CN207791163U - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
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- CN207791163U CN207791163U CN201721828170.4U CN201721828170U CN207791163U CN 207791163 U CN207791163 U CN 207791163U CN 201721828170 U CN201721828170 U CN 201721828170U CN 207791163 U CN207791163 U CN 207791163U
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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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Abstract
The utility model provides a kind of unmanned plane, including main body and rotor module, the main body is equipped with multiple mounting bases for installing the rotor module, the rotor module is removably mounted in the mounting base, the mounting base is equipped with the first interface for powering and data communicate, and the rotor module is equipped with the connector being electrically connected with the first interface.Unmanned plane provided by the utility model can increase and decrease the quantity of rotor module according to the size of load weight, to be combined into more rotors of different layout types, so that the unmanned plane of the utility model can according to the transportation demand variation of express delivery more rotor types of flexible configuration unmanned plane, realize the optimization of power service efficiency, and due to that only can realize a variety of more rotor-hub configuration types by the increase and decrease of rotor module, and unmanned plane other component keeps identical, reduces design, production and the maintenance cost of configuration multiple types unmanned plane.
Description
Technical field
The utility model belongs to vehicle technology field, is to be related to a kind of unmanned plane more specifically.
Background technology
In recent years, with the development of science and technology, unmanned plane has been widely used in various fields, such as express delivery goods
Transport, the aviation of object are taken photo by plane.
Currently, the unmanned plane applied to express transportation includes a variety of aerodynamic arrangement's types, such as quadrotor drone, eight rotations
Wing unmanned plane and mixing lift unmanned plane.The efficiency optimization used from power, the unmanned plane of different aerodynamic arrangement's types
It is suitble to different aerial mission, such as quadrotor drone is generally suitable for the lighter express transportation of short distance, load, eight rotors
Unmanned plane is generally used for short distance, the heavier express transportation of load, and mixing lift unmanned plane is generally used for longer-distance fast
Pass transport.
However, in practical applications, the transportation demand of different time express delivery is not changeless, such as certain time
Remote express delivery demand may be more, and the express delivery demand of another a period of time closer distance may occupy the majority.If configuration is solid
The different type unmanned plane of fixed number amount then can not frequently change for express transportation demand and realize that unmanned plane resource optimization uses,
The use cost brought due to configuring different types of unmanned plane is also resulted in increase.
Utility model content
The purpose of this utility model is to provide a kind of unmanned planes, and to solve unmanned plane in the prior art, there are function lists
One, different occasions and the higher technical problem of maintenance cost can not be applicable in.
To achieve the above object, the technical solution adopted in the utility model is：A kind of unmanned plane, the unmanned plane packet are provided
Main body and rotor module are included, the main body is equipped with multiple mounting bases for installing the rotor module, the mounting base
It is equipped with the first interface for powering and data communicate, the rotor module is equipped with and is connect with what the first interface was electrically connected
Head.
Further, the quantity of the mounting base is eight, and eight mounting bases are distributed in upper layer and lower layer, and every layer is wrapped
Include four mounting bases.
Further, the unmanned plane further includes supporting rack, and support frame as described above is rotatablely connected the main body, the mounting base
It is also provided on support frame as described above.
Further, the quantity of the mounting base is eight, when support frame as described above is in closed configuration, eight peaces
It fills seat to be distributed in upper layer and lower layer, every layer includes four mounting bases；Mounting base described in the two of which on upper layer is set to institute
It states on supporting rack, other two mounting base on upper layer is set in the main body, and four mounting bases of lower layer are equal
It is set in the main body.
Further, the quantity of the rotor module is four, and four rotor modules are respectively arranged in the four of upper layer
In a mounting base；Alternatively, four rotor modules are respectively arranged in four mounting bases of lower layer；Alternatively, institute
The quantity for stating rotor module is eight, and eight rotor modules are respectively arranged in eight mounting bases.
Further, the mounting base includes pedestal and mounting ring, and the pedestal is connect with the main body, the installation
One end of ring is connected through a screw thread with the pedestal, and the other end of the mounting ring is connected through a screw thread with the rotor module.
Further, one end of the mounting ring is equipped with the first internal thread, and the other end of the mounting ring is equipped in second
Screw thread, and the diameter of first internal thread is less than the diameter of second internal thread, the inside projection of inner wall of the mounting ring
There is limited step；One end of the pedestal is equipped with for coordinating the flange limited with the limited step, the pedestal
The other end is equipped with the first external screw thread for being connect with first internal screw-thread screw, and the end face of the pedestal is equipped with positioning
Column；The rotor module is equipped with the second external screw thread for being connect with second internal screw-thread screw and is used for and the positioning
The location hole of column cooperation positioning.
Further, the unmanned plane further includes lift wing module, and installation position, the lift wing are additionally provided in the main body
Module is removably mounted on the installation position.
Further, the unmanned plane further includes for the lift wing module to be detachably connected with the installation position
Quick-dismantle component, the Quick-dismantle component include being set to the fixed card slot on the installation position and being set in the lift wing module simultaneously
For coordinating fixed fixed card buckle with the fixed card slot；Alternatively, the Quick-dismantle component includes being set on the installation position
It fixed card buckle and in the lift wing module and is used for and the fixed card buckle coordinates fixed fixed card slot；Alternatively,
The Quick-dismantle component includes the movable clamp groove being set in the lift wing module, for coordinating fixed work with the movable clamp groove
Move block tongue and for driving the movable block tongue to stretch out to lock the lift wing module or retract to unlock the lift
The switch of wing module, the activity block tongue are set in the main body.
Further, the unmanned plane includes the battery for power supply, and the main body is equipped with battery mounting bin, described
Battery-disassembled is installed in the battery mounting bin；Or the main body is equipped with multiple battery mounting bins, the electricity
Pond is removably mounted in the battery mounting bin；Alternatively, the unmanned plane includes the battery for power supply, in the main body
Equipped with battery mounting bin, the battery is installed in the battery mounting bin；The battery includes shell and multiple battery moulds
Group, the multiple battery modules are removably mounted in shell.
The advantageous effect of unmanned plane provided by the utility model is：Compared with prior art, the utility model provides one
Kind unmanned plane, by the way that rotor module to be removable installed in above-mentioned mounting base, and passes through the cooperation of first interface and connector
Realize that rotor module and main body, can be according to the numbers of the size of load weight increase and decrease rotor module for be electrically connected and data communication
Amount, to be combined into more rotors of different layout types, so that the unmanned plane of the utility model can be according to the fortune of express delivery
More rotor types of defeated changes in demand and flexible configuration unmanned plane realize the optimization of power service efficiency, and due to only passing through
The increase and decrease of rotor module can realize a variety of more rotor-hub configuration types, and unmanned plane other component keeps identical, reduces configuration
The design of multiple types unmanned plane, production and maintenance cost.
Description of the drawings
It, below will be to embodiment or the prior art in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing needed in description is briefly described, it should be apparent that, the accompanying drawings in the following description is only that this practicality is new
Some embodiments of type for those of ordinary skill in the art without having to pay creative labor, can be with
Obtain other attached drawings according to these attached drawings.
Fig. 1 is the structural schematic diagram of the one of which embodiment for the unmanned plane that the utility model embodiment provides；
Fig. 2 is the structural schematic diagram of another embodiment for the unmanned plane that the utility model embodiment provides；
The rotor module and the structural representation after mounting base assembling that Fig. 3 is the unmanned plane that the utility model embodiment provides
Figure；
Fig. 4 is the decomposition diagram of Fig. 3；
Fig. 5 is the schematic cross-section of Fig. 3；
Fig. 6 is the structural schematic diagram of the rotor module for the unmanned plane that the utility model embodiment provides；
Fig. 7 is the structural schematic diagram that the unmanned plane that the utility model embodiment provides is equipped with lift wing module；
Fig. 8 is another angle schematic diagrames of Fig. 7；
Fig. 9 is the decomposition diagram that the unmanned plane that the utility model embodiment provides is equipped with lift wing module；
Figure 10 is the structural schematic diagram for the lift wing module that the utility model embodiment provides；
Figure 11 is the structural schematic diagram for the battery that the utility model embodiment provides；
Figure 12 is the schematic cross-section for the battery that the utility model embodiment provides.
Wherein, each reference numeral in figure：
10- main bodys；The first connecting shafts of 11-；12- protect-ing frame structure；The installation positions 13-；20- rotor modules；21- connectors；22- spiral shells
Revolve paddle；23- motors；30- supporting racks；The second connecting shafts of 31-；50- mounting bases；51- pedestals；52- mounting rings；53- limited steps；
54- flanges；55- positioning columns；56- location holes；70- lift wing modules；The 71- lift wings；72- support columns；73- interfaces；The side 74-
To rudder；80- Quick-dismantle components；81- fixed card buckles；91- is switched；1- batteries；101- shells；102- battery units.
Specific implementation mode
In order to make technical problem to be solved in the utility model, technical solution and advantageous effect be more clearly understood, with
Lower combination accompanying drawings and embodiments, the present invention will be further described in detail.It should be appreciated that specific reality described herein
It applies example to be only used to explain the utility model, is not used to limit the utility model.
It should be noted that when element is referred to as " being fixed on " or " being set to " another element, it can be directly another
On one element or it is connected on another element.When an element is known as " being connected to " another element, it can
To be directly to another element or be indirectly connected on another element.
It is to be appreciated that term " length ", " width ", "upper", "lower", "front", "rear", "left", "right", "vertical",
The orientation or positional relationship of the instructions such as "horizontal", "top", "bottom" "inner", "outside" is that orientation based on ... shown in the drawings or position are closed
System, is merely for convenience of describing the present invention and simplifying the description, does not indicate or imply the indicated device or element is necessary
With specific orientation, with specific azimuth configuration and operation, therefore should not be understood as limiting the present invention.
In addition, term " first ", " second " are used for description purposes only, it is not understood to indicate or imply relative importance
Or implicitly indicate the quantity of indicated technical characteristic.Define " first " as a result, the feature of " second " can be expressed or
Implicitly include one or more this feature.The meaning of " plurality " is two or two in the description of the present invention,
More than, unless otherwise specifically defined.
Also referring to Fig. 1 to Figure 12, now unmanned plane provided by the utility model is illustrated.Above-mentioned unmanned plane includes
Main body 10 and rotor module 20, aforementioned body 10 are equipped with multiple mounting bases 50 for installing above-mentioned rotor module 20, on
Rotor module 10 is stated to be removably mounted in above-mentioned mounting base 50；Above-mentioned mounting base 50 is equipped with for powering and data communication
First interface (not shown), above-mentioned rotor module 20 are equipped with the connector 21 being electrically connected with the first interface.Above-mentioned first
The thimble phase mutual connection that either shrapnel passes through first interface and thimble or shrapnel on connector 21 is equipped at interface and connector 21
It touches, realize the power supply of rotor module 10 and is communicated to connect with the data of main body 10.
Wherein, compared with prior art, the unmanned plane of the utility model, by the way that rotor module 20 to be removable installed in
In above-mentioned mounting base 50, and by the cooperation of first interface and connector 21 realize rotor module 20 and main body 10 for being electrically connected and
Data communication can increase and decrease the quantity of rotor module 20, to be combined into the more of different layout types according to the size of load weight
Rotor so that the unmanned plane of the utility model can according to the transportation demand variation of express delivery and flexible configuration unmanned plane it is more
Rotor type, realizes the optimization of power service efficiency, and can be realized by the increase and decrease of rotor module 20 due to only a variety of more
Rotor-hub configuration type, and unmanned plane other component keeps identical, reduces the design of configuration multiple types unmanned plane, production and dimension
Protect cost.
Further, shown in as shown in Figure 1, Figure 2, Fig. 3 and Fig. 4, the quantity of above-mentioned mounting base 50 is eight, eight above-mentioned installations
Seat 50 is distributed in upper layer and lower layer, and every layer includes four above-mentioned mounting bases 50.Every layer of four mounting bases, 50 rectangular arrangement, and
Every layer of four mounting bases 50 are located on four angles of rectangle.Four mounting bases 50 on upper layer and four mounting bases of lower layer
50 be in symmetrical structure.It should be noted that the quantity of above-mentioned mounting base 50 is not limited thereto, the utility model other compared with
In good embodiment, the quantity of above-mentioned mounting base 50 can be multiple, can be arranged according to actual needs, such as can be 12,
14,16.
Further, as shown in Figure 3, Figure 4, above-mentioned unmanned plane further includes the first connecting shaft for supporting above-mentioned mounting base 50
11, above-mentioned first connecting shaft 11 is connected with aforementioned body 10.In the present embodiment, the quantity of above-mentioned first connecting shaft 11 is four
A, four above-mentioned first connecting shafts 11 are symmetrically disposed on the opposite sides of aforementioned body 10 two-by-two, each first connecting shaft 11
The same end is all provided with there are two above-mentioned mounting base 50, i.e., two mounting bases 50 are coaxially disposed, and about above-mentioned first connecting shaft 11
Symmetrically.It should be noted that the quantity and set-up mode of above-mentioned first connecting shaft 11 are not limited thereto, in the utility model
In other preferred embodiments, the quantity of above-mentioned first connecting shaft 11 may be arranged as eight, eight above-mentioned first connecting shafts 11
It is connect respectively with eight above-mentioned mounting bases 50.
Further, as shown in Figure 1, the quantity of above-mentioned rotor module 20 is four, four above-mentioned rotor modules 20 are distinguished
It is installed in four above-mentioned mounting bases 50 on upper layer, to form quadrotor layout.Since the unmanned plane of quadrotor is suitable for short
In distance, the lighter express transportation of load, when needing the lighter express transportation of short distance, load, by by four rotor moulds
Block 20 is installed in four mounting bases 50 on upper layer, forms quadrotor layout, in the case where meeting transportation demand, realize
The optimization of unmanned mechanomotive force service efficiency.Alternatively, four rotor modules 20 can also be respectively arranged in four mounting bases of lower layer
On 50.
Further, as shown in Fig. 2, the quantity of above-mentioned rotor module 20 is eight, eight above-mentioned rotor modules 20 are distinguished
It is installed in eight mounting bases 50, forms eight rotor-hub configurations.The unmanned plane of eight rotors is suitable for short distance, compared with the express delivery of big load
In transport.
Further, as shown in Fig. 3, Fig. 4, Fig. 5, above-mentioned mounting base 50 includes pedestal 51 and mounting ring 52, above-mentioned seat
Body 51 is connect with the first connecting shaft 11, and one end of above-mentioned mounting ring 52 is connected through a screw thread with above-mentioned pedestal 51, above-mentioned mounting ring
52 other end is connected through a screw thread with above-mentioned rotor module 20.Specifically, in a preferred embodiment of the utility model,
One end of above-mentioned mounting ring 52 is equipped with the first internal thread, and the other end of above-mentioned mounting ring 52 is equipped with the second internal thread, and above-mentioned the
The diameter of one internal thread is less than the diameter of the second internal thread, and the inner wall of the mounting ring 52 is inwardly convexly equipped with limited step 53.It is above-mentioned
One end of pedestal 51 is equipped with for coordinating the flange 54 limited, the other end of above-mentioned pedestal 51 to set with the limited step 53
It is useful for the first external screw thread being connect with above-mentioned first internal screw-thread screw, the end face of above-mentioned pedestal 51 is equipped with positioning column 55.On
Rotor module 20 is stated to be equipped with the second external screw thread for connecting with second internal screw-thread screw and be used for and above-mentioned positioning column
The location hole 56 of 55 cooperation positioning, makes the relatively above-mentioned seat of rotor module 20 by the mutual cooperation of positioning column 55 and location hole 56
Body 51 realizes that positioning, certain above-mentioned rotor module 20 realize that the mode positioned is not limited thereto with pedestal 51, for example, can be
Location hole is set on pedestal 51, positioning column is set in rotor module 20.It is understood that it is all can realize pedestal 51 with
The structure that rotor module 20 is positioned should belong to the scope of protection of the utility model.When the number for needing increase rotor module 20
When amount, it would be desirable to which increased rotor module 20 is located in above-mentioned pedestal 51 by the mutual cooperation of positioning column 55 and location hole 56
In screens；Then, then rotate mounting ring 52, by the second internal thread and second it is externally threaded cooperate so that mounting ring 52 with
Above-mentioned rotor module 20 is connected and fixed, and when rotating to screw tip, due to the mutual cooperation of limited step 53 and flange 54,
Finally realize being connected and fixed between mounting ring 52, pedestal 51,20 three of rotor module.When needing to reduce rotor module 20
When quantity, needing first to rotate mounting ring 52 along the direction of release so that mounting ring 52 is unclamped with above-mentioned rotor module 20, from
And rotor module 20 can be reduced, and above-mentioned first internal thread is just screwed together with the first external screw thread at this time, so that peace
Dress ring 52 is connected and fixed with the holding of pedestal 51, avoids loosening.The connection type of above-mentioned mounting base 50 and above-mentioned rotor module 20 is simultaneously
It is not limited to this, for example, in other preferred embodiments of the utility model, can also be blocked by being arranged in mounting base 50
It detains, card slot is set in rotor module 20, or by the way that card slot is arranged in mounting base 50, buckle is arranged in rotor module 20, leads to
Cross buckle and the fastening realization mounting base 50 of card slot and being connected and fixed for above-mentioned rotor module 20.
Further, as shown in Figure 5, Figure 6, above-mentioned rotor module 20 is including propeller 22 and for driving above-mentioned spiral
The motor 23 that paddle 22 rotates, propeller 22 are installed on the output shaft of motor 23.The unmanned plane has control system, control system
It is controlled for the posture of unmanned plane and position, set-up of control system is in main body 10.Above-mentioned motor 23 is controlled by control system
Output power size, to control propeller 22 rotating speed size, and then control rotor module 20 generate pulling force size.On
It states mounting ring 52 and the direction locked of above-mentioned rotor module 20 is consistent with the direction of rotation of above-mentioned propeller 22, i.e., when propeller 22
For rotationally clockwise when, the locking direction of mounting ring 52 and above-mentioned rotor module 20 is also clockwise；Work as propeller
22 is when rotating in an anti-clockwise direction, mounting ring 52 are also square counterclockwise with the locking direction of pedestal 51 and above-mentioned rotor module 20
To so can be to avoid causing mounting ring 52 and rotor module 20 to loosen when propeller 22 rotates the case where.Certainly, should
The direction that mounting ring 52 is locked with above-mentioned rotor module 20 can be arranged according to actual needs, such as can be with the rotation of propeller 22
Direction is opposite.In addition, since there are areas for the direction up and down of the rotor module 20 positioned at different mounting bases and propeller direction of rotation
Not, in order to avoid accidentally installing, can by by the matching thread of the mounting ring of different mounting bases and corresponding rotor module 20 or
Person coordinates positioning column and location hole to be arranged to different specifications, can also facilitate installation personnel area by the way that different colours label is arranged
Point.
Further, above-mentioned rotor module 20 further includes ESC (Electronic Speed Control, electronic speed regulation
Device), LED light and for monitor motor or rotor operation sensor.
Further, above-mentioned unmanned plane further includes protect-ing frame structure 12, for protecting rotor module 20, prevents rotor module 20
It is collided by foreign matter.Above-mentioned protect-ing frame structure 12 is connect with aforementioned body 10, and the rotor module 20 after assembling is located at above-mentioned protecting frame
In frame 12.In the present embodiment, above-mentioned protect-ing frame structure 12 is a hollow quadrangle frame structure, naturally it is also possible to be designed as it
His shape.Above-mentioned protect-ing frame structure 12 can be dismantled.
Further, as shown in Figure 7, Figure 8, above-mentioned unmanned plane further includes supporting rack 30, and above-mentioned supporting rack 30 is rotatablely connected
Aforementioned body 10, specifically, above-mentioned supporting rack 30 is connected in main body 10 and protect-ing frame structure 12, above-mentioned mounting base 50 is also set up
In on the supporting rack 30.Specifically, in the preferred embodiment of one of the utility model, the quantity of above-mentioned mounting base 50 is
Eight, wherein two mounting bases 50 are set on supporting rack 30, and in addition six mounting bases 50 are set in main body 10.When above-mentioned
When supporting rack 30 is in closed configuration, eight above-mentioned mounting bases 50 are distributed in upper layer and lower layer, and every layer of four mounting bases 50 are in square
Shape is arranged, and every layer of four mounting bases 50 are located on four angles of rectangle.Four mounting bases 50 on upper layer and lower layer
Four mounting bases 50 are in symmetrical structure.Specifically, the two of which mounting base 50 on upper layer is set on supporting rack 30, upper layer it is another
Outer two mounting bases 50 are set in main body 10, and four mounting bases 50 of lower layer may be contained in aforementioned body 10.Preferably,
Above-mentioned supporting rack 30 is connect by the second connecting shaft 31 with above-mentioned mounting base 50, and two above-mentioned mounting bases 50 be located at it is above-mentioned
The opposite sides of main body 10.Above-mentioned supporting rack 30 is swung relative to aforementioned body 10, to open and close in aforementioned body 10, works as unmanned plane
In landing state or as conventional more rotors in use, above-mentioned supporting rack 30 is in closed configuration, it is installed on supporting rack 30
Two rotor modules 20 propeller Plane of rotation is parallel with horizontal plane or less parallel, lift can be provided for unmanned plane,
And the propeller Plane of rotation that is installed on rotor module 20 in main body 10 is parallel with horizontal plane or less parallel, can be simultaneously
Unmanned plane provides lift；When unmanned plane such as mixes lift layout as unconventional more rotors cruising level flight state is in using lower
When, above-mentioned supporting rack 30 is in the open state, is installed on the propeller Plane of rotation of two rotor modules 20 on supporting rack 30
With horizontal plane or near normal, before capable of being provided for unmanned plane to thrust, unmanned plane compared with the existing technology passes through
It lifts to for thrust before low head mode obtains, the utility model can effectively increase unmanned plane cruising level flight state acceleration
Energy and max level speed, and improve the preceding response speed to the big minor adjustment of thrust.
Further, above-mentioned unmanned plane further includes the locking device (not shown) for locking above-mentioned supporting rack 30, on
It states locking device to connect with aforementioned body 10, above-mentioned unmanned plane further includes the driving device for controlling the rotation of above-mentioned supporting rack 30
(not shown), above-mentioned locking device, above-mentioned driving device are connect with above-mentioned control system, when needing rotating support 30
When, above-mentioned locking device unlock is first controlled by control system, then the rotation of supporting rack 30 is driven by driving device, to realize branch
The rotation of support 30, when supporting rack 30 turns to required angle, supporting rack 30 is locked by control locking device.
Further, as shown in Fig. 8, Fig. 9 and Figure 10, above-mentioned unmanned plane further includes lift wing module 70, aforementioned body 10
And/or installation position 13 is additionally provided in protect-ing frame structure.Above-mentioned lift wing module 70 is removably mounted on installation position 13.Specifically,
Above-mentioned lift wing module 70 can generate aerodynamic lift, to improve power service efficiency when unmanned plane cruising level flight.It is specific and
Speech, in the present embodiment, above-mentioned lift wing module 70 includes：The lift wing 71, support column 72 and the first driver, above-mentioned support
One end of column 72 is articulated with above-mentioned 71 lower surface of the lift wing and has the second articulated shaft, the other end of above-mentioned support column 72 respectively with
The tail portion of aforementioned body 10 and/or protect-ing frame structure are detachably connected；Above-mentioned first driver is for driving above-mentioned second articulated shaft
Rotation to drive the above-mentioned lift wing 71 to rotate, and then increases or decreases the angle of attack of the above-mentioned lift wing 71 with respect to incoming.On alternatively,
It states lift wing module 70 to be fixedly connected with support column, and lift wing module includes a pneumatic rudder face (not shown), first drives
Dynamic device can drive above-mentioned pneumatic rudder face to deflect downward or upward to increase or decrease the camber of the above-mentioned lift wing 71, above-mentioned pneumatic
Rudder face is articulated with above-mentioned 71 rear of the lift wing.
The unmanned plane of the utility model is detachably arranged at by above-mentioned lift wing module 70 on installation position 13, is needing to hold
It, can be by installing lift wing module 70 additional when row long-distance flight task, and supporting rack is combined to use, form mixing lift cloth
Office, promotes the max level speed of unmanned plane, while promoting the power service efficiency of unmanned plane, to increase the flight of unmanned plane
Voyage.
Further, as shown in Figure 9, Figure 10, above-mentioned unmanned plane further include for by above-mentioned lift wing module 70 with installation
The Quick-dismantle component 80 that position 13 is detachably connected, in the preferred embodiment of one of the utility model, above-mentioned Quick-dismantle component 80
Include fixed card slot in aforementioned body 10 and/or protect-ing frame structure and in above-mentioned lift wing module 70 and for
Above-mentioned fixed card slot coordinates fixed fixed card buckle 81；Alternatively, above-mentioned Quick-dismantle component 80 includes being set to consolidating in aforementioned body 10
Surely 81 are buckled and in above-mentioned lift wing module 70 and for coordinating fixed fixed card slot with above-mentioned fixed card buckle 81.When
Right above-mentioned Quick-dismantle component 80 can also be arranged to other structures, such as be fixed by the connection of Quick Release bolt.It is new in this practicality
In another preferred embodiment of type, above-mentioned Quick-dismantle component 80 includes the movable clamp groove (figure being set in above-mentioned lift wing module 70
In do not show), for the fixed movable block tongue (not shown) of above-mentioned active card cooperation and for driving above-mentioned movable block tongue
It stretches out to lock above-mentioned lift wing module 70 or retract to unlock the switch 91 of above-mentioned lift wing module 70, above-mentioned activity block tongue
In aforementioned body 10.
Further, above-mentioned lift wing module 70 further includes the rudder 74 for assisting control course, and rudder 74 is logical
The rear that third articulated shaft is rotationally connected with support column 72 is crossed, which further includes the second driver, and above-mentioned second
Driver is connect with rudder 74, can be rotated around third articulated shaft with driving direction rudder 74.
Further, above-mentioned mounting base 50 is equipped with the first protection cap (not shown), and above-mentioned first protection cap is for sealing
Above-mentioned first interface is covered, above-mentioned first protection cap has dustproof and waterproof function.Above-mentioned first protection cap is detachably arranged at peace
It fills on seat 50.Alternatively, above-mentioned first protection cap is articulated in above-mentioned mounting base 50.Aforementioned body 10 is equipped with the second protection cap
(not shown), above-mentioned second protection cap equally have dust-proof anti-for covering above-mentioned installation position 13, above-mentioned second protection cap
Water function, above-mentioned second protection cap are detachably arranged in aforementioned body 10；Alternatively, above-mentioned second protection cap is articulated in above-mentioned master
On body 10.
Further, above-mentioned lift wing module 70 is equipped with for realizing that power supply and data communicate slotting with aforementioned body 10
Interface 73, above-mentioned installation position 13 are equipped with the second interface coordinated with the interface 73, and above-mentioned control system passes through the interface 73
It is connect with the first driver and the second driver, thimble or shrapnel is equipped at above-mentioned interface 73 and second interface.Pass through
Interface 73 in second interface thimble or shrapnel contact with each other, realize lift wing module 70 power supply and with main body 10
Data communication connection.
Further, above-mentioned unmanned plane includes the battery for power supply, preferably real in one of the utility model
It applies in example, aforementioned body 10 is equipped with battery mounting bin (not shown), and above-mentioned battery-disassembled is installed on above-mentioned battery installation
In storehouse.Above-mentioned battery there are many different capabilities battery, when unmanned plane execute short distance task when, low capacity can be installed
Battery can install the battery of high power capacity when unmanned plane executes remote task, and the power to optimize unmanned plane uses effect
Rate.In another preferred embodiment of the utility model, aforementioned body 10 is equipped with multiple battery mounting bins, and above-mentioned battery can
Dismounting is installed in the battery mounting bin, can increase and decrease the quantity of battery according to actual needs, when unmanned plane executes short distance task
When, it is possible to reduce number of batteries can increase number of batteries, to reach optimization nothing when unmanned plane executes remote task
The purpose of man-machine power service efficiency.Alternatively, as shown in Figure 11, Figure 12, above-mentioned unmanned plane includes the battery for power supply
1, which is equipped with battery mounting bin (not shown), which is installed in above-mentioned battery mounting bin.The battery 1 wraps
Shell 101 and multiple battery modules 102 are included, each battery modules 102 include one or more battery core units, multiple battery moulds
Group 102 is removably mounted in shell 101.The quantity of above-mentioned battery modules 102 can be set according to actual needs, and work as unmanned plane
When executing short distance task, it is possible to reduce the quantity of battery modules 102 can increase when unmanned plane executes remote task
The quantity of battery modules 102, to achieve the purpose that optimize the power service efficiency of unmanned plane.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
All any modification, equivalent and improvement etc., should be included in the utility model made by within the spirit and principle of utility model
Protection domain within.
Claims (10)
1. unmanned plane, it is characterised in that：The unmanned plane includes main body and rotor module, and the main body is equipped with multiple be used for
The mounting base of the rotor module is installed, the rotor module is removably mounted in the mounting base, is set in the mounting base
It is useful for the first interface of power supply and data communication, the rotor module is equipped with the connector being electrically connected with the first interface.
2. unmanned plane as described in claim 1, it is characterised in that：The quantity of the mounting base is eight, eight installations
Seat is distributed in upper layer and lower layer, and every layer includes four mounting bases.
3. unmanned plane as described in claim 1, it is characterised in that：The unmanned plane further includes supporting rack, and support frame as described above turns
The dynamic connection main body, the mounting base are also provided on support frame as described above.
4. unmanned plane as claimed in claim 3, it is characterised in that：The quantity of the mounting base is eight, works as support frame as described above
When in closed configuration, eight mounting bases are distributed in upper layer and lower layer, and every layer includes four mounting bases；Upper layer its
In two mounting bases be set on support frame as described above, other two mounting base on upper layer is set in the main body,
And four mounting bases of lower layer may be contained in the main body.
5. such as claim 2-4 any one of them unmanned planes, it is characterised in that：The quantity of the rotor module be four, four
A rotor module is respectively arranged in four mounting bases on upper layer；Alternatively, four rotor modules are installed respectively
In in four mounting bases of lower layer；Alternatively, the quantity of the rotor module is eight, eight rotor modules are pacified respectively
Loaded in eight mounting bases.
6. unmanned plane as described in claim 1, it is characterised in that：The mounting base includes pedestal and mounting ring, the seat
Body is connect with the main body, and one end of the mounting ring is connected through a screw thread with the pedestal, the other end of the mounting ring with
The rotor module is connected through a screw thread.
7. unmanned plane as claimed in claim 6, it is characterised in that：One end of the mounting ring is equipped with the first internal thread, described
The other end of mounting ring is equipped with the second internal thread, and the diameter of first internal thread is less than the diameter of second internal thread,
The inner wall of the mounting ring is inwardly convexly equipped with limited step；One end of the pedestal be equipped with for the limited step coordinate into
The flange of row limit, the other end of the pedestal are equipped with the first external screw thread for being connect with first internal screw-thread screw, institute
The end face for stating pedestal is equipped with positioning column；The rotor module is equipped with outside second for being connect with second internal screw-thread screw
Screw thread and for the positioning column cooperation positioning location hole.
8. unmanned plane as described in claim 1, it is characterised in that：The unmanned plane further includes lift wing module, the main body
On be additionally provided with installation position, the lift wing module is removably mounted on the installation position.
9. unmanned plane as claimed in claim 8, it is characterised in that：The unmanned plane further includes for by the lift wing module
The Quick-dismantle component being detachably connected with the installation position, the Quick-dismantle component include be set to the installation position on fixed card slot with
And in the lift wing module and for coordinating fixed fixed card buckle with the fixed card slot；Alternatively, the Quick Release group
Part includes the fixed card buckle being set on the installation position and in the lift wing module and is used for and the fixed card buckle
Coordinate fixed fixed card slot；Alternatively, the Quick-dismantle component include be set to the lift wing module on movable clamp groove, for
The movable clamp groove coordinates fixed movable block tongue and for driving the movable block tongue to stretch out to lock the lift wing mould
Block is retracted to unlock the switch of the lift wing module, and the activity block tongue is set in the main body.
10. unmanned plane as described in claim 1, it is characterised in that：The unmanned plane includes the battery for power supply, described
Main body is equipped with battery mounting bin, and the battery-disassembled is installed in the battery mounting bin；Or the main body is equipped with
Multiple battery mounting bins, the battery-disassembled are installed in the battery mounting bin；Alternatively, the unmanned plane includes
For the battery of power supply, the main body is equipped with battery mounting bin, and the battery is installed in the battery mounting bin；The electricity
Pond includes shell and multiple battery modules, and the multiple battery modules are removably mounted in shell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721828170.4U CN207791163U (en) | 2017-12-22 | 2017-12-22 | Unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721828170.4U CN207791163U (en) | 2017-12-22 | 2017-12-22 | Unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207791163U true CN207791163U (en) | 2018-08-31 |
Family
ID=63280804
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721828170.4U Active CN207791163U (en) | 2017-12-22 | 2017-12-22 | Unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207791163U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111509153A (en) * | 2019-01-31 | 2020-08-07 | 深圳市卓派自动化技术有限公司 | Battery, parcel case, unmanned aerial vehicle, transportation center and automatic access cabinet |
| CN113104458A (en) * | 2020-01-13 | 2021-07-13 | 深圳市卓派自动化技术有限公司 | Battery, cargo container, unmanned aerial vehicle, automatic access cabinet and transfer center |
-
2017
- 2017-12-22 CN CN201721828170.4U patent/CN207791163U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111509153A (en) * | 2019-01-31 | 2020-08-07 | 深圳市卓派自动化技术有限公司 | Battery, parcel case, unmanned aerial vehicle, transportation center and automatic access cabinet |
| CN113104458A (en) * | 2020-01-13 | 2021-07-13 | 深圳市卓派自动化技术有限公司 | Battery, cargo container, unmanned aerial vehicle, automatic access cabinet and transfer center |
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