CN110816873A - Unmanned aerial vehicle transmission machine and transmission method thereof - Google Patents
Unmanned aerial vehicle transmission machine and transmission method thereof Download PDFInfo
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- CN110816873A CN110816873A CN201911109542.1A CN201911109542A CN110816873A CN 110816873 A CN110816873 A CN 110816873A CN 201911109542 A CN201911109542 A CN 201911109542A CN 110816873 A CN110816873 A CN 110816873A
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/40—Maintaining or repairing aircraft
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16N—LUBRICATING
- F16N31/00—Means for collecting, retaining, or draining-off lubricant in or on machines or apparatus
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- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C17/00—Arrangements for transmitting signals characterised by the use of a wireless electrical link
- G08C17/02—Arrangements for transmitting signals characterised by the use of a wireless electrical link using a radio link
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Abstract
The invention discloses an unmanned aerial vehicle transmission machine and a transmission method thereof, the unmanned aerial vehicle transmission machine comprises a bottom plate, wherein the front surface and the back surface of the bottom plate are fixedly connected with fixed rods, the top of each fixed rod is fixedly connected with a supporting rod, the top of the bottom plate is provided with a main motor, an empennage motor, a storage battery and a signal adapter, the side surface of the storage battery is provided with a data interface, a data lead is electrically connected between the data interface and the signal adapter, the front surface of the empennage motor is movably connected with an empennage motor rotating shaft, one end of the empennage motor rotating shaft, which is far away from the empennage motor, is fixedly connected with an empennage rotating disc, and the outer side of the empennage rotating disc is clamped with empennage blades. The problem that leads to unmanned aerial vehicle load to increase and the control degree of difficulty to increase like this.
Description
Technical Field
The invention relates to the field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle transmission machine and a transmission method thereof.
Background
Unmanned aircraft, abbreviated "drone" and abbreviated "UAV", is an unmanned aircraft that is operated by a radio remote control device and self-contained programmed control means, or autonomously by an onboard computer, either completely or intermittently, and is often more suited to tasks that are too "fool, dirty, or dangerous" than a manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.
Present unmanned aerial vehicle transmission all will correspond corresponding motor at a plurality of top wing paddle of during operation, to leading to the unmanned aerial vehicle load to increase and the control degree of difficulty to increase like this, and present unmanned aerial vehicle complex operation when changing machine oil, it is inconvenient to lead to adding machine oil and discharging machine oil, machine oil simultaneously with correspond between the rack utilization ratio not high enough.
Therefore, the market urgently needs to develop an unmanned aerial vehicle transmission machine and a transmission method thereof to help people solve the existing problems.
Practical contents
The invention aims to provide an unmanned aerial vehicle transmission machine and a transmission method thereof, and aims to solve the problems that in the background technology, a plurality of top wing blades are required to correspond to corresponding motors when in work, so that the load of the unmanned aerial vehicle is increased and the control difficulty is increased, the existing unmanned aerial vehicle is complicated to operate when engine oil is replaced, the engine oil is inconvenient to add and discharge, and the utilization rate of the engine oil between the engine oil and a corresponding rack is not high enough.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides an unmanned aerial vehicle transmission machine and transmission method thereof, includes the bottom plate, the front and the back of bottom plate all fixedly connected with dead lever, the top fixedly connected with bracing piece of dead lever, main motor, fin motor and battery and signal adapter are installed to the top of bottom plate, data interface has been seted up to the side of battery, electric connection has the data wire between data interface and the signal adapter.
Further preferably, the front face of the empennage motor is movably connected with an empennage motor rotating shaft, one end, far away from the empennage motor, of the empennage motor rotating shaft is fixedly connected with an empennage rotating disk, and empennage blades are clamped on the outer side of the empennage rotating disk.
Preferably, the front surface of the signal adapter is electrically connected with a switch, and a GPS signal transmitter is embedded in one side of the signal adapter, which is far away from the data wire.
Preferably, the top of the support rod is fixedly connected with a bottom cover, the back of the bottom cover is movably connected with a rotating shaft, the bottom cover is movably connected with a top cover through the rotating shaft, the front of the top cover is welded with a fixing block, the fixing block is positioned on the front of the bottom cover, a fixing screw penetrates through the front of the bottom cover, the top of the top cover is provided with a speed reducer and an engine oil inlet, and the bottom of the bottom cover is provided with an engine oil outlet.
Preferably, the top of the main motor is movably connected with a main motor rotating shaft, the inner sides of the bottom cover and the top cover are fixedly connected with a main turntable through the top of the main motor rotating shaft, a rack is installed on the outer side of the main turntable, and the main turntable is rotatably connected with a top wing turntable through the rack.
Preferably, the top of the top wing rotating disc is rotatably connected with a top wing rotating shaft through a speed reducer, the top end of the top wing rotating shaft is fixedly connected with a top wing rotating disc, and the outer side of the top wing rotating disc is fixedly connected with a top wing blade.
Preferably, the number of the fixing rods is two, the two fixing rods are parallel to each other, the two fixing rods are respectively located on the front side and the back side of the bottom plate, and the fixing rods are fixedly connected with the bottom plate.
Further preferably, the top wing rotating disks are provided with six, and the shortest distance between the six top wing rotating disks is greater than the total length of the two top wing blades.
Further preferably, the method comprises the following working steps:
s1, firstly, an operator adds engine oil through an engine oil inlet, a switch is turned on to start a power supply, and a control main board in the storage battery sends a signal to a GPS signal transmitter on the side surface of the signal adapter through a data lead;
s2, a handle on the hand of an operator is in butt joint connection with the GPS signal transmitter, and then the handle controls the tail motor and the main motor to start;
s3, ascending and descending and direction changing of the unmanned aerial vehicle are achieved through rotating speeds of the handle to the empennage motor, the main motor and the speed reducer, during flying, the empennage motor and the main motor are started firstly, then the main motor drives the main motor rotating shaft to rotate, then the main motor rotating shaft drives the main rotating disc to rotate, the rack on the outer side of the main rotating disc drives the top wing rotating disc to rotate, then the top wing rotating disc is driven to rotate through the top wing rotating shaft, then the top wing blades rotate at a high speed, meanwhile, the empennage motor is controlled to be started, further, the empennage motor drives the empennage motor rotating shaft to rotate, then, the empennage motor drives the empennage rotating disc to rotate, the emp;
s4, when the direction needs to be changed, the handle sends a signal to control the speed reducer to increase the rotating speed of the four top wing rotating shafts except the two top wing rotating shafts on the left side, so that the ascending force on the right side is increased, the right side is more than the left side through the airflow flow velocity, the left side is inclined downwards, and finally the unmanned aerial vehicle changes the direction to the left side;
s5, when the unmanned aerial vehicle needs to ascend, the handle sends a signal to control the speed reducer to increase the rotating speed of all top wing rotating shafts, and the unmanned aerial vehicle can ascend by increasing the flow speed of airflow;
s6, after the device is used, the handle controls the speed reducer to slowly reduce the rotating speed of the top wing rotating shaft, the handle controls the main motor to be turned off after the device is finally descended to the ground, then the handle controls the tail wing motor to be turned off, and finally the switch is turned off;
s7, when using, engine oil can be along with unmanned aerial vehicle' S flight and the contact of rack maximize, when needing to be changed engine oil, operating personnel opens the engine oil discharge port can with engine oil discharge.
Further preferably, the transmission method of the invention comprises the following steps: when flying, start fin motor and main motor earlier, then the main motor drives main motor shaft and rotates, then main motor shaft drives main carousel and rotates, the rack in the main carousel outside can drive the top wing carousel rotatory, drive the top wing rotary disk through the top wing pivot afterwards and rotate, the top wing paddle carries out high-speed the rotation afterwards, the simultaneous control fin motor starts, and then the fin motor drives fin motor shaft and rotates, it is rotatory that fin motor shaft drives the fin rotary disk afterwards, the fin motor drives the high-speed rotation of fin paddle through the fin rotary disk, last unmanned aerial vehicle carries out flight work.
Compared with the prior art, the invention has the beneficial effects that:
the invention is through the empennage motor, the main motor, the storage battery, the data interface, the data wire, the signal adapter, the GPS signal emitter and the speed reducer that are arranged, when the work is started, firstly the operator adds the engine oil through the engine oil inlet, the switch is turned on to start the power supply, the control mainboard in the storage battery sends a signal to the GPS signal emitter on the side surface of the signal adapter through the data wire, the handle on the hand of the operator is in butt joint connection with the GPS signal emitter, then the handle controls the empennage motor and the main motor to start, the rotation speed of the empennage motor, the main motor and the speed reducer is controlled by the handle to realize the ascending and descending and the direction changing of the unmanned aerial vehicle, when the flight, the empennage motor and the main motor are started firstly, then the main motor drives the main motor rotating shaft to rotate, then the main, then the top wing rotating disc is driven to rotate by the top wing rotating shaft, then the top wing paddle rotates at a high speed, the empennage motor is controlled to start, further the empennage motor drives the empennage motor rotating shaft to rotate, then the empennage motor drives the empennage rotating disc to rotate at a high speed by the empennage rotating disc, finally the unmanned aerial vehicle carries out flight work, when the direction needs to be changed, the handle sends out a signal, the control speed reducer raises the rotating speeds of the four top wing rotating shafts except for the two top wing rotating shafts on the left side, the rising force on the right side is increased, the right side is greater than the left side flowing speed by the airflow flowing speed, so that the left side is inclined downwards, finally the unmanned aerial vehicle changes the direction to the left side, when the direction needs to be raised, the handle sends out a, after using, the handle control speed reducer slowly reduces the rotational speed of top wing pivot, and it closes to descend at last to subaerial back handle control main motor, and then the handle is controlled the fin motor again and is closed, closes the switch at last, and when using, machine oil can be along with unmanned aerial vehicle's flight and the contact of rack maximize, and when needing to be changed machine oil, operating personnel opens the machine oil discharge port can with machine oil discharge.
The invention has the following advantages:
1. realized two motors and driven unmanned aerial vehicle, reduced the control degree of difficulty, alleviateed unmanned aerial vehicle's the purpose of load to solved current unmanned aerial vehicle transmission and all to correspond corresponding motor at a plurality of top wing paddles of during operation, to the problem that leads to the unmanned aerial vehicle load to increase and the control degree of difficulty to increase like this.
2. Realized that machine oil changes the convenience to solved current unmanned aerial vehicle complex operation's when changing machine oil purpose, leaded to adding machine oil and the inconvenient problem of discharging machine oil.
3. The purpose of high engine oil utilization rate is realized, and the problem that the utilization rate of the engine oil between the corresponding racks is not high enough is solved.
Drawings
FIG. 1 is a front view of the overall structure of the present invention;
FIG. 2 is a schematic view of the inner structure of the bottom cover and the top cover after being unfolded;
FIG. 3 is a partial structural view of the battery of the present invention;
fig. 4 is a flow chart of the operation of the present invention.
In the figure: 1. fixing the rod; 2. a support bar; 3. a base plate; 4. an empennage paddle; 5. a tail rotating disc; 6. a tail motor shaft; 7. a tail motor; 8. a main motor; 801. a main turntable; 802. a main motor shaft; 803. a storage battery; 804. a data interface; 9. a data conductor; 10. a signal adapter; 11. a switch; 12. a GPS signal transmitter; 13. fixing screws; 14. a fixed block; 15. a bottom cover; 1501. an engine oil outlet; 16. a top cover; 17. a rotating shaft; 18. a speed reducer; 19. a top wing shaft; 1901. a top wing turntable; 1902. a rack; 20. a top wing rotating disc; 21. a top wing paddle; 22. an engine oil inlet.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.
Referring to fig. 1-4, an embodiment of the present invention is shown: the utility model provides an unmanned aerial vehicle transmission machine and transmission method thereof, includes bottom plate 3, and the front of bottom plate 3 all is fixedly connected with dead lever 1 with the back, and the top fixedly connected with bracing piece 2 of dead lever 1, main motor 8, fin motor 7 and battery 803 and signal adapter 10 are installed to the top of bottom plate 3, and data interface 804 has been seted up to the side of battery 803, and electric connection has data wire 9 between data interface 804 and the signal adapter 10.
In this embodiment, specifically, the front surface of the empennage motor 7 is movably connected with an empennage motor rotating shaft 6, one end of the empennage motor rotating shaft 6, which is far away from the empennage motor 7, is fixedly connected with an empennage rotating disk 5, and the outer side of the empennage rotating disk 5 is clamped with empennage blades 4.
In this embodiment, specifically, the front surface of the signal adapter 10 is electrically connected to the switch 11, and a GPS signal transmitter 12 is embedded in a side of the signal adapter 10 away from the data wire 9.
In this embodiment, specifically, the top of the support rod 2 is fixedly connected with a bottom cover 15, the back of the bottom cover 15 is movably connected with a rotating shaft 17, the bottom cover 15 is movably connected with a top cover 16 through the rotating shaft 17, the front of the top cover 16 is welded with a fixing block 14, the fixing block 14 is located on the front of the bottom cover 15 and penetrates through a fixing screw 13, the top of the top cover 16 is provided with a speed reducer 18 and an engine oil inlet 22, and the bottom of the bottom cover 15 is provided with an engine oil outlet 1501.
In this embodiment, specifically, the top of the main motor 8 is movably connected with a main motor rotating shaft 802, the inner sides of the bottom cover 15 and the top cover 16 are fixedly connected with a main turntable 801 through the top of the main motor rotating shaft 802, the outer side of the main turntable 801 is provided with a rack 1902, and the main turntable 801 is rotatably connected with a top wing turntable 1901 through the rack 1902.
In this embodiment, specifically, the top of the top wing turntable 1901 is rotatably connected to a top wing rotating shaft 19 through a speed reducer 18, the top end of the top wing rotating shaft 19 is fixedly connected to a top wing rotating disk 20, and the outer side of the top wing rotating disk 20 is fixedly connected to a top wing blade 21.
In this embodiment, specifically, the fixing rods 1 are provided with two fixing rods 1, and the two fixing rods 1 are parallel to each other, and simultaneously the two fixing rods 1 are respectively located on the front and the back of the bottom plate 3, and the fixing rods 1 are fixedly connected with the bottom plate 3, so as to fix the bottom of the transmission machine.
In this embodiment, specifically, six top wing rotating disks 20 are provided, and the shortest distance between the six top wing rotating disks 20 is greater than the total length of two top wing blades 21, thereby preventing collision between the top wing blades 21.
In this embodiment, specifically, the following working steps are included:
s1, firstly, an operator adds engine oil through the engine oil inlet 22, turns on the switch 11 to start the power supply, and the control main board in the storage battery 803 sends a signal to the GPS signal transmitter 12 on the side surface of the signal adapter 10 through the data wire 9;
s2, connecting a handle on the hand of an operator with a GPS signal transmitter 12 in a butt joint mode, and then controlling the tail wing motor 7 and the main motor 8 to start by the handle;
s3, ascending and descending and direction changing of the unmanned aerial vehicle are achieved through rotating speeds of the empennage motor 7, the main motor 8 and the speed reducer 18 through the handle, when the unmanned aerial vehicle flies, the empennage motor 7 and the main motor 8 are started firstly, then the main motor 8 drives the main motor rotating shaft 802 to rotate, then the main motor rotating shaft 802 drives the main rotating disc 801 to rotate, the rack 1902 on the outer side of the main rotating disc 801 drives the top wing rotating disc 1901 to rotate, then the top wing rotating disc 20 is driven to rotate through the top wing rotating shaft 19, then the top wing blades 21 rotate at a high speed, meanwhile, the empennage motor 7 is controlled to be started, further the empennage motor 7 drives the empennage motor rotating shaft 6 to rotate, then the empennage motor rotating disc 5 is driven by the empennage motor 7 to rotate at;
s4, case when direction needs to be changed: the handle sends a signal to the left, the speed reducer 18 is controlled to increase the rotating speed of the four top wing rotating shafts 19 except the two top wing rotating shafts 19 on the left side, so that the ascending force on the right side is increased, the flow rate on the right side of the airflow is greater than that on the left side, the left side is inclined downwards, and finally the unmanned aerial vehicle changes direction to the left side;
s5, when the unmanned aerial vehicle needs to ascend, the handle sends a signal to control the speed reducer 18 to increase the rotating speed of all top wing rotating shafts 19, and the unmanned aerial vehicle can ascend by increasing the airflow speed;
s6, after the device is used, the handle control speed reducer 18 slowly reduces the rotating speed of the top wing rotating shaft 19, the handle controls the main motor 8 to be closed after the device is finally descended to the ground, then the handle controls the tail wing motor 7 to be closed, and finally the switch 11 is closed;
s7, when using, the contact of oil meeting along with unmanned aerial vehicle' S flight and rack 1902 maximize, when needing to change oil, operating personnel open oil discharge port 1501 with the oil discharge can.
In this embodiment, specifically, the transmission method of the present invention is: when flying, start fin motor 7 and main motor 8 earlier, main motor 8 drives main motor pivot 802 afterwards and rotates, main motor pivot 802 drives main carousel 801 afterwards and rotates, the rack 1902 in the main carousel 801 outside can drive top wing carousel 1901 rotatory, drive top wing rotary disk 20 through top wing pivot 19 afterwards and rotate, top wing paddle 21 carries out high-speed the rotation afterwards, the start of simultaneous control fin motor 7, and then fin motor 7 drives fin motor pivot 6 and rotates, fin motor pivot 6 drives fin rotary disk 5 rotatory afterwards, fin motor 7 drives fin paddle 4 high-speed the rotation through fin rotary disk 5, unmanned aerial vehicle carries out flight work at last.
Further, in the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", and the like, indicate orientations and positional relationships based on those shown in the drawings, and are used only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.
Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically defined otherwise.
The working principle is as follows: when the unmanned aerial vehicle starts working, firstly, an operator adds engine oil through the engine oil adding opening 22, the switch 11 is turned on to start the power supply, the control main board in the storage battery 803 sends a signal to the GPS signal transmitter 12 on the side surface of the signal adapter 10 through the data wire 9, the handle on the hand of the operator is in butt joint connection with the GPS signal transmitter 12, then the handle controls the tail motor 7 and the main motor 8 to start, the ascending and descending and the direction changing of the unmanned aerial vehicle are realized through the rotating speed of the tail motor 7, the main motor 8 and the speed reducer 18 through the handle, during flying, the tail motor 7 and the main motor 8 are started firstly, then the main motor 8 drives the main motor rotating shaft 802 to rotate, then the main motor rotating shaft 802 drives the main rotating disc 801 to rotate, the rack 1902 on the outer side of the main rotating disc 801 drives the top wing rotating disc 1901 to rotate, then the top wing rotating disc 20 is, control fin motor 7 simultaneously and start, and then fin motor 7 drives fin motor shaft 6 and rotates, and fin motor shaft 6 drives fin rotary disk 5 rotatory afterwards, and fin motor 7 drives fin paddle 4 through fin rotary disk 5 and rotates at a high speed, and last unmanned aerial vehicle carries out flight work, when needs redirecting the time example: leftwards, the handle sends a signal, the speed reducer 18 is controlled to increase the rotating speed of the four top wing rotating shafts 19 except the two top wing rotating shafts 19 on the left side, so that the ascending force on the right side is increased, the right side is greater than the left side flowing speed through the airflow flowing speed, the left side is downwards inclined, finally, the unmanned aerial vehicle changes the direction to the left side, when the unmanned aerial vehicle needs to ascend, the handle sends a signal, the speed reducer 18 is controlled to increase the rotating speed of all the top wing rotating shafts 19, the unmanned aerial vehicle realizes the position ascending through the increase of the airflow flowing speed, after the unmanned aerial vehicle is used, the rotating speed of the top wing rotating shafts 19 is slowly reduced through the handle control speed reducer 18, finally, the handle controls the main motor 8 to be closed after the unmanned aerial vehicle descends to the ground, then the handle controls the tail wing motor 7 to be closed, finally, the switch, the operator opens the oil discharge port 1501 to discharge the oil.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof, and it is therefore intended that the present embodiments be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (10)
1. The utility model provides an unmanned aerial vehicle driving machine and transmission method thereof, includes bottom plate (3), its characterized in that: the utility model discloses a signal adapter, including bottom plate (3), the equal fixedly connected with dead lever (1) in front and the back of bottom plate (3), the top fixedly connected with bracing piece (2) of dead lever (1), main motor (8), fin motor (7) and battery (803) and signal adapter (10) are installed to the top of bottom plate (3), data interface (804) have been seted up to the side of battery (803), electric connection has data wire (9) between data interface (804) and signal adapter (10).
2. The unmanned aerial vehicle transmission machine and the transmission method thereof according to claim 1, wherein: the front swing joint of fin motor (7) has fin motor shaft (6), the one end fixedly connected with fin rotary disk (5) of fin motor (7) are kept away from in fin motor shaft (6), the outside joint of fin rotary disk (5) has fin paddle (4).
3. The unmanned aerial vehicle transmission machine and the transmission method thereof according to claim 1, wherein: the front surface of the signal adapter (10) is electrically connected with a switch (11), and a GPS signal transmitter (12) is embedded in one side of the signal adapter (10) far away from the data wire (9).
4. The unmanned aerial vehicle transmission machine and the transmission method thereof according to claim 1, wherein: the top fixedly connected with bottom (15) of bracing piece (2), the back swing joint of bottom (15) has rotation axis (17), bottom (15) have top cap (16) through rotation axis (17) swing joint, the front welding of top cap (16) has fixed block (14), fixed block (14) are located the front of bottom (15) and have run through fixed screw (13), speed reducer (18) and machine oil inlet (22) are installed at the top of top cap (16), machine oil discharge port (1501) has been seted up to the bottom of bottom (15).
5. The unmanned aerial vehicle transmission machine and the transmission method thereof according to claims 1 and 4, wherein: the top swing joint of main motor (8) has main motor shaft (802), bottom (15) and the inboard top fixedly connected with main carousel (801) of main motor shaft (802) of passing through of top (16), rack (1902) are installed to the outside of main carousel (801), main carousel (801) rotate through rack (1902) and are connected with top wing carousel (1901).
6. The unmanned aerial vehicle transmission machine and the transmission method thereof according to claim 4 and 5, wherein: the top of top wing carousel (1901) is rotated through speed reducer (18) and is connected with top wing pivot (19), the top fixedly connected with top wing rotary disk (20) of top wing pivot (19), the outside fixedly connected with top wing paddle (21) of top wing rotary disk (20).
7. The unmanned aerial vehicle transmission machine and the transmission method thereof according to claim 2, wherein: the fixing rods (1) are arranged in two numbers, the two fixing rods (1) are parallel to each other, the two fixing rods (1) are respectively located on the front side and the back side of the bottom plate (3), and the fixing rods (1) are fixedly connected with the bottom plate (3).
8. The unmanned aerial vehicle transmission machine and the transmission method thereof according to claim 2, wherein: the six top wing rotating disks (20) are arranged, and the shortest distance between the six top wing rotating disks (20) is larger than the total length of the two top wing blades (21).
9. The unmanned aerial vehicle transmission machine and the transmission method thereof according to the claims 1-8, comprising the following working steps:
s1, firstly, an operator adds engine oil through the engine oil adding port (22), turns on the switch (11) to start the power supply, and the control main board in the storage battery (803) sends a signal to the GPS signal transmitter (12) on the side of the signal adapter (10) through the data wire (9);
s2, a handle on the hand of an operator is in butt joint connection with a GPS signal transmitter (12), and then the handle controls the tail wing motor (7) and the main motor (8) to start;
s3, the ascending and descending and the direction changing of the unmanned aerial vehicle are realized by the rotating speed of the empennage motor (7), the main motor (8) and the speed reducer (18) through the handle, when flying, the empennage motor (7) and the main motor (8) are started firstly, then the main motor (8) drives the main motor rotating shaft (802) to rotate, then the main motor rotating shaft (802) drives the main rotating disc (801) to rotate, a rack (1902) on the outer side of the main rotating disc (801) can drive the top wing rotating disc (1901) to rotate, then the top wing rotating disc (20) is driven to rotate through the top wing rotating shaft (19), then the top wing blades (21) rotate at high speed, the empennage motor (7) is controlled to be started simultaneously, then the empennage motor (7) drives the empennage motor rotating shaft (6) to rotate, then the empennage motor rotating shaft (6) drives the rotating disc (5) to rotate, and the empennage motor (, finally, the unmanned aerial vehicle carries out flying work;
s4, when the direction needs to be changed (for example, leftward), the handle sends a signal to control the speed reducer (18) to increase the rotating speed of the four top wing rotating shafts (19) except the two top wing rotating shafts (19) on the left side, so that the ascending force on the right side is increased, the flow speed on the right side is greater than that on the left side through the airflow, the left side is inclined downward, and finally the unmanned aerial vehicle changes the direction to the left side;
s5, when the unmanned aerial vehicle needs to ascend, the handle sends a signal to control the speed reducer (18) to increase the rotating speed of all top wing rotating shafts (19), and the unmanned aerial vehicle can ascend by increasing the flow speed of air flow;
s6, after the device is used, the handle control speed reducer (18) slowly reduces the rotating speed of the top wing rotating shaft (19), finally the handle controls the main motor (8) to be closed after the device descends to the ground, then the handle controls the empennage motor (7) to be closed, and finally the switch (11) is closed;
s7, when using, the contact of engine oil can be along with unmanned aerial vehicle' S flight and rack (1902) maximize, when needing to change engine oil, operating personnel open engine oil discharge port (1501) with the engine oil discharge can.
10. The unmanned aerial vehicle transmission machine and the transmission method thereof according to claims 1 to 9, characterized in that the transmission method of the invention is: when flying, start fin motor (7) and main motor (8) earlier, then main motor (8) drive main motor pivot (802) and rotate, then main motor pivot (802) drive main carousel (801) and rotate, rack (1902) in main carousel (801) outside can drive top wing carousel (1901) rotatory, drive top wing rotary disk (20) through top wing pivot (19) afterwards and rotate, top wing paddle (21) carry out high-speed rotation afterwards, control fin motor (7) and start simultaneously, and then fin motor (7) drive fin motor pivot (6) and rotate, fin motor pivot (6) drive fin rotary disk (5) rotatory afterwards, fin motor (7) drive fin paddle (4) high-speed rotation through rotary disk fin (5), unmanned aerial vehicle carries out the flight work at last.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
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