CN109466261A - A kind of land and air double-used multi-functional unmanned plane - Google Patents

A kind of land and air double-used multi-functional unmanned plane Download PDF

Info

Publication number
CN109466261A
CN109466261A CN201811359603.5A CN201811359603A CN109466261A CN 109466261 A CN109466261 A CN 109466261A CN 201811359603 A CN201811359603 A CN 201811359603A CN 109466261 A CN109466261 A CN 109466261A
Authority
CN
China
Prior art keywords
gear
land
unmanned plane
camera
engine
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.)
Withdrawn
Application number
CN201811359603.5A
Other languages
Chinese (zh)
Inventor
甘乾盛
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201811359603.5A priority Critical patent/CN109466261A/en
Publication of CN109466261A publication Critical patent/CN109466261A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60FVEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
    • 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
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/10Rotorcrafts
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00UAVs specially adapted for particular uses or applications
    • B64U2101/30UAVs specially adapted for particular uses or applications for imaging, photography or videography

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Transportation (AREA)
  • Manipulator (AREA)

Abstract

It is related that the present invention relates to a kind of unmanned planes, it in particular is a kind of land and air double-used multi-functional unmanned plane, including aviation mechanism, land forward mechanism, camera mechanism, the present apparatus can not only take photo by plane in the sky, track up can also be carried out in land, with extremely strong practicability, camera can be adjusted freely up and down, more convenient during taking photo by plane.Aviation mechanism is connected with the forward mechanism in land by fastening screw, and the forward mechanism in land is connect with camera mechanism movable contact, and the forward mechanism in land and camera mechanism are adapted by through-hole.

Description

A kind of land and air double-used multi-functional unmanned plane
Technical field
It is related that the present invention relates to a kind of unmanned planes, is in particular a kind of land and air double-used multi-functional unmanned plane.
Background technique
With the development of society, most of take photo by plane is shot by unmanned plane, although bringing convenient, nothing for shooting Man-machine in addition to shooting, there is no other use, in order to increase the practicability of unmanned plane, so designing a kind of land and air double-used more Function unmanned plane solves the problems, such as this.
Summary of the invention
The invention mainly solves the technical problem of providing a kind of land and air double-used multi-functional unmanned plane, the present apparatus not only may be used To take photo by plane in the sky, can also land carry out track up, have extremely strong practicability, camera can up and down from It is more convenient during taking photo by plane by adjusting.
In order to solve the above technical problems, being in particular a kind of land and air double-used the present invention relates to a kind of unmanned plane correlation Multi-functional unmanned plane, including aviation mechanism, land move ahead mechanism, camera mechanism, and the present apparatus can not only carry out in the sky It takes photo by plane, track up can also be carried out in land, there is extremely strong practicability, camera can be adjusted freely up and down, navigated It is more convenient during bat.
The aviation mechanism includes power spin paddle, device connecting rod, fixed connecting rod, and power spin paddle is mounted on dress One end of connecting rod is set, the other end of device connecting rod is connected with unmanned plane main casing by fastening screw, fixed connecting rod There are two numbers, and fixed connecting rod is meshed with device connecting rod by screw thread, the number of power spin paddle and device connecting rod There are three;
The forward mechanism in land includes unmanned plane main casing, power mechanism, land elevating mechanism, steering assembly, unmanned plane main casing It is connected with power mechanism by fastening screw, unmanned plane main casing is connect with land elevating mechanism movable contact, camera mechanism It is connect with unmanned plane main casing movable contact, steering assembly is mutually engaged with camera mechanism, steering assembly and land elevating mechanism phase Occlusion, power mechanism are mutually engaged with land elevating mechanism;
Power mechanism include gear one, gear fixing piece, gear two, gear three, engine gear, the fixed lid of engine, Wheel chain, engine, the fixed lid of engine are connected with engine by fastening screw, the fixed lid of engine and unmanned plane main casing It is connected by fastening screw, gear one is connected by gear fixing piece with unmanned plane main casing, gear one and engine gear It is connected by wheel chain, engine gear is connected with gear two by wheel chain, and gear two passes through gear fixing piece and nothing Man-machine main casing is connected, and gear two is engaged with gear three-phase, and gear three is connected by gear fixing piece with unmanned plane main casing, tooth Wheel one is mutually engaged with land elevating mechanism, and gear three is mutually engaged with land elevating mechanism, gear one, gear two, engine gear It is located in same horizontal line with gear three, engine gear is connected by welding with engine and connects;
Land elevating mechanism includes lifting drive gear, assistance for lifting gear, idler wheel power mechanism, lifting drive gear with Unmanned plane main casing is connected, and assistance for lifting gear is connected with unmanned plane main casing, lifting drive gear and idler wheel power mechanism phase Occlusion, idler wheel power mechanism are mutually engaged with lifting drive gear, and lifting drive gear is engaged with one phase of gear, lifting drive gear It is mutually engaged with steering assembly;
Idler wheel power mechanism include top layer sealing lifter plate, motor, T shape lifting tooth wheel shell, connection gear, middle rotating disk, Roller shaft, idler wheel, top layer sealing lifter plate are connected with motor by fastening screw, and motor passes through recessed with T shape lifting tooth wheel shell Slot is adapted, and top layer sealing lifter plate is connected by welding with T shape lifting tooth wheel shell to be connect, T shape lifting tooth wheel shell and connection gear It is connected, motor is mutually engaged with connection gear, and connection gear is connected with middle rotating disk by wheel chain, middle rotating disk and idler wheel Axis is connected by wheel chain, and roller shaft is connect with idler wheel movable contact, and middle rotating disk is connect with T shape lifting gear shell phase, top Layer sealing lifter plate is mutually engaged with motor, the uniform lifting drive gear of T shape lifting tooth wheel shell, and the number of roller shaft and idler wheel has Two, middle rotating disk, roller shaft and idler wheel are located in same horizontal line, wherein middle rotating disk is with connection gear positioned at same vertical On line;
Steering assembly includes L shape gear locating piece, tooth sector, and L shape gear locating piece is connected with tooth sector, is turned to Gear is mutually engaged with lifting drive gear, and tooth sector is mutually engaged with rotation gear, and L shape gear locating piece and unmanned plane main casing are logical It crosses to be weldingly connected and connect;
Camera mechanism includes camera rotating member, cylindrical connector, servo, sealing cover, is telescopically connected to bar, camera Connector, it is universal turn part, camera, auxiliary bearing, rotation gear, camera rotating member is connected by welding with cylindrical connector It connects, cylindrical connector is connected by welding with auxiliary bearing and connects, and auxiliary bearing is connected by welding with unmanned plane main casing and connects, rotation Gear is connected by welding with cylindrical connector and connects, and camera rotating member and servo are adapted by groove, servo with stretch One end of contracting connecting rod is fixedly connected, and the other end for being telescopically connected to bar is connected by welding with camera connector to be connect, sealing cover Be connected with camera rotating member by fastening screw, sealing cover and be telescopically connected to bar by through-hole be adapted, it is universal turn part with Camera connector is connected by fastening screw, and camera is mounted on universal turn on part;
Aviation mechanism is connected with the forward mechanism in land by fastening screw, the forward mechanism in land and the activity of camera mechanism It connects, the forward mechanism in land and camera mechanism are adapted by through-hole.
As advanced optimizing for the technical program, cylindricality described in a kind of land and air double-used multi-functional unmanned plane of the present invention There are two the number of connector, auxiliary bearing and rotation gear is equal.
As advanced optimizing for the technical program, auxiliary described in a kind of land and air double-used multi-functional unmanned plane of the present invention The material of bearing is bearing steel.
As advanced optimizing for the technical program, steering described in a kind of land and air double-used multi-functional unmanned plane of the present invention There are two the numbers of component.
As advanced optimizing for the technical program, land described in a kind of land and air double-used multi-functional unmanned plane of the present invention There are two the numbers of elevating mechanism.
As advanced optimizing for the technical program, flight described in a kind of land and air double-used multi-functional unmanned plane of the present invention There are two the numbers of mechanism, and position is symmetrical.
As advanced optimizing for the technical program, device described in a kind of land and air double-used multi-functional unmanned plane of the present invention Connecting rod, fixed connecting rod material be stainless steel.
A kind of land and air double-used multi-functional unmanned plane of the invention has the beneficial effect that
Land and air double-used multi-functional unmanned plane of the invention a kind of, the present apparatus can not only take photo by plane in the sky, can also be with Track up is carried out in land, there is extremely strong practicability, camera can be adjusted freely up and down, during taking photo by plane more What is added is convenient.
Detailed description of the invention
The present invention will be further described in detail with specific implementation method with reference to the accompanying drawing.
Fig. 1 is a kind of structural schematic diagram of the main view of land and air double-used multi-functional unmanned plane of the present invention.
Fig. 2 is a kind of structural schematic diagram of the form two of land and air double-used multi-functional unmanned plane of the present invention.
Fig. 3 is a kind of structural schematic diagram of the top view of land and air double-used multi-functional unmanned plane of the present invention.
Fig. 4 is a kind of structural schematic diagram of the aviation mechanism 1 of land and air double-used multi-functional unmanned plane of the present invention.
Fig. 5 is a kind of structural schematic diagram of the forward mechanism 2 in the land of land and air double-used multi-functional unmanned plane of the present invention.
Fig. 6 is a kind of structural schematic diagram of the power mechanism 2-2 of land and air double-used multi-functional unmanned plane of the present invention.
Fig. 7 is the cross-sectional structure schematic diagram of A-A in Fig. 5.
Fig. 8 is a kind of structural schematic diagram of the idler wheel power mechanism 2-3-3 of land and air double-used multi-functional unmanned plane of the present invention.
Fig. 9 is a kind of stereochemical structure signal of the middle rotating disk 2-3-3-5 of land and air double-used multi-functional unmanned plane of the present invention Figure.
Figure 10 is a kind of schematic perspective view of the steering assembly 2-4 of land and air double-used multi-functional unmanned plane of the present invention.
Figure 11 is a kind of structural schematic diagram of the camera mechanism 3 of land and air double-used multi-functional unmanned plane of the present invention.
In figure: aviation mechanism 1;Power spin paddle 1-1;Device connecting rod 1-2;Fixed connecting rod 1-3;Land moves ahead mechanism 2;Unmanned plane main casing 2-1;Power mechanism 2-2;One 2-2-1 of gear;Gear fixing piece 2-2-2;Two 2-2-3 of gear;Three 2- of gear 2-4;Engine gear 2-2-5;The fixed lid 2-2-6 of engine;Wheel chain 2-2-7;Engine 2-2-8;Land elevating mechanism 2- 3;Lifting drive gear 2-3-1;Assistance for lifting gear 2-3-2;Idler wheel power mechanism 2-3-3;Top layer seals lifter plate 2-3-3- 1;Motor 2-3-3-2;T shape lifting tooth wheel shell 2-3-3-3;Connection gear 2-3-3-4;Middle rotating disk 2-3-3-5;Roller shaft 2-3- 3-6;Idler wheel 2-3-3-7;Steering assembly 2-4;L shape gear locating piece 2-4-1;Tooth sector 2-4-2;Camera mechanism 3;Camera shooting Head rotating member 3-1;Cylindrical connector 3-2;Servo 3-3;Sealing cover 3-4;It is telescopically connected to bar 3-5;Camera connector 3-6; It is universal to turn part 3-7;Camera 3-8;Auxiliary bearing 3-9;Rotate gear 3-10.
Specific embodiment
Specific embodiment 1:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11, the present invention relates to a kind of unmanned planes In particular correlation is a kind of land and air double-used multi-functional unmanned plane, including aviation mechanism 1, the forward mechanism 2 in land, camera shooting Head mechanism 3, the present apparatus can not only take photo by plane in the sky, can also carry out track up in land, have extremely strong reality With property, camera can be adjusted freely up and down, more convenient during taking photo by plane.
The aviation mechanism 1 includes power spin paddle 1-1, device connecting rod 1-2, fixed connecting rod 1-3, power spin Paddle 1-1 is mounted on one end of device connecting rod 1-2, and the other end and unmanned plane main casing 2-1 of device connecting rod 1-2 passes through fastening spiral shell Nail is connected, and there are two the numbers of fixed connecting rod 1-3, and fixed connecting rod 1-3 and device connecting rod 1-2 is mutually nibbled by screw thread There are three the number of conjunction, power spin paddle 1-1 and device connecting rod 1-2 are equal;
The forward mechanism 2 in land includes unmanned plane main casing 2-1, power mechanism 2-2, land elevating mechanism 2-3, steering assembly 2- 4, unmanned plane main casing 2-1 are connected with power mechanism 2-2 by fastening screw, unmanned plane main casing 2-1 and land elevating mechanism 2-3 Movable contact connection, camera mechanism 3 are connect with unmanned plane main casing 2-1 movable contact, steering assembly 2-4 and camera mechanism 3 It is mutually engaged, steering assembly 2-4 is engaged with land elevating mechanism 2-3 phase, and power mechanism 2-2 is engaged with land elevating mechanism 2-3 phase;
Power mechanism 2-2 includes one 2-2-1 of gear, gear fixing piece 2-2-2, two 2-2-3 of gear, three 2-2-4 of gear, hair The fixed lid 2-2-6, wheel chain 2-2-7, engine 2-2-8 of motivation gear 2-2-5, engine, the fixed lid 2-2-6 of engine and hair Motivation 2-2-8 is connected by fastening screw, and the fixed lid 2-2-6 of engine is connected with unmanned plane main casing 2-1 by fastening screw It connects, one 2-2-1 of gear is connected by gear fixing piece 2-2-2 with unmanned plane main casing 2-1, one 2-2-1 of gear and engine tooth Wheel 2-2-5 is connected by wheel chain 2-2-7, and engine gear 2-2-5 is connected with two 2-2-3 of gear by wheel chain 2-2-7 It connects, two 2-2-3 of gear is connected by gear fixing piece 2-2-2 with unmanned plane main casing 2-1, two 2-2-3 of gear and three 2- of gear 2-4 phase is engaged, and three 2-2-4 of gear is connected by gear fixing piece 2-2-2 with unmanned plane main casing 2-1, one 2-2-1 of gear and land Ground elevating mechanism 2-3 phase is engaged, and three 2-2-4 of gear is engaged with land elevating mechanism 2-3 phase, one 2-2-1 of gear, two 2-2- of gear 3, engine gear 2-2-5 and three 2-2-4 of gear are located in same horizontal line, and engine gear 2-2-5 and engine 2-2-8 are logical It crosses to be weldingly connected and connect, start engine 2-2-8, engine 2-2-8 drives engine gear 2-2-5, engine gear 2-2-5 band Moving gear one 2-2-1, engine gear 2-2-5 are also with two 2-2-3 of moving gear, gear two 2-2-3 band three 2-2-4 of moving gear;
Land elevating mechanism 2-3 includes lifting drive gear 2-3-1, assistance for lifting gear 2-3-2, idler wheel power mechanism 2- 3-3, lifting drive gear 2-3-1 are connected with unmanned plane main casing 2-1, assistance for lifting gear 2-3-2 and unmanned plane main casing 2-1 phase Connection, lifting drive gear 2-3-1 are engaged with idler wheel power mechanism 2-3-3 phase, idler wheel power mechanism 2-3-3 and lifting drive tooth Wheel 2-3-1 phase is engaged, and lifting drive gear 2-3-1 is engaged with one 2-2-1 phase of gear, lifting drive gear 2-3-1 and steering group Part 2-4 phase is engaged, the liter of lifting drive gear 2-3-1 and assistance for lifting gear 2-3-2 cooperation realization idler wheel power mechanism 2-3-3 Drop;
Idler wheel power mechanism 2-3-3 includes top layer sealing lifter plate 2-3-3-1, motor 2-3-3-2, T shape lifting tooth wheel shell 2-3-3-3, connection gear 2-3-3-4, middle rotating disk 2-3-3-5, roller shaft 2-3-3-6, idler wheel 2-3-3-7, top layer sealing rise Drop plate 2-3-3-1 is connected with motor 2-3-3-2 by fastening screw, motor 2-3-3-2 and T shape lifting tooth wheel shell 2-3-3-3 It is adapted by groove, top layer sealing lifter plate 2-3-3-1 and T shape lifting tooth wheel shell 2-3-3-3, which is connected by welding, to be connect, T shape Lifting tooth wheel shell 2-3-3-3 is connected with connection gear 2-3-3-4, and motor 2-3-3-2 is engaged with connection gear 2-3-3-4 phase, Connection gear 2-3-3-4 is connected with middle rotating disk 2-3-3-5 by wheel chain, middle rotating disk 2-3-3-5 and roller shaft 2-3- 3-6 is connected by wheel chain, and roller shaft 2-3-3-6 is connect with idler wheel 2-3-3-7 movable contact, middle rotating disk 2-3-3-5 and T Shape lifting tooth wheel shell 2-3-3-3 is connected, and top layer seals lifter plate 2-3-3-1 and motor 2-3-3-2, T shape lifting tooth wheel shell 2- The uniform lifting drive gear 2-3-1 phase of 3-3-3 is engaged, there are two the number of roller shaft 2-3-3-6 and idler wheel 2-3-3-7 are equal, in Rotating disk 2-3-3-5, roller shaft 2-3-3-6 and idler wheel 2-3-3-7 are located in same horizontal line, wherein middle rotating disk 2-3-3-5 It is located in same vertical line with connection gear 2-3-3-4, starts motor 2-3-3-2, motor 2-3-3-2 drives connection gear 2-3- Rotating disk 2-3-3-5, middle rotating disk 2-3-3-5 drive roller shaft 2-3-3-6 in 3-4, connection gear 2-3-3-4 drive, thus Rotate idler wheel 2-3-3-7, the purpose that realization device moves on the ground, top layer sealing lifter plate 2-3-3-1 plays constant zero The effect of part and connection;
Steering assembly 2-4 include L shape gear locating piece 2-4-1, tooth sector 2-4-2, L shape gear locating piece 2-4-1 with Tooth sector 2-4-2 is connected, and tooth sector 2-4-2 is engaged with lifting drive gear 2-3-1 phase, tooth sector 2-4-2 and rotation Rotating disk 3-10 phase is engaged, and L shape gear locating piece 2-4-1 is connected by welding with unmanned plane main casing 2-1 and connects, the positioning of L shape gear Part 2-4-1 plays the role of fixed tooth sector 2-4-2, tooth sector 2-4-2 play change it is nyctitropic;
Camera mechanism 3 includes camera rotating member 3-1, cylindrical connector 3-2, servo 3-3, sealing cover 3-4, stretches Connecting rod 3-5, camera connector 3-6, it is universal turn part 3-7, camera 3-8, auxiliary bearing 3-9, rotation gear 3-10, camera shooting Head rotating member 3-1 is connected by welding with cylindrical connector 3-2 to be connect, and cylindrical connector 3-2 and auxiliary bearing 3-9 passes through welding phase Connection, auxiliary bearing 3-9 are connected by welding with unmanned plane main casing 2-1 and connect, and rotation gear 3-10 and cylindrical connector 3-2 passes through It is weldingly connected and connects, camera rotating member 3-1 and servo 3-3 are adapted by groove, servo 3-3 and are telescopically connected to bar 3-5 One end be fixedly connected, the other end for being telescopically connected to bar 3-5 is connected by welding with camera connector 3-6 to be connect, sealing cover 3-4 Be connected with camera rotating member 3-1 by fastening screw, sealing cover 3-4 and be telescopically connected to bar 3-5 by through-hole be adapted, ten thousand Be connected to part 3-7 is turned with camera connector 3-6 by fastening screw, camera 3-8 be mounted on it is universal turn on part 3-7, ten thousand It can adjust the shooting angle of camera 3-8 to part 3-7 is turned, servo 3-3 drive is telescopically connected to bar 3-5 and moves up, to make Camera 3-8 is shunk, and realizes that forward mechanism 2 of camera mechanism 3 and land is adapted by through-hole, sealing cover 3-4 plays fixation The effect of part, auxiliary bearing 3-9 play the role of auxiliary rotation;
Aviation mechanism 1 is connected with the forward mechanism 2 in land by fastening screw, the forward mechanism 2 in land and camera mechanism 3 Movable contact connection, the forward mechanism 2 in land are adapted with camera mechanism 3 by through-hole.
Specific embodiment 2:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11, present embodiment is to embodiment One is described further, the cylindrical connector 3-2, auxiliary bearing 3-9 and rotate gear 3-10 number it is equal there are two.
Specific embodiment 3:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11, present embodiment is to embodiment One is described further, and the material of the auxiliary bearing 3-9 is bearing steel.
Specific embodiment 4:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11, present embodiment is to embodiment One is described further, and there are two the numbers of the steering assembly 2-4.
Specific embodiment 5:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11, present embodiment is to embodiment One is described further, and there are two the numbers of the land elevating mechanism 2-3.
Specific embodiment 6:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11, present embodiment is to embodiment One is described further, and there are two the numbers of the aviation mechanism 1, and position is symmetrical.
Specific embodiment 7:
Illustrate present embodiment below with reference to Fig. 1,2,3,4,5,6,7,8,9,10,11, present embodiment is to embodiment One is described further, the device connecting rod 1-2, fixed connecting rod 1-3 material be stainless steel.
The application method of device: starting unmanned plane, for unmanned plane when taking photo by plane, the universal part 3-7 that turns can adjust camera The shooting angle of 3-8.
When unmanned plane landing, servo 3-3 drive is telescopically connected to bar 3-5 and moves up, to make camera 3-8 It shrinks, realizes that forward mechanism 2 of camera mechanism 3 and land is adapted by through-hole, start engine 2-2-8, engine 2-2-8 Engine gear 2-2-5 is driven, engine gear 2-2-5 band one 2-2-1 of moving gear, one 2-2-1 of gear drive lifting drive tooth 2-3-1 is taken turns, lifting drive gear 2-3-1 is engaged with idler wheel power mechanism 2-3-3 phase, to make under idler wheel power mechanism 2-3-3 Drop, while lifting drive gear 2-3-1 rotates tooth sector 2-4-1, tooth sector 2-4-2 drives rotation gear 3-10 to turn It is dynamic, to realize that camera rotating member 3-1 rotates, to realize that camera mechanism 3 rotates to top by lower section, wherein asessory shaft It holds 3-9 and plays the role of auxiliary rotation, engine gear 2-2-5 is also with two 2-2-3 of moving gear, gear two 2-2-3 band moving gear Three 2-2-4, three 2-2-4 of gear drive the lifting drive gear 2-3-1 of the other side, three 2-2-4 of middle gear to play change direction Effect.
After device completes above-mentioned adjustment, unmanned plane is made to drop to ground, starts motor 2-3-3-2, motor 2-3-3-2 band Rotating disk 2-3-3-5, middle rotating disk 2-3-3-5 drive idler wheel in dynamic connection gear 2-3-3-4, connection gear 2-3-3-4 drive Axis 2-3-3-6, so that idler wheel 2-3-3-7 is rotated, the purpose that realization device moves on the ground, and camera mechanism 3 at this time Positioned at the top of device, can be shot.
Make when device flies in the sky, camera mechanism 3 can also be adjusted to the top of device by above-mentioned method, It at this time can scene right above filming apparatus.
The present apparatus can not only take photo by plane in the sky, can also carry out track up in land, have extremely strong reality With property, camera can be adjusted freely up and down, more convenient during taking photo by plane.
Certainly, above description is not limitation of the present invention, and the present invention is also not limited to the example above, the art The variations, modifications, additions or substitutions that those of ordinary skill is made within the essential scope of the present invention also belong to guarantor of the invention Protect range.

Claims (7)

1. a kind of land and air double-used multi-functional unmanned plane, including aviation mechanism (1), land forward mechanism (2), camera mechanism (3), it is characterised in that: the aviation mechanism (1) includes power spin paddle (1-1), device connecting rod (1-2), is fixedly connected Bar (1-3), power spin paddle (1-1) are mounted on one end of device connecting rod (1-2), the other end of device connecting rod (1-2) with Unmanned plane main casing (2-1) is connected by fastening screw, and there are two the numbers of fixed connecting rod (1-3), fixed connecting rod (1-3) It is meshed with device connecting rod (1-2) by screw thread, the number of power spin paddle (1-1) and device connecting rod (1-2) has three It is a;
The land mechanism (2) that moves ahead includes unmanned plane main casing (2-1), power mechanism (2-2), land elevating mechanism (2-3), steering group Part (2-4), unmanned plane main casing (2-1) are connected with power mechanism (2-2) by fastening screw, unmanned plane main casing (2-1) and land The connection of ground elevating mechanism (2-3) movable contact, camera mechanism (3) are connect with unmanned plane main casing (2-1) movable contact, steering group Part (2-4) is mutually engaged with camera mechanism (3), and steering assembly (2-4) is mutually engaged with land elevating mechanism (2-3), power mechanism (2-2) is mutually engaged with land elevating mechanism (2-3);
Power mechanism (2-2) includes gear one (2-2-1), gear fixing piece (2-2-2), gear two (2-2-3), three (2- of gear 2-4), fixed lid (2-2-6), wheel chain (2-2-7), engine (2-2-8) of engine gear (2-2-5), engine, engine Fixed lid (2-2-6) is connected with engine (2-2-8) by fastening screw, the fixed lid (2-2-6) of engine and unmanned owner Shell (2-1) is connected by fastening screw, and gear one (2-2-1) passes through gear fixing piece (2-2-2) and unmanned plane main casing (2-1) It is connected, gear one (2-2-1) is connected with engine gear (2-2-5) by wheel chain (2-2-7), engine gear (2- 2-5) it is connected with gear two (2-2-3) by wheel chain (2-2-7), gear two (2-2-3) passes through gear fixing piece (2-2-2) It is connected with unmanned plane main casing (2-1), gear two (2-2-3) is mutually engaged with gear three (2-2-4), and gear three (2-2-4) passes through Gear fixing piece (2-2-2) is connected with unmanned plane main casing (2-1), and gear one (2-2-1) is mutually stung with land elevating mechanism (2-3) It closes, gear three (2-2-4) is mutually engaged with land elevating mechanism (2-3), gear one (2-2-1), gear two (2-2-3), engine Gear (2-2-5) and gear three (2-2-4) are located in same horizontal line, and engine gear (2-2-5) and engine (2-2-8) are logical It crosses to be weldingly connected and connect;
Land elevating mechanism (2-3) includes lifting drive gear (2-3-1), assistance for lifting gear (2-3-2), idler wheel power mechanism (2-3-3), lifting drive gear (2-3-1) are connected with unmanned plane main casing (2-1), assistance for lifting gear (2-3-2) and nobody Owner's shell (2-1) is connected, and lifting drive gear (2-3-1) is mutually engaged with idler wheel power mechanism (2-3-3), idler wheel power mechanism (2-3-3) is mutually engaged with lifting drive gear (2-3-1), and lifting drive gear (2-3-1) is mutually engaged with gear one (2-2-1), Lifting drive gear (2-3-1) is mutually engaged with steering assembly (2-4);
Idler wheel power mechanism (2-3-3) includes top layer sealing lifter plate (2-3-3-1), motor (2-3-3-2), T shape lifting gear Shell (2-3-3-3), connection gear (2-3-3-4), middle rotating disk (2-3-3-5), roller shaft (2-3-3-6), idler wheel (2-3-3- 7), top layer sealing lifter plate (2-3-3-1) is connected with motor (2-3-3-2) by fastening screw, motor (2-3-3-2) and T Shape lifting tooth wheel shell (2-3-3-3) is adapted by groove, and top layer seals lifter plate (2-3-3-1) and T shape lifting tooth wheel shell (2- It 3-3-3) is connected by welding and connects, T shape lifting tooth wheel shell (2-3-3-3) is connected with connection gear (2-3-3-4), motor (2- It 3-3-2) is mutually engaged with connection gear (2-3-3-4), connection gear (2-3-3-4) and middle rotating disk (2-3-3-5) pass through gear Chain is connected, and middle rotating disk (2-3-3-5) is connected with roller shaft (2-3-3-6) by wheel chain, roller shaft (2-3-3-6) with The connection of idler wheel (2-3-3-7) movable contact, middle rotating disk (2-3-3-5) are connected with T shape lifting tooth wheel shell (2-3-3-3), push up Layer sealing lifter plate (2-3-3-1) and the uniform lifting drive gear of motor (2-3-3-2), T shape lifting tooth wheel shell (2-3-3-3) (2-3-1) is mutually engaged, there are two the number of roller shaft (2-3-3-6) and idler wheel (2-3-3-7) is equal, middle rotating disk (2-3-3-5), Roller shaft (2-3-3-6) and idler wheel (2-3-3-7) are located in same horizontal line, wherein middle rotating disk (2-3-3-5) and tooth connection Wheel (2-3-3-4) is located in same vertical line;
Steering assembly (2-4) includes L shape gear locating piece (2-4-1), tooth sector (2-4-2), L shape gear locating piece (2-4- 1) it is connected with tooth sector (2-4-2), tooth sector (2-4-2) is mutually engaged with lifting drive gear (2-3-1), tooth sector (2-4-2) is mutually engaged with rotation gear (3-10), and L shape gear locating piece (2-4-1) passes through welding phase with unmanned plane main casing (2-1) Connection;
Camera mechanism (3) includes camera rotating member (3-1), cylindrical connector (3-2), servo (3-3), sealing cover (3- 4), be telescopically connected to bar (3-5), camera connector (3-6), it is universal turn part (3-7), camera (3-8), auxiliary bearing (3-9), It rotates gear (3-10), camera rotating member (3-1) is connected by welding with cylindrical connector (3-2) and connects, cylindrical connector (3- 2) it being connected by welding and connects with auxiliary bearing (3-9), auxiliary bearing (3-9) is connected by welding with unmanned plane main casing (2-1) and connects, Rotation gear (3-10) is connected by welding with cylindrical connector (3-2) to be connect, camera rotating member (3-1) and servo (3-3) It is adapted by groove, servo (3-3) is fixedly connected with the one end for being telescopically connected to bar (3-5), is telescopically connected to the another of bar (3-5) One end is connected by welding with camera connector (3-6) and connects, and sealing cover (3-4) and camera rotating member (3-1) pass through fastening Screw is connected, and sealing cover (3-4) and is telescopically connected to bar (3-5) and is adapted by through-hole, and universal part (3-7) and the camera of turning connects Fitting (3-6) is connected by fastening screw, and camera (3-8) is mounted on universal turn on part (3-7);
Aviation mechanism (1) and land move ahead mechanism (2) be connected by fastening screw, land moves ahead mechanism (2) and camera machine The connection of structure (3) movable contact, move ahead mechanism (2) and camera mechanism (3) of land are adaptable by through-hole.
2. the land and air double-used multi-functional unmanned plane of one kind according to claim 1, it is characterised in that: the cylindricality connection There are two the number of part (3-2), auxiliary bearing (3-9) and rotation gear (3-10) is equal.
3. the land and air double-used multi-functional unmanned plane of one kind according to claim 1, it is characterised in that: the auxiliary bearing The material of (3-9) is bearing steel.
4. the land and air double-used multi-functional unmanned plane of one kind according to claim 1, it is characterised in that: the steering assembly There are two the numbers of (2-4).
5. the land and air double-used multi-functional unmanned plane of one kind according to claim 1, it is characterised in that: the land lifting There are two the numbers of mechanism (2-3).
6. the land and air double-used multi-functional unmanned plane of one kind according to claim 1, it is characterised in that: the aviation mechanism (1) there are two numbers, and position is symmetrical.
7. the land and air double-used multi-functional unmanned plane of one kind according to claim 1, it is characterised in that: the device connection Bar (1-2), fixed connecting rod (1-3) material be stainless steel.
CN201811359603.5A 2018-11-15 2018-11-15 A kind of land and air double-used multi-functional unmanned plane Withdrawn CN109466261A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811359603.5A CN109466261A (en) 2018-11-15 2018-11-15 A kind of land and air double-used multi-functional unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811359603.5A CN109466261A (en) 2018-11-15 2018-11-15 A kind of land and air double-used multi-functional unmanned plane

Publications (1)

Publication Number Publication Date
CN109466261A true CN109466261A (en) 2019-03-15

Family

ID=65673423

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201811359603.5A Withdrawn CN109466261A (en) 2018-11-15 2018-11-15 A kind of land and air double-used multi-functional unmanned plane

Country Status (1)

Country Link
CN (1) CN109466261A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114537065A (en) * 2022-02-28 2022-05-27 重庆交通大学 Air-ground dual-purpose multifunctional unmanned aerial vehicle

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2005128893A (en) * 2005-09-15 2007-03-20 Открытое Акционерное общество Таганрогский Авиационный научно-технический комплекс им. Г.М. Бериева(RU) FLIGHT VEHICLE-CONVERPLOIN-AMPHIBIA (OPTIONS)
US20140034776A1 (en) * 2012-08-02 2014-02-06 Neurosciences Research Foundation Vehicle capable of in-air and on-ground mobility
US20150191246A1 (en) * 2012-11-14 2015-07-09 Illinois Institute Of Technology Hybrid aerial and terrestrial vehicle
CN106080070A (en) * 2016-08-03 2016-11-09 安徽啄木鸟无人机科技有限公司 One can self-service change type land and air double-used aircraft
CN106827992A (en) * 2017-03-07 2017-06-13 上海机电工程研究所 Land and air double-used six rotorcraft device
CN107284166A (en) * 2017-06-08 2017-10-24 杭州师范大学钱江学院 A kind of control method of land and air double-used rotor craft
CN107323192A (en) * 2017-06-21 2017-11-07 北京理工大学 A kind of air-ground amphibious mobile robot
CN108016225A (en) * 2017-12-29 2018-05-11 安徽理工大学 A kind of land and air double-used aircraft
CN108189633A (en) * 2017-12-20 2018-06-22 深圳先进技术研究院 A kind of land and air double-used machine people Reconnaissance system

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2005128893A (en) * 2005-09-15 2007-03-20 Открытое Акционерное общество Таганрогский Авиационный научно-технический комплекс им. Г.М. Бериева(RU) FLIGHT VEHICLE-CONVERPLOIN-AMPHIBIA (OPTIONS)
US20140034776A1 (en) * 2012-08-02 2014-02-06 Neurosciences Research Foundation Vehicle capable of in-air and on-ground mobility
US20150191246A1 (en) * 2012-11-14 2015-07-09 Illinois Institute Of Technology Hybrid aerial and terrestrial vehicle
CN106080070A (en) * 2016-08-03 2016-11-09 安徽啄木鸟无人机科技有限公司 One can self-service change type land and air double-used aircraft
CN106827992A (en) * 2017-03-07 2017-06-13 上海机电工程研究所 Land and air double-used six rotorcraft device
CN107284166A (en) * 2017-06-08 2017-10-24 杭州师范大学钱江学院 A kind of control method of land and air double-used rotor craft
CN107323192A (en) * 2017-06-21 2017-11-07 北京理工大学 A kind of air-ground amphibious mobile robot
CN108189633A (en) * 2017-12-20 2018-06-22 深圳先进技术研究院 A kind of land and air double-used machine people Reconnaissance system
CN108016225A (en) * 2017-12-29 2018-05-11 安徽理工大学 A kind of land and air double-used aircraft

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
马建: "陆空两栖机器人飞行系统设计", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114537065A (en) * 2022-02-28 2022-05-27 重庆交通大学 Air-ground dual-purpose multifunctional unmanned aerial vehicle

Similar Documents

Publication Publication Date Title
CN103029126B (en) Flexibly controllable joint driver
CN105501422A (en) All deflection propeller vector boost mechanism and underwater navigation vehicle
JPS6397495A (en) Pitch regulator for variable pitch propeller blade
CN109466261A (en) A kind of land and air double-used multi-functional unmanned plane
CN107719676A (en) It is a kind of to spray the intelligent agricultural plant protection unmanned plane precisely and having a smooth flight
CN102700701B (en) Vector propulsion system applied to small-size underwater unmanned aircraft
CN107486358A (en) Coating apparatus
CN103600631B (en) A kind of amphibious wheel mechanism based on eccentric paddle mechanism
CN109733571A (en) A kind of modularization underwater robot vector propulsion mechanism
CN113086149A (en) Multi-link mechanism based on VSP novel cycloidal propeller
CN213974406U (en) Underwater robot
CN103630119A (en) Image motion compensation device and method for aerial survey of unmanned aerial vehicle
CN106014491A (en) Novel turbofan engine blade adjusting mechanism with variable attack angle
CN203864996U (en) Tapered rotating flapping wing air vehicle
CN205854531U (en) Modular steering engine drives two axle many spellings camera aerial survey The Cloud Terraces
CN206766312U (en) High pulling torque self-locking steering wheel
CN107719672A (en) A kind of quick-detachable unmanned plane propeller fixed mechanism
CN113639595A (en) Steering engine system
CN203543557U (en) Amphibious vehicle wheel mechanism based on eccentric oar mechanism
CN110919689B (en) Joint driving device, joint robot with driving device and driving method
JPS61500487A (en) Automatic propeller pitch adjustment device
CN107031834A (en) Multi-rotor unmanned aerial vehicle variable propeller pitch device
CN213197606U (en) Servo-driven mechanical arm device
CN211442740U (en) Jet type vertical landing unmanned aerial vehicle
CN207326802U (en) A kind of regulation panel assembly being conveniently adjusted

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
WW01 Invention patent application withdrawn after publication

Application publication date: 20190315

WW01 Invention patent application withdrawn after publication