CN108820231A - A kind of motor cabinet of unmanned plane - Google Patents
A kind of motor cabinet of unmanned plane Download PDFInfo
- Publication number
- CN108820231A CN108820231A CN201810575267.1A CN201810575267A CN108820231A CN 108820231 A CN108820231 A CN 108820231A CN 201810575267 A CN201810575267 A CN 201810575267A CN 108820231 A CN108820231 A CN 108820231A
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- Prior art keywords
- motor
- motor cabinet
- unmanned plane
- steering engine
- cabinet
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- 230000007246 mechanism Effects 0.000 claims abstract description 34
- 238000012546 transfer Methods 0.000 claims abstract description 34
- 238000009434 installation Methods 0.000 claims description 12
- 230000003044 adaptive effect Effects 0.000 abstract description 5
- 230000008859 change Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 238000013519 translation Methods 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/52—Tilting of rotor bodily relative to fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of motor cabinet of unmanned plane, unmanned plane includes the fuselage equipped with controller and electric-motor drive unit, fuselage is equipped with several arbors, the motor cabinet for installing motor and the steering engine for adjusting unmanned plane during flying direction are connected on arbor, the output shaft of motor is connected with propeller, motor is connect with electric-motor drive unit, and electric-motor drive unit, steering engine are connect with controller；Motor cabinet includes the second motor cabinet for being installed on the first motor seat of arbor and being flexibly connected with first motor seat, and the motor is fixedly installed on the second motor cabinet；It further include the transfer bar mechanism for being flexibly connected the steering engine and the second motor cabinet, steering engine drives the second motor cabinet to move by transfer bar mechanism.It is rotated using the second motor cabinet of servo driving to realize the amendment and adjusting of rotor Yu fuselage angle, it can satisfy the demand of different flight state, the adaptive capacity to environment for improving unmanned plane keeps unmanned plane more stable in flight course, improves the service life of unmanned plane.
Description
Technical field
The present invention relates to the technical fields of unmanned plane, more particularly, to a kind of motor cabinet of unmanned plane.
Background technique
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Especially four axis unmanned planes have light weight, structure simple, and flying quality is superior, being capable of spot takeoff, drop
The advantages that falling and hovering in the sky has in fields such as disaster relief, mapping, electric inspection process, the disaster relief at present and widely answers
With.
Unmanned plane is usually to carry camera the work such as to be shot and be detected during use.However, traditional
The motor cabinet of unmanned plane is usually to use stationary structure, that is, is horizontally fixed on arbor tail end.Its most prominent disadvantage is exactly not
It is able to achieve the amendment and adjusting of rotor Yu fuselage angle.So the translational motion of traditional unmanned plane is turned by promoting unilateral rotor
Speed then increases unilateral lift, so that a degree of inclination occurs for fuselage, so that rotor lift be made to generate a horizontal component
Come what is realized.But such method can make unmanned plane during flying state change when（Such as floating state becomes translation state）, fuselage
Meeting run-off the straight, causes the offset of camera picture, this is highly detrimental to smoothly winged required for such as investigating or shooting
Row environment.When especially high frequency switches unmanned plane during flying state, this influence is even more serious.
Summary of the invention
The present invention in order to overcome at least one of the drawbacks of the prior art described above, provides a kind of motor cabinet of unmanned plane, benefit
The amendment and adjusting that rotor Yu fuselage angle are realized with the rotation of the second motor cabinet of servo driving, can satisfy different flight shapes
The demand of state improves the adaptive capacity to environment of unmanned plane, keeps unmanned plane more stable in flight course, improves unmanned plane
Service life.
In order to solve the above technical problems, technical scheme is as follows：
A kind of motor cabinet of unmanned plane, the unmanned plane include the fuselage equipped with controller and electric-motor drive unit, the fuselage
Equipped with several arbors, the motor cabinet for installing motor is connected on the arbor and for adjusting unmanned plane during flying direction
Steering engine, the output shaft of the motor are connected with propeller, and the motor is connect with electric-motor drive unit, the motor driven list
Member, steering engine are connect with controller；The motor cabinet include be installed on arbor first motor seat and with first motor seat
The second motor cabinet being flexibly connected, the motor are fixedly installed on the second motor cabinet；It further include described for being flexibly connected
The transfer bar mechanism of steering engine and the second motor cabinet, steering engine drive the second motor cabinet to move by transfer bar mechanism.
Controller can send relevant control and instruct to steering engine, so that the servo driving steering engine wing on the steering engine seat of side rotates
Certain angle, the rotation for then push rod being pushed to make the second motor cabinet of the side connecting with push rod that certain angle also occur are inclined
Tiltedly, and remaining motor cabinet still remains unchanged, inclined second motor cabinet drives the motor inclination being mounted thereon at this time,
Then propeller tilt is driven, that is, realizes that controlling transfer bar mechanism by steering engine drives the rotation of the second motor cabinet to realize peace
Amendment and adjusting loaded on rotor and fuselage angle on the second motor cabinet improve to meet the needs of different flight state
The adaptive capacity to environment of unmanned plane；Make unmanned plane take off and flight course in it is more stable, state of flight change when do not send out
Raw inclination.
Preferably, the first motor seat includes U-shaped, and U-shaped opening is equipped with shaft, and the second motor cabinet is by turning
Axis is flexibly connected with first motor seat.Steering engine drives the second motor cabinet to rotate around the shaft by transfer bar mechanism, in turn
Drive is installed on propeller and fuselage angle change on the second motor cabinet, realizes the amendment and adjusting of rotor and fuselage angle.
Preferably, the first motor seat further includes the connecting plate connecting with U-shaped；The arbor is equipped with for installing
The axle bed connector of connecting plate.First motor seat is fixed on arbor by connecting plate, the installation for improving first motor seat is stablized
Property；First motor seat is installed using axle bed connector, realizes the Fast Installation of first motor seat.
Preferably, second motor cabinet includes mounting base for installing motor and set on the convex of mounting base bottom
Platform；The steering engine is equipped with the steering engine wing connecting with transfer bar mechanism.Steering engine is controlled by the driving steering engine wing, by transfer bar mechanism
The movement of boss finally drives the movement for the mounting base connecting with boss.
Preferably, the mounting base is the cross-shaped structure of the bar shape composition of two integrally connecteds, and the shaft runs through
In one of bar shape and vertical with another bar shape.The mounting base of cross-shaped structure is that motor installation improves installation enough
The weight of the second motor cabinet is alleviated while area, improves the response efficiency that the rotation of the second motor cabinet adjusts the angle.
Preferably, the transfer bar mechanism includes push rod, the collet set on push rod both ends；One end of push rod passes through collet and the
The boss of two motor cabinets is flexibly connected, and the other end of push rod is flexibly connected by collet with the steering engine wing.Use collet as
Connect push rod with steering engine, connect the connector of push rod and the second motor cabinet.
Preferably, the collet includes Y shape body, set on the connecting shaft of Y shape body opening；The steering engine wing, boss lead to respectively
Connecting shaft is crossed to be flexibly connected with transfer bar mechanism.The steering engine wing is hinged by connecting shaft with transfer bar mechanism, and boss passes through with transfer bar mechanism
Connecting shaft is hinged, improves steering engine by transfer bar mechanism and adjusts the flexibility ratio that boss adjusts the rotation of the second motor cabinet, so that
The adjusting that rotor Yu fuselage angle can in-flight be fast implemented, the environment for improving unmanned plane adapt to efficiency.
Preferably, the thickness of the bar shape vertical with shaft is less than the thickness of another bar shape.Pass through vertical bar shaped
Body also can be further improved the stability of equilibrium of the second support base rotation.
Preferably, the arbor is equipped with the steering engine seat for installing steering engine, and the steering engine seat includes the seat for being installed on arbor
Cylinder, seat cylinder are connected with a pair of of hangers, and steering engine is installed on the hangers.Rudder is installed using the steering engine seat being fixedly connected with arbor
Machine facilitates the installation and replacement of steering engine.
Preferably, the number of the motor cabinet is four.
Compared with prior art, beneficial effect is：
（1）Compared with the unmanned plane of existing fixed motor cabinet, motor is installed on rotatable second motor cabinet by the present invention,
Controlling transfer bar mechanism by steering engine drives the rotation of the second motor cabinet to realize the amendment and adjusting of rotor Yu fuselage angle,
Solve the problems, such as that fixed motor cabinet cannot achieve rotor and fuselage angle modification and adjust, to meet different flight state
Demand, improve the adaptive capacity to environment of unmanned plane；
（2）Motor cabinet of the invention improves the motion of translation of traditional unmanned plane, make unmanned plane in flight course more
Stablize, guarantee fuselage take off and state of flight change when not run-off the straight, ensure that the stabilization of camera picture, provide investigation or
Smooth flight environment required for shooting；
（3）Motor of the present invention uses split type first motor seat and the second motor cabinet, and structure is simple, is conducive on the second motor cabinet
The installation and replacement of motor and propeller.
Detailed description of the invention
Fig. 1 is overall structure of the present invention.
Fig. 2 is the side structure schematic diagram of motor cabinet of the present invention.
Fig. 3 is the structural schematic diagram of transfer bar mechanism of the present invention.
Fig. 4 is steering engine seat structural schematic diagram of the present invention.
Specific embodiment
The attached figures are only used for illustrative purposes and cannot be understood as limitating the patent；In order to better illustrate this embodiment, attached
Scheme certain components to have omission, zoom in or out, does not represent the size of actual product；To those skilled in the art,
The omitting of some known structures and their instructions in the attached drawings are understandable.Being given for example only property of positional relationship is described in attached drawing
Illustrate, should not be understood as the limitation to this patent.
As shown in Figs. 1-2, a kind of motor cabinet of unmanned plane, including connect with unmanned aerial vehicle body arbor 1, be installed on arbor
The steering engine 4 at 1 end, the motor 2 for driving propeller 3, the motor cabinet for installing motor 2, the propeller 3 being connect with motor 2；
Motor cabinet includes the first motor seat 12 for being installed on arbor 1, the second motor cabinet 13 being flexibly connected with first motor seat 12, motor
2 are fixedly installed on the second motor cabinet 13；It further include the transfer bar mechanism for being flexibly connected steering engine 4 and the second motor cabinet 13, rudder
Machine 4 drives the movement of the second motor cabinet 13 by transfer bar mechanism.First motor seat 12 is installed on arbor 1 by fixing screws, the
Two motor cabinets 13 are rotatablely connected with first motor seat 12, and motor 2 is fixed on the second motor cabinet 13 by press strip fitted bolt, or
Motor is installed on the second motor cabinet by person using other fixed forms of the prior art；Propeller 3 is fixed by fixing screws
It is installed on motor 2；Controlling transfer bar mechanism by steering engine 4 drives the second motor cabinet 13 to rotate, to adjust on the second motor cabinet 13
The motor 2 and propeller 3 of side rotate, and the amendment and adjusting of rotor and fuselage angle are realized, to meet different flight state
Demand improves the adaptive capacity to environment of unmanned plane；Make unmanned plane take off and flight course in it is more stable, state of flight changes
Not run-off the straight when change.The unmanned plane of the present embodiment is four axis unmanned planes, can also be any multi-rotor unmanned aerial vehicle.
Wherein, first motor seat 12 includes U-shaped 121, and U-shaped 121 openings are equipped with shaft 10, the second motor cabinet 13
It is flexibly connected by shaft 10 with first motor seat 12.Shaft 10 by bearing block be installed on U-shaped 121 opening both ends it
Between, the second motor cabinet 13 can be rotated around the shaft 10 for being installed on first motor seat 12, and steering engine 4 drives the by transfer bar mechanism
Two motor cabinets 12 are rotated around shaft 10, and then drive the propeller 3 being installed on the second motor cabinet 12 and fuselage angle change,
Realize the amendment and adjusting of rotor and fuselage angle.
In addition, first motor seat 12 further includes and U-shaped 121 connecting plate connecting 122；Arbor 1 is equipped with for the company of installation
The axle bed connector 9 of fishplate bar 122.The connecting plate 122 of first motor seat 12 is fixedly connected by welding with U-shaped 121, in steering engine
The both ends installation of seat 8 is there are two axle bed connector 9, and axle bed connector 9 is fixedly connected with arbor 1 by key, connecting plate 122 and two
A axle bed connector 9 is fixedly connected by screw respectively.The fixation of first motor seat 12 and arbor 1 is realized by connecting plate 122
Connection improves the mounting stability of first motor seat 12；First motor seat 12 is installed using axle bed connector 9, realizes the first electricity
The Fast Installation of base 12.
Wherein, the second motor cabinet 12 includes for installing the mounting base 131 of motor 2,131 bottom of mounting base equipped with for connecting
Connect the boss 132 of transfer bar mechanism；Steering engine 4 is equipped with the steering engine wing 5 for connecting transfer bar mechanism.132 one of mounting base 131 and boss
Molding constitutes the second motor cabinet 13, and transfer bar mechanism is realized hingedly by the through-hole and boss 132 opened up on boss 132；The steering engine wing 5
Bottom also offer for the through-hole hinged with transfer bar mechanism, steering engine 4 drives the swing of the steering engine wing 5 to pass through transfer bar mechanism
Drive the rotation of the second motor cabinet 13.
Above-mentioned mounting base 131 is the cross-shaped structure that the bar shape of two integrally connecteds is constituted, shaft 10 through its
In a bar shape and vertical with another bar shape.The mounting base 131 of cross-shaped structure is integrally formed, shaft 10 through
A bar shape in parallel.The mounting base 131 of cross-shaped structure is that the installation of motor 2 subtracts while improving enough mounting areas
The light weight of second motor cabinet 13, improves the response efficiency that the rotation of the second motor cabinet 13 adjusts the angle.
Wherein, transfer bar mechanism includes push rod 7, the collet 6 set on 7 both ends of push rod, as shown in Figure 3；One end of push rod 7 passes through
Collet 6 is flexibly connected with the boss 132 of the second motor cabinet 13, and the other end of push rod 7 is flexibly connected by collet 6 with the steering engine wing 5.
Use collet 6 as connection push rod 7 with steering engine 4, connect the connector of push rod 7 and the second motor cabinet 13, the collet at 7 both ends of push rod
6 are threadedly connected with push rod 7, guarantee connection reliability, while collet 6 due to rotation abrasion need replacing when, spiral shell
Line is fastenedly connected the quick of achievable collet 6 and removes and installs replacement.
Above-mentioned collet 6 includes Y shape body, set on the connecting shaft 61 of Y shape body opening；The steering engine wing 5, boss 132 pass through respectively
Connecting shaft 6 is flexibly connected with transfer bar mechanism.The connecting shaft 61 on collet 6 connecting with boss 132 opens up logical across boss 132
The articulated connection of the second motor cabinet 13 and transfer bar mechanism is realized in hole, and the connecting shaft 61 on collet 6 connecting with the steering engine wing 5 passes through rudder
Through-hole on wing 5 realizes the articulated connection of the steering engine wing 5 and transfer bar mechanism.Realize that articulated connection improves steering engine by connecting shaft 6
Adjusting boss 132 by transfer bar mechanism is the flexibility ratio for adjusting the rotation of the second motor cabinet 13, so that in-flight can be quickly real
The adjusting of existing rotor and fuselage angle, the environment for further increasing unmanned plane adapt to efficiency.
Wherein, the thickness of the bar shape vertical with shaft 10 is less than the thickness of another bar shape parallel with shaft.With
Adjustment both wings of the vertical bar shape of shaft 10 as the second motor cabinet 13 lead in 13 rotary course of the second motor cabinet
It crosses the bar shape vertical with shaft 10 also and can be further improved the stability of equilibrium of the second motor cabinet 13 rotation.
Wherein, arbor 1 is equipped with steering engine seat 8 for installing steering engine 4, steering engine seat 8 include the seat cylinder 81 for being installed on arbor 1,
Seat cylinder 81 is connected with a pair of of hangers 82, and steering engine 4 is installed on hangers 82, as shown in Figure 4.Steering engine seat 8 is also designed to other
Structure；Wherein seat cylinder 81 is socketed on arbor 1 and is fixed by the positioning shaft shoulder of arbor 1, hangers 82 and seat cylinder 81 be one at
Type, steering engine 4 are installed among a pair of of hangers 82 and are fixedly mounted respectively by fixing screws with a pair of of hangers 82.Using with arbor
1 steering engine seat 8 being fixedly connected installs steering engine 4, facilitates the installation and replacement of steering engine 4.
The number of the motor cabinet is four.
During unmanned plane during flying, for unmanned plane in floating state, unmanned aerial vehicle body passes through four electricity that arbor 1 connects
Base unit keeps horizontal.When unmanned plane needs to do the translational motion of horizontal direction, controller can send relevant control and refer to
It enables to steering engine 4, so that the steering engine 4 on side steering engine seat 8 drives the steering engine wing 5 to rotate certain angle, then push rod 7 is pushed to make
The rotation inclination of certain angle also occurs for the second motor cabinet 13 of the side connecting with push rod 7, and remaining motor cabinet is still kept
Level, inclined second motor cabinet 13 drives the motor 2 being mounted thereon to tilt at this time, then propeller 3 is driven to tilt,
Inclined propeller 3 can provide a component in the horizontal direction, and the component of this horizontal direction can be such that unmanned aerial vehicle body is being not necessarily to
The translational motion of horizontal direction is carried out in the state of inclination, so that camera picture be kept to stablize.Similarly, when unmanned plane is by translating
When movement is changed into floating state, the angle that the steering engine 4 of the side drives the rotation of 5 opposite direction of the steering engine wing certain can control, after
And keep 13 guarantee of the second motor cabinet of the side horizontal, so that lift provided by the rotor of four horizontal directions keeps unmanned plane
Hovering.The angle of adjustment rotor and fuselage is controlled using steering engine 4, it is more stable to meet the needs of different flight state, it mentions
The high adaptability of unmanned plane.
Obviously, the above embodiment of the present invention be only to clearly illustrate example of the present invention, and not be pair
The restriction of embodiments of the present invention.For those of ordinary skill in the art, may be used also on the basis of the above description
To make other variations or changes in different ways.There is no necessity and possibility to exhaust all the enbodiments.It is all this
Made any modifications, equivalent replacements, and improvements etc., should be included in the claims in the present invention within the spirit and principle of invention
Protection scope within.
Claims (10)
1. a kind of motor cabinet of unmanned plane, the unmanned plane includes the fuselage equipped with controller and electric-motor drive unit, the machine
Body is equipped with several arbors, motor cabinet for installing motor is connected on the arbor and for adjusting unmanned plane during flying direction
Steering engine, the output shaft of the motor is connected with propeller, and the motor is connect with electric-motor drive unit, the motor driven list
Member, steering engine are connect with controller；It is characterized in that：
The motor cabinet includes being installed on arbor（1）First motor seat（12）And with first motor seat（12）It is flexibly connected
The second motor cabinet（13）, the motor（2）It is fixedly installed in the second motor cabinet（13）On；
It further include for being flexibly connected the steering engine（4）With the second motor cabinet（13）Transfer bar mechanism, steering engine（4）Pass through push rod machine
Structure drives the second motor cabinet（13）Movement.
2. a kind of motor cabinet of unmanned plane according to claim 1, it is characterised in that：The first motor seat（12）Including
U-shaped（121）, U-shaped（121）Opening shaft is installed（10）, the second motor cabinet（13）Pass through shaft（10）With first
Motor cabinet（12）It is flexibly connected.
3. a kind of motor cabinet of unmanned plane according to claim 2, it is characterised in that：The first motor seat（12）Also
Including with U-shaped（121）The connecting plate of connection（122）；The arbor（1）Equipped with installation connecting plate（122）Axle bed connector
（9）.
4. a kind of motor cabinet of unmanned plane according to claim 2, it is characterised in that：Second motor cabinet（13）Including
For installing motor（2）Mounting base（131）And it is set to mounting base（131）The boss of bottom（132）, the boss（132）
It is connect with transfer bar mechanism；The steering engine（4）Equipped with the steering engine wing being connect with transfer bar mechanism（5）.
5. a kind of motor cabinet of unmanned plane according to claim 4, it is characterised in that：The mounting base（131）It is two
The cross-shaped structure that the bar shape of integrally connected is constituted, the shaft（10）Through one of bar shape and with another
Body is vertical.
6. a kind of motor cabinet of unmanned plane according to claim 4, it is characterised in that：The transfer bar mechanism includes push rod
（7）, collet set on push rod both ends（6）；Push rod（7）One end pass through collet（6）With boss（132）It is flexibly connected, push rod（7）
The other end pass through collet（6）With the steering engine wing（5）It is flexibly connected.
7. a kind of motor cabinet of unmanned plane according to claim 6, it is characterised in that：The collet（6）Including Y shape body,
Set on the connecting shaft of Y shape body opening（61）；The steering engine wing（5）, boss（132）Pass through connecting shaft respectively（61）With transfer bar mechanism
It is flexibly connected.
8. a kind of motor cabinet of unmanned plane according to claim 7, it is characterised in that：With shaft（10）Vertical bar shape
Thickness be less than another bar shape thickness.
9. a kind of motor cabinet of unmanned plane according to claim 8, it is characterised in that：The arbor（1）Equipped with for pacifying
Fill steering engine（4）Steering engine seat（8）.
10. a kind of motor cabinet of unmanned plane according to any one of claims 1 to 9, it is characterised in that：The motor cabinet
Number is four.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810575267.1A CN108820231A (en) | 2018-06-06 | 2018-06-06 | A kind of motor cabinet of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810575267.1A CN108820231A (en) | 2018-06-06 | 2018-06-06 | A kind of motor cabinet of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108820231A true CN108820231A (en) | 2018-11-16 |
Family
ID=64144106
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810575267.1A Pending CN108820231A (en) | 2018-06-06 | 2018-06-06 | A kind of motor cabinet of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108820231A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114954913A (en) * | 2022-07-01 | 2022-08-30 | 吉林化工学院 | Precision balancing device for improving flight stability of unmanned aerial vehicle |
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| CN208429243U (en) * | 2018-06-06 | 2019-01-25 | 广东工业大学 | A kind of motor cabinet of unmanned plane |
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| US20170015412A1 (en) * | 2015-07-17 | 2017-01-19 | iDrone LLC | Thrust vectoring on a rotor-based remote vehicle |
| CN205366069U (en) * | 2015-12-25 | 2016-07-06 | 湖南云顶智能科技有限公司 | A motor mechanism of verting for unmanned aerial vehicle |
| CN105857605A (en) * | 2016-04-11 | 2016-08-17 | 河北科技大学 | Single sitting type fixed-wing unmanned aerial vehicle taking off and landing vertically |
| CN106986019A (en) * | 2017-04-17 | 2017-07-28 | 四川建筑职业技术学院 | A kind of motor cabinet for changing multi-rotor unmanned aerial vehicle rotor face angle of inclination |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN114954913A (en) * | 2022-07-01 | 2022-08-30 | 吉林化工学院 | Precision balancing device for improving flight stability of unmanned aerial vehicle |
| CN114954913B (en) * | 2022-07-01 | 2022-11-01 | 吉林化工学院 | Precision balancing device for improving flight stability of unmanned aerial vehicle |
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