CN214356664U - Multi-rotor unmanned aerial vehicle - Google Patents
Multi-rotor unmanned aerial vehicle Download PDFInfo
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- CN214356664U CN214356664U CN202023352348.7U CN202023352348U CN214356664U CN 214356664 U CN214356664 U CN 214356664U CN 202023352348 U CN202023352348 U CN 202023352348U CN 214356664 U CN214356664 U CN 214356664U
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/50—Foldable or collapsible UAVs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
- B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
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- Aviation & Aerospace Engineering (AREA)
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Abstract
The utility model discloses a many rotor unmanned aerial vehicle, it includes main part, power unit and interaction mechanism, and power unit is connected with main part mechanical coupling for provide flight power, interaction mechanism installs in main part or power unit, and interaction mechanism includes the touch screen or includes the combination of display screen and instruction input device, and interaction mechanism is used for receiving instruction input and shows the operational information that is correlated with many rotor unmanned aerial vehicle. The utility model discloses a many rotor unmanned aerial vehicle, not only convenience of customers direct input one-level or multistage instruction on interactive mechanism, but also can real-time visual feedback operational information, the user need not remote control equipment and controls many rotor unmanned aerial vehicle, the equipment quantity that the trip was carried can have been reduced, and the user is behind interactive mechanism input instruction, many rotor unmanned aerial vehicle can directly take off in user's hand, connect earlier stage operations such as remote control equipment before having reduced to take off, many rotor unmanned aerial vehicle's ease of use has been improved.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a many rotor unmanned aerial vehicle.
Background
The existing unmanned aerial vehicle is matched with a remote control device, when the unmanned aerial vehicle is controlled by the remote control device, an operator needs to carry the additional remote control device, the remote control device is opened, the remote control device is wirelessly connected with the unmanned aerial vehicle, and an operation instruction is input through the remote control device, so that the burden of carrying the operator in a trip is increased, the preparation time before use is also increased, and the unmanned aerial vehicle can not be started to fly.
The existing unmanned aerial vehicle is not matched with remote control equipment, an operator inputs instructions through keys of a fuselage of the unmanned aerial vehicle, but the number and the levels of the instructions input through the keys of the fuselage are limited, and the unmanned aerial vehicle is inconvenient to use.
SUMMERY OF THE UTILITY MODEL
In view of this, the utility model provides a many rotor unmanned aerial vehicle.
The utility model provides a many rotor unmanned aerial vehicle, include:
a main body;
the power mechanism is mechanically coupled with the main body and used for providing flight power; and
install in main part or/and power unit's interaction mechanism, interaction mechanism includes the touch screen or includes the combination of display screen and instruction input device, interaction mechanism be used for receiving instruction input and show with many rotor unmanned aerial vehicle's associated operating information.
According to the technical scheme, the utility model provides a many rotor unmanned aerial vehicle includes the touch-control screen or includes display screen and instruction input device combination through setting up interactive mechanism and interactive mechanism, and not only convenience of customers directly inputs one-level or multistage instruction on interactive mechanism, and touch-control screen or display screen can real-time visual feedback operational information in addition, and are directly considerable. In addition, through set up the input that the interaction device carries out the instruction on many rotor unmanned aerial vehicle, the user need not remote control equipment and controls many rotor unmanned aerial vehicle, can reduce the equipment quantity that the trip carried. Moreover, the user is behind interactive mechanism input instruction, and many rotor unmanned aerial vehicle can directly take off in user's hand, has reduced to connect operation in earlier stages such as remote control equipment before taking off, has improved many rotor unmanned aerial vehicle's ease for use.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required to be used in the description of the embodiments are briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without any creative effort.
Fig. 1 is a schematic diagram of a user input command for a multi-rotor drone according to an embodiment of the present invention;
fig. 2 is a schematic view of the multi-rotor drone of fig. 1 in a user's hand for takeoff;
fig. 3 is a schematic structural view of the multi-rotor drone of fig. 1 in a deployed state;
fig. 4 is a schematic structural view of a variant embodiment of the multi-rotor drone of fig. 1;
fig. 5 is a schematic diagram of a gesture provided by an embodiment of the present invention;
fig. 6 is a schematic structural view of the multi-rotor drone of fig. 1 in a folded state;
fig. 7 is a schematic structural view of the multi-rotor drone of fig. 1 in a deployed state;
fig. 8 is a schematic structural diagram of a plunger according to an embodiment of the present invention;
fig. 9 is a schematic side view of the multi-rotor drone of fig. 1 in a deployed state;
fig. 10 is a schematic structural view of another variant embodiment of the multi-rotor drone of fig. 1;
fig. 11 is a schematic side view of another variation of the multi-rotor drone of fig. 1;
fig. 12 is a schematic structural view of another multi-rotor drone provided by an embodiment of the present invention;
fig. 13 is a schematic structural view of a variant embodiment of the multi-rotor drone of fig. 12.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, not all, of the embodiments of the present invention. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
It is also to be understood that the terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used in the specification and the appended claims, the singular forms "a", "an", and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise.
It should be further understood that the term "or/and" as used in the specification and the appended claims refers to any and all possible combinations of one or more of the associated listed items, and includes such combinations.
As shown in fig. 1 to 3, an embodiment of the utility model provides a multi-rotor unmanned aerial vehicle 100, it includes main part 10, power unit 20 and interaction mechanism 30, power unit 20 is connected with main part 10 mechanical coupling, power unit 20 is used for providing flight power, interaction mechanism 30 is installed in main part 10, interaction mechanism 30 is used for receiving instruction input and shows the operating information who is correlated with multi-rotor unmanned aerial vehicle 100, interaction mechanism 30 includes touch screen 31, the user passes through touch screen 31 and inputs the instruction to multi-rotor unmanned aerial vehicle 100.
During the use, the user can hold main part 10 or power unit 20 with one hand, and the other hand is operated in order to input the instruction to multi-rotor unmanned aerial vehicle 100 on touch screen 31, accomplishes instruction input back, and multi-rotor unmanned aerial vehicle 100 can directly take off and fly and carry out relevant operation according to the instruction of user input on user's hand, for example, the user inputs with clapping the mode instruction through touch screen 31, after taking off, and multi-rotor unmanned aerial vehicle 100 hovers and shoots beside the user. Of course, it is not necessary for the user to hold the main body 10 or the power mechanism 20 with one hand and operate the multi-rotor drone on the touch screen 31 with the other hand, for example, in an airplane mode, the multi-rotor drone 100 may be controlled to hover at a distance from the touch screen 31 visible to the user, and the user may input commands on the touch screen 31 with one hand.
It should be noted that the interaction means 30 is not limited to be mounted on the main body 10, and for example, the interaction means 30 may be mounted on the power mechanism 20. It should be noted that the interaction mechanism 30 is not limited to the input mode using the touch screen 31, for example, as shown in fig. 4, the interaction mechanism 30 may also use an input mode combining a display screen 31a and an instruction input device 31b, where the instruction input device 31b is used for receiving an instruction input, and the display screen 31a is used for displaying related operation information.
According to the multi-rotor unmanned aerial vehicle 100 provided by the embodiment, by arranging the interaction mechanism 30 and enabling the interaction mechanism 30 to comprise the touch screen 31 or comprise the combination of the display screen 31a and the instruction input device 31b, not only is the user convenient to directly input one-level or multi-level instructions on the interaction mechanism 30, but also the touch screen 31 or the display screen 31a can visually feed back operation information in real time, and the operation information is directly observable. In addition, through set up the input that interaction device 30 carries out the instruction on many rotor unmanned aerial vehicle 100, the user need not remote control equipment and controls many rotor unmanned aerial vehicle 100, can reduce the equipment quantity that the trip carried. Furthermore, the user is behind interactive mechanism 30 input instruction, and many rotor unmanned aerial vehicle 100 can directly take off in user's hand, has reduced earlier stage operations such as connecting remote control equipment before taking off, has improved many rotor unmanned aerial vehicle 100's ease of use.
It can be understood that, the multi-rotor drone 100 has one or more processors built therein, and the interaction mechanism 30 and the power mechanism 20 are electrically connected to the processors, and the processors receive the instructions input by the interaction mechanism 30 and control the multi-rotor drone 100 to perform the relevant operations according to the instructions. The Processor may be a Central Processing Unit (CPU), and the Processor may be other general purpose Processor, a Digital Signal Processor (DSP), an Application Specific Integrated Circuit (ASIC), a Field Programmable Gate Array (FPGA) or other Programmable logic device, discrete Gate or transistor logic, discrete hardware components, etc.
Alternatively, the instruction input device 31b includes at least one of a key, a voice acquisition device, a gesture recognition device, and a user gesture recognition device. Illustratively, the keys include a left key, a right key, a reset key, a confirm key, and the like which are mounted on the main body 10 or the power mechanism 20, an operation menu is provided on the display screen 31a, a user can select a target operation and confirm the target operation in the operation menu through the keys, and the multi-rotor drone 100 executes a relevant operation according to the selected target operation. Pronunciation collection system includes that one or more install in main part 10 or power unit 20's microphone, and the microphone is used for gathering user's voice command and transmits the voice command who gathers for the treater, and the treater carries out relevant operation according to voice command control multi-rotor unmanned aerial vehicle 100, for example, when the user says "carry out five continuous shooting after five seconds" the treater control multi-rotor unmanned aerial vehicle 100 carries out five continuous shooting operations after five seconds. The gesture recognition device includes one or more cameras installed in the main body 10 or the power mechanism 20, the cameras are used for collecting gesture instructions of a user and transmitting the collected gesture instructions to the processor, and the processor controls the multi-rotor drone 100 to execute related operations according to the gesture instructions, for example, as shown in fig. 5, when the user puts out a gesture for taking a picture, the processor controls the multi-rotor drone 100 to execute a picture taking action. User gesture recognition device includes one or more and installs in main part 10 or power unit 20's camera, and the camera is used for gathering user's gesture instruction and gives the processor with the gesture instruction transmission of gathering, and the relevant operation is carried out according to gesture instruction control multi-rotor unmanned aerial vehicle 100 to the processor, for example, when the user circles at the top of the head with the forefinger, and the processor control multi-rotor unmanned aerial vehicle 100 is hovering at user's top of the head.
Optionally, the multi-rotor drone 100 further includes a pan-tilt camera 40, the pan-tilt camera 40 is installed in the main body 10 or the power mechanism 20, and the picture shot by the pan-tilt camera 40 is transmitted to the touch screen 31 or the display screen 31a for display. In some embodiments, the pan-tilt camera 40 is configured as part of a gesture recognition device and a user gesture recognition device in addition to being used for taking pictures, in particular, the pan-tilt camera 40 is configured for acquiring gestures of a user and for acquiring user gestures.
Optionally, the power mechanism 20 includes two flying assemblies 21 rotatably connected to the main body 10, the power mechanism 20 includes a folded state and an unfolded state, and when the power mechanism 20 is in the unfolded state, the two flying assemblies 21 are respectively unfolded to two opposite sides of the main body 10. Through setting up power unit 20 collapsible, when not using, the user can fold power unit 20, reduces many rotor unmanned aerial vehicle 100's overall size, is convenient for accomodate and carry.
Optionally, when the power mechanism 20 is in the unfolded state, an included angle between the two flying assemblies 21 is 180 °, and the power mechanism 20 and the main body 10 are T-shaped. Of course, when the power mechanism 20 is in the unfolded state, the included angle between the two flying assemblies 21 is not limited to 180 °, and may be other angles, which is determined according to the actual design requirement.
As shown in fig. 3 and 6 to 8, optionally, the flying assembly 21 is provided with an avoiding groove 21a, the main body 10 is rotatably disposed in the avoiding groove 21a, when the power mechanism 20 is in the folded state, the two avoiding grooves 21a are combined to form an accommodating groove 21b, and the main body 10 is accommodated in the accommodating groove 21 b. Through being equipped with on flight subassembly 21 and dodging groove 21a and accept main part 10, after folding, main part 10 is acceptd and can further reduce many rotor unmanned aerial vehicle 100's overall dimension in accepting groove 21b, is convenient for accomodate and carry.
Exemplarily, the flying assembly 21 includes a connecting portion 211, a first extending portion 212 disposed at one side of the connecting portion 211, and a second extending portion 213 disposed at one side of the connecting portion 211 and spaced from the first extending portion 212, wherein the connecting portion 211, the first extending portion 212, and the second extending portion 213 enclose the avoiding groove 21a, one side of the main body 10 is rotatably connected to the first extending portion 212, and the other side of the main body 10 is rotatably connected to the second extending portion 213.
Optionally, the groove sidewall of the avoiding groove 21a is provided with a first positioning portion 22, the outer sidewall of the main body 10 is provided with a second positioning portion 11, when the main body 10 is accommodated in the accommodating groove 21b, the first positioning portion 22 and the second positioning portion 11 are connected to maintain the folded state of the power mechanism 20, so that the multi-rotor unmanned aerial vehicle 100 can form a stable whole after being folded, and is not loose, and a user can unfold the two flying assemblies 21 by overcoming the connection stress of the first positioning portion 22 and the second positioning portion 11.
Illustratively, the first positioning portion 22 is a positioning hole, the second positioning portion 11 is a plunger, and when the main body 10 is received in the receiving groove 21b, the plunger extends into the positioning hole to maintain the folded state of the power mechanism 20. The first positioning portion 22 and the second positioning portion 11 may be interchanged, that is, the first positioning portion 22 is a plunger, and the second positioning portion 11 is a positioning hole.
The plunger comprises a shell 111, an elastic part 112 and a top bead 113, the shell 111 is provided with a mounting groove 114, the top bead 113 can be movably mounted in the mounting groove 114, the elastic part 112 is elastically compressed between the bottom surfaces of the top bead 113 and the mounting groove 114, when the flying component 21 is folded, the top bead 113 retracts into the mounting groove 114 when encountering the groove side wall of the avoiding groove 21a, and when the flying component moves to the positioning hole, the top bead 113 extends into the positioning hole under the action of the elastic force of the elastic part 112. The use of the plunger can prevent the second positioning portion 11 from scratching the groove side wall of the escape groove 21 a. Of course, the second positioning portion 11 may also be provided in a convex manner.
Alternatively, the outer side wall of the main body 10 is provided with two second positioning portions 11, the two flying assemblies 21 are provided with the first positioning portions 22, and the two flying assemblies 21 are kept in the folded state by the cooperation of the first positioning portions 22 and the second positioning portions 11. Of course, the above-mentioned manner may not be adopted, for example, only one second positioning portion 11 is provided on the outer side wall of the main body 10, only one of the flying assemblies 21 is provided with the first positioning portion 22, the flying assembly 21 is kept in the folded state with the main body 10 by the cooperation of the first positioning portion 22 and the second positioning portion 11, and the other flying assembly 21 is detachably connected with the above-mentioned flying assembly 21.
The two flying assemblies 21 are respectively defined as a first flying assembly 21c and a second flying assembly 21d, illustratively, the first flying assembly 21c is provided with a first installation slot 21c1, the second flying assembly 21d is provided with a second installation slot 21d1, a magnetic member is embedded in the first installation slot 21c1, a magnetic member or a magnetic adsorption member is embedded in the second installation slot 21d1, and the first flying assembly 21c and the second flying assembly 21d are detachably connected through magnetic attraction. The magnetic member refers to a member having a magnetic attraction force, such as a magnet, and the magnetic attraction member refers to a member that can be attracted by the magnetic member, such as iron, cobalt, nickel, and alloys thereof. Of course, the detachable connection between the two flying assemblies 21 is not limited to the magnetic attraction, and may be a snap connection, for example.
Alternatively, the first mounting groove 21c1 is provided on the groove side wall of the escape groove 21a of the first flying assembly 21c, and the second mounting groove 21d1 is provided on the groove side wall of the escape groove 21a of the second flying assembly 21 d. Of course, the first mounting groove 21c1 may be provided on the side of the first flying unit 21c that is attached to the second flying unit 21d in the folded state, and the second mounting groove 21d1 may be provided on the side of the second flying unit 21d that is attached to the first flying unit 21c in the folded state.
Optionally, the flying assembly 21 comprises a protective cover 214 and a propeller mechanism 215, the protective cover 214 is provided with a through hole 2141, and the propeller mechanism 215 is provided within the through hole 2141. Through locating screw mechanism 215 in through-hole 2141, screw mechanism 215 establishes not exposing, avoids the user to carry out instruction input to many rotor unmanned aerial vehicle 100 through touch screen 31, and screw mechanism 215 rotates and causes the injury to the user.
Illustratively, each flight assembly 21 is provided with two through holes 2141 and two propeller mechanisms 215, one propeller mechanism 215 is provided in each through hole 2141, and the propeller mechanisms 215 on the two flight assemblies 21 are symmetrically provided with respect to the roll axis of the multi-rotor drone 100. Of course, each flying assembly 21 is not limited to two through holes 2141 and two propeller mechanisms 215, and may also be provided with one through hole 2141 and one propeller mechanism 215, or more than two through holes 2141 and more than two propeller mechanisms 215, depending on the actual design requirements.
Optionally, the multi-rotor drone 100 further includes a mesh enclosure 23 disposed at the through hole 2141, the mesh enclosure 23 and the protective enclosure 214 enclose a protective cavity 261, and the propeller mechanism 215 is located in the protective cavity 261. By arranging the mesh enclosure 23, the propeller mechanism 215 is further protected, and the propeller mechanism 215 is prevented from hurting a user. Optionally, the mesh enclosure 23 is integrally formed with the protective enclosure 214.
Optionally, one of the flying assemblies 21 is provided with a first fixing portion 24, the other flying assembly 21 is provided with a second fixing portion 25, and when the power mechanism 20 is in the unfolded state, the first fixing portion 24 and the second fixing portion 25 cooperate to maintain the unfolded state of the power mechanism 20.
Optionally, the first fixing portion 24 is a magnetic member, the second fixing portion 25 is a magnetic member or a magnetic attraction member, and the first fixing portion 24 and the second fixing portion 25 attract each other to maintain the unfolding state of the power mechanism 20.
The two flying assemblies 21 are respectively defined as a first flying assembly 21c and a second flying assembly 21d, for example, when the power mechanism 20 is in the unfolded state, the first flying assembly 21c is abutted with the second flying assembly 21d, a first groove 21c2 is formed on one side of the first flying assembly 21c abutted with the second flying assembly 21d, a magnetic member is embedded in the first groove 21c1, a second groove 21d2 is formed on one side of the second flying assembly 21d abutted with the first flying assembly 21c, and a magnetic member or a magnetic adsorbing member is embedded in the second groove 21d 2. When the first flying assembly 21c is docked with the second flying assembly 21d, the magnetic member located in the first groove 21c2 and the magnetic member or the magnetic attraction member located in the second groove 21d2 attract each other, so that the power mechanism 20 is maintained in the unfolded state.
Of course, the first groove 21c2 and the second groove 21d2 are not necessarily required to be provided, and the side where the first flying component 21c and the second flying component 21d are butted can be made of a magnetic material, and the side where the second flying component 21d and the first flying component 21c are butted can be made of a magnetic material or a magnetically attractive material, so that when the first flying component 21c and the second flying component 21d are butted, the magnetic attraction fixation of the first flying component 21c and the second flying component 12d can be realized.
In other embodiments, the first fixing portion 24 is a fastener, the second fixing portion 25 is a slot, and the first fixing portion 24 and the second fixing portion 25 are fastened to maintain the expansion state of the power mechanism 20.
As shown in fig. 9, optionally, a limit component 26 is disposed between the main body 10 and the flying component 21, and the limit component 26 is used for forming a limit after the flying component 21 rotates to the deployed state. Illustratively, the limiting assembly 26 includes a first stopping portion 261 disposed on the main body 10 and a second stopping portion 262 disposed on the flying assembly 21, and when the flying assembly rotates to the unfolded state, the first stopping portion 261 and the second stopping portion 262 abut against each other to limit the flying assembly from further rotating.
It should be noted that, the formation of the limit position after the flying assembly 21 rotates to the deployed state is not limited to the mode of matching the first stopping portion 261 and the second stopping portion 262, and other modes may also be adopted, for example, the multi-rotor drone 100 includes a hinge rotating shaft, and the flying assembly 21 and the main body 10 are rotatably connected through the hinge rotating shaft. The hinge shaft can also enable the flying assembly 21 to rotate to the unfolding state to form a limit position through the damping effect of the hinge shaft.
As shown in fig. 10 to 11, the propeller mechanism 215 optionally includes a motor 2151 and a propeller (not shown) mounted on the motor 2151, and when the power mechanism 20 is in the folded state, the motor 2151 of one of the flying assemblies 21 is offset from the motor 2151 of the other flying assembly 21. This embodiment can reduce the thickness when many rotor unmanned aerial vehicle 100 is fold condition, reduces the size, conveniently carries.
As shown in fig. 12 to 13, another embodiment of the present invention provides a multi-rotor drone 100 ', which includes a main body 10', a power mechanism 20 ', and an interaction mechanism 30', wherein the power mechanism 20 'is mechanically coupled to the main body 10', the power mechanism 20 'is configured to provide flight power, the interaction mechanism 30' is installed in the main body 10 ', the interaction mechanism 30' includes a touch screen 31 ', and the interaction mechanism 30' is configured to receive a user command and display operation information associated with the multi-rotor drone. The main body 10 ' comprises a protective cover 11 ', the power mechanism 20 ' comprises a propeller mechanism 21 ', the protective cover 11 ' is provided with two groups of through holes 111 ', the propeller mechanism 21 ' is arranged in the through holes 111 ', the two groups of through holes 111 ' are arranged on the protective cover 11 ' at intervals to form a hand holding area 112 ', and the interaction mechanism 30 ' is arranged in the hand holding area 112 '. It should be noted that the through holes of the same set of through holes 111 'may be spaced apart from each other to form the hand holding area 112'.
During the use, the user can hold the hand-holding area 112 'of holding the safety cover 11' with one hand, and the other hand is operated on touch screen 31 'to input the instruction to multi-rotor unmanned aerial vehicle 100', and after accomplishing the instruction input, multi-rotor unmanned aerial vehicle 100 'can directly take off on user's hand and fly and carry out relevant operation according to the instruction that the user input, for example, the user inputs with shooting mode instruction through touch screen 31 ', and after taking off, multi-rotor unmanned aerial vehicle 100' follows and shoots next to the user.
Optionally, the multi-rotor drone 100 'further includes a mesh enclosure (not shown) disposed at the through hole 111', the mesh enclosure and the protective cover 11 'enclose to form a protective cavity, and the propeller mechanism 21' is located in the protective cavity. Through setting up the screen panel, further form the protection to screw mechanism 21 ', avoid screw mechanism 21' to cause the injury to the user. Optionally, the mesh is integrally formed with the shield 11'.
The multi-rotor drone 100 ' further comprises one or more processors, the interaction mechanism 30 ' and the power mechanism 20 ' are electrically connected with the processors, and the processors receive instructions input by the interaction mechanism 30 ' and control the multi-rotor drone 100 ' to execute related operations according to the instructions.
It should be noted that the interaction mechanism 30 ' is not limited to the input mode using the touch screen 31 ', for example, the interaction mechanism 30 ' may also use an input mode combining the display screen 31a ' and the instruction input device 31b ', wherein the instruction input device 31b ' is used for receiving the input of the instruction, and the display screen 31a ' is used for displaying the related operation information.
Alternatively, the instruction input device 31 b' includes at least one of a key, a voice capturing device, a gesture recognition device, and a user gesture recognition device. Illustratively, the keys include up, down, left and right keys, a reset key, a confirm key, and the like, which are mounted on the main body 10 ' or the power mechanism 20 ', an operation menu is provided on the display screen 31a, a user can select a target operation and confirm the target operation in the operation menu through the keys, and the multi-rotor drone 100 ' performs a relevant operation according to the selected target operation. Pronunciation collection system includes that one or more install in main part 10 'or power unit 20' microphone, and the microphone is used for gathering user's voice command and transmits the voice command who gathers for the treater, and the treater carries out relevant operation according to voice command control many rotor unmanned aerial vehicle, for example, when the user says "five seconds back and carries out five continuous shooting", treater control many rotor unmanned aerial vehicle 100' carries out five continuous shooting operations after five seconds. The gesture recognition device comprises one or more cameras installed on the main body 10 'or the power mechanism 20', the cameras are used for acquiring gesture instructions of users and transmitting the acquired gesture instructions to the processor, and the processor controls the multi-rotor unmanned aerial vehicle to execute related operations according to the gesture instructions. The user gesture recognition device comprises one or more cameras installed on the main body 10 'or the power mechanism 20', the cameras are used for acquiring gesture instructions of a user and transmitting the acquired gesture instructions to the processor, and the processor controls the multi-rotor unmanned aerial vehicle to execute related operations according to the gesture instructions, for example, when the user circles at the top of the head with an index finger, the processor controls the multi-rotor unmanned aerial vehicle 100 to hover at the top of the head of the user.
Optionally, the multi-rotor drone 100 ' further includes a pan/tilt camera 40 ', the pan/tilt camera 40 ' is installed on the main body 10 ', and a picture taken by the pan/tilt camera 40 ' is transmitted to the display screen 31a ' or the touch screen 31 ' for display. In some embodiments, the pan-tilt camera 40' is configured as part of a gesture recognition device and a user gesture recognition device in addition to being used to take pictures.
Other components and connection relationships of the multi-rotor drone 100' provided in this embodiment may refer to the above embodiments, and are not described herein again.
The above description is only for the specific embodiments of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art can easily think of various equivalent modifications or replacements within the technical scope of the present invention, and these modifications or replacements should be covered within the scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (16)
1. A multi-rotor unmanned aerial vehicle, comprising:
a main body;
the power mechanism is mechanically coupled with the main body and used for providing flight power; and
install in main part or/and power unit's interaction mechanism, interaction mechanism includes the touch screen or includes the combination of display screen and instruction input device, interaction mechanism be used for receiving instruction input and show with many rotor unmanned aerial vehicle's associated operating information.
2. A multi-rotor drone according to claim 1, wherein the interaction means comprises a combination of a display screen and command input means, the command input means comprising at least one of a key, a voice capture device, a gesture recognition device, and a user gesture recognition device.
3. The multi-rotor unmanned aerial vehicle of claim 1, wherein the power mechanism includes two flying assemblies rotatably coupled to the main body, the power mechanism includes a folded state and an unfolded state, and when the power mechanism is in the unfolded state, the two flying assemblies are respectively unfolded to opposite sides of the main body.
4. The multi-rotor unmanned aerial vehicle of claim 3, wherein the flight assembly comprises an avoidance slot, the main body is rotatably disposed in the avoidance slot, and when the power mechanism is in a folded state, the avoidance slots are combined to form an accommodating slot, and the main body is accommodated in the accommodating slot.
5. The multi-rotor unmanned aerial vehicle of claim 4, wherein one of the slot sidewall of the dodging slot and the outer sidewall of the main body is provided with a first positioning portion, the other of the slot sidewall of the dodging slot and the outer sidewall of the main body is provided with a second positioning portion, and when the main body is received in the receiving slot, the first positioning portion and the second positioning portion are connected to maintain the folded state.
6. The multi-rotor drone of claim 5, wherein the first positioning portion is a plunger and the second positioning portion is a positioning hole, the plunger extending into the positioning hole to maintain the folded state when the body is received in the receiving slot.
7. A multi-rotor drone according to claim 3, wherein a stop assembly is provided between the main body and the flight assembly, the stop assembly being configured to limit rotation of the flight assembly to the deployed state.
8. A multi-rotor drone according to claim 3, wherein the drone includes a hinge shaft through which the flying assembly is rotatably connected to the body.
9. A multi-rotor unmanned aerial vehicle as claimed in claim 3, wherein one of the flight assemblies is provided with a first fixing portion, the other flight assembly is provided with a second fixing portion, and the first fixing portion and the second fixing portion cooperate to maintain the deployed state when the power mechanism is in the deployed state.
10. The multi-rotor drone of claim 9, wherein the first securing portion is a magnetic member and the second securing portion is a magnetic member or a magnetically attracted member, the first and second securing portions attracting each other to maintain the deployed state.
11. The multi-rotor unmanned aerial vehicle of claim 9, wherein the first securing portion is a snap fit and the second securing portion is a snap fit, the first securing portion snap-fitting with the second securing portion to maintain the deployed state.
12. A multi-rotor unmanned aerial vehicle as recited in claim 3, wherein the flight assembly comprises a shroud provided with a through-hole and a propeller mechanism provided within the through-hole.
13. The multi-rotor drone of claim 12, wherein the propeller mechanism includes a motor and a propeller mounted to the motor, and wherein the power mechanism is in a folded configuration with the motor of one of the flight assemblies staggered from the motor of the other of the flight assemblies.
14. The multi-rotor unmanned aerial vehicle of claim 1, wherein the body comprises a protective covering, the power mechanism comprises a propeller mechanism, the protective covering is provided with two sets of through holes, the propeller mechanism is disposed in the through holes, wherein the two sets of through holes are spaced apart on the protective covering to form a hand holding area, and the interaction mechanism is disposed in the hand holding area.
15. A multi-rotor unmanned aerial vehicle as recited in claim 12 or 14, further comprising a mesh enclosure disposed at the through-hole, the mesh enclosure and the protective enclosure enclosing a protective cavity, the propeller mechanism being located within the protective cavity.
16. The multi-rotor unmanned aerial vehicle of claim 1, further comprising a pan/tilt camera, the pan/tilt camera being mounted on the main body or the power mechanism, and a picture taken by the pan/tilt camera being transmitted to the display screen or the touch screen for display.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNPCT/CN2020/139505 | 2020-12-25 | ||
| PCT/CN2020/139505 WO2022134024A1 (en) | 2020-12-25 | 2020-12-25 | Unmanned aerial vehicle with user-interactive components and a foldable structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214356664U true CN214356664U (en) | 2021-10-08 |
Family
ID=77952863
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202080103877.7A Pending CN116194369A (en) | 2020-12-25 | 2020-12-25 | Unmanned aerial vehicle with user interaction component and foldable structure |
| CN202023352348.7U Expired - Fee Related CN214356664U (en) | 2020-12-25 | 2020-12-31 | Multi-rotor unmanned aerial vehicle |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202080103877.7A Pending CN116194369A (en) | 2020-12-25 | 2020-12-25 | Unmanned aerial vehicle with user interaction component and foldable structure |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN116194369A (en) |
| WO (1) | WO2022134024A1 (en) |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20160041697A (en) * | 2014-10-08 | 2016-04-18 | 한화테크윈 주식회사 | Unmanned flying vehicle |
| CN104580606B (en) * | 2015-02-02 | 2017-03-29 | 金陵科技学院 | A kind of mobile phone shell that can be changed into unmanned plane |
| CN105035303A (en) * | 2015-08-19 | 2015-11-11 | 无锡觅睿恪科技有限公司 | Folding type aerial photography aircraft |
| US9977434B2 (en) * | 2016-06-23 | 2018-05-22 | Qualcomm Incorporated | Automatic tracking mode for controlling an unmanned aerial vehicle |
| US10649469B2 (en) * | 2017-01-19 | 2020-05-12 | Vtrus Inc. | Indoor mapping and modular control for UAVs and other autonomous vehicles, and associated systems and methods |
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2020
- 2020-12-25 WO PCT/CN2020/139505 patent/WO2022134024A1/en active Application Filing
- 2020-12-25 CN CN202080103877.7A patent/CN116194369A/en active Pending
- 2020-12-31 CN CN202023352348.7U patent/CN214356664U/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN116194369A (en) | 2023-05-30 |
| WO2022134024A1 (en) | 2022-06-30 |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
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Granted publication date: 20211008 |