CN205602086U

CN205602086U - Unmanned vehicles's frame and unmanned vehicles

Info

Publication number: CN205602086U
Application number: CN201620318278.8U
Authority: CN
Inventors: 陈星元; 张永生; 王佳迪; 梁贵彬
Original assignee: Shenzhen Dajiang Innovations Technology Co Ltd
Current assignee: Shenzhen Dajiang Innovations Technology Co Ltd
Priority date: 2016-04-15
Filing date: 2016-04-15
Publication date: 2016-09-28
Anticipated expiration: 2026-04-15

Abstract

The utility model provides a unmanned vehicles's frame, includes: centre frame (1), divide circuit board (2) and fly to control installation component (3), centre frame (1) including the top surface and with the bottom surface that the top surface is relative, divide circuit board (2) to reach locate for one that flies to control in installation component (3) the top surface of centre frame (1), the another one is located the bottom surface of centre frame (1), wherein, centre frame (1) with divide circuit board (2) can dismantle the connection. The embodiment of the utility model provides an unmanned vehicles's frame and unmanned vehicles, because the flight controller unit mount in the top surface or the bottom surface of centre frame, makes the flight controller mounted position confirm, easy installation and maintenance. And the centre frame can be dismantled with branch circuit board to be connected, make and divide circuit board omission knot components are installed on the centre frame, be difficult for impairedly. Dismouting and maintenance and be convenient for.

Description

The frame of unmanned vehicle and unmanned vehicle

Technical field

This utility model relates to vehicle technology field, particularly relates to frame and the unmanned vehicle of a kind of unmanned vehicle.

Background technology

Unmanned vehicle, is a kind of flight instruments being in developing rapidly, its have maneuverability, reaction quickly, unmanned flight, operation require low advantage.At present, the range of unmanned plane has widened military affairs, scientific research, civilian three big fields.Use battery to be powered in unmanned vehicle, use flight controller to control flight.

Unmanned vehicle in the prior art typically uses lithium battery power supply, uses point electricity circuit board distribution electric energy to each rotor.A point electricity circuit board used is sometimes to be installed on the centre frame of aircraft as structural member, sometimes uses simple welding manner that the electric energy of battery is assigned to each rotor.It is installed on the centre frame of aircraft as structural member, when by bigger External Force Acting so that point electricity circuit board is the most impaired, brings unnecessary loss to user.When using simple welding manner, the dismounting of point electricity circuit board and maintenance more inconvenience.

In the prior art, the flight controller of unmanned vehicle needs user to install voluntarily, and installation site is more freely mixed and disorderly, it is not easy to installs and safeguards.

Utility model content

First aspect, this utility model embodiment provides the frame of a kind of unmanned vehicle, including: centre frame, point electricity circuit board and fly to control mounting assembly；

Described centre frame includes end face and the bottom surface relative with described end face；Described centre frame is provided with the battery installation position for installing battery；

Described point of electric circuit board and described in fly to control an end face being located at described centre frame in mounting assembly, another one is located at the bottom surface of described centre frame；

Wherein, described centre frame removably connects with described point of electric circuit board, and described point of electric circuit board includes the substrate for carrying electrical equipment.

Further, the frame of unmanned vehicle as above, described centre frame is connected by connector is fixing with described point of electric circuit board.

Further, the frame of unmanned vehicle as above, described connector include following at least one: threaded fastener, pin, buckle, latch.

Further, the frame of unmanned vehicle as above, described point of electric circuit board is arranged on the bottom surface of described centre frame.

Further, the frame of unmanned vehicle as above, described in fly to control mounting assembly and be fixedly installed on the end face of described centre frame.

Further, the frame of unmanned vehicle as above, also include that resilient cushion member, described resilient cushion member are connected with the substrate of described point of electric circuit board, carry out damping with the substrate to described point of electric circuit board.

Further, the frame of unmanned vehicle as above, the substrate of described point of electric circuit board is provided with cushion hole；

Described resilient cushion member, is removably connected through described cushion hole with described substrate by deformation.

Further, the frame of unmanned vehicle as above, symmetrical structure centered by described substrate, described cushion hole is multiple, and is evenly provided on described substrate along the circumferential direction of described substrate.

Further, the frame of unmanned vehicle as above, described substrate is provided with power control circuit, and multiple electrical interfaces are installed on the substrate, and electrically connect with described power control circuit；

Wherein, described power control circuit is for being controlled the connection in series-parallel relation of multiple batteries, and the total electric energy after the plurality of battery series-parallel connection is distributed to the plurality of electrical interface.

Further, the frame of unmanned vehicle as above, described electrical interface includes power interface and communication interface, and described power interface is for being connected with positive pole and the negative electricity of described battery, and described communication interface is for being connected with the control circuit communication in described battery.

Further, the frame of unmanned vehicle as above, described power interface is spaced apart and arranged in the edge of described substrate.

Further, the frame of unmanned vehicle as above, described communication interface is spaced apart and arranged in the inner side of described power interface along the circumferential direction of described substrate.

Further, the frame of unmanned vehicle as above, described substrate be provided with fly control signaling interface, described in fly control mounting assembly include flight controller, described in fly control signaling interface be connected with described flight controller communication.

Further, the frame of unmanned vehicle as above, described substrate is provided with multiple electricity and adjusts connection terminal, is respectively used to adjust with the electricity on multiple horns electrically connect.

Further, the frame of unmanned vehicle as above, described electricity adjusts connection terminal to include that electricity adjusts signaling interface, for being connected with the communication interface communication of described electricity tune, makes described electricity adjust and is connected with described flight controller communication by a point electricity circuit board.

Further, the frame of unmanned vehicle as above, described electricity is adjusted connection terminal to include electricity tune power supply interface, is electrically connected for the power interface adjusted with electricity, powers for described electric tune.

Further, the frame of unmanned vehicle as above, described substrate is provided with at least one expansion interface, and described expansion interface is for electrically connecting with external equipment.

Further, the frame of unmanned vehicle as above, also include that insulating protective layer, described insulating protective layer are bonded in the lower surface of described substrate；

Offer hollow out window on described insulating protective layer, described hollow out window corresponding with described substrate on fastening connection piece and/or interface.

Further, the frame of unmanned vehicle as above, described in fly to control mounting assembly and also include flying controlling installing plate, described in fly to control installing plate and be fixedly installed on the end face of described centre frame, described flight controller be fixedly installed on described in fly to control the upper surface of installing plate.

Further, the frame of unmanned vehicle as above, described in fly control installing plate include that central plate, described flight controller are fixedly installed on the upper surface of described central plate.

Further, the frame of unmanned vehicle as above, described central plate extends outward multiple side plate, described in fly control installing plate removably connected by side plate with described centre frame.

Further, the frame of unmanned vehicle as above, described in fly to control installing plate and the described centre frame through hole by described side plate and fly control installing plate locking member and carry out being spirally connected fixing.

Further, the frame of unmanned vehicle as above, described flight controller is bonded in the upper surface of described central plate.

Further, the frame of unmanned vehicle as above, described in fly to control mounting assembly and also include flying controlling lock bracket and flying to control locking member；

Described fly control lock bracket described flight controller is pressed on described in fly control installing plate；

Described fly to control locking member by described fly to control lock bracket be removably attached to described in fly to control on installing plate.

Further, the frame of unmanned vehicle as above, the described control lock bracket that flies is connected in sequence by the first side slat, the first top bar, the head and the tail of the second side slat, the lower end of described first side slat and described second side slat is symmetrically arranged with through hole, described first top bar is against the upper surface of described flight controller, described in fly to control locking member through described through hole be locked at described in fly to control the side of installing plate.

Further, the frame of unmanned vehicle as above, also include that the first heat conductive silica gel, described first heat conductive silica gel fly to control between lock bracket and the upper surface of described flight controller described in being arranged on.

Further, the frame of unmanned vehicle as above, described in fly control mounting assembly also include power management module, described power management module electrically connects with described flight controller, described point of electric circuit board respectively.

Further, the frame of unmanned vehicle as above, power management module be fixedly installed on described in fly control installing plate lower section.

Further, the frame of unmanned vehicle as above, the described control mounting assembly that flies also includes power management module installing plate, described power management module installing plate be fixedly installed on described in fly control installing plate lower surface, described power management module is fixedly installed on the lower surface of described power management module installing plate.

Further, the frame of unmanned vehicle as above, the circumferential edge of described power management module installing plate is provided with through hole, and described power management module installing plate flies to control installing plate carry out being spirally connected by through hole and power management module installing plate locking member fixing with described.

Further, the frame of unmanned vehicle as above, described in fly control mounting assembly also include power management module lock bracket and power management module locking member；

Described power management module is pressed on described power management module installing plate by described power management module lock bracket；

Described power management module lock bracket is removably attached on described power management module installing plate by described power management module locking member.

Further, the frame of unmanned vehicle as above, described power management module lock bracket is connected in sequence by the 3rd side slat, the first sill strip, the 4th side slat head and the tail, the upper end of described 3rd side slat and described 4th side slat is symmetrically arranged with through hole, described first sill strip is against the lower surface of described power management module, and described power management module locking member is locked at the side of described power management module installing plate through described through hole.

Further, the frame of unmanned vehicle as above, described power management module installing plate is provided with radiating fin.

Further, the frame of unmanned vehicle as above, also include that the second heat conductive silica gel, described second heat conductive silica gel are arranged between described power management module lock bracket and the lower surface of described power management module.

Further, the frame of unmanned vehicle as above, described power management module also includes plug；

Correspondingly, fly to control mounting assembly described in also to include: plug-locking part and plug-locking part；

Described plug-locking part by described plug-locking part by described plug-locking at the lower surface of described power management module lock bracket.

Further, the frame of unmanned vehicle as above, also include a point electricity circuit board lower cover, described point of electric circuit board lower cover is arranged on the lower section of described point of electricity circuit board, and connects and fixes with described point of electric circuit board.

Further, the frame of unmanned vehicle as above, also include that centre frame upper cover, described centre frame upper cover cover described flight controller, and fixing with described centre frame be connected.

Further, the frame of unmanned vehicle as above, the top of described centre frame upper cover is built-in with radiator fan, and described radiator fan electrically connects with described flight controller.

Further, the frame of unmanned vehicle as above, the side of described radiator fan is provided with air-guiding aisle and vent.

Further, the frame of unmanned vehicle as above, described centre frame covers and on two adjacent with vent side, is respectively arranged with anti-skid structure.

Second aspect, this utility model embodiment provides a kind of unmanned vehicle, including: the frame of the unmanned vehicle described in dynamical system and any of the above-described item；

Wherein, described dynamical system is arranged in the frame of described unmanned vehicle, and electrically connects with described flight controller.

Further, unmanned vehicle as above, the frame of described unmanned vehicle also includes the horn being connected with described centre frame, and described dynamical system includes the power set providing flying power, and described power set are arranged on described horn.

Further, unmanned vehicle as above, described power set include propeller and drive the motor of described propeller rotational.

Further, unmanned vehicle as above, described dynamical system also includes that electricity tune, described electricity are adjusted and electrically connected with described motor, for controlling the duty of motor.

Further, unmanned vehicle as above, described electricity is adjusted and is arranged on multiple horn, and is connected terminal electrical connection with the multiple electricity tune on described substrate respectively.

Further, unmanned vehicle as above, described electricity stealthily substitutes and includes communication interface, and the communication interface that described electricity is adjusted adjusts signaling interface communication to be connected with the electricity on described substrate, makes described electricity adjust by dividing an electric circuit board to be connected with described flight controller communication.

The frame of the unmanned vehicle that this utility model embodiment provides and unmanned vehicle.Frame at unmanned vehicle includes: centre frame, point electricity circuit board and fly control mounting assembly；Central plate includes end face and the bottom surface relative with described end face；Point electricity circuit board and described in fly to control an end face being located at described centre frame in mounting assembly, another one is located at the bottom surface of described centre frame；Centre frame removably connects with described point of electric circuit board.Owing to flight controller assembly is arranged on end face or the bottom surface of centre frame, flight controller installation site is made to determine, it is easy to install and safeguard.And centre frame removably connects with described point of electric circuit board, make a point electricity circuit board be installed on centre frame not as structural member, be difficult to impaired.And it is easy to dismounting and safeguards.

Accompanying drawing explanation

First structural representation of the frame of the unmanned vehicle that Fig. 1 provides for this utility model embodiment one；

Second structural representation of the frame of the unmanned vehicle that Fig. 2 provides for this utility model embodiment one；

First structural representation of point electricity circuit board in the frame of the unmanned vehicle that Fig. 3 provides for this utility model embodiment two；

Second structural representation of point electricity circuit board in the frame of the unmanned vehicle that Fig. 4 provides for this utility model embodiment two；

Flying in the frame of the unmanned vehicle that Fig. 5 provides for this utility model embodiment two controls the structural blast schematic diagram of mounting assembly；

The structural representation of point electricity circuit board lower cover in the frame of the unmanned vehicle that Fig. 6 provides for this utility model embodiment three；

The structural representation of centre frame upper cover in the frame of the unmanned vehicle that Fig. 7 provides for this utility model embodiment four；

The structural representation of the unmanned vehicle that Fig. 8 provides for this utility model embodiment five；

Fig. 9 is the a-quadrant in Fig. 8 and the partial enlarged drawing in B region.

Reference:

null1-centre frame, 2-divides electricity circuit board, 21-substrate, 22-divides electricity circuit board securing member, 23-resilient cushion member, 24-cushion hole, 25-power interface, 26-communication interface, 27-flies to control signaling interface 28-electricity and adjusts signaling interface, 29-electricity adjusts power supply interface, 210-the first expansion interface, 211-the second expansion interface, 212-the 3rd expansion interface, 213-insulating protective layer, 3-flies to control mounting assembly, 31-flight controller, 32-flies to control installing plate, 321-central plate, 322-side plate, 33-flies to control installing plate locking member, 34-double faced adhesive tape, 35-flies to control lock bracket, 36-flies to control locking member, 37-the first heat conductive silica gel 38-power management module, 39-power management module installing plate, 310-power management module installing plate locking member, 311-power management module lock bracket, 312-power management module locking member, 313-radiating fin, 314-the second heat conductive silica gel, 315-plug, 316-plug-locking part, 317-plug-locking part 4-divides electricity circuit board lower cover, 41-buckle, 5-centre frame upper cover, 51-radiator fan, 52-air-guiding aisle, 53-vent, 54-anti-skid structure, 6-horn, 63-motor mount, 7-dynamical system 71-propeller, 72-motor, 73-electricity is adjusted

Detailed description of the invention

Below in conjunction with the accompanying drawing in this utility model embodiment, the technical scheme in this utility model embodiment is clearly and completely described, it is clear that described embodiment is only a part of embodiment of this utility model rather than whole embodiments.Based on the embodiment in this utility model, the every other embodiment that those of ordinary skill in the art are obtained under not making creative work premise, broadly fall into the scope of this utility model protection.

It should be noted that be referred to as " being fixed on " another assembly when assembly, it can be directly on another assembly or can also there is assembly placed in the middle.When an assembly is considered as " connection " another assembly, and it can be directly to another assembly or may be simultaneously present assembly placed in the middle.

Unless otherwise defined, all of technology used herein and scientific terminology are identical with belonging to the implication that those skilled in the art of the present utility model are generally understood that.It is intended merely to describe the purpose of specific embodiment at term used in the description of the present utility model herein, it is not intended that in limiting this utility model.Term as used herein "and/or" includes the arbitrary and all of combination of one or more relevant Listed Items.

Below in conjunction with the accompanying drawings, embodiments more of the present utility model are elaborated.In the case of not conflicting, the feature in following embodiment and embodiment can be mutually combined.

Embodiment one

This utility model embodiment one provides the frame of a kind of unmanned vehicle.First structural representation of the frame of the unmanned vehicle that Fig. 1 provides for this utility model embodiment one, its expression is from the structural representation of the bottom upward of the frame of unmanned vehicle, second structural representation of the frame of the unmanned vehicle that Fig. 2 provides for this utility model embodiment one, its expression is from the structural representation of the overhead view of the frame of unmanned vehicle.The structure of the frame of the unmanned vehicle that this utility model embodiment one provides is not limited to the structure shown in Fig. 1 and Fig. 2.Fig. 1 and Fig. 2 combines the schematic diagram of the simply one of which structure of the frame of unmanned vehicle.

As depicted in figs. 1 and 2, the frame of unmanned vehicle that the present embodiment provides includes: centre frame 1, point electricity circuit board 2 and fly to control mounting assembly 3.

Wherein, centre frame 1 includes end face and the bottom surface relative with end face.Dividing electricity circuit board 2 and fly to control an end face being located at centre frame 1 in mounting assembly 3, another one is located at the bottom surface of centre frame 1；Centre frame 1 removably connects with a point electricity circuit board 2.

In the present embodiment, centre frame 1 can be a structure with cavity, is oppositely arranged including end face and bottom surface, end face and bottom surface.Specifically, centre frame 1 includes upper backup pad, lower supporting plate, multiple dividing plate.Described upper backup pad is arranged with described lower supporting plate relative spacing.The plurality of dividing plate is fixedly connected between described upper backup pad and described lower supporting plate, and jointly surrounds multiple battery compartment for accommodating battery with upper backup pad and lower supporting plate.Certainly, in this utility model, centre frame is not limited to the structure of diagram, it is also possible to for other structures, such as, centre frame is the shell structure of hollow.

In the present embodiment, being provided with the battery installation position for installing battery on centre frame 1, battery installation position is arranged in the particular location the present embodiment on centre frame 1 and does not limits.As it is shown in figure 1, can be by the edge of centrally disposed for battery installation position frame.Battery installation position can be one or more, and when battery installation position is multiple, multiple battery installation positions are spaced apart and arranged in the edge of centre frame.The concrete structure of battery installation position does not limits.As being battery compartment, battery is put in battery compartment.

It is appreciated that and can be located at the end face of centre frame 1 by flying to control mounting assembly 3, point electricity circuit board 2 is located at the bottom surface of centre frame 1.Or, the bottom surface of centre frame 1 can be located at by flying to control mounting assembly 3, point electricity circuit board 2 is located at the end face of centre frame 1.

In the present embodiment, to flying to control mounting assembly 3, divide the particular location of electricity the end face or bottom surface that centre frame 1 be located at by circuit board 2 not to be defined.As mounting assembly 3 can be controlled by flying, divides an electricity circuit board 2 to be oppositely arranged, all it is located at the central region of centre frame 1 end face or bottom surface.Also can control mounting assembly 3 by flying, divide an electricity circuit board 2 not to be oppositely arranged.As can be flown to control the left field of the end face of the centrally disposed frame of mounting assembly 31, by a point right side area for the bottom surface of the electricity centrally disposed frame of circuit board 21.

In the present embodiment, fly to control mounting assembly 3 and can removably connect with centre frame 1.Such as clamping, it is spirally connected.Also non-dismountable connection can be carried out.Such as welding, riveting etc., this is not limited by the present embodiment.

In the present embodiment, centre frame 1 removably connects with a point electricity circuit board 2.As being clamping, be spirally connected.

The frame of unmanned vehicle that the present embodiment provides, including: centre frame 1, point electricity circuit board 2 and fly to control mounting assembly 3.Centre frame 1 includes end face and the bottom surface relative with end face.Dividing electricity circuit board 2 and fly to control an end face being located at centre frame 1 in mounting assembly 3, another one is located at the bottom surface of centre frame 1.Centre frame 1 removably connects with a point electricity circuit board 2.It is arranged on end face or the bottom surface of centre frame 1 owing to flying control mounting assembly 3, makes flight controller installation site determine, it is easy to install and safeguard.And centre frame 1 removably connects with a point electricity circuit board 2, make a point electricity circuit board 2 be installed on centre frame 1 not as structural member, be difficult to impaired.And it is easy to dismounting and safeguards.

Embodiment two

This utility model embodiment two provides the frame of a kind of unmanned vehicle.First structural representation of point electricity circuit board in the frame of the unmanned vehicle that Fig. 3 provides for this utility model embodiment two.It is a point structural blast figure for electricity circuit board 2, the second structural representation of point electricity circuit board in the frame of the unmanned vehicle that Fig. 4 provides for this utility model embodiment two, and it is the upward view of point electricity circuit board 2 after installing.Flying in the frame of the unmanned vehicle that Fig. 5 provides for this utility model embodiment two controls the structural blast schematic diagram of mounting assembly 3.The structure of point electricity circuit board 2 of the frame of the unmanned vehicle that this utility model embodiment two provides is not limited to the structure shown in Fig. 3 and Fig. 4.Fig. 3 and Fig. 4 is the structural representation that one of which divides electricity circuit board 2.The structure flying to control mounting assembly 3 of the frame of the unmanned vehicle that this utility model embodiment two provides is not limited to the structure shown in Fig. 5.As shown in Fig. 3, Fig. 4 and Fig. 5, the present embodiment, on the basis of the technical scheme that embodiment one provides, also includes following characteristics.

Further, in the present embodiment, centre frame 1 is connected by connector is fixing with point electricity circuit board 2.Such as, connector can be threaded fastener, pin, buckle, latch etc..

Specifically, in the present embodiment, centre frame 1 is not limited with the number dividing electricity circuit board 2 to be fixed the connector being connected by connector and position.If connector is one, then connector can be arranged on a point center for the substrate 21 of electricity circuit board 2.Connector is the most multiple, and as in figure 3, centre frame 1 is fixed with point electricity circuit board securing member 22 dividing electricity circuit board 2 to pass through in threaded fastener and is connected.Specifically, multiple through hole can be set in point the circumferentially-spaced of substrate 21 for electricity circuit board 2, by point electricity circuit board securing member 22, a point electricity circuit board 2 is fixed on centre frame 1.The most in the illustrated embodiment, a point electricity circuit board securing member 22 is for installing screw.

In the present embodiment, centre frame 1 is connected by connector is fixing with point electricity circuit board 2.Such as, connector can be threaded fastener, pin, buckle, latch etc..Make centre frame 1 simple with point attachment structure of electricity circuit board 2, it is easy to installation and removal.

Further, in the present embodiment, the bottom surface of centre frame 1 is located at by point electricity circuit board 2, flies to control mounting assembly 3 and is located at the end face of centre frame 1.

Specifically, in the present embodiment, centre frame 1 can be the cavity body structure of cylindricality, is located at the end face of centre frame 1 by flying to control mounting assembly 3, and the bottom surface of centre frame 1 is located at by point electricity circuit board 2.Fly to control mounting assembly 3, divide electricity circuit board 2 to be oppositely arranged on the central area of end face, bottom surface.

In the present embodiment, point electricity circuit board 2 is located at the bottom surface of centre frame 1, flies to control mounting assembly 3 and be located at the end face of centre frame 1, it is simple to divide electricity circuit board and fly to control the connection between mounting assembly and other system and wiring.

Further, the frame of the unmanned vehicle that the present embodiment provides, also include: resilient cushion member 23, resilient cushion member 23 is connected with a point substrate 21 for electricity circuit board 2, so that a point substrate 21 for electricity circuit board 2 is carried out damping.

Specifically, in the present embodiment, resilient cushion member 23 can be made up of silica gel elastomeric material.Resilient cushion member 23 is connected with a point substrate 21 for electricity circuit board 2, specifically can be respectively connected with resilient cushion member 23 above and below at substrate 21.Not interfere with a point electricity circuit board 2 when the frame stress deformation of unmanned vehicle, a point substrate 21 for electricity circuit board 2 is carried out damping.

Preferably, the substrate 21 dividing electricity circuit board 2 is provided with cushion hole 24；Resilient cushion member 23, is removably connected through cushion hole 24 with substrate 21 by deformation.

It is appreciated that symmetrical structure centered by substrate 21, cushion hole 24 are multiple, and is evenly provided on substrate 21 along the circumferential direction of substrate 21.When the frame stress deformation of unmanned vehicle, the stop above and below with resilient cushion member 23 of substrate 21, substrate 21 can be played more effective cushioning effect.

Such as, substrate 21 can be the centrosymmetric structures such as circle, rectangle, rhombus.Certainly, in other embodiments in this utility model, substrate can also be non-centrosymmetric structure, such as, isosceles trapezoidal structure.

Further, in the present embodiment, substrate 21 is provided with power control circuit, and multiple electrical interfaces are installed on the base plate (21, and electrically connect with power control circuit.Wherein, power control circuit is for being controlled the connection in series-parallel relation of multiple batteries, and the total electric energy after multiple battery series-parallel connections is distributed to multiple electrical interface.

Specifically, in the present embodiment, power control circuit distributes according to average voltage, total electric energy is distributed to multiple electrical interface by electric current demand assigned mode.

In the present embodiment, the number of electrical interface can be identical with the number of intelligent battery, the horn of unmanned vehicle, as being six or other numerical value, does not limits in the present embodiment.

In the present embodiment, battery installation position can be set on centre frame, intelligent battery is fixedly installed in battery installation position.

In the present embodiment, multiple electrical interfaces can use dismountable mode to install on the base plate (21, it is possible to uses non-removable mode to install on the base plate (21, does not limits in the present embodiment.

Wherein, electrical interface includes power interface 25 and communication interface 26, and power interface 25 is for being connected with positive pole and the negative electricity of battery, and communication interface 26 is for being connected with the control circuit communication in battery.

It is appreciated that as it is shown on figure 3, in the present embodiment, the anode interface of power interface 25 can be separated with negative pole interface, often group power interface 25 includes positive source interface and power cathode interface, is specifically as follows six groups, and power interface 25 is spaced apart and arranged in the edge of substrate 21.Preferably, power interface 25 can be evenly provided on the edge of substrate 21 by group.Communication interface 26 can also be six, and communication interface 26 is spaced apart and arranged in the inner side of power interface 25 along the circumferential direction of substrate 21.Preferably, communication interface 26 can be evenly provided on the inner side of power interface 25 along the circumferential direction of substrate 21.

Further, in the present embodiment, substrate 21 is provided with and flies to control signaling interface 27, flies to control mounting assembly 3 and includes flight controller 31, flies to control signaling interface 27 and is connected with flight controller 31 communication.

In the present embodiment, fly to control signaling interface 27 and may be provided at the center of substrate 21, reduce the connection difficulty flying to control signaling interface 27 with flight controller 31 to greatest extent.

Further, in the present embodiment, substrate 21 is provided with multiple electricity and adjusts connection terminal, is respectively used to adjust with the electricity on multiple horns electrically connect.Electricity adjusts connection terminal to include that electricity adjusts signaling interface 28, is connected for the communication interface communication adjusted with electricity, makes electric tune be connected with flight controller 31 communication by a point electricity circuit board 2.Electricity adjusts connection terminal to include that electricity adjusts power supply interface 29, electrically connects for the power interface adjusted with electricity, for electricity tune power supply.

In the present embodiment, multiple electricity adjust connection terminal dismountable mode can be used to install on the base plate (21, such as the mode being spirally connected.May be used without non-removable mode and install on the base plate (21, such as the mode of welding, the present embodiment does not limits.

In the present embodiment, connection terminal can be adjusted to be arranged on the lower surface of substrate 21 multiple electricity.Specifically, as shown in Figure 4, electricity can be adjusted power supply interface 29 be disposed on the lower surface of substrate 21 along substrate 21 circumferential direction.Preferably, electricity can be adjusted power supply interface 29 be evenly provided on the lower surface of substrate 21 along substrate 21 circumferential direction.Electricity is adjusted signaling interface 28 be disposed on electricity along substrate 21 circumferential direction and adjusts the inner side of power supply interface 29.Preferably, electricity can be adjusted signaling interface 28 be evenly provided on electricity along substrate 21 circumferential direction and adjust the inner side of power supply interface 29.

In actual applications, user sends control signal by remote controller to flight controller 31, flight controller 31 by flying to control signaling interface 27, electricity adjusts signaling interface 28 to readjust the distribution to electricity to send control signal.Electricity is adjusted to send to the motor that is electrically connected according to control signal and is driven signal, drives the change rotating speed of motor, the parameter such as turns to, to change the kinestate of unmanned vehicle.

Further, in the present embodiment, substrate 21 is provided with at least one expansion interface, and expansion interface is for electrically connecting with external equipment.Such as, expansion interface can externally provide 18 volts, and the DC sources such as 22 volts, the boarded parts for unmanned vehicle is powered

Specifically, in the present embodiment, it is provided with at least one expansion interface on the base plate (21.Expansion interface position is set and the mode that is connected with substrate 21 does not limits.In Fig. 3 and Fig. 4, the first expansion interface 210 and the 3rd expansion interface 212 are arranged on the lower surface of substrate 21, the second expansion interface 211 is arranged on the upper surface of substrate 21.External equipment can be the equipment such as The Cloud Terrace, photographing unit, video camera.

In the present embodiment, substrate 21 is provided with at least one expansion interface, and expansion interface, for electrically connecting with external equipment, reserves external interface for external equipment, it is possible to make unmanned vehicle frame meet different application scenarios.

Further, the frame of the unmanned vehicle that the present embodiment provides, also include insulating protective layer 213, insulating protective layer 213 offer hollow out window, insulating protective layer 213 is bonded in the lower surface of substrate 21.

In the present embodiment, the shape of insulating protective layer 213 is identical with the shape of substrate 21.Insulating protective layer 213 is insulation protection cotton layer.In other embodiments, insulating protective layer 213 can also be electro-insulating rubber layer.

Specifically, in the present embodiment, adjust connection terminal, at least one expansion interface and resilient cushion member 23 owing to being provided with multiple electricity at substrate 21 lower surface, in order to a point electricity circuit board 2 is insulated and protected, at the lower surface bonds insulating protective layer 213 of substrate 21.The hollow out window offered on insulating protective layer 213.Hollow out window can be for interface, connector, resilient cushion member 23 etc..Expose in shape the present embodiment of hollow out window and do not limit.As in the diagram; insulating protective layer 213 generally circular in shape, hollow out window includes arrowhead-shaped hollow out window and from edge to the hollow out window of central concave, and arrowhead-shaped hollow out window is radially distributed on insulating protective layer 213; head is the direction deviating from the center of circle, and afterbody is near the direction in the center of circle.It is to the hollow out window of central concave from edge between adjacent arrowhead-shaped hollow out window.Head at arrow exposes resilient cushion member 23, and the afterbody at arrowhead-shaped hollow out window exposes electricity and adjusts signaling interface 28, adjusts power supply interface 29 exposing electricity from edge to the hollow out window of central concave.

The frame of the unmanned vehicle that the present embodiment provides, also includes insulating protective layer 213, insulating protective layer 213 offers hollow out window, insulating protective layer 213 is bonded in the lower surface of substrate 21.A point electricity circuit board 2 can be insulated and protects, improve a point safety for electricity circuit board 2.

Further, flying to control mounting assembly 3 and also include flying to control installing plate 32, fly to control installing plate 32 and be fixedly installed on the end face of centre frame 1, flight controller 31 is fixedly installed on and flies to control installing plate 32 upper surface.

Specifically, in the present embodiment, fly control installing plate 32 can be removably connected by connector with centre frame 1, connector include following at least one: threaded fastener, pin, buckle 41, latch.Also non-dismountable connection can be carried out, as being welding, riveting etc..Flight controller 31 with the mode of fixing connection flying to control installing plate 32 can be spirally connected, clamping, bonding etc..Fly to control the central region of the end face that installing plate 32 can be fixedly installed on centre frame 1.Flight controller 31 can be fixedly installed on the central region flying to control installing plate 32 upper surface.

Preferably, in the present embodiment, fly to control installing plate 32 and include that central plate 321, flight controller 31 are fixedly installed on the upper surface of central plate 321.Central plate 321 extends outward multiple side plate 322, flies to control installing plate 32 and is removably connected by side plate 322 with centre frame 1.Specifically, fly to control installing plate 32 and the centre frame 1 through hole by side plate 322 and fly control installing plate locking member 33 and carry out being spirally connected fixing.The most in the illustrated embodiment, fly to control installing plate locking member 33 for lock screw.In other embodiments, control installing plate locking member 33 can also be latch, buckle etc..

Preferably, flight controller is bonded in the upper surface of central plate 321.Specifically, as it is shown in figure 5, flight controller 31 can be bonded in the upper surface of central plate 321 by double faced adhesive tape 34.

As it is shown in figure 5, in the present embodiment, the central plate 321 flying to control installing plate 32 is rectangular configuration, and flight controller 31 is rectangular configuration, and flight controller 31 is fixedly installed on the upper surface of central plate 321.Extend four side plates 322 from four sides of central plate 321, each side plate 322 arranges through hole, control installing plate locking member 33 by the through hole of side plate 322 and flying and be fixed on the end face of centre frame 1 by flying to control installing plate 32.

In the present embodiment, fly to control installing plate 32 and include that central plate 321, flight controller 31 are fixedly installed on the upper surface of central plate 321.Central plate 321 extends outward multiple side plate 322, flies to control installing plate 32 and is removably connected by side plate 322 with centre frame 1.Fly to control installing plate 32 and the centre frame 1 through hole by side plate 322 and fly control installing plate locking member 33 and carry out being spirally connected fixing.Flight controller 31 is bonded in the upper surface of central plate 321.Flight controller 31 is made to be more convenient for dismounting and safeguarding.

Further, fly to control mounting assembly 3 also to include flying control lock bracket 35 and fly to control locking member 36.Fly control lock bracket 35 flight controller 31 is pressed on fly control installing plate 32.Fly to control locking member 36 will fly to control lock bracket 35 and be removably attached to fly on control installing plate 32.

Specifically, in the present embodiment, the shape flying to control lock bracket 35 can be configured according to the shape of flight controller 31, and the form fit of flight controller 31, makes to fly to control lock bracket 35 and can be pressed on by flight controller 31 and fly to control on installing plate 32.Flying to control locking member 36 can be threaded fastener, pin, buckle, latch etc..It is removably attached to fly control on installing plate 32 will fly to control lock bracket 35.

Preferably, as shown in Figure 5, in the present embodiment, fly to control lock bracket 35 to be connected in sequence by the first side slat, the first top bar, the head and the tail of the second side slat, the lower end of the first side slat and the second side slat is symmetrically arranged with through hole, first top bar is against the upper surface of flight controller 31, flies to control locking member 36 and is locked at the side flying to control installing plate 32 through through hole.

Specifically, in the present embodiment, fly to control lock bracket 35 and be connected in sequence by the first side slat, the first top bar, the head and the tail of the second side slat.Angle between first side slat and the first top bar is 90 degree, and the angle between the first top bar and the second side slat is 90 degree.Flying to control lock bracket 35 is a frame-shaped construction.Being symmetrically arranged with through hole in the lower end of the first side slat and the second side slat, will fly to control lock bracket 35 and be pressed on flight controller 31, the i.e. first top bar is against the upper surface of flight controller 31, and the first side slat and the second side slat are against the side of flight controller 31.Pass through to fly to control locking member 36 again and be locked at the side flying to control installing plate 32 through through hole.

In the present embodiment, fly to control mounting assembly 3 and also include flying controlling lock bracket 35 and flying to control locking member 36, fly to control lock bracket 35 and flight controller 31 is pressed on flies to control installing plate 32.Fly to control locking member 36 will fly to control lock bracket 35 and be removably attached to fly on control installing plate 32.Make flight controller 31 be more solidly fixed on centre frame 1, and then make the frame of whole unmanned vehicle more firm.

In the present embodiment, fly to control lock bracket 35 and be connected in sequence by the first side slat, the first top bar, the head and the tail of the second side slat.The lower end of the first side slat and the second side slat is symmetrically arranged with through hole, and the first top bar is against the upper surface of flight controller 31, flies to control locking member 36 and is locked at the side flying to control installing plate 32 through through hole.While making flight controller 31 be more solidly fixed on centre frame 1, be more convenient for dismounting and maintenance.

Further, in the frame of the unmanned vehicle that the present embodiment provides, the first heat conductive silica gel 37 is also included.First heat conductive silica gel 37 is arranged on and flies to control between lock bracket 35 and the upper surface of flight controller 31.

In the present embodiment, the first heat conductive silica gel 37 can be to push up the bar strip structure with size with first.First heat conductive silica gel 37 is arranged on and flies to control between lock bracket 35 and the upper surface of flight controller 31; make to fly to control the first of lock bracket 35 to push up between bar and flight controller 31 as non-rigid contact; but carry out excessively by heat conductive silica gel; both ensure that and flight controller 31 can have been locked; the outward appearance of flight controller 31 can be protected again; and can be transmitted to the heat that flight controller 31 produces fly to control on lock bracket 35, strengthen the heat sinking function of flight controller 31.

Further, in the present embodiment, flying to control mounting assembly 3 and also include power management module 38, power management module 38 electrically connects with flight controller 31, a point electricity circuit board 2 respectively.Power management module 38 is fixedly installed on the lower section flying to control installing plate 32.

In the present embodiment, power management module 38 is for being managed the electric energy of multiple intelligent batteries.Dismountable mode can be used to be fixedly installed on the lower section flying to control installing plate 32.Specifically, flying to control mounting assembly 3 and also include that power management module installing plate 39, power management module installing plate 39 are fixedly installed on the lower surface flying to control installing plate 32, power management module 38 is fixedly installed on the lower surface of power management module installing plate 39.

In the present embodiment, power management module installing plate 39 is fixedly installed on the lower surface flying to control installing plate 32 by dismountable mode, specifically may be provided at the lower surface flying to control the central plate 321 of installing plate 32.Power management module 38 is fixedly installed on the lower surface of power management module installing plate 39 by dismountable mode, specifically may be provided at the central area of the lower surface of power management module installing plate 39.

Preferably, as it is shown in figure 5, in the present embodiment, the circumferential edge of power management module installing plate 39 is provided with through hole, and power management module installing plate 39 carries out being spirally connected fixing with flying to control installing plate 32 by through hole and power management module installing plate locking member 310.

Specifically, power management module installing plate 39 can be rectangular configuration, can arrange through hole on each side of power management module installing plate 39, and each power management module installing plate locking member 310 is spirally connected fixing through through hole with flying control installing plate 32.

Further, fly to control mounting assembly 3 and also include power management module lock bracket 311 and power management module locking member 312.Power management module 38 is pressed on power management module installing plate 39 by power management module lock bracket 311.Power management module lock bracket 311 is removably attached on power management module installing plate 39 by power management module locking member 312.

Specifically, in the present embodiment, the shape of power management module lock bracket 311 can be configured according to the shape of power management module 38, with the form fit of power management module 38.Power management module lock bracket 311 is made to be pressed on power management module installing plate 39 by power management module 38.Power management module lock bracket 311 can be threaded fastener, pin, buckle, latch etc..So that power management module lock bracket 311 is removably attached on power management module 38.

Preferably, as it is shown in figure 5, in the present embodiment, power management module lock bracket 311 is connected in sequence by the 3rd side slat, the first sill strip, the 4th side slat head and the tail.The upper end of the 3rd side slat and the 4th side slat is symmetrically arranged with through hole.First sill strip is against the lower surface of power management module 38, and power management module locking member 312 is locked at the side of power management module installing plate 39 through through hole.

Specifically, in the present embodiment, power management module lock bracket 311 is connected in sequence by the 3rd side slat, the first sill strip, the 4th side slat head and the tail.Angle between 3rd side slat and the first sill strip is 90 degree, and the angle between the first sill strip and the 4th side slat is 90 degree.Power management module lock bracket 311 is a frame-shaped construction, it is symmetrically arranged with through hole in the lower end of the 3rd side slat and the 4th side slat, power management module lock bracket 311 is pressed on power management module 38, i.e. first sill strip is against the lower surface of power management module 38, and the 3rd side slat and the 4th side slat are against the side of power management module 38.It is locked at the side of power management module installing plate 39 again through through hole by power management module locking member 312.

In the present embodiment, fly to control mounting assembly 3 and also include power management module lock bracket 311 and power management module locking member 312.Power management module 38 is pressed on power management module installing plate 39 by power management module lock bracket 311.Power management module lock bracket 311 is removably attached on power management module installing plate 39 by power management module locking member 312.Make power management module 38 be more solidly fixed to fly control on installing plate 32, and then make the frame of whole unmanned vehicle more firm.

In the present embodiment, power management module lock bracket 311 is connected in sequence by the 3rd side slat, the first sill strip, the 4th side slat head and the tail.The upper end of the 3rd side slat and the 4th side slat is symmetrically arranged with through hole.First sill strip is against the lower surface of power management module 38.Power management module locking member 312 is locked at the side of power management module installing plate 39 through through hole.While making power management module 38 be more solidly fixed to fly to control on installing plate 32, be more convenient for dismounting and maintenance.

Further, power management module installing plate 39 is provided with radiating fin 313.

Specifically, in the present embodiment, radiating fin 313 can be set the upper surface on power management module installing plate 39, it is possible to be respectively provided with radiating fin 313 in upper and lower surface.

In the present embodiment, power management module installing plate 39 is provided with radiating fin 313, improves the radiating effect of power management module 38.

Further, the frame of the unmanned vehicle that the present embodiment provides, also include that the second heat conductive silica gel 314, the second heat conductive silica gel 314 are arranged between the lower surface of power management module lock bracket 311 and power management module 38.

Specifically, the second heat conductive silica gel 314 can be with the strip structure of size with the first sill strip.Second heat conductive silica gel 314 is arranged between the lower surface of power management module lock bracket 311 and power management module 38; make between the first sill strip of power management module lock bracket 311 and power management module 38 as non-rigid contact; but carry out excessively by heat conductive silica gel; both ensure that and power management module 38 can have been locked; the outward appearance of power management module 38 can be protected again; and the heat that power management module 38 produces can be transmitted on power management module lock bracket 311, strengthen the heat sinking function of power management module 38.

Further, the frame of the unmanned vehicle that the present embodiment provides, power management module 38 also includes plug 315.Correspondingly, fly to control mounting assembly 3 also to include: plug-locking part 316 and plug-locking part 317.Plug 315 is locked at the lower surface of power management module lock bracket 311 by plug-locking part 317 by plug-locking part 316.

Specifically, as it is shown in figure 5, in the present embodiment, the plug 315 that power management module 38 extends is a part of unsettled, in order to plug 315 is protected, fly to control mounting assembly 3 and also include: plug-locking part 316 and plug-locking part 317.Plug 315 is locked at the lower surface of power management module lock bracket 311 by plug-locking part 317 by plug-locking part 316.

Embodiment three

This utility model embodiment three provides the frame of a kind of unmanned vehicle.The structural representation of point electricity circuit board lower cover in the frame of the unmanned vehicle that Fig. 6 provides for this utility model embodiment three.As shown in Figure 6, the present embodiment is on the basis of the technical scheme that embodiment one or embodiment two provide, the further refinement to the rack construction of unmanned vehicle.Then the frame of the unmanned vehicle that the present embodiment provides, also includes following structure.

Further, the frame of the unmanned vehicle that the present embodiment provides, also include a point electricity circuit board lower cover 4.Divide electricity circuit board lower cover 4 to be arranged on a point lower section for electricity circuit board 2, and connect and fix with a point electricity circuit board 2.

Specifically, in the present embodiment, the shape of point electricity circuit board lower cover 4 does not limits, only need to be with a point form fit for electricity circuit board 2.One or more buckle 41 can be set up week in point inner side of electricity circuit board lower cover 4, by buckle 41, point electricity circuit board 2 lower cover is fixedly installed on point the lower section of electric circuit board 2.

The frame of the unmanned vehicle that the present embodiment provides, also includes a point electricity circuit board lower cover 4.Divide electricity circuit board lower cover 4 to be arranged on a point lower section for electricity circuit board 2, and connect and fix with a point electricity circuit board 2.A point electricity circuit board 2 can be protected further, prevent point electricity circuit board 2 impaired.

Embodiment four

This utility model embodiment four provides the frame of a kind of unmanned vehicle.The structural representation of centre frame upper cover in the frame of the unmanned vehicle that Fig. 7 provides for this utility model embodiment four.As it is shown in fig. 7, the present embodiment is on the basis of the technical scheme of embodiment one or embodiment two or embodiment three offer, the further refinement to the rack construction of unmanned vehicle.Then the frame of the unmanned vehicle that the present embodiment provides, also includes following structure.

Further, the frame of unmanned vehicle that the present embodiment provides, also include that centre frame upper cover 5, centre frame upper cover 5 cover flight controller 31, and fixing with centre frame 1 be connected.

Specifically, the shape of centre frame upper cover 5 does not limits, and only need to be shaped as rectangle with the form fit of flight controller 31 such as flight controller 31, then the shape of centre frame upper cover 5 can be hexagon.Centre frame upper cover 5 covers flight controller 31, can carry out dismountable connection with centre frame 1.As can be spirally connected, clamping etc..

The frame of unmanned vehicle that the present embodiment provides, also includes that centre frame upper cover 5, centre frame upper cover 5 cover flight controller 31, and fixing with centre frame 1 is connected.Flight controller 31 can be protected, prevent flight controller 31 impaired.

Further, the top of centre frame upper cover 5 is built-in with radiator fan, and radiator fan 51 electrically connects with flight controller 31.The side of radiator fan is provided with air-guiding aisle 52 and vent 53.

Specifically, as it is shown in fig. 7, can electrically connect with flight controller 31 at the built-in radiator fan in the top of the upper cover of centre frame 1, radiator fan 51, to obtain electric energy from flight controller 31.A side of radiator fan is provided with air-guiding aisle 52, vent 53 is set in the side of air-guiding aisle 52 outside bearing of trend.Flight controller 31 effectively can be dispelled the heat.

Further, two adjacent with vent 53 on centre frame upper cover 5 sides are respectively arranged with anti-skid structure 54.

Specifically, in the present embodiment, can be anti-skidding salient point or other anti-skid structures at anti-skid structure 54, the present embodiment does not limits.

In the present embodiment, two sides adjacent with vent 53 on centre frame upper cover 5 are respectively arranged with anti-skid structure 54, are more convenient for centre frame upper cover 5 is dismounted and safeguarded.

Embodiment five

This utility model embodiment five provides a kind of unmanned vehicle.The structural representation of the unmanned vehicle that Fig. 8 provides for this utility model embodiment five.As shown in Figure 8, the unmanned vehicle that the present embodiment provides includes: the frame of the unmanned vehicle that dynamical system and any of the above-described embodiment provide.

Wherein, dynamical system is arranged in the frame of unmanned vehicle, and electrically connects with flight controller.

In the present embodiment, the 26S Proteasome Structure and Function of the frame of the unmanned vehicle in unmanned vehicle is identical with the 26S Proteasome Structure and Function of the frame of the unmanned vehicle in any embodiment in embodiment one to embodiment four, and this is no longer going to repeat them.

In the present embodiment, dynamical system is arranged in the frame of unmanned vehicle, and electrically connects with flight controller.In practicing, user sends control signal by remote controller to flight controller, flies to control controller and controls the parameter in dynamical system according to control signal, to change the kinestate of unmanned vehicle.

The unmanned vehicle that the present embodiment provides, including: the frame of the unmanned vehicle that dynamical system 7 and any of the above-described embodiment provide.Wherein, dynamical system 7 is arranged in the frame of unmanned vehicle, and electrically connects with flight controller.Frame at unmanned vehicle includes: centre frame, point electricity circuit board and fly control mounting assembly；Central plate includes end face and the bottom surface relative with described end face；Point electricity circuit board and described in fly to control an end face being located at described centre frame in mounting assembly, another one is located at the bottom surface of described centre frame；Centre frame removably connects with described point of electric circuit board.Owing to flight controller assembly is arranged on end face or the bottom surface of centre frame, flight controller installation site is made to determine, it is easy to install and safeguard.And centre frame removably connects with described point of electric circuit board, make a point electricity circuit board be installed on centre frame not as structural member, be difficult to impaired.And it is easy to dismounting and safeguards.

Further, the frame of unmanned vehicle also includes the horn 6 being connected with centre frame 1, and dynamical system 7 includes the power set providing flying power, and power set are arranged on horn 6.

Specifically, in the present embodiment, in the frame of unmanned vehicle, centre frame 1 can carry out dismountable connection with horn 6.As being connected by connector is fixing with horn 6 by centre frame 1.Connector can be threaded fastener, pin, buckle, in latch any one.Dynamical system 7 includes that power set, power set are arranged on horn 6, does not limits in concrete mounting means the present embodiment.

Further, power set include propeller 71 and the motor 72 driving propeller 71 to rotate.Specifically, in the present embodiment, propeller 71 and the motor 72 driving propeller 71 to rotate may be provided at the end of each horn 6.

Further, dynamical system 7 also includes that electricity adjusts 73, and electricity adjusts 73 to electrically connect with motor 72, for controlling the duty of motor 72.Specifically, in the present embodiment, electricity adjusts 73 to electrically connect with motor 72, for controlling the duty of motor 72, as controlled the rotating speed of motor 72, turning to.Concrete motor 72 is arranged on motor cabinet in the illustrated embodiment, and motor mount 63 is fixed on horn 6, and electricity adjusts 73 to be arranged in motor mount 63.

Further, the a-quadrant during Fig. 9 is Fig. 8 and the partial enlarged drawing in B region.As it is shown in figure 9, described electricity adjusts 73 to be arranged on multiple horn, and 73 are adjusted to be connected terminal electrical connection with the multiple electricity on described substrate respectively.Electricity tune 73 includes that communication interface, described electricity adjust the communication interface of 73 to adjust signaling interface 28 communication to be connected with the electricity on described substrate, makes described electric tune be connected with the communication of described flight controller 31 by a point electricity circuit board 2.Electricity is stealthily substituted and is included power interface, and the power interface that described electricity is adjusted adjusts power supply interface 29 to electrically connect with the electricity on described substrate 21, adjusts power supply for described electricity.

Specifically, in the present embodiment, can arrange electricity tune on multiple horns 6, electricity is adjusted to adjust with the electricity on substrate respectively and is connected terminal electrical connection.It is appreciated that, it is provided with communication interface and power interface on electricity is adjusted, the electricity being provided with on the base plate (21 adjusts the electricity connecting in terminal to adjust signaling interface 28 to adjust the communication interface communication being provided with to be connected with electricity, makes electricity adjust and is connected with flight controller 31 communication by a point electricity circuit board 2.The electricity that substrate 21 is provided with adjusts the electricity connecting in terminal to adjust power supply interface 29 to adjust the power interface being provided with to electrically connect with electricity, adjusts power supply for electricity.

In the unmanned vehicle provided in the present embodiment, the electricity on substrate 21 adjusts the set-up mode connecting terminal identical with embodiment two, does not repeats them here, and does not limits in set-up mode the present embodiment of the electric communication interface adjusted and power interface.

The unmanned vehicle that the present embodiment provides, electricity is adjusted and is arranged on multiple horn, and is connected terminal electrical connection with the multiple electricity tune on described substrate respectively.Electricity is stealthily substituted and is included communication interface, and the communication interface 71 that described electricity is adjusted adjusts signaling interface 28 communication to be connected with the electricity on described substrate, makes described electricity adjust and is connected with the communication of described flight controller 31 by a point electricity circuit board 2.Electricity is stealthily substituted and is included power interface, and the power interface 72 that described electricity is adjusted adjusts power supply interface 29 to electrically connect with the electricity on described substrate 21, adjusts power supply for described electricity.The layout making whole unmanned vehicle is compacter, and then makes unmanned vehicle have more preferable stability.

The foregoing is only embodiment of the present utility model; not thereby the scope of the claims of the present utility model is limited; every equivalent structure utilizing this utility model description and accompanying drawing content to be made or equivalence flow process conversion; or directly or indirectly it is used in other relevant technical fields, the most in like manner it is included in scope of patent protection of the present utility model.

Last it is noted that various embodiments above is only in order to illustrate the technical solution of the utility model, it is not intended to limit；Although this utility model being described in detail with reference to foregoing embodiments, it will be understood by those within the art that: the technical scheme described in foregoing embodiments still can be modified by it, or the most some or all of technical characteristic is carried out equivalent；And these amendments or replacement, do not make the essence of appropriate technical solution depart from the scope of this utility model each embodiment technical scheme.

Claims

1. the frame of a unmanned vehicle, it is characterised in that including: centre frame, point electricity circuit board and fly control mounting assembly；

The frame of unmanned vehicle the most according to claim 1, it is characterised in that described centre frame is connected by connector is fixing with described point of electric circuit board.

The frame of unmanned vehicle the most according to claim 1, it is characterised in that described point of electric circuit board is arranged on the bottom surface of described centre frame, described in fly to control mounting assembly and be fixedly installed on the end face of described centre frame.

The frame of unmanned vehicle the most according to claim 3, it is characterised in that also include that resilient cushion member, described resilient cushion member are connected with the substrate of described point of electric circuit board, carry out damping with the substrate to described point of electric circuit board.

The frame of unmanned vehicle the most according to claim 4, it is characterised in that the substrate of described point of electric circuit board is provided with cushion hole；

The frame of unmanned vehicle the most according to claim 5, it is characterised in that symmetrical structure centered by described substrate, described cushion hole is multiple, and is evenly provided on described substrate along the circumferential direction of described substrate.

The frame of unmanned vehicle the most according to claim 1, it is characterised in that described substrate is provided with power control circuit, multiple electrical interfaces are installed on the substrate, and electrically connect with described power control circuit；

The frame of unmanned vehicle the most according to claim 7, it is characterized in that, described electrical interface includes power interface and communication interface, and described power interface is for being connected with positive pole and the negative electricity of described battery, and described communication interface is for being connected with the control circuit communication in described battery.

The frame of unmanned vehicle the most according to claim 8, it is characterised in that described power interface is spaced apart and arranged in the edge of described substrate；

Described communication interface is spaced apart and arranged in the inner side of described power interface along the circumferential direction of described substrate.

The frame of unmanned vehicle the most according to claim 1, it is characterised in that described substrate be provided with fly control signaling interface, described in fly control mounting assembly include flight controller, described in fly control signaling interface be connected with described flight controller communication.

The frame of 11. unmanned vehicles according to claim 10, it is characterised in that described substrate is provided with multiple electricity and adjusts connection terminal, is respectively used to adjust with the electricity on multiple horns electrically connect.

The frame of 12. unmanned vehicles according to claim 11, it is characterized in that, described electricity adjusts connection terminal to include that electricity adjusts signaling interface, for being connected with the communication interface communication of described electricity tune, makes described electricity adjust and is connected with described flight controller communication by a point electricity circuit board；

Or/and, described electricity adjusts connection terminal to include electricity tune power supply interface, electrically connects for the power interface adjusted with electricity, powers for described electric tune.

The frame of 13. unmanned vehicles according to claim 1, it is characterised in that described substrate is provided with at least one expansion interface, described expansion interface is for electrically connecting with external equipment.

The frame of 14. unmanned vehicles according to claim 1, it is characterised in that also include that insulating protective layer, described insulating protective layer are bonded in the lower surface of described substrate；

The frame of 15. unmanned vehicles according to claim 1, it is characterized in that, described fly to control mounting assembly and also include flying controlling installing plate, described in fly to control installing plate and be fixedly installed on the end face of described centre frame, described flight controller be fixedly installed on described in fly to control the upper surface of installing plate.

The frame of 16. unmanned vehicles according to claim 15, it is characterised in that described in fly control installing plate include that central plate, described flight controller are fixedly installed on the upper surface of described central plate.

The frame of 17. unmanned vehicles according to claim 16, it is characterised in that described central plate extends outward multiple side plate, described in fly control installing plate removably connected by side plate with described centre frame.

The frame of 18. unmanned vehicles according to claim 17, it is characterised in that described in fly to control installing plate and described centre frame and by described side plate and fly control installing plate locking member and be fixed.

The frame of 19. unmanned vehicles according to claim 18, it is characterised in that described flight controller is bonded in the upper surface of described central plate.

The frame of 20. unmanned vehicles according to claim 19, it is characterised in that described in fly to control mounting assembly and also include flying controlling lock bracket and flying to control locking member；

The frame of 21. unmanned vehicles according to claim 20, it is characterised in that also include that the first heat conductive silica gel, described first heat conductive silica gel fly to control between lock bracket and the upper surface of described flight controller described in being arranged on.

22. according to the frame of the unmanned vehicle described in any one of claim 15-21, it is characterised in that described in fly to control mounting assembly and also include power management module, described power management module electrically connects with described flight controller, described point of electric circuit board respectively；

Described power management module be fixedly installed on described in fly control installing plate lower section.

23. according to the frame of unmanned vehicle described in claim 22, it is characterized in that, the described control mounting assembly that flies also includes power management module installing plate, described power management module installing plate be fixedly installed on described in fly control installing plate lower surface, described power management module is fixedly installed on the lower surface of described power management module installing plate.

24. according to the frame of unmanned vehicle described in claim 23, it is characterized in that, the circumferential edge of described power management module installing plate is provided with through hole, and described power management module installing plate flies to control installing plate carry out being spirally connected by through hole and power management module installing plate locking member fixing with described.

25. according to the frame of unmanned vehicle described in claim 24, it is characterised in that described in fly to control mounting assembly and also include power management module lock bracket and power management module locking member；

26. according to the frame of unmanned vehicle described in claim 23, it is characterised in that be provided with radiating fin on described power management module installing plate.

27. according to the frame of unmanned vehicle described in claim 26, it is characterised in that also include that the second heat conductive silica gel, described second heat conductive silica gel are arranged between described power management module lock bracket and the lower surface of described power management module.

28. according to the frame of unmanned vehicle described in claim 27, it is characterised in that described power management module also includes plug；

29. according to the frame of the unmanned vehicle described in any one of claim 23-28, it is characterised in that also include a point electricity circuit board lower cover, and described point of electric circuit board lower cover is arranged on the lower section of described point of electricity circuit board, and connects and fixes with described point of electric circuit board.

The frame of 30. unmanned vehicles according to claim 29, it is characterised in that also include that centre frame upper cover, described centre frame upper cover cover described flight controller, and fixing with described centre frame be connected.

The frame of 31. unmanned vehicles according to claim 30, it is characterised in that the top of described centre frame upper cover is built-in with radiator fan, described radiator fan electrically connects with described flight controller.

The frame of 32. unmanned vehicles according to claim 31, it is characterised in that the side of described radiator fan is provided with air-guiding aisle and vent.

The frame of 33. unmanned vehicles according to claim 32, it is characterised in that cover on described centre frame and be respectively arranged with anti-skid structure on two adjacent with vent side.

34. 1 kinds of unmanned vehicles, it is characterised in that including: the frame of the unmanned vehicle described in dynamical system and any one of claim 1-33；