CN205460998U - Unmanned aerial vehicle's operating mechanism controlling means - Google Patents
Unmanned aerial vehicle's operating mechanism controlling means Download PDFInfo
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- CN205460998U CN205460998U CN201620134653.3U CN201620134653U CN205460998U CN 205460998 U CN205460998 U CN 205460998U CN 201620134653 U CN201620134653 U CN 201620134653U CN 205460998 U CN205460998 U CN 205460998U
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- gear
- motor
- steering wheel
- aerial vehicle
- unmanned aerial
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Abstract
The utility model discloses an unmanned aerial vehicle's operating mechanism controlling means, include: motor, motor gear, intermediate gear, lead screw gear, ball screw, steering wheel pole, steering wheel guide pin bushing, slip electronic ruler, controller and shell, this kind of controlling means utilize ball screw as ultimate transmission parts, reduce the gear and use quantity to chooseing high accuracy CNC gear for use, adopting the direct current motor who has the electric arc function that disappears and have brush steering engine control circuit, this outer motor and circuit have very strong overload -resistant capability, thereby have guaranteed the reliability of steering wheel.
Description
Technical field
The present invention relates to steering engine for unmanned plane technical field, the operating mechanism particularly relating to a kind of unmanned aerial vehicle controls device.
Background technology
Along with modern science and technology is fast-developing, the application of unmanned aerial vehicle is more and more extensive, heavy－duty, and during long boat, the demand of the unmanned aerial vehicle of high reliability is increasing, and common airplane model steering engine is can not meet the requirement of large-scale unmanned helicopter.Conventional airplane model steering engine belongs to swing arm steering wheel, and average life is the lowest, and precision is the most very poor, it is difficult to ensure that the flight safety of large-scale unmanned helicopter.
Summary of the invention
In order to overcome above-mentioned the deficiencies in the prior art, the operating mechanism that the invention provides a kind of unmanned aerial vehicle controls device.
The technical solution adopted in the present invention is: the operating mechanism of a kind of unmanned aerial vehicle controls device, including: motor, motor gear, idler gear, screw gear, ball screw, steering wheel bar, steering wheel guide pin bushing, slip electronic ruler, controller and shell, described motor is connected with controller by motor lines, described slip electronic ruler is connected with controller by electronic ruler feedback line, described motor gear is positioned at the downside of motor, described idler gear drives between gear at motor gear and screw mandrel, described ball screw drives gear to be connected with screw mandrel, described steering wheel guide pin bushing is enclosed within ball screw, described slip electronic ruler is connected with shell.
Preferably, this control device utilizes ball screw as final transferring element.
Preferably, this control device reduces gear usage quantity.
Preferably, controlling the gear selected by device is High Precision CNC gear.
Preferably, described motor is the direct current generator with electric eliminating arc function,Circuit used is for there being brush helm control circuit, and motor and circuit have the strongest anti-overload ability.
The invention has the beneficial effects as follows: compact conformation, light weight, precision is high, and reliability anti-overload ability is the best, runs safety and stability.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the front view of the present invention.
Fig. 3 is the side view of the present invention.
In figure: 1. motor, 2. motor gear, 3. idler gear, 4. screw mandrel drive gear, 5. ball screw, 6. steering wheel guide pin bushing, 7. steering wheel bar, 8. slip electronic ruler, 9. controller, 10. shell, 11. motor wires, 12. electronic ruler feedback lines.
Detailed description of the invention
In order to be able to be more clearly understood that technical scheme, the present invention is further described below in conjunction with the accompanying drawings.
Unmanned aerial vehicle straight line steering wheel as shown in Figure 1, Figure 2, Figure 3 shows, including: motor, motor gear, idler gear, screw gear, ball screw, steering wheel bar, steering wheel guide pin bushing, slip electronic ruler, controller and shell are constituted, this unmanned aerial vehicle straight line steering wheel utilizes ball screw as final transferring element, reduce gear usage quantity, and select High Precision CNC gear, use and there is the direct current generator of electric eliminating arc function and have brush helm control circuit, this motor and circuit have the strongest anti-overload ability, thus ensure that the reliability of steering wheel.
Operation principle: when aircraft flight controller send instruction received by steering engine controller after, control motor and just make the rotation of respective direction, this gear rotarily driving ball screw also begins to rotate, move so that respective direction made by steering wheel bar, now electronic ruler accurately measures shift position, and feedback gives steering engine controller, steering wheel just can control aircraft flight by the instruction of the flight controller of aircraft accurately.
Present configuration is compact, light weight, and precision is high, and reliability anti-overload ability is the best, runs safety and stability.
The above is only the better embodiment of the present invention, therefore all equivalence changes done according to structure, feature and the principle described in present patent application scope or modification, in the range of being all included in present patent application.
Claims (5)
- null1. the operating mechanism of a unmanned aerial vehicle controls device，Including: motor (1)、Motor gear (2)、Idler gear (3)、Screw mandrel drives gear (4)、It is characterized in that: also include ball screw (5)、Steering wheel guide pin bushing (6)、Steering wheel bar (7)、Slip electronic ruler (8)、Controller (9) and shell (10)，Described motor (1) is connected with controller (9) by motor lines (11)，Described slip electronic ruler (8) is connected with controller (9) by electronic ruler feedback line (12)，Described motor gear (2) is positioned at the downside of motor，Described idler gear (3) is positioned at motor gear (2) and screw mandrel drives between gear (3)，Described ball screw (5) drives gear (4) to be connected with screw mandrel，Described steering wheel guide pin bushing (6) is sleeved on ball screw (5)，Described slip electronic ruler (8) is connected with shell (10).
- The operating mechanism of a kind of unmanned aerial vehicle the most according to claim 1 controls device, it is characterised in that: utilize ball screw (5) as final transferring element.
- The operating mechanism of a kind of unmanned aerial vehicle the most according to claim 1 controls device, it is characterised in that: described steering wheel decreases gear usage quantity.
- The operating mechanism of a kind of unmanned aerial vehicle the most according to claim 1 controls device, it is characterised in that: gear used is High Precision CNC gear.
- The operating mechanism of a kind of unmanned aerial vehicle the most according to claim 1 controls device, it is characterised in that: motor used (1) is the direct current generator with electric eliminating arc function,Circuit used is for there being brush helm control circuit, and motor and circuit have the strongest anti-overload ability.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620134653.3U CN205460998U (en) | 2016-02-23 | 2016-02-23 | Unmanned aerial vehicle's operating mechanism controlling means |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620134653.3U CN205460998U (en) | 2016-02-23 | 2016-02-23 | Unmanned aerial vehicle's operating mechanism controlling means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205460998U true CN205460998U (en) | 2016-08-17 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620134653.3U Expired - Fee Related CN205460998U (en) | 2016-02-23 | 2016-02-23 | Unmanned aerial vehicle's operating mechanism controlling means |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205460998U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105727570A (en) * | 2016-02-23 | 2016-07-06 | 山西微风无人***科技有限公司 | Control device of control mechanism of unmanned aerial vehicle |
-
2016
- 2016-02-23 CN CN201620134653.3U patent/CN205460998U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105727570A (en) * | 2016-02-23 | 2016-07-06 | 山西微风无人***科技有限公司 | Control device of control mechanism of unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160817 Termination date: 20210223 |