CN111824440A - Novel unmanned aerial vehicle - Google Patents

Novel unmanned aerial vehicle Download PDF

Info

Publication number
CN111824440A
CN111824440A CN202010720341.1A CN202010720341A CN111824440A CN 111824440 A CN111824440 A CN 111824440A CN 202010720341 A CN202010720341 A CN 202010720341A CN 111824440 A CN111824440 A CN 111824440A
Authority
CN
China
Prior art keywords
support
bracket
arm
paddle
driven
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN202010720341.1A
Other languages
Chinese (zh)
Other versions
CN111824440B (en
Inventor
金国强
金祚顺
辛华翔
丁晓俐
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guangzhou Litai Energy Technology Co ltd
Original Assignee
Zhejiang Dianchen Aviation Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Zhejiang Dianchen Aviation Technology Co ltd filed Critical Zhejiang Dianchen Aviation Technology Co ltd
Priority to CN202010720341.1A priority Critical patent/CN111824440B/en
Publication of CN111824440A publication Critical patent/CN111824440A/en
Application granted granted Critical
Publication of CN111824440B publication Critical patent/CN111824440B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • B64D47/08Arrangements of cameras
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/473Constructional features
    • B64C27/50Blades foldable to facilitate stowage of aircraft
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Forklifts And Lifting Vehicles (AREA)

Abstract

The invention discloses a novel unmanned aerial vehicle, which comprises a body, a bracket fixed below the body, and a paddle component connected with the body, wherein the paddle component comprises a paddle arm with a rod-shaped structure; the driving machine seat is connected to one end of the paddle arm; the foldable paddle is arranged on the driving base and driven to rotate by the rotary driving device, and the bracket comprises a supporting frame connected below the machine body, a first bracket arranged on the supporting frame, a second bracket rotationally connected to the bottom of the first bracket, and third brackets respectively connected to two ends of the second bracket and arranged perpendicular to the second bracket; a fixing bracket for fixing the camera body. The invention is provided with the bracket, can realize the adjustment of the camera body in multiple angles and positions, and is also provided with the foldable paddle which is folded when falling, thereby preventing the foldable paddle from being damaged due to the contact with the ground.

Description

Novel unmanned aerial vehicle
Technical Field
The invention relates to a novel unmanned aerial vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle controlled by a radio remote control device or an onboard computer program control system. The unmanned aerial vehicle has the advantages of simple structure and low use cost, not only can complete the task executed by the piloted aircraft, but also is more suitable for the task which is not suitable for being executed by the piloted aircraft. The emergency early warning device has great effects on emergency and early warning of emergencies. Unmanned aerial vehicles are usually equipped with a camera for surveying and mapping functions such as aerial photography, and such unmanned aerial vehicles in the prior art have at least the following defects:
(1) however, the angle and height of the camera in the prior art cannot be freely adjusted.
(2) During the normal landing or forced landing process of the unmanned aerial vehicle, the unmanned aerial vehicle is laterally turned over due to unstable landing or other reasons, so that the blades are smashed on the ground to break the blades.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle capable of solving the problems.
In order to solve the problems, the invention provides a novel unmanned aerial vehicle, which comprises a body, a bracket fixed below the body, and a paddle component connected with the body, and is characterized in that,
the blade assembly includes:
-a paddle arm of rod-like construction;
-a drive housing connected to one end of the paddle arm, the drive housing having a rotary drive mounted therein;
-a blade mounted on said driving frame and driven in rotation by rotary driving means, said rotating blade being foldable;
the bracket includes:
-a support frame connected below the fuselage, said support frame being provided with at least three legrest tubes for supporting with the ground,
-a first carriage mounted on said support frame, said first carriage being capable of an elevating movement and being provided with first braking means capable of stopping it during the elevating movement;
a second bracket rotatably connected to the bottom of the first bracket, the second bracket being horizontally disposed, being driven by a first rotating mechanism to rotate around the first bracket at a substantially middle position, and being provided with a second brake device for stopping the second bracket;
-a third support connected to two ends of the second support and arranged perpendicular to the second support, the third support being capable of telescopic movement along its length and being provided with a third brake device capable of stopping the third support during its telescopic movement;
the fixed support is used for fixing the camera body, two ends of the fixed support are respectively and rotatably connected to the free ends of the two third supports, the fixed support is driven to rotate by the second rotating mechanism and is provided with a fourth brake device for stopping the fixed support.
As a further improvement of the present invention, a first adjusting tube and a second adjusting tube are arranged above the driving machine base, wherein the upper end portion of the second adjusting tube is inserted into the first adjusting tube and is fixedly connected with the first adjusting tube, the second adjusting tube is provided with two first sliding chutes symmetrically arranged along the central axis of the second adjusting tube, the first sliding chutes penetrate through the inner wall and the outer wall of the second adjusting tube and the upper end surface and the lower end surface of the second adjusting tube, two first sliding blocks capable of being respectively inserted into the first sliding chutes are arranged in the first adjusting tube, and the first sliding blocks are driven by a lifting mechanism to slide in the first sliding chutes;
every the paddle is provided with two paddle bodies and fixes the connector in paddle body one end, the connector passes first spout and swivelling joint and is in the second is adjusted intraductal, the free end of connector is in first slider is located when the top stroke of first spout with the free end contact of connector, and by first slider is with it is spacing in the second is adjusted intraductal, works as first slider is located when the bottom stroke of first spout, the free end of connector can pass through first spout, and two adjacent the free end of connector passes through spring coupling.
As a further improvement of the present invention, a limiting groove is further provided on the side wall of the free end of the connecting body, the limiting groove is communicated with the side wall and the bottom wall of the free end of the connecting body, a rotating block is rotatably connected in the limiting groove, the rotating block is limited by the side wall of the limiting groove when being positioned in the limiting groove, the rotating block is limited by the bottom wall of the limiting groove when rotating out of the limiting groove and forming an angle of 90 ° with the limiting groove, and two ends of the spring are respectively connected to the side walls of the two rotating blocks.
As a further improvement of the invention, the second brake device and the fourth brake device both comprise a fixed disc and a movable disc, a plurality of telescopic rods are arranged on the fixed disc, and friction force for limiting relative movement of the telescopic rods and the movable disc is generated by the contact of the telescopic rods and the surface of the movable disc.
As a further improvement of the present invention,
the first support comprises a first support seat fixed below the support frame and vertically arranged, and a first support arm connected below the first support seat in a telescopic mode, and the first support arm is of a cylindrical structure.
The third support comprises a third support seat fixed at the end part of the second support and a third support arm which is connected to the third support seat and can do telescopic motion, and the third support arm is of a cylindrical structure.
As a further improvement of the present invention, each of the first and third brake devices includes two arc-shaped brake pads capable of moving relatively and reversely, and generating a frictional force for restricting the movement of the first or third support arm by contacting with a surface of the first or third support arm.
As a further improvement of the invention, the support frame comprises a support frame main body fixedly connected with the machine body, the support frame main body is provided with at least three extending arms, each extending arm is rotatably connected with a rotating arm, the foot frame tube is fixed on the rotating arm, and the rotating arm can be driven by a driving device to rotate.
As a further improvement of the present invention, one end of the fixing bracket is rotatably connected to one of the third brackets and is driven to rotate by a motor, and the other end of the fixing bracket is rotatably connected to the other third bracket and is provided with the fourth brake device.
As a further improvement of the invention, the lifting mechanism is an air cylinder driving one of the cross bars to lift.
As a further improvement of the invention, the first bracket and the third bracket are driven by a pneumatic device to do lifting movement or telescopic movement; the first rotating mechanism and the second rotating mechanism are both motors; the telescopic rod is driven by the pneumatic device to stretch, and the arc brake block is driven by the pneumatic device to move relatively or reversely.
The invention has the advantages that the camera body can be adjusted in multiple angles and positions by arranging the support, and the foldable paddle is folded when the camera body is descended, so that the camera body is prevented from being damaged due to contact with the ground.
Drawings
Fig. 1 is a schematic structural view of the present invention.
Fig. 2 is a schematic structural view of the stent of the present invention.
FIG. 3 is a top view of FIG. 2;
FIG. 4 is a schematic structural view of a second brake device and a fourth brake device;
FIG. 5 is a schematic structural view of the first brake device and the third brake device;
FIG. 6 is a schematic structural view of a blade assembly of the present invention;
FIG. 7 is a schematic view of the blade in a horizontal position;
FIG. 8 is a schematic structural view of the blade in an upright position;
in the figure: 1-paddle arm; 2-a support frame; 202-a scaffold tube; 204-a scaffold body; 206-a cantilever arm; 208-a rotating arm; 3-driving the engine base; 302-a first conditioning tube; 304-a second conditioning tube; 306-a first runner; 308-a first slider; 310-a second runner; 312-a second slider; 314-a crossbar; 4-a first scaffold; -a blade; 502-a blade body; 504-a linker; 506-a spring; 508-a limit groove; 510-a turning block; 512-first split; 514-a second body; 516-third division; 6-a second bracket; 7-a fuselage; 702-connecting the stent. 8-a third scaffold; 802-a third leg rest; 804-a third support arm; 10-a camera body; 12-a fixed support; 1402-fixing the disc; 1404-an active disk; 1406-telescoping pole; 1602-arc brake block.
Detailed Description
The technical scheme of the invention is further explained by the specific implementation mode in combination with the attached drawings.
As shown in fig. 1-8, the present invention includes
Comprises a machine body 7, a bracket fixed below the machine body 7 and a blade 5 component connected with the machine body 7, and is characterized in that,
the blade 5 assembly comprises:
a paddle arm 1 of rod-like construction;
a driving machine base 3 connected to one end of the paddle arm 1, wherein a rotary driving device is installed in the driving machine base 3;
a blade 5 mounted on said driving frame 3 and driven in rotation by rotary driving means, said rotating blade 5 being foldable;
the bracket includes:
a support frame 2 connected below the fuselage 7, said support frame 2 being provided with at least three foot tubes 202 for supporting with the ground,
a first support 4 mounted on said support frame 2, said first support 4 being capable of an elevating movement and being provided with first braking means capable of stopping it during the elevating movement;
a second bracket 6 rotatably connected to the bottom of the first bracket 4, the second bracket 6 being horizontally disposed, being driven by a first rotating mechanism in a substantially middle position thereof to rotate around the first bracket 4, and being provided with a second braking device for stopping the vehicle;
third brackets 8 respectively connected to both ends of the second bracket 6 and arranged perpendicular to the second bracket 6, wherein the third brackets 8 can perform telescopic movement along the length direction thereof and are provided with third brake devices capable of stopping the third brackets during the telescopic movement thereof;
a fixed bracket 12 for fixing the camera body 10, wherein two ends of the fixed bracket 12 are respectively rotatably connected to the free ends of the two third brackets 8, are driven by the second rotating mechanism to rotate, and are provided with a fourth brake device for stopping the camera body.
As a further improvement of the present invention, a first adjusting pipe 302 and a second adjusting pipe 304 whose upper end portion is inserted into the first adjusting pipe 302 and fixedly connected with the first adjusting pipe 302 are arranged above the driving machine base 3, the second adjusting pipe 304 is provided with two first sliding grooves 306 symmetrically arranged along a central axis thereof, the first sliding grooves 306 penetrate through an inner wall and an outer wall thereof and an upper end surface and a lower end surface thereof, two first sliding blocks 308 capable of being respectively inserted into the first sliding grooves 306 are arranged in the first adjusting pipe 302, and the first sliding blocks 308 are driven by a lifting mechanism to slide in the first sliding grooves 306;
each blade 5 is provided with two blade bodies 502 and a connecting body 504 fixed at one end of each blade body 502, each connecting body 504 passes through the corresponding first sliding groove 306 and is rotatably connected in the corresponding second adjusting pipe 304, the free end of each connecting body 504 is in contact with the free end of each connecting body 504 when the corresponding first sliding block 308 is located at the top stroke of the corresponding first sliding groove 306, the connecting bodies are limited in the corresponding second adjusting pipes 304 by the corresponding first sliding blocks 308, when the corresponding first sliding blocks 308 are located at the bottom stroke of the corresponding first sliding grooves 306, the free ends of the connecting bodies 504 can pass through the corresponding first sliding grooves 306, and the free ends of two adjacent connecting bodies 504 are connected through springs 506.
As a further improvement of the present invention, a limiting groove 508 is further disposed on a sidewall of the free end of the connecting body 504, the limiting groove 508 is communicated with a sidewall and a bottom wall of the free end of the connecting body 504, a rotating block 510 is rotatably connected in the limiting groove 508, the rotating block 510 is limited by the sidewall of the limiting groove 508 when being located in the limiting groove 508, the rotating block 510 is limited by the bottom wall of the limiting groove 508 when rotating out of the limiting groove 508 and forming an angle of 90 ° with the limiting groove 508, and two ends of the spring 506 are respectively connected to the sidewalls of the two rotating blocks 510.
As a further improvement of the present invention, the second brake device and the fourth brake device each comprise a fixed disc 1402 and a movable disc 1404, wherein a plurality of telescopic rods 1406 are disposed on the fixed disc 1402, and friction force for limiting relative movement is generated by the contact of the telescopic rods 1406 and the surface of the movable disc 1404.
As a further improvement of the present invention,
the first support 4 comprises a first support seat fixed below the support frame 2 and vertically arranged, and a first support arm connected below the first support seat in a telescopic manner, and the first support arm is of a cylindrical structure.
The third support 8 includes a third support base 802 fixed to an end of the second support 6 and a third support arm 804 connected to the third support base 802 and capable of performing a telescopic motion, and the third support arm 804 is a tubular structure.
As a further improvement of the present invention, each of the first brake device and the third brake device includes two arc-shaped brake pads 1602, and the arc-shaped brake pads 1602 can move relatively and reversely, and generate a friction force for limiting the movement of the first support arm or the third support arm by contacting with the surface of the first support arm or the third support arm 804.
As a further improvement of the present invention, the supporting frame 2 includes a supporting frame main body 204 fixedly connected to the body 7, the supporting frame main body 204 is provided with at least three protruding arms 206, each protruding arm 206 is rotatably connected to a rotating arm 208, the stand pipe 202 is fixed to the rotating arm 208, and the rotating arm 208 can be driven by a driving device to rotate.
As a further improvement of the present invention, one end of the fixing bracket 12 is rotatably connected to one of the third brackets 8 and is driven to rotate by a motor, and the other end is rotatably connected to the other third bracket 8 and is provided with the fourth brake device.
As a further improvement of the present invention, the lifting mechanism is a cylinder driving one of the cross bars 314 to lift.
As a further improvement of the invention, the first support 4 and the third support 8 are driven by a pneumatic device to do lifting movement or telescopic movement; the first rotating mechanism and the second rotating mechanism are both motors; the extension rod 1406 is driven by a pneumatic device to extend and retract, and the arc brake block 1602 is driven by the pneumatic device to move relatively or reversely.
As a further improvement of the present invention, one end of the fixing bracket 12 is rotatably connected to one of the third brackets 8 and is driven to rotate by a motor, and the other end is rotatably connected to the other third bracket 8 and is provided with the fourth brake device.
As a further improvement of the present invention, the lifting mechanism is a cylinder driving one of the cross bars 314 to lift.
As a further improvement of the present invention, the connecting body 504 includes a first sub-body 512 disposed at an obtuse angle with respect to the blade body 502, a second sub-body 514 fixed to the first sub-body 512 and disposed perpendicular thereto, and a third sub-body 516 connected to the second sub-body 514 and disposed at an obtuse angle therewith, the rotational connection position of the connecting body 504 and the first sliding groove 306 is located at the connection position of the first sub-body 512 and the second sub-body 514, and the limiting groove 508 and the rotating block 510 are located on the third sub-body 516.
As a further improvement of the present invention, two vertical second sliding grooves 310 are disposed in the first adjusting tube 302, a second sliding block 312 capable of sliding in the second sliding grooves 310 is disposed in the second sliding grooves 310, the two second sliding blocks 312 are fixedly connected to a horizontally disposed cross bar 314, and the bottom of the first sliding block 308 is fixed on the upper surface of the cross bar 314.
Folding principle of paddle
(1) During normal use, the cylinder drives the cross rod 314 to move upwards, so that the first sliding block 308 is on the top stroke of the first sliding groove 306, at the moment, the side surface of the first sliding block 308 is in contact with the third split 516 on the connecting body 504 and limits the third split 516 in the second adjusting pipe 304, meanwhile, the spring 506 compresses, deforms and stores the force of the spring 506, at the moment, the two blade bodies 502 are horizontally arranged, and the power output device on the driving base 3 drives the two blade bodies 502 to rotate through the first adjusting pipe 302 and the second adjusting pipe 304;
(2) when unmanned aerial vehicle descends, the cylinder drives horizontal pole 314 downstream, make first slider 308 be located its bottom stroke of playing, at this moment, third components of a whole that can function independently 516 on the connector 504 loses the limiting displacement of first slider 308, spring 506 releases spring 506 power and makes the connector 504 outwards strut, connector 504 is rotary motion around the pivot in the second regulating tube 304, thereby make 5 components of a whole that can function independently of paddle rotate to vertical position just, this vertical position is realized by turning block 510 and spacing groove 508, because spacing groove 508 has the spacing of two positions to turning block 510, when the lateral wall contact of turning block 510 and spacing groove 508, 5 components of a whole that can function independently of paddle was horizontal setting this moment, when the top wall contact of turning block 510 and spacing groove 508, paddle 5 is vertical setting.
Motion principle of camera
(1) The first support 4 is provided with a first support seat and a first support arm, the first support seat is fixed below the support frame 2, and the first support arm drives the second support 6 to do lifting motion under the driving of the cylinder;
(2) the middle part of the second bracket 6 is rotationally connected to the first bracket arm and is driven by a motor to rotate;
(3) the two ends of the second bracket 6 are connected with a horizontally arranged third bracket 8, a third bracket seat 802 of the third bracket 8 is fixed at the end part of the second bracket 6, and a third bracket arm 804 can do telescopic motion under the action of the cylinder;
(4) the third cylinder arms are rotatably connected with fixed brackets 12 for mounting the camera body 10, the free end of one third cylinder arm is connected with a motor, the fixed bracket 12 is driven to rotate by the motor, and the other third cylinder arm is provided with a fourth brake device for braking after the motor rotates;
(5) in addition, a first brake device and a third brake device are respectively arranged on the first support arm and the third support arm 804, the first brake device and the third brake device are respectively provided with two arc-shaped brake blocks 1602, the arc-shaped brake blocks 1602 move relatively under the action of the air cylinder to clamp the first support arm or the second support 6 arm, and braking is achieved.
(6) The second brake device comprises a fixed disc 1402 arranged on the first support 4 and a movable disc 1404 arranged on the second support 6, and an expansion link 1406 on the fixed disc 1402 expands and contracts under the action of the air cylinder to tightly push the movable disc 1404 to realize braking;
(7) the third brake device comprises a fixed disc 1402 arranged on one of the third brackets 8 and a movable disc 1404 arranged at one end of the fixed bracket 12, wherein the telescopic rod 1406 on the fixed disc 1402 stretches out and draws back under the action of the air cylinder to push against the movable disc 1404 to realize braking.
The technical principle of the present invention is described above in connection with specific embodiments. The description is made for the purpose of illustrating the principles of the invention and should not be construed in any way as limiting the scope of the invention. Based on the explanations herein, those skilled in the art will be able to conceive of other embodiments of the present invention without inventive effort, which would fall within the scope of the present invention.

Claims (10)

1. A novel unmanned aerial vehicle comprises a body (7), a bracket fixed below the body, and a paddle component connected with the body (7), and is characterized in that,
the blade assembly includes:
-a paddle arm (1) of rod-like construction;
-a drive housing (3) connected to one end of the paddle arm (1), the drive housing (3) having a rotational drive mounted therein;
-a blade (5) mounted on said driving frame (3) and driven in rotation by rotary driving means, said rotating blade (5) being foldable;
the bracket includes:
-a support frame (2) connected below the fuselage, said support frame (2) being provided with at least three legrest tubes (202) for supporting with the ground,
-a first carriage (4) mounted on said support frame (2), said first carriage (4) being capable of an elevating movement and being provided with first braking means capable of stopping it during the elevating movement;
-a second support (6) rotatably connected to the bottom of said first support (4), said second support (6) being arranged horizontally, being driven in a substantially central position by a first rotation mechanism in a rotary motion about said first support (4), and being provided with second braking means for stopping the vehicle;
-third brackets (8) respectively connected to both ends of the second bracket (6) and arranged perpendicular to the second bracket (6), the third brackets (8) being telescopically movable in their length direction and provided with third brake means enabling them to stop during their telescopic movement;
-a fixed bracket (12) for fixing the camera body (10), wherein both ends of the fixed bracket (12) are respectively and rotatably connected with the free ends of the two third brackets (8), the fixed bracket is driven by a second rotating mechanism to rotate, and a fourth brake device for stopping the fixed bracket is arranged.
2. The novel unmanned aerial vehicle of claim 1, wherein a first adjusting pipe (302) and a second adjusting pipe (304) with an upper end portion inserted into the first adjusting pipe (302) and fixedly connected with the first adjusting pipe (302) are arranged above the driving base (3), the second adjusting pipe (304) is provided with two first sliding grooves (306) symmetrically arranged along a central axis thereof, the first sliding grooves (306) penetrate through an inner wall and an outer wall thereof and an upper end surface and a lower end surface thereof, two first sliding blocks (308) capable of being respectively inserted into the first sliding grooves (306) are arranged in the first adjusting pipe (302), and the first sliding blocks (308) are driven by a lifting mechanism to slide in the first sliding grooves (306);
each paddle (5) is provided with two paddle bodies (502) and a connecting body (504) fixed at one end of each paddle body (502), each connecting body (504) penetrates through the corresponding first sliding groove (306) and is rotatably connected into the corresponding second adjusting pipe (304), the free end of each connecting body (504) is in contact with the free end of each connecting body (504) when the corresponding first sliding block (308) is located at the top stroke of the corresponding first sliding groove (306), the connecting bodies are limited in the corresponding second adjusting pipes (304) through the corresponding first sliding blocks (308), when the corresponding first sliding blocks (308) are located at the bottom stroke of the corresponding first sliding grooves (306), the free ends of the connecting bodies (504) can pass through the corresponding first sliding grooves (306), and the free ends of two adjacent connecting bodies (504) are connected through springs (506).
3. The novel unmanned aerial vehicle of claim 2, wherein a limiting groove (508) is further formed in a side wall of the free end of the connecting body (504), the limiting groove (508) is communicated with the side wall and the bottom wall of the free end of the connecting body (504), a rotating block (510) is rotatably connected in the limiting groove (508), the rotating block (510) is limited by the side wall of the limiting groove (508) when being located in the limiting groove (508), the rotating block (510) is limited by the bottom wall of the limiting groove (508) when rotating out of the limiting groove (508) and forming an angle of 90 degrees with the limiting groove, and two ends of the spring (506) are respectively connected to the side walls of the two rotating blocks (510).
4. The novel unmanned aerial vehicle of claim 3, wherein the second brake device and the fourth brake device each comprise a fixed disc (1402) and a movable disc (1404), a plurality of telescopic rods (1406) are arranged on the fixed disc (1402), and friction force for limiting relative movement of the telescopic rods (1406) is generated by surface contact of the telescopic rods (1406) and the movable disc (1404).
5. A new type of drone, according to claim 4,
the first support (4) comprises a first support seat fixed below the support frame (2) and vertically arranged and a first support arm connected below the first support seat in a telescopic mode, the first support arm is of a cylindrical structure, the third support (8) comprises a third support seat (802) fixed at the end of the second support (6) and a third support arm (804) connected to the third support seat (802) and capable of doing telescopic motion, and the third support arm (804) is of a cylindrical structure.
6. A novel unmanned aerial vehicle as claimed in claim 5, wherein the first and third brake devices each comprise two arcuate brake shoes (1602), the arcuate brake shoes (1602) being capable of relative and opposite movement, which generates frictional forces that limit movement of the first (404) or third (804) support arms by contact with surfaces of the first (404) or third (804) support arms.
7. The novel unmanned aerial vehicle of claim 6, wherein the support frame (2) comprises a support frame main body (204) fixedly connected with the fuselage, the support frame main body (204) is provided with at least three protruding arms (206), each protruding arm (206) is rotatably connected with a rotating arm (208), the foot stand pipe (202) is fixed on the rotating arm (208), and the rotating arm (208) can be driven by a driving device to rotate.
8. A new type of unmanned aerial vehicle according to claim 7, characterized in that the fixed support (12) is rotatably connected to one of the third supports (8) at one end and is driven to rotate by a motor, and is rotatably connected to the other third support (8) at the other end and is provided with the fourth brake device.
9. A novel drone according to claim 8, characterised in that the lifting mechanism is a pneumatic cylinder driving one of the crossbars (314) to lift.
10. A new type of unmanned aerial vehicle according to claim 9, characterized in that the first support (4) and the third support (8) are driven by pneumatic means to perform lifting or telescoping movements; the first rotating mechanism and the second rotating mechanism are both motors; the telescopic rod (1406) is driven by a pneumatic device to stretch, and the arc-shaped brake block (1602) is driven by the pneumatic device to move relatively or reversely.
CN202010720341.1A 2020-07-24 2020-07-24 Novel unmanned aerial vehicle Active CN111824440B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010720341.1A CN111824440B (en) 2020-07-24 2020-07-24 Novel unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010720341.1A CN111824440B (en) 2020-07-24 2020-07-24 Novel unmanned aerial vehicle

Publications (2)

Publication Number Publication Date
CN111824440A true CN111824440A (en) 2020-10-27
CN111824440B CN111824440B (en) 2023-07-28

Family

ID=72925194

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010720341.1A Active CN111824440B (en) 2020-07-24 2020-07-24 Novel unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN111824440B (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104176199A (en) * 2014-07-17 2014-12-03 武汉船用机械有限责任公司 Horizontal cable lifter brake structure
CN104696690A (en) * 2015-03-18 2015-06-10 零度智控(北京)智能科技有限公司 Onboard holder
CN206327559U (en) * 2016-12-13 2017-07-14 西安昂翼机器人科技有限公司 A kind of foldable cantilever rotor and its aircraft using the cantilever rotor
CN206694765U (en) * 2016-09-09 2017-12-01 深圳市大疆创新科技有限公司 A kind of unmanned plane of the load component and carry load component
CN208565338U (en) * 2018-01-26 2019-03-01 天津息通科技有限公司 A kind of self-regulation pneumatically operated brake
CN208699041U (en) * 2018-08-16 2019-04-05 深圳市奥贝尔电子有限公司 A kind of unmanned plane wing that can be folded
CN110104161A (en) * 2019-04-25 2019-08-09 北京理工大学 Folding fin unfolding mechanism and its method of deploying

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104176199A (en) * 2014-07-17 2014-12-03 武汉船用机械有限责任公司 Horizontal cable lifter brake structure
CN104696690A (en) * 2015-03-18 2015-06-10 零度智控(北京)智能科技有限公司 Onboard holder
CN206694765U (en) * 2016-09-09 2017-12-01 深圳市大疆创新科技有限公司 A kind of unmanned plane of the load component and carry load component
CN206327559U (en) * 2016-12-13 2017-07-14 西安昂翼机器人科技有限公司 A kind of foldable cantilever rotor and its aircraft using the cantilever rotor
CN208565338U (en) * 2018-01-26 2019-03-01 天津息通科技有限公司 A kind of self-regulation pneumatically operated brake
CN208699041U (en) * 2018-08-16 2019-04-05 深圳市奥贝尔电子有限公司 A kind of unmanned plane wing that can be folded
CN110104161A (en) * 2019-04-25 2019-08-09 北京理工大学 Folding fin unfolding mechanism and its method of deploying

Also Published As

Publication number Publication date
CN111824440B (en) 2023-07-28

Similar Documents

Publication Publication Date Title
US8321976B1 (en) Height adjustable apparatus with control arm
JPH0544507B2 (en)
CN109110700B (en) A tunnel overhauls operation locomotive that is used for operation platform of tunnel to overhaul and includes it
CN210526835U (en) Wing folding and unfolding mechanism suitable for variable-backswept-wing unmanned aerial vehicle
BR112012030095B1 (en) helicopter with fixed-pitch coaxial counter-rotation
CN107298137B (en) Lying type walking robot
CN116608389A (en) Monitoring system
CN207078313U (en) A kind of interlinking lifting structure undercarriage with cushioning effect
CN101723243A (en) Supporting mechanism
CN105667772B (en) Undercarriage and aircraft, aircraft landing method
JPH02200262A (en) Elevating/lowering mechanism for floor part supporting frame in laying stand and laying stand equipped with elevating/lowering mechanism
US7421748B1 (en) Support frame with articulating structures
CN112192608A (en) Robot head neck structure and robot
US3104103A (en) Merry-go-round
CN201082707Y (en) Movable concrete pump vehicle
CN111824440A (en) Novel unmanned aerial vehicle
CN202704979U (en) Operation platform lifter for assembling and maintaining large devices
CN110374490A (en) A kind of folded ladder
CN214697128U (en) Arm type lifting platform
CN111824439A (en) Unmanned aerial vehicle support
JP4515600B2 (en) Aircraft landing gear
ES2564139T3 (en) Tilt and fold device for a treadmill
CN109109834B (en) Vehicle auxiliary support device and vehicle with same
CN207693578U (en) A kind of rotary-type tablet DR equipment of console mode lifting platform
CN214495512U (en) Steel structure hoisting device for large-span air cinema

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
TA01 Transfer of patent application right
TA01 Transfer of patent application right

Effective date of registration: 20230628

Address after: Self prepared E21, Floor 2, No. 77, Nan'an Road, Liwan District, Guangzhou, Guangdong 510000 (office only)

Applicant after: Guangzhou Litai Energy Technology Co.,Ltd.

Address before: 322013 building 19, bazutang village, Niansanli street, Yiwu City, Jinhua City, Zhejiang Province

Applicant before: ZHEJIANG DIANCHEN AVIATION TECHNOLOGY CO.,LTD.

GR01 Patent grant
GR01 Patent grant