CN207956058U - A kind of unmanned plane rotor motor - Google Patents
A kind of unmanned plane rotor motor Download PDFInfo
- Publication number
- CN207956058U CN207956058U CN201721908521.2U CN201721908521U CN207956058U CN 207956058 U CN207956058 U CN 207956058U CN 201721908521 U CN201721908521 U CN 201721908521U CN 207956058 U CN207956058 U CN 207956058U
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- unmanned plane
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- moving block
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- 241000883990 Flabellum Species 0.000 claims description 10
- 229910000975 Carbon steel Inorganic materials 0.000 claims description 3
- 239000010962 carbon steel Substances 0.000 claims description 3
- 230000001737 promoting effect Effects 0.000 abstract description 2
- 238000006243 chemical reaction Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 238000011161 development Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000009987 spinning Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Abstract
The utility model discloses a kind of unmanned plane rotor motors, including link block, the side of the link block is fixed with carrier block, the other side upper end of the carrier block is rotatably connected to moving block, one end of the moving block is equipped with attachment device, one end of the attachment device is equipped with mounting blocks, and the upper end of the mounting blocks is equipped with the first driver slot, and the bottom in first driver slot is fixed with first driving means.The utility model is realized can not operate when a certain rotor occurs in unmanned plane; prevent unmanned plane spin from even falling; it ensure that unmanned plane held stationary can be run in the case where emergency case or a certain rotor are damaged; unmanned plane is protected, solves when one in one group of opposite rotor of unmanned plane breaks down, often only leans on a rotor that can not provide the torque for balance; frequently result in unmanned plane spin, the problem of falling even out of control; it is simple in structure, facilitate and operated, suitable for promoting.
Description
Technical field
The utility model is related to air vehicle technique field more particularly to a kind of unmanned plane rotor motors.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates, or fully or intermittently automatically operated by car-mounted computer, with someone
It drives an airplane and compares, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Unmanned plane presses application field,
Can be divided into it is military with it is civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane+sector application are
Unmanned plane has really just needed;It taking photo by plane at present, agricultural, plant protection, miniature self-timer, express transportation, disaster relief, observing wild move
The application in object, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making, manufacture romance etc. field, greatly
The big purposes for having expanded unmanned plane itself, developed country are domestic also in actively extension sector application and development unmanned air vehicle technique
The rapid development of outer unmanned plane the relevant technologies, UAV system type is various, the wide distinct characteristics of purposes, cause its size, quality,
Voyage, endurance, flying height, flying speed, task dispatching various aspects have larger difference, due to the diversity of unmanned plane, for
Different considering has different sorting techniques, when flight, reaction force caused by one group of opposite rotor wing rotation and another
Reaction force direction that one group of opposite rotor wing rotation generates is on the contrary, when two reaction forces are equal in magnitude, then mutually completely
It offsets, unmanned aerial vehicle body can keep stable, and when a certain rotor cannot operate, two reaction force sizes are unequal, nothing
Man-machine will spin, and it is out of control to be easy to cause unmanned plane, for multi-rotor unmanned aerial vehicle, when one group of opposite rotor of unmanned plane
In one when breaking down, often only lean on one by one a rotor the torque for balance can not be provided, frequently result in unmanned plane from
Rotation, it is even out of control fall, for this purpose, we have proposed a kind of unmanned plane rotor motors to solve the above problems.
Utility model content
Purpose of the utility model is to solve disadvantages existing in the prior art, and a kind of unmanned plane rotor proposed
Motor.
To achieve the goals above, the utility model uses following technical solution:
The side of a kind of unmanned plane rotor motor, including link block, the link block is fixed with carrier block, the carrier block
Other side upper end be rotatably connected to moving block, one end of the moving block is equipped with attachment device, one end of the attachment device
Equipped with mounting blocks, the upper end of the mounting blocks is equipped with the first driver slot, and the bottom in first driver slot is fixed with the first drive
The output shaft end of dynamic device, the first driving means runs through the first driver slot and extends to the upper end of mounting blocks, and described the
The output shaft end of one driving device is fixed with shaft, and multiple flabellums, the moving block lower end are equidistantly equipped in the shaft
Equipped with mounting plate, and mounting plate is rotatably connected on the side lower end of link block, and the side of the mounting plate is fixed with support plate, institute
The side for stating support plate is equipped with cross bar, and cross bar is fixedly connected on the side of mounting plate, runs through on the cross bar and is equipped with rotating bar,
Casing is rotatably connected in the support plate, the bottom in described sleeve pipe is fixed with resetting spring, the upper end of the resetting spring
It is fixed with backing plate, the upper end of the backing plate is fixed with litter, and the upper end of the litter is rotatably connected on the lower end side of moving block,
The side of the link block is equipped with the second driver slot, and the second driver slot, between moving block and mounting plate, described second drives
Bottom in dynamic slot is fixed with the second driving device, and the output shaft end of second driving device through the second driver slot and prolongs
The side of link block is extended to, the output shaft end of second driving device is fixed with turntable, the upper end rotation of the rotating bar
It is connected to the side of turntable.
Preferably, the attachment device includes the fixed plate being arranged in moving block side, is equidistantly set in the fixed plate
There are multiple first tapped through holes, and be provided through threaded rod in the first tapped through hole, the side of the mounting blocks is equidistant
Equipped with multiple second tapped through holes, and the first tapped through hole and the second tapped through hole are corresponding, and one end of the threaded rod is run through
First tapped through hole simultaneously extends in the second tapped through hole.
Preferably, institute's first driving means and the second driving device are servo motor.
Preferably, the quantity of the flabellum be-it is a.
Preferably, the threaded rod is made of carbon steel.
Preferably, the lower end of the link block is equipped with groove, and the top in the groove is fixed with lighting device.
In the utility model, in use, the second driving device drives turntable rotation, to make rotating bar move and drive peace
Loading board is waved, and to make casing rotate, casing drives litter rotation, litter to drive moving block rotation, when moving block pushes litter
When, litter ensures that the rotation of moving block, moving block drive mounting blocks rotation, first driving means by backing plate pressed home spring
Flabellum rotation is driven to prevent unmanned plane from spinning to preferably be offset to power, lighting device uses LED light, driving device
Ai Sidun servo motor EMJ-08APB22 are all made of, the utility model is realized can not operate when a certain rotor occurs in unmanned plane, prevent
Only unmanned plane spin is even fallen, ensure that unmanned plane can in the case where emergency case or a certain rotor damage held stationary
Unmanned plane is protected in operation, is solved when one in one group of opposite rotor of unmanned plane breaks down, is often only leaned on a rotation
The wing can not provide the torque for balance, frequently result in unmanned plane spin, the problem of falling even out of control, simple in structure, convenient
It is operated, suitable for promoting.
Description of the drawings
Fig. 1 be the utility model proposes a kind of unmanned plane rotor motor front view;
Fig. 2 be the utility model proposes a kind of unmanned plane rotor motor connecting block structure schematic diagram;
Fig. 3 be the utility model proposes a kind of unmanned plane rotor motor A at schematic enlarged-scale view;
Fig. 4 be the utility model proposes a kind of unmanned plane rotor motor inside pipe casing structural schematic diagram
In figure:1 mounting blocks, 2 first driving means, 3 shafts, 4 flabellums, 5 fixed plates, 6 threaded rods, 7 link blocks, 8 carryings
Block, 9 second driving devices, 10 moving blocks, 11 turntables, 12 rotating bars, 13 casings, 14 support plates, 15 mounting plates, 16 litter, 17
Backing plate, 18 resetting springs.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
Referring to Fig.1-4, the side of a kind of unmanned plane rotor motor, including link block 7, link block 7 is fixed with carrier block 8,
Convenient for being connected with fuselage, the other side upper end of carrier block 8 is rotatably connected to moving block 10, facilitates and rotates and be adjusted, and rotates
One end of block 10 is equipped with attachment device, and one end of attachment device is equipped with mounting blocks 1, and the upper end of mounting blocks 1 is equipped with the first driver slot,
Bottom in first driver slot is fixed with first driving means 2, and the output shaft end of first driving means 2 runs through the first driver slot
And the upper end of mounting blocks 1 is extended to, the output shaft end of first driving means 2 is fixed with shaft 3, is equidistantly equipped in shaft 3
Multiple flabellums 4, first driving means 2 drive the rotation of shaft 3 to be that flabellum 4 rotates, generate lift, 10 lower end of moving block is equipped with
Mounting plate 15, and mounting plate 15 is rotatably connected on the side lower end of link block 7, the side of mounting plate 15 is fixed with support plate 14,
The side of support plate 14 is equipped with cross bar, and cross bar is fixedly connected on the side of mounting plate 15, common rotation, through being equipped on cross bar
Rotating bar 12 is rotatably connected to casing 13 in support plate 14, and the bottom in casing 13 is fixed with resetting spring 18, resetting spring 18
Upper end be fixed with backing plate 17, the upper end of backing plate 17 is fixed with litter 16, and the upper end of litter 16 is rotatably connected on moving block 10
Lower end side, when moving block 10 rotates, squeezing litter 16 makes resetting spring 18 shrink, and moving block 10 is facilitated to complete rotation, connection
The side of block 7 is equipped with the second driver slot, and the second driver slot is between moving block 10 and mounting plate 15, in the second driver slot
Bottom is fixed with the second driving device 9, and the output shaft end of the second driving device 9 through the second driver slot and extends to link block
The output shaft end of 7 side, the second driving device 9 is fixed with turntable 11, and the upper end of rotating bar 12 is rotatably connected on turntable 11
Side, the second driving device 9 drive turntable 11 rotate, turntable 11 drive rotating bar 12 rotate, rotating bar 12 drive mounting plate
15 rotations, to be that casing 13 rotates, and then moving block 10 is driven to rotate.
In the utility model, attachment device includes the fixed plate 5 being arranged in 10 side of moving block, in fixed plate 5 equidistantly
Equipped with multiple first tapped through holes, and it is provided through threaded rod 6 in the first tapped through hole, facilitates adjusting to install, mounting blocks 1
Side be equidistantly equipped with multiple second tapped through holes, and the first tapped through hole and the second tapped through hole are corresponding, threaded rod 6
One end is through the first tapped through hole and extends in the second tapped through hole, carries out screwing tight connection, institute's first driving means 2 and second
Driving device 9 is servo motor, and the quantity of flabellum 4 is 2-4, generates lift and unmanned plane is facilitated to lift, threaded rod 6 uses carbon
Steel is made, durable, and the lower end of link block 7 is equipped with groove, and the top in groove is fixed with lighting device, night is facilitated to make
With.
In the utility model, in use, the second driving device 9 drives turntable 11 to rotate, to make the movement of rotating bar 12 simultaneously
Mounting plate 15 is driven to wave, to make casing 13 rotate, casing 13 drives litter 16 to rotate, and litter 16 drives 10 turns of moving block
Dynamic, when moving block 10 pushes litter 16, litter 16 ensures the rotation of moving block 10 by 17 pressed home spring 18 of backing plate, turns
Motion block 10 drives mounting blocks 1 to rotate, and first driving means 2 drive flabellum 4 to rotate, and to preferably be offset to power, prevents
Unmanned plane spins, and lighting device uses LED light, driving device to be all made of Ai Sidun servo motors EMJ-08APB22.
More than, the only preferable specific implementation mode of the utility model, but the scope of protection of the utility model is not limited to
In this, any one skilled in the art within the technical scope disclosed by the utility model, according to the utility model
Technical solution and its utility model design be subject to equivalent substitution or change, should all cover the scope of protection of the utility model it
It is interior.
Claims (6)
1. a kind of unmanned plane rotor motor, including link block (7), which is characterized in that the side of the link block (7), which is fixed with, holds
Block (8) is carried, the other side upper end of the carrier block (8) is rotatably connected to moving block (10), and one end of the moving block (10) is set
There are attachment device, one end of the attachment device to be equipped with mounting blocks (1), the upper end of the mounting blocks (1) is equipped with the first driver slot,
Bottom in first driver slot is fixed with first driving means (2), and the output shaft end of the first driving means (2) passes through
It wears the first driver slot and extends to the upper end of mounting blocks (1), the output shaft end of the first driving means (2) is fixed with shaft
(3), multiple flabellums (4) are equidistantly equipped on the shaft (3), moving block (10) lower end is equipped with mounting plate (15), and pacifies
Loading board (15) is rotatably connected on the side lower end of link block (7), and the side of the mounting plate (15) is fixed with support plate (14), institute
The side for stating support plate (14) is equipped with cross bar, and cross bar is fixedly connected on the side of mounting plate (15), runs through on the cross bar and sets
There is rotating bar (12), casing (13) is rotatably connected on the support plate (14), the bottom in described sleeve pipe (13) is fixed with multiple
Position spring (18), the upper end of the resetting spring (18) are fixed with backing plate (17), and the upper end of the backing plate (17) is fixed with litter
(16), the upper end of the litter (16) is rotatably connected on the lower end side of moving block (10), and the side of the link block (7) is equipped with
Second driver slot, and the second driver slot is located between moving block (10) and mounting plate (15), the bottom in second driver slot
It is fixed with the second driving device (9), the output shaft end of second driving device (9) runs through the second driver slot and the company of extending to
The side of block (7) is connect, the output shaft end of second driving device (9) is fixed with turntable (11), the rotating bar (12)
Upper end is rotatably connected on the side of turntable (11).
2. a kind of unmanned plane rotor motor according to claim 1, which is characterized in that the attachment device includes that setting exists
The fixed plate (5) of moving block (10) side is equidistantly equipped with multiple first tapped through holes, and the first spiral shell on the fixed plate (5)
Threaded rod (6) is provided through in line through-hole, the side of the mounting blocks (1) is equidistantly equipped with multiple second tapped through holes,
And first tapped through hole and the second tapped through hole it is corresponding, one end of the threaded rod (6) is through the first tapped through hole and extends
To the second tapped through hole.
3. a kind of unmanned plane rotor motor according to claim 1, which is characterized in that institute's first driving means (2) and
Two driving devices (9) are servo motor.
4. a kind of unmanned plane rotor motor according to claim 1, which is characterized in that the quantity of the flabellum (4) is 2-4
It is a.
5. a kind of unmanned plane rotor motor according to claim 2, which is characterized in that the threaded rod (6) uses carbon
Steel is made.
6. a kind of unmanned plane rotor motor according to claim 1, which is characterized in that the lower end of the link block (7) is set
Fluted, the top in the groove is fixed with lighting device.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201721908521.2U CN207956058U (en) | 2017-12-30 | 2017-12-30 | A kind of unmanned plane rotor motor |
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Application Number | Priority Date | Filing Date | Title |
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CN201721908521.2U CN207956058U (en) | 2017-12-30 | 2017-12-30 | A kind of unmanned plane rotor motor |
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Publication Number | Publication Date |
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CN207956058U true CN207956058U (en) | 2018-10-12 |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113767352A (en) * | 2020-05-07 | 2021-12-07 | 深圳市大疆创新科技有限公司 | Control method, data processing method, device, unmanned aerial vehicle and storage medium |
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2017
- 2017-12-30 CN CN201721908521.2U patent/CN207956058U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113767352A (en) * | 2020-05-07 | 2021-12-07 | 深圳市大疆创新科技有限公司 | Control method, data processing method, device, unmanned aerial vehicle and storage medium |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
EE01 | Entry into force of recordation of patent licensing contract |
Assignee: Hebei Xinsheng Environmental Technology Co.,Ltd. Assignor: TIANJIN ZHUOYOU ZHISHUN TECHNOLOGY CO.,LTD. Contract record no.: X2024980003058 Denomination of utility model: A drone rotor motor Granted publication date: 20181012 License type: Common License Record date: 20240319 |
|
EE01 | Entry into force of recordation of patent licensing contract |