CN207433797U - Four axis gyroplanes balance remedies device - Google Patents
Four axis gyroplanes balance remedies device Download PDFInfo
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- CN207433797U CN207433797U CN201721517068.2U CN201721517068U CN207433797U CN 207433797 U CN207433797 U CN 207433797U CN 201721517068 U CN201721517068 U CN 201721517068U CN 207433797 U CN207433797 U CN 207433797U
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- blade
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- cabane
- motor
- balance
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Abstract
The utility model discloses a kind of four axis gyroplanes balances to remedy device, and including body, cabane, blade bar, motor and blade, the body is fixedly connected with the cabane；The cabane is connected with described blade bar one end to rotate coaxially；The blade bar other end is rotatablely connected with the motor；The motor output shaft is fixedly connected with the blade.The utility model is simple in structure, and construction is ingenious, with reference to the blade bar of bending so that blade rotates always in horizontal plane, generates effect of increasing power.
Description
Technical field
The utility model is related to four axis gyroplane technical fields, especially a kind of four axis gyroplanes balance remedies device.
Background technology
Four axis gyroplanes are that four rotors are symmetrically distributed in body all around on four direction, and four rotors are in same
One elevation plane, and the structure of four rotors and radius are all identical, four motors are symmetrically installed on the bracket end of aircraft, branch
Frame intermediate space places flight-control computer and external equipment.Change variable rotor speed by adjusting four motor speeds, it is real
The variation of existing lift, so as to control the posture of aircraft and position.Quadrotor is a kind of vertical lift of six degree of freedom
Machine, but only there are four input power, while but there are six state output, so it is a kind of under-actuated systems again.
And four axis gyroplanes are in practical operation, fall repeatedly due to balance loses or even generate substantial risk.
Utility model content
The utility model in view of the deficiencies of the prior art, proposes that a kind of four axis gyroplanes balance remedies device, can be effectively
Prevent phenomenon of falling occur during four axis gyroplane disequilibrium.
In order to realize above-mentioned purpose of utility model, the utility model provides following technical scheme：A kind of four axis gyroplanes are put down
Weighing apparatus remedies device, and including body, cabane, blade bar, motor and blade, the body is fixedly connected with the cabane；The wing
Column is connected with described blade bar one end to rotate coaxially；The blade bar other end is rotatablely connected with the motor；The motor
Output shaft is fixedly connected with the blade.
Further, the cabane and described blade bar one end is be coaxial docking, and each other axis and mutually rotate.
Further, the blade bar other end is connected through axis pin with the motor；The motor is swung around the axis pin
Face, form face with the cabane and the blade bar and overlap.
Further, the blade bar is bent rod；The bent rod is fixedly connected by two sections of bars with 90 ° of -180 ° of angles
It forms.
Further, the angle of two sections of bars is 135 °.
Further, there are four the cabane, blade bar, motor and blade are all provided with, the both sides of the body are symmetrically arranged at
And front and rear side.
Compared with prior art, the utility model has the following advantages：Using on the blade bar being rotatablely connected with cabane
Swingable blade mechanism is set, and when four axis gyroplanes lose balance or even disequilibrium, the blade surfaces of revolution is adjusted to level
It is most important upward, necessary useful lift can be provided, so as to which unbalance remedy existing for overcoming traditional wing bar fixed structure is asked
Topic.
The utility model is simple in structure, and construction is ingenious, with reference to the blade bar of bending so that blade revolves always in horizontal plane
Turn, generate effect of increasing power.
Description of the drawings
Fig. 1 is the structure diagram that four axis gyroplane of the utility model balance remedies device；
Fig. 2 is a kind of action schematic diagram that four axis gyroplane of the utility model balance remedies device；
Fig. 3 is another action schematic diagram that four axis gyroplane of the utility model balance remedies device；
Fig. 4 is the third action schematic diagram that four axis gyroplane of the utility model balance remedies device；
Diagram mark：
1- bodies, 2- cabanes, 3- blades bar, 4- motors, 5- blades.
Specific embodiment
The utility model is described in detail below in conjunction with the accompanying drawings, the description of this part be only it is exemplary and explanatory,
There should not be any restriction effect to the scope of protection of the utility model.
As shown in Figures 1 to 4, a kind of four axis gyroplanes balance remedies device, including body 1, cabane 2, blade bar 3, motor 4
With blade 5, the cabane 2 is fixedly connected with the body 1, and described 3 one end of blade bar is connected with the cabane 2 to rotate coaxially,
The other end is rotatablely connected with the motor 4；4 output shaft of motor is fixedly connected with the blade 5.
The present apparatus is by setting cabane 2 in 1 side of body, and cabane 2 is to be rotatably connected with blade bar 3, in blade bar 3
The other end be equipped with motor 4 and blade 5, motor 4 drives blade 5 to rotate, and forms climbing power, and motor 4 and blade bar 3 are the company of rotation
It connects.Due to by body 1 to, there are two rotation connections, even if in 1 disequilibrium of body, also revolving blade 5 between blade 5
Turn face and be in horizontal plane, so as to which the climbing power generated may proceed to maintain.
Preferred embodiment is that blade bar 3 is set to bent rod, the blade bar 3 in bending state, since one end and cabane 2 are
Rotation connection, the other end are rotation connection with motor 4；The climbing power generated using the rotation of blade 5 so that blade bar 3 is with respect to water
The blade 5 of Plane Rotation can convert multiple positions.Meanwhile for during non-standard state, blade to rotate at a high speed at gyroplane cabane 2
The stream pressure of pressure avoids rotor horn.
Preferred scheme is that blade bar 3 is set to the structure that two sections of bars are fixedly connected, and the angle of two sections of bars is 90-
180 °, most preferred angle is 135 °；With cabane 2 to be coaxial docking, this section of bar can be connected to rotation on cabane 2 one section of bar,
Another section of bar is connected through axis pin with motor 4 so that motor 4 is rotated in rod end around axis pin.In 1 disequilibrium of body, blade 5 revolves
It changes the line of production raw climbing power so that motor 4 can be rotated around axis pin, in conjunction with the rotation of blade bar 3, it is ensured that the surfaces of revolution of blade 5 begins
Eventually lift is provided on horizontal plane.
It is coincidence status for motor 4 around face where the face that axis pin rotates, with two sections of bars of blade bar 3；This coincidence face
It sets, it is ensured that blade bar 3 can occur to rotate at two in 1 disequilibrium of body in time, it is ensured that 5 surfaces of revolution of blade is in level
Lift is provided on face.
In practical applications, steady to preferably keep body 1, cabane 2, blade bar 3, motor 4 and blade 5 are equipped with four
It is a, it is symmetrically arranged at both sides and the front and rear side of body 1.
As shown in Figure 1, a kind of four axis gyroplane balance remedies being produced as follows for device：
First, gyroplane body 1 and cabane 2 connect.
Secondly, cabane 2 and blade bar 3 connect；Wherein：Cabane 2 makees shaft, and blade bar 3 can rotate in fixed axis.
Again, 3 form of blade bar is bent, and end and blade electric rotating machine 4 connect；Wherein：Blade electric rotating machine 4 is with even
Contact makees that axis is swingable, and swinging plane is located in the plane that curved blade bar 3 and cabane 2 are formed.
Once more, blade electric rotating machine 4 and blade 5 connect, and it is exactly blade rotation that blade, which rotates occupied plane space,
Face.
As shown in Fig. 2, at opposite cabane 2 during horizontality, 1 state of body regardless of gyroplane passes through paddle
Leaf bar 3 does fixed-axis rotation, and blade surfaces of revolution level can be made to provide lift upward.
As shown in figure 3, at opposite cabane 2 during vertical state, 1 state of body regardless of gyroplane passes through paddle
Leaf electric rotating machine is swung, and blade surfaces of revolution level can be made to provide lift upward.
As shown in figure 4, at opposite cabane 2 during heeling condition, linked together by above-mentioned rotation and swing, it can
Blade surfaces of revolution level is made to provide lift upward.
It is flown and required from four axis gyroplanes, the lift combination of blade offer, which takes, keeps balance uniform upward at quarter；
Adjusting to the horizontal lift that provides upward for the blade surfaces of revolution is exactly purpose of utility model when gyroplane is unbalance, in rotor horn (bag
Include cabane, blade bar, blade electric rotating machine) on adjustment be exactly the utility model content, particular content is rotation, swing, curved
It is bent.
When blade, rotation provides lift at a high speed, by the work of rotor horn (including cabane, blade bar, blade electric rotating machine)
Dynamic adjustment, be adjusted in a manner of most directly efficient the blade surfaces of revolution to it is horizontal upward, lift is both in a manner of most directly efficient
It conducts to gyroplane main body.
The above is only the preferred embodiment of the utility model, it is noted that for the common skill of the art
For art personnel, on the premise of the utility model principle is not departed from, several improvements and modifications can also be made, these improve and
Retouching also should be regarded as the scope of protection of the utility model.
Claims (6)
1. a kind of four axis gyroplanes balance remedies device, it is characterised in that：Including body, cabane, blade bar, motor and blade,
The body is fixedly connected with the cabane；The cabane is connected with described blade bar one end to rotate coaxially；The blade bar
The other end is rotatablely connected with the motor；The motor output shaft is fixedly connected with the blade.
2. four axis gyroplane balance as described in claim 1 remedies device, it is characterised in that：The cabane and the blade bar one
Hold to be coaxial docking, and each other axis and mutually rotate.
3. four axis gyroplane balance as described in claim 1 remedies device, it is characterised in that：The blade bar other end is through axis pin
It is connected with the motor；The motor forms face with the cabane and the blade bar and overlaps around the face that the axis pin is swung.
4. four axis gyroplane balance as described in claim 1 remedies device, it is characterised in that：The blade bar is bent rod；Institute
It states bent rod and is fixedly connected by two sections of bars with 90 ° of -180 ° of angles and formed.
5. four axis gyroplane balance as claimed in claim 4 remedies device, it is characterised in that：The angle of two sections of bars is 135 °.
6. four axis gyroplane balance as described in claim 1 remedies device, it is characterised in that：The cabane, blade bar, motor and
There are four blade is all provided with, both sides and the front and rear side of the body are symmetrically arranged at.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721517068.2U CN207433797U (en) | 2017-11-14 | 2017-11-14 | Four axis gyroplanes balance remedies device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721517068.2U CN207433797U (en) | 2017-11-14 | 2017-11-14 | Four axis gyroplanes balance remedies device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207433797U true CN207433797U (en) | 2018-06-01 |
Family
ID=62289347
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721517068.2U Active CN207433797U (en) | 2017-11-14 | 2017-11-14 | Four axis gyroplanes balance remedies device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207433797U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107902083A (en) * | 2017-11-14 | 2018-04-13 | 蔡伯旭 | Four axis gyroplanes balance remedies device |
-
2017
- 2017-11-14 CN CN201721517068.2U patent/CN207433797U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107902083A (en) * | 2017-11-14 | 2018-04-13 | 蔡伯旭 | Four axis gyroplanes balance remedies device |
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