouth end 23 slides in or out, and can avoid interfering, and after fixed body 31 slides into mounting rack 2, mounting rack 2 can be put down, then
Using the second locking part by 2 locking of mounting rack on the fuselage 1, to complete the installation or removal of battery, using more convenient.
In some instances, referring to fig. 4, and Fig. 3 is combined, mounting rack 2 can have bottom plate 24；Second locking part can wrap
It includes and is rotatablely connected with fuselage 1, and the rotating member 5 opposite with 24 end of bottom plate；Wherein, which turns to
First position and the second position, and when rotating member 5 turns to first position, rotating member 5 is pressed in bottom plate 24, forms the second lock
The lockup state of stop；When rotating member 5 turns to the second position, rotating member 5 is detached from bottom plate 24, forms the solution of the second locking part
Lock status.
According to above-described embodiment, when needing to install or remove battery, rotating member 5 can be turned into the second position, made
The bottom plate 24 that rotating member 5 is detached from mounting rack 2 is obtained, mounting rack 2 can be lifted at this time, the fixed body 31 to be accommodated for having battery slides into
Or after skidding off mounting rack 2, rotating member 5 can be turned into first position, so that rotation shoulder compresses the bottom plate 24 of mounting rack 2, from
And mounting rack 2 is fixed on the fuselage 1, using more convenient.
In some instances, referring to fig. 4, on the fuselage 1 being previously mentioned positioned at mounting rack 2 end it is that may be present its
Its structure or components can be the step for protruding from the bottom plate 24 of mounting rack 2, and opposite with 24 end of the bottom plate of mounting rack 2
11, i.e. carbon plate.And one end of rotating member 5 can be rotatably connected on 11 face of step of the step 11, the other end can protrude from platform
11 face of step of rank 11, and it is provided with the convex edge 51 extended to bottom plate 24, which can be arc；Rotating member 5 is with respect to machine
When body 1 rotates between the first position and the second position, convex edge 51 can be pressed in bottom plate 24 or is detached from around the wedge angle of step 11
Bottom plate 24.By the way that camber is arranged in the convex edge 51 of rotating member 5, it is facilitated around step 11 to compress or be detached from bottom plate 24,
Using more convenient.Specifically, the quantity of the rotating member 5 can be two, and be rotatably arranged in the step of step 11 side by side
On 11 faces.
Finally, it should be noted that the above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations；Although
Present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that: it still may be used
To modify the technical solutions described in the foregoing embodiments or equivalent replacement of some of the technical features；
And these are modified or replaceed, technical solution of various embodiments of the present invention that it does not separate the essence of the corresponding technical solution spirit and
Range.
Claims (10)
1. a kind of unmanned plane characterized by comprising
Fuselage is provided with mounting rack on the fuselage, the first locking part is provided on the mounting rack；
Battery fixing structure, the battery fixing structure include fixed body, are provided with chamfered shape and battery in the fixed body
Chamfered shape be adapted, and for accommodating the accommodating chamber of the battery；
Wherein, the fixed physical efficiency slides into the mounting rack, and the fixed body can be locked in described by first locking part
In mounting rack.
2. unmanned plane according to claim 1, which is characterized in that
First locking part has lockup state and unlocked state；
When first locking part is in lockup state, the fixed physical efficiency is locked in the mounting rack；
When first locking part is in the unlocked state, the fixed physical efficiency skids off the mounting rack.
3. unmanned plane according to claim 2, which is characterized in that first locking part includes:
It is respectively arranged on the mounting rack and the fixed body and opposite first through hole and the second through-hole；
Connector, the connector are connected to the mounting rack bottom；
Handle, the handle are rotatablely connected by elastic component and the connector；
Positioning pin, one end of the positioning pin and the handle are rotatablely connected, and the other end penetrates the first through hole and described the
Two through-holes；
Wherein, when the handle is pressed, the positioning pin can be retracted in the first through hole, form first locking
The unlocked state in portion；When the handle is released, the handle capable of being resets under the action of the elastic component, and described in drive
Positioning pin resets, and forms the lockup state of first locking part.
4. unmanned plane according to claim 1, which is characterized in that
The end of the mounting rack is provided with limit plate；
When the fixed body slides into the mounting rack, and abuts against with the limit plate, first locking part can be by institute
Fixed body is stated to be locked in the mounting rack.
5. unmanned plane according to claim 1, which is characterized in that
The first sliding rail is provided on the mounting rack；
The second sliding rail for being slidably connected with first sliding rail is provided on the fixed body, the fixed physical efficiency passes through institute
It states the first sliding rail and second sliding rail slides in or out the mounting rack.
6. unmanned plane according to claim 1, which is characterized in that
Charging interface is provided on the fixed body, the charging interface with the battery for being electrically connected.
7. unmanned plane according to claim 1, which is characterized in that
The battery fixing structure further includes the connecting plate for being set to the fixed body top surface；
Second sliding rail is set on the connecting plate.
8. unmanned plane according to any one of claim 1 to 7, which is characterized in that
The mounting rack, which has, slides in or out its internal open end for the fixed body, and is away from each other with the open end
Connecting pin, the connecting pin and the fuselage are rotatablely connected；
The unmanned plane further includes the second locking part, and second locking part has lockup state and unlocked state；
When second locking part is in lockup state, the mounting rack can be locked in the fuselage；
When second locking part is in the unlocked state, the open end of the mounting rack can be rotated relative to the fuselage and by
It lifts.
9. unmanned plane according to claim 8, which is characterized in that
The mounting rack has bottom plate；
Second locking part includes being rotatablely connected with the fuselage, and the rotating member opposite with the bottom end；
Wherein, the rotating member can the relatively described fuselage turn to first position and the second position, and when the rotating member rotates
When to the first position, the rotating member is pressed in the bottom plate, forms the lockup state of second locking part；When described
When rotating member turns to the second position, the rotating member is detached from the bottom plate, forms the unlock shape of second locking part
State.
10. unmanned plane according to claim 9, which is characterized in that
The fuselage, which has, protrudes from the bottom plate, and the step opposite with the bottom end；
One end of the rotating member is rotationally connected with the step surface of the step, and the other end protrudes from the step surface of the step,
And it is provided with the convex edge extended to the bottom plate, the convex edge is arc；
When the rotating member rotates between the first position and the second position relative to the fuselage, the convex edge can be around
The wedge angle for crossing the step is pressed in the bottom plate or is detached from the bottom plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910470892.4A CN110217399A (en) | 2019-05-31 | 2019-05-31 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910470892.4A CN110217399A (en) | 2019-05-31 | 2019-05-31 | Unmanned plane |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN203707201U (en) * | 2013-09-25 | 2014-07-09 | 深圳一电科技有限公司 | Electronic device |
| CN106275461A (en) * | 2016-08-26 | 2017-01-04 | 深圳电航空技术有限公司 | The battery box structure of unmanned plane and unmanned plane |
| CN207896168U (en) * | 2018-03-21 | 2018-09-21 | 深圳市八方通达科技有限公司 | Battery cover component and mobile terminal with the battery cover component |
| CN210526863U (en) * | 2019-05-31 | 2020-05-15 | 沈阳无距科技有限公司 | Unmanned plane |
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Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN203707201U (en) * | 2013-09-25 | 2014-07-09 | 深圳一电科技有限公司 | Electronic device |
| CN106275461A (en) * | 2016-08-26 | 2017-01-04 | 深圳电航空技术有限公司 | The battery box structure of unmanned plane and unmanned plane |
| CN207896168U (en) * | 2018-03-21 | 2018-09-21 | 深圳市八方通达科技有限公司 | Battery cover component and mobile terminal with the battery cover component |
| CN210526863U (en) * | 2019-05-31 | 2020-05-15 | 沈阳无距科技有限公司 | Unmanned plane |
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