CN112340010A

CN112340010A - Unmanned plane

Info

Publication number: CN112340010A
Application number: CN202010956492.7A
Authority: CN
Inventors: 何建兵; 肖锭锋; 吴旭民
Original assignee: Guangzhou Xaircraft Technology Co Ltd
Current assignee: Guangzhou Xaircraft Technology Co Ltd
Priority date: 2020-09-11
Filing date: 2020-09-11
Publication date: 2021-02-09
Anticipated expiration: 2040-09-11
Also published as: CN112340010B

Abstract

The invention discloses an unmanned aerial vehicle, which comprises: the length both ends of horn device are inner and outer end respectively, the inner of horn device is installed in the fuselage assembly, power device installs in the outer end of horn device, and power device includes power pack, power pack includes power motor and installs in power motor's screw, drive arrangement includes actuating mechanism and acts as go-between, actuating mechanism installs in the fuselage assembly, act as go-between and link to each other respectively with actuating mechanism and power device to make actuating mechanism drive power pack through acting as go-between and around predetermineeing the axis rotation around the horn device. According to the unmanned aerial vehicle disclosed by the embodiment of the invention, the structural compactness of the unmanned aerial vehicle is favorably improved, and the weight of the horn is reduced.

Description

Unmanned plane

Technical Field

The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle.

Background

Along with the development of unmanned aerial vehicle technique, people can utilize unmanned aerial vehicle to accomplish a lot of work, for example: the fire extinguishing liquid spraying, aerial photography, electric power inspection, environment monitoring, disaster patrol and other works in forest fires. Unmanned aerial vehicle among the correlation technique, including fuselage, horn, screw and driver, the screw sets up in the outer end of horn, and the screw includes the rotation axis, and the screw is rotatable around the rotation axis, and the driver drive screw's rotation axis, relative horn's the central axis, around pivot axis perpendicular to the central axis rotation to revise the angle of fuselage, adapt to different flight condition demands. However, since the driver needs to drive the propeller, the driver is usually disposed close to the propeller, i.e., the driver is also disposed at the outer end of the horn, which results in a heavy weight of the horn and a poor compactness of the drone.

Disclosure of Invention

The present invention is directed to solving at least one of the problems of the prior art. Therefore, the invention provides an unmanned aerial vehicle, which has improved structure compactness and can reduce the weight of a horn.

According to the embodiment of the invention, the unmanned aerial vehicle comprises: a fuselage assembly; the inner end of the machine arm device is arranged on the machine body assembly; the power device is arranged at the outer end of the horn device and comprises a power unit, and the power unit comprises a power motor and a propeller arranged on the power motor; and the driving device comprises a driving mechanism and a stay wire, the driving mechanism is arranged on the machine body assembly, and the stay wire is respectively connected with the driving mechanism and the power device, so that the driving mechanism drives the power unit to rotate around a preset axis relative to the machine arm device through the stay wire.

According to the unmanned aerial vehicle disclosed by the embodiment of the invention, the driving mechanism in the driving device is arranged on the body assembly, and the power unit is driven to rotate relative to the arm device through the pull wire, so that on the premise of ensuring that the power unit can be reliably and effectively driven to rotate, the space of the body assembly is fully utilized by arranging the driving mechanism on the body assembly, the whole structure compactness of the unmanned aerial vehicle is favorably improved, the weight of the arm can be reduced, the gravity center of the whole unmanned aerial vehicle is concentrated, and the flight stability is higher.

In some embodiments, the predetermined axis is coincident with or parallel to a central axis of the outer end of the horn device.

In some embodiments, the power plant further comprises: the mounting assembly comprises a mounting column and a rotating column, the mounting column is connected with the outer end of the horn device, the power motor is connected with the rotating column, the pull line is connected with the rotating column, the rotating column is in running fit with the mounting column, and the pull line pulls the rotating column to be opposite to the mounting column, so that the power unit is opposite to the horn device to wind the preset axis to rotate when the mounting column rotates.

In some embodiments, the rotating column is rotatably sleeved outside the mounting column or rotatably disposed in the mounting column in a penetrating manner, so that the pulling wire pulls the rotating column to rotate around a central axis of the mounting column, and the central axis of the mounting column is the preset axis.

In some embodiments, the outer peripheral wall of the rotation column has driving arms respectively located at two sides of the rotation column, the pull wire is respectively connected to the driving arms at two sides, and the driving mechanism pulls the driving arms at two sides to move oppositely through the pull wire so as to pull the rotation column to rotate.

In some embodiments, the power plant further comprises: and the pulley assembly comprises a support frame and a pulley, the support frame is connected with the outer end of the machine arm device, the pulley is rotatably arranged on the support frame, and the stay wire is guided and slid by the pulley.

In some embodiments, the drive mechanism comprises: the adapter comprises a central column and a rotating arm, the rotating arm is arranged on the peripheral wall of the central column, and the pull wire is connected with the rotating arm; and the steering engine is connected with the adaptor to drive the adaptor to rotate around the central axis of the central column.

In some embodiments, the drive mechanism further comprises: a drive assembly, the drive assembly comprising: the steering engine is installed outside the installation shell, the gear set is stored in the installation shell, a driving shaft of the steering engine stretches into the installation shell and is connected with a first-stage gear of the gear set, one end of the output shaft stretches into the installation shell and is connected with a final-stage gear of the gear set, and the other end of the output shaft stretches out of the installation shell and is connected with the central column.

In some embodiments, the central column has a central axial hole therein, the side wall of the central column has a positioning hole, the other end of the output shaft is inserted into the central axial hole, and the peripheral wall of the other end of the output shaft has a positioning column, the positioning column is inserted into the positioning hole, so that the output shaft drives the central column to rotate.

In some embodiments, the horn device comprises: the machine arm body, one end of the said machine arm body couples to assembly of the said fuselage; the horn end seat, the horn end seat install in the other end of horn body, the horn end seat includes first section and second section, first section cover is located the horn body outside the other end, in the both ends on the second section extending direction with first section links to each other, the other end is used for installing power device, the second section conduct the outer end of horn device, just the axis of second section is the axis of horn device the axis of outer end.

In some embodiments, the central axis of the second section coincides with or intersects the central axis of the horn body at an obtuse angle.

The power device is arranged at the outer end of each horn device, and the power unit in each power device is driven by one driving device to rotate.

Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.

Drawings

Fig. 1 is a perspective view of a drone according to one embodiment of the present invention;

figure 2 is a top view of the drone shown in figure 1;

fig. 3 is a bottom view of the drone shown in fig. 1;

figure 4 is a partial exploded view of the drone shown in figure 1;

FIG. 5 is a perspective view of the rotating post shown in FIG. 4;

FIG. 6 is an enlarged view of section A shown in FIG. 1;

FIG. 7 is a perspective view of the transmission assembly shown in FIG. 1;

FIG. 8 is a perspective view of the adapter shown in FIG. 1;

fig. 9 is a front view of the first mounting frame, the second mounting frame and the partition plate shown in fig. 3.

Reference numerals:

unmanned aerial vehicle 100:

a fuselage assembly 1;

a storage device 11; a power supply device 12; a movement device 13; a landing gear 14;

an assembly body 15; a top plate 151; a base plate 152;

a first mounting frame 16; a fixed plate 161; a first connecting plate 162; the first installation space 160;

a second mounting frame 17; the second connecting plate 171; a third connecting plate 172; a second installation space 170;

a separator plate 18;

a horn device 2;

a horn body 21; a horn end mount 22; a first segment 221; a second segment 222;

a power plant 3;

a power unit 31; a power motor 311; a propeller 312; a holder member 313; a fixed frame 314;

a mounting assembly 32; mounting posts 321; a rotating post 322; a drive arm 323; a bearing member 324;

a pulley assembly 33; a support frame 331; a pulley 332;

a drive device 4;

a drive mechanism 41;

an adaptor 411;

a central post 4111; a central shaft hole 41111; positioning hole 41112; a rotating arm 4112;

a steering engine 412;

a drive assembly 413;

a mounting housing 4131; gear set 4132; a primary gear 41321; a final stage gear 41322;

an output shaft 4133; positioning posts 41331;

a pull wire 42; a first end 421; second end 422.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative and intended to be illustrative of the invention and are not to be construed as limiting the invention.

The following disclosure provides many different embodiments, or examples, for implementing different features of the invention. To simplify the disclosure of the present invention, the components and arrangements of specific examples are described below. Of course, they are merely examples and are not intended to limit the present invention. Furthermore, the present invention may repeat reference numerals and/or letters in the various examples. This repetition is for the purpose of simplicity and clarity and does not in itself dictate a relationship between the various embodiments and/or configurations discussed. In addition, the present invention provides examples of various specific processes and materials, but one of ordinary skill in the art may recognize the applicability of other processes and/or the use of other materials.

Next, with reference to the drawings, a drone 100 according to an embodiment of the present invention is described.

As shown in fig. 1 to 3, the drone 100 according to the embodiment of the present invention may include: the robot comprises a body assembly 1, a machine arm device 2, a power device 3 and a driving device 4. The inner end and the outer end are respectively arranged at the two ends of the length of the horn device 2, the inner end of the horn device 2 is arranged on the machine body assembly 1, the power device 3 is arranged at the outer end of the horn device 2, the power device 3 comprises a power unit 31, and the power unit 31 comprises a power motor 311 and a propeller 312 arranged on the power motor 311. From this, when power device 3 during operation, power motor 311 can drive screw 312 and rotate to provide power for the flight of unmanned aerial vehicle 100.

As shown in fig. 1, 4 and 6, the driving device 4 may include a driving mechanism 41 and a pulling wire 42, the driving mechanism 41 is mounted to the body assembly 1, the pulling wire 42 is connected to the driving mechanism 41, and the pulling wire 42 is also connected to the power device 3, for example, the pulling wire 42 may pass through the inside of the arm device 2 or be pulled along the arm device 2 outside the arm device 2, so that the driving mechanism 41 drives the power unit 31 to rotate around the predetermined axis L relative to the arm device 2 through the pulling wire 42.

From this, install actuating mechanism 41 on fuselage assembly 1 can be through acting as go-between 42, the power pack 31 that the pulling is located the outer end of horn device 2 rotates around predetermineeing axis L, in order to change unmanned aerial vehicle 100's flight gesture, for example, change flight direction etc., therefore, install in fuselage assembly 1 through actuating mechanism 41 with among the drive arrangement 4, thereby can make full use of fuselage assembly 1's space, be favorable to improving unmanned aerial vehicle 100's overall structure compactness, and can make unmanned aerial vehicle 100's complete machine focus comparatively concentrate, structural stability is high, compare in the scheme of installing drive arrangement 4 in horn device 2, can reduce the bearing of horn device 2, improve the life of horn device 2.

And, because can rotate around predetermineeing axis L through drive power unit 31, thereby only need set up two horn devices 2, the rotational speed of screw 312 is adjusted in the cooperation simultaneously, can adjust unmanned aerial vehicle 100's flight gesture, therefore need not to set up 4 again, 6, more horn devices such as 8, change flight direction with the mode through the rotational speed of adjusting the screw on the different horn devices, therefore, can reduce the use quantity of horn device 2, thereby can improve unmanned aerial vehicle 100's small and exquisite and compactness of structure, and can reduce unmanned aerial vehicle 100's cost.

In some embodiments, in connection with fig. 6, the predetermined axis L coincides with or is parallel to the central axis L5 of the outer end of the horn device 2. Therefore, the driving mechanism 41 installed on the fuselage assembly 1 can pull the power unit 31 located at the outer end of the arm device 2 to rotate around the preset axis L through the pull wire 42, so that the propeller 312 rotates around the preset axis L relative to the arm device 2, thereby changing the flight state of the unmanned aerial vehicle 100 more simply, reliably and effectively, for example, changing the flight direction, and the like, thereby reducing the number of the arm devices 2 used, for example, 4, 6, 8, and the like, without setting more arm devices 2, changing the flight direction by adjusting the rotating speed of the propeller 312 on different arm devices 2, but changing the flight direction by rotating the power unit 31 through the driving device 4, so that the unmanned aerial vehicle 100 can only adopt two arm devices 2, thereby making the structure of the unmanned aerial vehicle 100 simpler, smaller and more compact in size, and the like, The whole structure is more compact.

Note that, when the flight direction of the drone 100 is controlled by the drive device 4, for example, when the drone 100 flies in a vertical direction, the propeller 312 provides the drone 100 with a vertically upward lift, and the resultant force applied to the unmanned aerial vehicle 100 is in a vertical upward direction (it should be explained that the main force applied to the unmanned aerial vehicle 100 at this time may be a vertical upward lifting force and a gravity applied to the unmanned aerial vehicle 100 itself, and the lifting force is greater than the gravity), the propeller 312 can be driven by the driving device 4 to rotate around the preset axis L to incline to a certain angle relative to the arm device 2, at this time, the direction of the force provided by the propeller 312 is correspondingly changed, the direction of the resultant force applied to the unmanned aerial vehicle 100 is also correspondingly changed, for example, if the propeller 312 rotates forward, the resultant force tilts forward, and the drone 100 flies forward; similarly, the propellers 312 recline to rotate, then resultant force reclines, and the unmanned aerial vehicle 100 flies backward and so on, and in addition, through adjusting the rotational speed of the propellers 312 on two horn devices 2 respectively, the unmanned aerial vehicle 100 can also realize actions such as turning left and right, and no description is given here.

In some embodiments of the present invention, as shown in fig. 4, the power unit 3 may further include: the mounting assembly 32, the mounting assembly 32 may include a mounting post 321 and a rotating post 322, the mounting post 321 is connected to an outer end of the boom device 2, the power motor 311 is connected to the rotating post 322, the pull wire 42 is connected to the rotating post 322, the rotating post 322 is in a rotation fit with the mounting post 321, and when the pull wire 42 pulls the rotating post 322 to rotate relative to the mounting post 321, the power unit 31 is rotated relative to the boom device 2 around the preset axis L. That is to say, when rotating post 322 and rotating relative erection column 321 through the pulling wire 42 pulling, rotate post 322 and just can drive motor 311 and rotate, motor 311 can drive screw 312 and rotate when rotating to change unmanned aerial vehicle 100's flight direction, moreover, installation component 32's simple structure, simple to operate.

In some embodiments of the present invention, the rotating post 322 is rotatably sleeved outside the mounting post 321 or rotatably disposed through the mounting post 321, so that the pulling wire 42 pulls the rotating post 322 to rotate around a central axis of the mounting post 321, where the central axis of the mounting post 321 is a predetermined axis L. Thus, the mounting post 321 can more simply and effectively limit the rotation post 322, and the rotational stability of the rotation post 322 can be improved.

In some embodiments of the present invention, as shown in fig. 4, the outer peripheral wall of the rotation post 322 has driving arms 323 respectively located at two sides of the rotation post 322 (where the two sides refer to two sides of a plane passing through the axis of the rotation post 322), the pulling wires 42 are respectively connected to the driving arms 323 at two sides, and the driving mechanism 41 pulls the driving arms 323 at two sides to move oppositely through the pulling wires 42, for example, in the example shown in fig. 4, one pulling wire 42 moves upward and the other pulling wire 42 moves downward to pull the rotation post 322 to rotate. Thus, the pull wire 42 can simply and efficiently pull the rotation post 322 to rotate.

In some embodiments, when the rotating post 322 is rotatably disposed through the mounting post 321, a plurality of through holes may be formed in a side arm of the mounting post 321, the driving arm 323 on the rotating post 322 in the mounting post 321 extends out of the through hole to be fixedly connected to the power motor 311, and the driving arm 323 may move in the through hole, so that the rotating post 322 can rotate relative to the mounting post 321 within a certain angle range, and thus the rotating post 322 can drive the power motor 311 to rotate.

In some embodiments, as shown in fig. 4, the power device 3 may further include a bearing member 324, when the rotating post 322 is rotatably sleeved outside the mounting post 321, the rotating post 322 is rotatably sleeved outside the mounting post 321 through the bearing member 324, when the rotating post 322 is rotatably disposed inside the mounting post 321, the rotating post 322 is rotatably disposed inside the mounting post 321 through the bearing member 324, thereby, when the rotating post 322 rotates around the central axis of the mounting post 321, the bearing member 324 may be utilized to avoid a problem of an excessive friction force when the rotating post 322 and the mounting post 321 are directly contacted and rotated, and a problem of wear when the rotating post 322 and the mounting post 321 are directly contacted and rotated, and further, flexibility and reliability when the rotating post 322 rotates around the central axis of the mounting post 321 can be improved. However, the present invention is not limited thereto, and the mounting post 321 and the rotating post 322 may be made of wear-resistant material.

For example, in some embodiments of the present invention, as shown in fig. 5, the outer circumferential wall of the rotation column 322 may have two driving arms 323 spaced apart along the circumference of the rotation column 322 (for example, the two driving arms 323 may be respectively located at two sides of the diameter direction of the rotation column 322), and as shown in fig. 4 and 6, the driving device 4 may include two pulling wires 42, each pulling wire 42 having a first end 421 and a second end 422, the first ends 421 of the two pulling wires 42 being respectively connected to the driving mechanism 41, the second ends 422 of the two pulling wires 42 being respectively connected to the two driving arms 323, and the driving mechanism 41 being configured to drive the two pulling wires 42 to move relatively to pull the rotation column 322 to rotate. Therefore, the pull wire 42 can simply and effectively pull the rotating post 322 to rotate, and the connection between the rotating post 322 and the pull wire 42 is convenient. Of course, the present invention is not limited thereto, for example, in other embodiments of the present invention, the driving device 4 may further include only one pulling wire, both ends of the pulling wire are respectively connected to the two driving arms 323, and the rotation of the rotation column 322 may also be driven by winding the pulling wire forward and backward.

It should be noted that, when the power motor 311 is connected to the rotating column 322, the power motor 311 may be directly connected to the rotating column 322, or may be indirectly connected to the rotating column 322, for example, in the specific embodiment shown in fig. 4, the power unit 31 further includes a support member 313 and a fixing frame 314, and the power motor 311 is connected to the rotating column 322 under the combined action of the support member 313 and the fixing frame 314 (for example, the support member 313 is located above the rotating column 322 and fixed at the bottom of the power motor 311, and the fixing frame 314 surrounds the bottom of the rotating column 322 and is fixedly connected to the rotating column 322 and the support member 313), so that the power motor 311 is more firmly installed, and the stability and reliability of the power unit 31 during rotation are further improved.

In some embodiments of the present invention, as shown in fig. 4, the power unit 3 may further include: pulley assembly 33, pulley assembly 33 includes a support frame 331 and a pulley 332, support frame 331 is connected to the outer end of the arm device 2, pulley 332 is rotatably installed on support frame 331, and the pull wire 42 is guided by pulley 332. Therefore, the pulley 332 can be fixed on the arm device 2 through the support frame 331, and the guide direction of the wire 42 is changed by the guide sliding action of the pulley 332, so that the working efficiency of the driving device 4 can be improved.

For example, in a specific example, as shown in fig. 5, the pulley assembly 33 may include a support frame 331 and two pulleys 332, the support frame 331 is connected to the outer end of the arm device 2, the two pulleys 332 are respectively rotatably mounted on the support frame 331, and the two pull wires 42 are respectively guided and slid by the two pulleys 332. Therefore, the pulley 332 can be fixed on the arm device 2 through the support frame 331, and the guide direction of the two wires 42 is changed through the guide sliding action of the pulley 332, so that the working effectiveness of the driving device 4 can be improved.

In some embodiments of the present invention, as shown in fig. 6 and 7, the driving mechanism 41 may include: adaptor 411 and steering wheel 412, adaptor 411 include center post 4111 and rotor arm 4112, and on the periphery wall of center post 4111 was located to rotor arm 4112, it linked to each other with rotor arm 4112 to act as go-between 42, steering wheel 412 links to each other with adaptor 411 to drive adaptor 411 rotates around the axis of center post 4111. From this, actuating mechanism 41's simple structure, convenient processing, and convenient control when driving unmanned aerial vehicle 100 and turning to, the reliability is high.

As shown in fig. 8, the adaptor 411 may include a central column 4111 and two rotating arms 4112, the two rotating arms 4112 are disposed on the outer peripheral wall of the central column 4111 and are spaced apart from each other along the circumferential direction of the central column 4111 (for example, the two rotating arms 4112 may be respectively located on two sides of the central column 4111 in the diameter direction), as shown in fig. 6, the first end portions 421 of the two pull wires 42 are respectively connected to the two rotating arms 4112, and the steering engine 412 is connected to the adaptor 411 (where "connected" may be directly connected to each other or indirectly connected to each other), so as to drive the adaptor 411 to rotate around the central axis of the central column 4111. From this, actuating mechanism 41's simple structure, convenient processing, and convenient control when driving unmanned aerial vehicle 100 and turning to, the reliability is high.

For example, in some embodiments of the present invention, as shown in fig. 6 to fig. 8, when the steering engine 412 drives the adaptor 411 to rotate around the central axis of the central column 4111, the two rotating arms 4112 may be driven to rotate, so that the rotation of the rotating arms 4112 can drive the pull wires 42 to move relatively (i.e., the moving directions of the two pull wires 42 are opposite), so as to pull the rotating column 322 to rotate, thereby driving the propeller 312 to rotate, and changing the flight direction. For example, in some embodiments, after the steering engine 412 drives the adaptor 411 to rotate clockwise by a certain angle to change the flight direction and fly to a predetermined position, the steering engine 412 can drive the adaptor 411 to rotate counterclockwise by a certain angle to complete the flight actions of the drone 100, such as hovering or reverse flight.

The number of the driving arm 323, the rotating arm 4112, and the pulling wire 42 is not limited to 2, and may be four, six, eight, or the like. In addition, the number of the pulleys 332 is not limited to 2, for example, the number of the pulleys may be one or more, and the pulleys may be replaced by rollers or the like, which is not described herein.

For example, in some embodiments of the present invention, as shown in fig. 6 to 8, the steering engine 412 is indirectly connected to the adaptor 411, for example, the driving mechanism 41 may further include: drive assembly 413, drive assembly 413 may include: the steering engine 412 is installed outside the installation shell 4131, the gear set 4132 is contained in the installation shell 4131, a driving shaft of the steering engine 412 extends into the installation shell 4131 and is connected with a first-stage gear 41321 of the gear set 4132, one end of the output shaft 4133 extends into the installation shell 4131 and is connected with a last-stage gear 41322 of the gear set 4132, and the other end of the output shaft 4133 extends out of the installation shell 4131 and is connected with a central column 4111.

From this, steering wheel 412 is not directly continuous with adaptor 411, thereby can utilize gear train 4132 to produce the effect of speed reduction or acceleration rate, and then can set up the steering wheel 412 of different power according to the circumstances of difference, for example, when gear train 4132 is reduction gear train, can utilize reduction gear train's characteristic, when drive arrangement 4 drive power device 3, realize the fine setting of fine setting screw 312 inclination, thereby can improve the flight direction's of unmanned aerial vehicle 100 controllability, simultaneously, can also utilize meshing pivoted characteristic between the gear of each grade in gear train 4132, realize when steering wheel 412 stop work, make the stay wire 42 can keep in this position, thereby further improve the stability of the controllability and the flight of unmanned aerial vehicle 100.

In some embodiments of the present invention, as shown in fig. 8, a central shaft hole 41111 may be formed in the central column 4111, a positioning hole 41112 may be formed on a side wall of the central column 4111, as shown in fig. 7, the other end of the output shaft 4133 is inserted into the central shaft hole 41111, and a positioning column 41331 is formed on an outer peripheral wall of the other end of the output shaft 4133, as shown in fig. 6, the positioning column 41331 is inserted into the positioning hole 41112, so that the output shaft 4133 drives the adaptor 411 to rotate. From this, the equipment of adaptor 411 and output shaft 4133 is convenient, can also utilize reference column 41331 and locating hole 41112's cooperation simultaneously, avoids output shaft 4133 and center post 4111 to take place relative rotation for reliability when steering wheel 412 drive adaptor 411 rotates around the axis of center post 4111. In addition, adaptor 411's simple structure, processing is convenient, and manufacturing cost is lower.

In some embodiments of the present invention, as shown in fig. 3, the horn device 2 may include: the horn body 21 and the horn end seat 22, the one end of horn body 21 links to each other with fuselage assembly 1, the horn end seat 22 is installed in the other end of horn body 21, combine fig. 4, the horn end seat 22 includes first section 221 and second section 222, outside the other end of horn body 21 was located to first section 221 cover, one end in the both ends on the second section 222 extending direction links to each other with first section 221, the other end is used for installing power device 3, second section 222 is as the outer end of horn device 2, and the axis of second section 222 is the axis L5 of the outer end of horn device 2 promptly, thereby it coincides or is parallel with the axis of second section 222 to explain predetermined axis L.

From this, the horn device 2's simple structure, the processing degree of difficulty is lower, and horn body 21 and horn end seat 22 can machine shaping respectively to improve production efficiency, satisfy different actual requirements, for example, can process the horn body 21 of different length as required, process the horn end seat 22 of different shapes as required simultaneously, in addition, when the other end of horn body 21 was located to first section 221 cover, can also improve the structural strength of junction.

As shown in fig. 3, the central axis of the second segment 222 (i.e., the central axis L5 of the outer end of the horn device 2) may coincide with or intersect at an obtuse angle with the central axis L6 of the horn body 21. When the coincidence, convenient processing and manufacturing, when crossing obtuse angle, can adjust the resultant force direction that horn device 2 receives for unmanned aerial vehicle 100 realizes flying forward more easily.

In some embodiments of the present invention, as shown in fig. 1 to 3, the unmanned aerial vehicle 100 may include two arm devices 2, two power devices 3, and two driving devices 4, wherein one power device 3 is mounted at an outer end of each arm device 2, and the power unit 31 in each power device 3 is driven to rotate by one driving device 4. From this, through setting up two horn devices 2, can reduce unmanned aerial vehicle 100's volume to reduce unmanned aerial vehicle 100's occupation space. In addition, when unmanned aerial vehicle 100 flies, can rotate the same or different inclination through controlling two drive arrangement 4 drives power pack 31 that is located two horn device 2 outer ends respectively to and adjust power pack 31's rotational speed, accomplish actions such as advancing, reversing, turn in order to realize unmanned aerial vehicle 100, the operation is comparatively simple.

Furthermore, in some embodiments of the present invention, as shown in fig. 1 to 3, the fuselage assembly 1 may further include: the storage device 11, the power supply device 12, the movement device 13, the landing gear 14 and the like. Undercarriage 14 is fixed in the stability of fuselage assembly 1 below in order to guarantee that unmanned aerial vehicle 100 takes off and lands, and storage device 11 is carried and is used for the splendid attire to wait to spray or the article of waiting to transport in fuselage assembly 1, and power supply unit 12 is fixed in and provides electric power for unmanned aerial vehicle 100 on the fuselage assembly 1, and core device 13 is fixed in fuselage assembly 1 for control unmanned aerial vehicle 100's flight.

As shown in fig. 1 and 9, the body assembly 1 further includes an assembly body 15, a first mounting frame 16, a second mounting frame 17 and a partition plate 18, and the assembly body 15 may include a top plate 151 and a bottom plate 152 for carrying the movement device 13 and the driving device 4. Thereby, the structure of the body assembly 1 is made compact.

As shown in fig. 3 and 9, the fuselage assembly 1 may have a central line L8, and in the extending direction of the central line L8, the assembly body 15, the first mounting frame 16 and the second mounting frame 17 are sequentially connected, wherein the storage device 11 and the power supply device 12 are respectively disposed in the first mounting frame 16 and the second mounting frame 17, so that the fuselage assembly 1 is compact in structure, and the storage device 11 and the power supply device 12 are respectively disposed in the first mounting frame 16 and the second mounting frame 17, which is convenient for a user to take down the storage device 11 for operations such as charging, and for a user to take down the power supply device 12 for operations such as charging, and is convenient for installation.

Of course, the present invention is not limited thereto, and the locations of the storage device 11 and the power supply device 12 may be interchanged, for example, the storage device 11 is mounted on the second mounting frame 17, the power supply device 12 is mounted on the first mounting frame 16, and so on, which will not be described herein, but considering that the weight of the storage device 11 may be reduced during the operation of the unmanned aerial vehicle 100, the storage device 11 may be disposed in the middle of the whole machine, but the center is not required, so that the whole machine may be more easily kept in balance, which is beneficial to the smoothness of flight.

As shown in fig. 9, the first mounting frame 16 may include a fixing plate 161 fixedly coupled to the assembly body 15 and two first coupling plates 162 coupled to both ends of the fixing plate, the two first coupling plates 162 are symmetrically disposed about a center line L8, the second mounting frame 17 may include two second coupling plates 171 and two third coupling plates 172, the two second coupling plates 171 are symmetrically disposed about a center line L8, the two third coupling plates 172 are symmetrically disposed about a center line L8, one ends of the two second coupling plates 171 are respectively coupled to ends of the two first coupling plates 162 far from the fixing plate 161, the two third coupling plates 172 are respectively coupled to the other ends of the two second coupling plates 171, the partition plate 18 is located between the first mounting frame 16 and the second mounting frame 17, and the partition plate 18 is coupled to a side of the two second coupling plates 171 near the first coupling plate 161, such that the first mounting frame 16 and the second mounting frame 17 define a first mounting space 160 and a second mounting space 170, the magazine 11 may be mounted to the first mounting space 160, and the power supply device 12 may be mounted to the second mounting space 170. From this, first installing frame 16 and second installing frame 17's simple structure, the processing of being convenient for to unmanned aerial vehicle 100's manufacturing cost can further be reduced.

In the description herein, references to the description of the term "one embodiment," "some embodiments," "an example," "a specific example," or "some examples," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the invention. In this specification, the schematic representations of the terms used above are not necessarily intended to refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples. Furthermore, various embodiments or examples and features of different embodiments or examples described in this specification can be combined and combined by one skilled in the art without contradiction.

While embodiments of the invention have been shown and described, it will be understood by those of ordinary skill in the art that: various changes, modifications, substitutions and alterations can be made to the embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the claims and their equivalents.

Claims

1. A drone (100), characterized in that it comprises:

a fuselage assembly (1);

the device comprises a machine arm device (2), wherein the two ends of the length of the machine arm device (2) are respectively an inner end and an outer end, and the inner end of the machine arm device (2) is arranged on the machine body assembly (1);

the power device (3), the power device (3) is installed at the outer end of the horn device (2), the power device (3) comprises a power unit (31), and the power unit (31) comprises a power motor (311) and a propeller (312) installed on the power motor (311); and

drive arrangement (4), drive arrangement (4) include actuating mechanism (41) and act as go-between (42), actuating mechanism (41) install in fuselage assembly (1), act as go-between (42) with actuating mechanism (41) with power device (3) link to each other respectively, so that actuating mechanism (41) pass through act as go-between (42) drive power unit (31) are relative horn device (2) are rotated around predetermineeing axis (L).

2. The drone (100) according to claim 1, characterized in that the preset axis (L) coincides with or is parallel to a median axis (L5) of the outer end of the horn device (2).

3. The drone (100) of claim 1, wherein the power device (3) further comprises:

installation component (32), installation component (32) are including erection column (321) and rotation post (322), erection column (321) with horn device (2) the outer end links to each other, driving motor (311) with rotation post (322) link to each other, act as go-between (42) with rotation post (322) link to each other, rotation post (322) with erection column (321) normal running fit, and act as go-between (42) pulling it is relative to rotate post (322) when erection column (321) rotates, make power unit (31) are relative horn device (2) wind predetermine axis (L) and rotate.

4. The unmanned aerial vehicle (100) of claim 3, wherein the rotation post (322) is rotatably sleeved outside the mounting post (321) or rotatably disposed through the mounting post (321) so as to pull the rotation post (322) to rotate around a central axis of the mounting post (321) at the pull wire (42), and the central axis of the mounting post (321) is the preset axis (L).

5. The unmanned aerial vehicle (100) of claim 3, wherein the outer peripheral wall of the rotating column (322) is provided with driving arms (323) respectively located at two sides of the rotating column (322), the pull wire (42) is respectively connected with the driving arms (323) at two sides, and the driving mechanism (41) pulls the driving arms (323) at two sides to move oppositely through the pull wire (42) so as to pull the rotating column (322) to rotate.

6. The drone (100) of claim 1, wherein the power device (3) further comprises:

pulley assembly (33), pulley assembly (33) includes support frame (331) and pulley (332), support frame (331) with the outer end of horn device (2) links to each other, pulley (332) rotationally install in support frame (331), stay wire (42) are by pulley (332) are led and are slided.

7. The drone (100) of claim 1, wherein the drive mechanism (41) comprises:

the adapter piece (411) comprises a center column (4111) and a rotating arm (4112), the rotating arm (4112) is arranged on the outer peripheral wall of the center column (4111), and the pull wire (42) is connected with the rotating arm (4112); and

the steering gear (412), steering gear (412) with adaptor (411) link to each other to the drive adaptor (411) are around the axis of center post (4111) rotates.

8. The drone (100) of claim 7, wherein the drive mechanism (41) further comprises:

a transmission assembly (413), the transmission assembly (413) comprising: the steering engine comprises an installation shell (4131), a gear set (4132) and an output shaft (4133), wherein the steering engine (412) is installed outside the installation shell (4131), the gear set (4132) is contained in the installation shell (4131), a driving shaft of the steering engine (412) extends into the installation shell (4131) and is connected with a primary gear (41321) of the gear set (4132), one end of the output shaft (4133) extends into the installation shell (4131) and is connected with a final gear (41322) of the gear set (4132), and the other end of the output shaft (4133) extends out of the installation shell (4131) and is connected with a central column (4111).

9. The unmanned aerial vehicle (100) of claim 8, wherein the central column (4111) has a central shaft hole (41111), a side wall of the central column (4111) has a positioning hole (41112), the other end of the output shaft (4133) is inserted into the central shaft hole (41111), and a peripheral wall of the other end of the output shaft (4133) has a positioning post (41331), and the positioning post (41331) is inserted into the positioning hole (41112), so that the output shaft (4133) drives the central column (4111) to rotate.

10. The drone (100) of claim 1, wherein the horn device (2) comprises:

the aircraft body (21), one end of the said aircraft body (21) couples to assembly of said fuselage (1);

horn end seat (22), horn end seat (22) install in the other end of horn body (21), horn end seat (22) include first section (221) and second section (222), first section (221) cover is located horn body (21) outside the other end, one end in the both ends on second section (222) extending direction with first section (221) link to each other, the other end is used for the installation power device (3), second section (222) conduct the outer end of horn device (2), just the axis of second section (222) does horn device (2) the axis (L5) of outer end.

11. The drone (100) of claim 10, wherein the central axis of the second section (222) coincides with or intersects the central axis (L6) of the horn body (21) at an obtuse angle.

12. The unmanned aerial vehicle (100) of any one of claims 1-11, wherein the unmanned aerial vehicle (100) comprises two of the horn devices (2), two of the power devices (3), and two of the driving devices (4), one of the power devices (3) is respectively mounted at an outer end of each of the horn devices (2), and the power unit (31) in each of the power devices (3) is respectively driven to rotate by one of the driving devices (4).