CN206520750U - Unmanned vehicle - Google Patents

Abstract

The utility model discloses a kind of unmanned vehicle, it includes fuselage and battery module.Fuselage includes the bottom towards ground.Battery module includes battery, and battery has the top relative with bottom, and top is arranged at bottom part down, and battery module is electrically connected with bottom, so as to be powered for unmanned vehicle.In the unmanned vehicle of the utility model embodiment, the bottom that battery module is arranged on fuselage advantageously reduces the center of gravity of unmanned vehicle, to improve the wind resistance of unmanned vehicle.

Description

Unmanned vehicle

Technical field

The utility model is related to unmanned vehicle field, more particularly to a kind of unmanned vehicle.

Background technology

The battery of existing unmanned vehicle is inserted on the fuselage of unmanned vehicle, and this results in unmanned vehicle Center of gravity is higher, and wind resistance is weaker.

Utility model content

The utility model provides a kind of unmanned vehicle.

The unmanned vehicle of the utility model embodiment includes fuselage and battery module.The fuselage is included towards ground Bottom.The battery module includes battery, and the battery has the top relative with the bottom, and the top is arranged at institute Bottom part down is stated, battery module is electrically connected with bottom, so as to be powered for unmanned vehicle.

In the unmanned vehicle of the utility model embodiment, the bottom part down that battery is arranged on fuselage advantageously reduces nothing The center of gravity of people's aircraft, to improve the wind resistance of unmanned vehicle, in addition, so installing battery without being opened up on fuselage Patchhole so that unmanned vehicle makes simple.

In some embodiments, the battery module includes battery connecting seat, and the battery connecting seat is connected to described The bottom of fuselage, the battery connecting seat constitutes the battery compartment for housing the battery with the bottom.

In some embodiments, the battery is longitudinally arranged at the bottom along the roll axle of the fuselage.

In some embodiments, the fuselage is more than the battery mould towards the projected area in the battery module direction The projected area of block downward.

In some embodiments, it is provided with circuit board and electric connector, the battery and sets on the battery connecting seat There is electric connection terminal, the electric connection terminal butts up against the electric connector so that the battery is electrically connected with the battery connecting seat Connect, the circuit board is electrically connected to the fuselage.

In some embodiments, the battery connecting seat includes connecting portion and supporting part, and the circuit board is arranged at institute State in connecting portion, the supporting part is parallel with the bottom of the fuselage, and the battery compartment is formed at the supporting part and the machine Between the bottom of body.

In some embodiments, the battery can be slidably arranged in the battery compartment along the roll axle of the fuselage In.

In some embodiments, the bottom of the supporting part is provided with ultrasonic sensor and/or binocular vision sensing Device.

In some embodiments, power switch and/or indicator lamp are provided with the connecting portion.

In some embodiments, the unmanned vehicle includes the head for being arranged on the bottom, the head and institute State battery module and be located at the relative both sides of the fuselage respectively.

In some embodiments, the head is located at the front side of the bottom, and the battery module is located at the bottom Rear side.

In some embodiments, the quantity of the head is two, and two heads are disposed in parallel in the fuselage The same side.

In some embodiments, it is equiped with load on the head.

In some embodiments, the battery module includes the bottom opposite with the top, in the unmanned flight On the flying height direction of device, the bottom is higher than the load.

In some embodiments, the load includes camera.

In some embodiments, the load can be relative to the head around the 360 ° of rotations of course axle.

Additional aspect and advantage of the present utility model will be set forth in part in the description, partly by from following description In become obvious, or by it is of the present utility model practice recognize.

Brief description of the drawings

Of the present utility model above-mentioned and/or additional aspect and advantage are from description of the accompanying drawings below to embodiment is combined It will be apparent and be readily appreciated that, wherein：

Fig. 1 is the side schematic view of the unmanned vehicle of the utility model embodiment；

Fig. 2 is the schematic top plan view of Fig. 1 unmanned vehicle；

Fig. 3 is the side schematic view of the battery module of the unmanned vehicle of embodiment of the present invention；

Fig. 4 is the schematic bottom view of the battery module of the unmanned vehicle of embodiment of the present invention.

Main element symbol description：

Unmanned vehicle 100, roll axle 102, course axle 104；

Fuselage 10, bottom 11, upper casing 12, lower casing 13；

Horn 20；

Rotor assemblies 30, motor 31, propeller 32；

Battery module 40, top 41, bottom 42, battery 43, battery connecting seat 44, connecting portion 441, supporting part 442, battery Storehouse 45, switch 46, indicator lamp 47, ultrasonic sensor 48, vision sensor 49；

Head 50, connector 51, support 52；

Load 60.

Embodiment

Embodiment of the present utility model is described below in detail, the example of the embodiment is shown in the drawings, wherein Same or similar label represents same or similar element or the element with same or like function from beginning to end.Lead to below It is exemplary to cross the embodiment being described with reference to the drawings, and is only used for explaining the utility model, and it is not intended that to this practicality New limitation.

In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " length ", " width Degree ", " thickness ", " on ", " under ", "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outer ", The orientation or position relationship of the instructions such as " clockwise ", " counterclockwise " be based on orientation shown in the drawings or position relationship, be only for It is easy to description the utility model and simplifies describe, rather than to indicate or imply that signified device or element must have specific Orientation, with specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " first ", " second " is only used for describing purpose, and it is not intended that indicating or implying relative importance or imply the technology indicated by indicating The quantity of feature.Thus, " first " is defined, the feature of " second " can be expressed or implicitly include one or more The feature.In description of the present utility model, " multiple " are meant that two or more, unless otherwise clearly specific Limit.

, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly Connection；It can be mechanical connection or electrical connection or can mutually communicate；Can be joined directly together, can also be in Between medium be indirectly connected to, can be connection or the interaction relationship of two elements of two element internals.For this area For those of ordinary skill, concrete meaning of the above-mentioned term in the utility model can be understood as the case may be.

In the utility model, unless otherwise clearly defined and limited, fisrt feature second feature it " on " or it " under " can directly be contacted including the first and second features, it is not direct contact but logical that can also include the first and second features The other characterisation contact crossed between them.Moreover, fisrt feature second feature " on ", " top " and " above " include the One feature is directly over second feature and oblique upper, or is merely representative of fisrt feature level height higher than second feature.First is special Levy second feature " under ", " lower section " and " below " include fisrt feature immediately below second feature and obliquely downward, or only Represent that fisrt feature level height is less than second feature.

Following disclosure provides many different embodiments or example is used for realizing different structure of the present utility model. In order to simplify disclosure of the present utility model, hereinafter the part and setting of specific examples are described.Certainly, they are only Example, and purpose does not lie in limitation the utility model.In addition, the utility model can in different examples repeat reference numerals And/or reference letter, this repetition is for purposes of simplicity and clarity, discussed various embodiments itself not to be indicated And/or the relation between setting.In addition, various specific techniques and the example of material that the utility model is provided, but this Field those of ordinary skill can be appreciated that the application of other techniques and/or the use of other materials.

Also referring to Fig. 1 and Fig. 2, the unmanned vehicle 100 of the utility model embodiment is rotor unmanned aircraft, Unmanned vehicle 100 can in the air fly, hover to perform specific task, for example, flying, following the trail of, monitor, explore, searching Rescue, sow, spray insecticide, put out a fire, take photo by plane.Predetermined functional module can be carried on unmanned vehicle 100, for example, sensing Device, capture apparatus, medicine-chest etc., to realize specific function.

The unmanned vehicle 100 of the utility model embodiment includes fuselage 10, horn 20, rotor assemblies 30, battery mould Block 40 and head 50.Horn 20 is protruding from fuselage 10, and rotor assemblies 30 are arranged on horn 20, and positioned at the week of fuselage 10 Enclose.

In present embodiment, unmanned vehicle 100 is four rotor unmanned aircrafts, accordingly, the quantity of rotor assemblies 30 For four.Four rotor assemblies 30 are centrosymmetric distribution around the vertical centre axis of fuselage 10, so that unmanned vehicle 100 flies Row balance.

It is appreciated that in other embodiment, the quantity of rotor assemblies 30 can count for other according to the actual requirements Amount.For example, the quantity of rotor assemblies 30 is one, two, three, six, the quantity such as eight.

Fuselage 10 is the bearing part of unmanned vehicle 100, on fuselage 10 or inside can carry sensor, circuit board, The elements such as central processing unit, communication module.Fuselage 10 can reduce air drag during flight with streamlined.At other Embodiment, fuselage 10 can be other shapes, such as polygon, circle, ellipse.

Fuselage 10 includes the bottom 11 towards ground.It is appreciated that during 100 normal flight of unmanned vehicle, bottom 11 with Ground is relative.The surface on bottom 11 towards ground can be plane, or curve.In present embodiment, the direction of bottom 11 The surface on ground is plane.

In present embodiment, fuselage 10 includes upper casing 12 and lower casing 13.It is appreciated that upper casing 12 is engaged with lower casing 13. Upper casing 12 can be fixed together with lower casing 13 by connected modes such as snap, thread connecting modes, upper casing 12 and lower casing 13 combinations can form the inner space of fuselage 10.Lower casing 13 includes the bottom 11 of fuselage 10, therefore, and battery module 40 is connected to Lower casing 13.

Horn 20 is used to support rotor assemblies 30 and make rotor assemblies 30 be distributed in around fuselage 10 with predetermined pattern.This In embodiment, the quantity of horn 20 is four, and each horn 20 supports a rotor assemblies 30.The one of each horn 20 End connection fuselage 10, other end support rotor assemblies 30.

Rotor assemblies 30 include motor 31 and propeller 32.Motor 31 is arranged on horn 20, propeller 32 and motor 31 Connection.It is appreciated that motor 31 operationally can drive propeller 32 to rotate, so as to drive unmanned vehicle 100 to fly.

In present embodiment, battery module 40 is rectangular parallelepiped structure, and battery module 40 includes top 41 and bottom 42.Battery The top 41 of module 40 and the bottom 11 of fuselage 10 are relative, and the bottom 42 of battery module 40 is opposite with top 41 and towards ground. The top 41 of battery module 40 is connected with the bottom 11 of fuselage 10.The top 41 of such as battery module 40 and the bottom 11 of fuselage 10 It can be connected by guide rail structure or buckle structure is connected etc. that the structure that can dismantle connects to facilitate battery module 40 can be from Dismounted on fuselage 10.In some embodiments, battery module 40 can also be cylindrical structure, tri-prismoid structure, ellipse Column structure or be section in column structure of other regular polygons etc..

In some embodiments, fuselage 10 is more than the direction of battery module 40 towards the projected area in the direction of battery module 40 The projected area of lower section.In other words, the size of fuselage 10 is larger.

Battery module 40 is installed and is conducive to balancing the center of gravity of unmanned vehicle 100 for convenience, and battery module 40 is along machine The roll axle 102 of body 10 is connected to the bottom 11 of fuselage 10.Fore-and-aft direction extension of the roll axle 102 along unmanned vehicle 100.Can To understand, the forward direction of unmanned vehicle 100 is the direction that the flight of unmanned vehicle 100 is advanced, and the backward of unmanned vehicle 100 is With before unmanned vehicle 100 in the opposite direction.

Unmanned vehicle 100 can be tilted with change of flight posture during flight around roll axle 102.For example, nothing Turning flight can be realized with roll during the flight of people's aircraft 100.

Specifically, incorporated by reference to Fig. 3 and Fig. 4, battery module 40 includes battery 43, battery connecting seat 44, switch 46, indicator lamp 47th, ultrasonic sensor 48 and vision sensor 49.

Battery 43 has the top 41 relative with the bottom 11 of fuselage 10, and top 41 is arranged under the bottom 11 of fuselage 10 Side.Roll axle 102 of the longitudinal direction of battery 43 along fuselage 10 is arranged at the bottom 11 of fuselage 10, and thus, battery can be rotor assemblies 30 provide electric energy, to drive unmanned vehicle 100 to fly.

Battery connecting seat 44 is connected to the bottom 11 of fuselage 10, and battery connecting seat 44 is constituted for housing battery with bottom 11 43 battery compartment 45.The longitudinal direction of battery 43 is arranged in battery compartment 45 along the roll axle 102 of fuselage 10.

In one example, circuit board (not shown) and electric connector (not shown) are provided with battery connecting seat 44, electricity Pond 43 is provided with electric connection terminal (not shown), and electric connection terminal butts up against electric connector so that battery 43 and battery connecting seat 44 Electrical connection.For example, electric connector may include metal insert, the connection terminal of battery 43 may include and inserting that metal insert coordinates Mouthful, when installing battery 43, the socket of connection terminal can be made to insert in metal insert so that battery and battery connecting seat 44 Electrical connection.Circuit board is electrically connected to fuselage 10.For example, circuit board is electrically connected to fuselage 10 by cable.

Specifically, battery connecting seat 44 includes connecting portion 441 and supporting part 442, and circuit board is arranged in connecting portion 441, Supporting part 442 is parallel with the bottom 11 of fuselage 10, and battery compartment 45 is formed between supporting part 442 and the bottom 11 of fuselage 10.Even Socket part 441 is connected to fuselage 10.It is appreciated that battery 43 is carried on supporting part 442.Battery connecting seat 44 can be hollow type Structure, so as to mitigate the weight of battery connecting seat 44 while battery connecting seat 44 is ensured, so as to mitigate unmanned flight The weight of device 100 is to improve the endurance of unmanned vehicle 100.

Switch 46 is arranged on battery connecting seat 44 and electrically connected with battery 43, and switch 46 is used to control battery 43 to discharge. For example, when switch 46 is closed, battery 43 can export electric energy to unmanned vehicle 100, when switching 46 disconnection, battery 43 stops Electric energy is exported to unmanned vehicle 100.

In present embodiment, switch 46 is arranged on connecting portion 441.It is appreciated that in other embodiments, switch 46 It can be arranged on supporting part 442.

Indicator lamp 47 is arranged on battery connecting seat 44 and electrically connected with battery 43.Specifically, the company of being arranged on of indicator lamp 47 In socket part 441.Indicator lamp 47 is used for the electricity and/or working condition for showing battery 43.

For example, when indicator lamp 47 is shinny, representing that battery 43 can export electric energy to unmanned vehicle 100, when indicator lamp 47 During extinguishing, represent that battery 43 stops exporting electric energy to unmanned vehicle 100.

In present embodiment, the quantity of indicator lamp 47 is 4.The quantity of luminous indicator lamp 47 and the electricity of battery 43 into Positively related proportionate relationship.For example, when the electricity of battery 43 is 100%, then 4 indicator lamps 47 are all luminous.Work as battery When 43 electricity is 50%, then only 2 indicator lamps 47 light.User can judge electricity according to the luminous quantity of indicator lamp 47 The dump energy in pond 43.

It is appreciated that in other embodiments, the quantity of indicator lamp 47 and the implication of state representation can be according to actual need Ask and specifically set, for example the quantity of indicator lamp 47 is 6 or other quantity, can be that all luminous, part is luminous, Chang Lianghuo Glittering etc. state.

Ultrasonic sensor 48 sets the bottom 42 of battery module 40, and specifically, ultrasonic sensor 48 is arranged on carrying The bottom 42 in portion 442.It is appreciated that the bottom 42 of battery module 40 is towards ground, therefore, ultrasonic sensor 48 can be measured Unmanned vehicle 100 and the distance on ground, so as to control the flying height of unmanned vehicle 100, to ensure unmanned flight Device 100 safely flies.

Vision sensor 49 sets the bottom 42 of battery module 40, and specifically, ultrasonic sensor 48 is arranged on supporting part 442 bottom 42.Vision sensor 49 is, for example, binocular vision sensor 49.Vision sensor 49 can obtain unmanned vehicle The image of 100 lower sections, by the processing to image, unmanned vehicle 100 can judge the flight of unmanned vehicle 100 exactly Barrier around height and unmanned vehicle 100 so that unmanned vehicle 100 can circumvent barrier safely to fly in time OK.

Head 50 is arranged on the bottom 11 of fuselage 10, and head 50 is located at the phase of fuselage 10 respectively with the battery module 40 To both sides.Specifically, head 50 is located at the front side of the bottom 11 of fuselage 10, and battery module 40 is located at the bottom 11 of fuselage 10 Rear side.

In some embodiments, the quantity of head 50 can be two, the fuselage 10 that two heads 50 are set up in parallel it is same Side, for example, two heads 50 are disposed in parallel in the front side of fuselage 10, now, battery module 40 is located at two lines of head 50 Center line on.

Specifically, head 50 includes connector 51 and support 52.Connector 51 connects the bottom 11 of fuselage 10, for example, even Fitting 51 is fixed by screws in the bottom 11 of fuselage 10.Support 52 connects the connector 51, and can be relative to connector 51 rotate.For example, support 52 is connected by joint motor with connector 51, connector 51 can connect the stator of joint motor, branch Frame 52 connects the rotor of joint motor, so that support 52 can be rotated when joint motor works relative to connector 51.

Load 60 is equiped with head 50, specifically, load 60 is installed on support 52, and load 60 can cause nobody to fly Row device 100 completes predetermined task during flight.In one example, load 60 is camera, so that nobody flies Row device 100 completes to shoot in the process of flight, and head 50 can reduce the vibration of camera so that camera can stably be shot.

In another example, load 60 is to hang the goods being pulled on head 50, for example, key.User can use nothing Key is sent to ground by people's aircraft 100 from upstairs.

Load 60 can be relative to head 50 around (360 °) rotations of the 360 deg of course axle 104, so that load 60 During for camera, load 60 can carry out pan-shot, so as to obtain panoramic picture.

It is appreciated that flying height direction extension of the course axle 104 along unmanned vehicle 100, for example, course axle 104 Direction is the above-below direction in Fig. 1.

On the direction of the flying height of unmanned vehicle 100, the bottom 42 of battery module 40 is higher than load 60.Or Say, battery module 40 is located at the top of load 60.

In the unmanned vehicle 100 of the utility model embodiment, the bottom 11 that battery module 40 is arranged on fuselage 10 has Beneficial to the center of gravity of reduction unmanned vehicle 100, to improve the wind resistance of unmanned vehicle 100, in addition, so without in fuselage The patchhole for installing battery is opened up on 10 so that unmanned vehicle 100 makes simply.

In addition, head 50 and battery module 40 are located at the both sides that fuselage 10 is relative respectively so that the weight of unmanned vehicle 100 The center of the heart and unmanned vehicle 100 is substantially overlapped, and is conducive to unmanned vehicle 100 to fly.

Secondly, the bottom 42 of battery module 40 is higher than load 60, can prevent load 60 around course axle 104 rotate when with it is electric Pond module 40 is interfered.

In some embodiments, head 50 is located at the rear side of the bottom 11 of fuselage 10, and battery module 40 is located at fuselage 10 Bottom 11 front side.

In the description of this specification, reference term " embodiment ", " some embodiments ", " schematically implementation The description of mode ", " example ", " specific example " or " some examples " etc. means with reference to the embodiment or example description Specific features, structure, material or feature are contained at least one embodiment of the present utility model or example.In this explanation In book, identical embodiment or example are not necessarily referring to the schematic representation of above-mentioned term.Moreover, the specific spy of description Levy, structure, material or feature can in an appropriate manner be combined in any one or more embodiments or example.

While there has been shown and described that embodiment of the present utility model, one of ordinary skill in the art can manage Solution：A variety of to the progress of these embodiments can change in the case where not departing from principle of the present utility model and objective, change, Replace and modification, scope of the present utility model is limited by claim and its equivalent.

Claims (16)

1. a kind of unmanned vehicle, it is characterised in that including：

Fuselage, the fuselage includes the bottom towards ground；With

Battery module, the battery module includes battery, and the battery has the top relative with the bottom, and the top is set The bottom part down is placed in, the battery module is electrically connected with the bottom, so as to be powered for the unmanned vehicle.

2. unmanned vehicle as claimed in claim 1, it is characterised in that the battery module includes battery connecting seat, described Battery connecting seat is connected to the bottom of the fuselage, and the battery connecting seat is constituted for housing the electricity with the bottom The battery compartment in pond.

3. unmanned vehicle as claimed in claim 1, it is characterised in that the battery is longitudinally set along the roll axle of the fuselage It is placed in the bottom.

4. unmanned vehicle as claimed in claim 3, it is characterised in that throwing of the fuselage towards the battery module direction Shadow area is more than the projected area of the battery module downward.

5. unmanned vehicle as claimed in claim 2, it is characterised in that be provided with circuit board and electricity on the battery connecting seat Connector, the battery is provided with electric connection terminal, and the electric connection terminal butts up against the electric connector so that the battery Electrically connected with the battery connecting seat, the circuit board is electrically connected to the fuselage.

6. unmanned vehicle as claimed in claim 5, it is characterised in that the battery connecting seat includes connecting portion and carrying Portion, the circuit board is arranged in the connecting portion, and the supporting part is parallel with the bottom of the fuselage, and the battery compartment is formed Between the bottom of the supporting part and the fuselage.

7. unmanned vehicle as claimed in claim 6, it is characterised in that the bottom of the supporting part is provided with supersonic sensing Device and/or binocular vision sensor.

8. unmanned vehicle as claimed in claim 6, it is characterised in that be provided with the connecting portion power switch and/or Indicator lamp.

9. unmanned vehicle as claimed in claim 2, it is characterised in that the battery can be slided along the roll axle of the fuselage It is dynamic to be arranged in the battery compartment.

10. the unmanned vehicle as described in claim 1-9 any one, it is characterised in that the unmanned vehicle includes setting Put the head in the bottom, the head both sides that to be located at the fuselage respectively with the battery module relative.

11. unmanned vehicle as claimed in claim 10, it is characterised in that the head is located at the front side of the bottom, institute State the rear side that battery module is located at the bottom.

12. unmanned vehicle as claimed in claim 10, it is characterised in that the quantity of the head is two, described in two Head is disposed in parallel in the same side of the fuselage.

13. unmanned vehicle as claimed in claim 10, it is characterised in that load is equiped with the head.

14. unmanned vehicle as claimed in claim 13, it is characterised in that the battery module includes opposite with the top Bottom, on the flying height direction of the unmanned vehicle, the bottom be higher than the load.

15. unmanned vehicle as claimed in claim 13, it is characterised in that the load includes camera.

16. unmanned vehicle as claimed in claim 13, it is characterised in that the load can deviate from voyage route relative to the head To 360 ° of rotations of axle.