CN206968964U - A kind of unmanned airplane empennage rudder face directly drives control device - Google Patents
A kind of unmanned airplane empennage rudder face directly drives control device Download PDFInfo
- Publication number
- CN206968964U CN206968964U CN201720629084.4U CN201720629084U CN206968964U CN 206968964 U CN206968964 U CN 206968964U CN 201720629084 U CN201720629084 U CN 201720629084U CN 206968964 U CN206968964 U CN 206968964U
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- CN
- China
- Prior art keywords
- empennage
- rudder face
- motor
- control device
- unmanned airplane
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
The utility model discloses a kind of unmanned airplane empennage rudder face and directly drives control device, including empennage and fixed seat, the empennage end is provided with empennage rudder face, the fixed seat side is provided with motor, motor pivoted arm is connected with the motor, the empennage rudder face is being provided with control seat close to fixed seat side, and the control seat is provided with the mounting hole to match with motor pivoted arm；The unmanned airplane empennage rudder face, which directly drives control device, can improve flight control accuracy, contribute to the lifting of unmanned plane during flying operating efficiency, and improve equipment operation and maintainability, save space.
Description
Technical field
Unmanned airplane empennage technical field is the utility model is related to, more particularly to a kind of unmanned airplane empennage rudder face directly controls system dress
Put.
Background technology
Compared with manned aircraft, unmanned plane advantage is that rank is small, and maintenance is few, uses efficiency-cost ratio height；At some such as nothing
People area power-line patrolling, it is used widely in the Surveying and Mapping Industry of low latitude；The rotation control of the unmanned airplane empennage rudder face of current existing shaping
In scheme processed, controlling organization uses electric machine actuating mechanism of the output end for revolute pair mostly；Electric machine actuating mechanism end is provided with
Rocking arm is rotated, and rocking arm connecting rod is connected with empennage rudder face, and then control the rotation of rudder face.
Existing rudder plane controlling mechanism connects rudder face and actuating motor, in general using connecting rod mostly, and pull bar is held with motor
The rocking arm of row mechanism uses axle-hole connected mode, and the connected mode has certain spacious amount, and is eventually enlarged into empennage rudder
The diastema in face；On the other hand, because the length of connecting rod and its motion need certain activity space, therefore conventional rudder face controlling party
Formula can take space in bigger unmanned plane machine.
Utility model content
In view of above-mentioned technical problem, the purpose of this utility model is that providing a kind of unmanned airplane empennage rudder face directly controls system dress
Put, its unmanned airplane empennage rudder face, which directly drives control device, can improve flight control accuracy, contribute to unmanned plane during flying operating efficiency
Lifting, and improve equipment operation and maintainability, save space.
The utility model provides a kind of unmanned airplane empennage rudder face and directly drives control device, including empennage and fixed seat, the tail
Wing end is provided with empennage rudder face, and the fixed seat side is provided with motor, and motor pivoted arm, the empennage rudder are connected with the motor
Face is being provided with control seat close to fixed seat side, and the control seat is provided with the mounting hole to match with motor pivoted arm.
Preferably, the empennage is detachably connected with fixed seat.Empennage and fixed seat can be entered according to actual conditions
Row installation and dismounting.
Preferably, the rotating shaft of the motor pivoted arm and empennage rudder face rotation axis are concentric.
Preferably, the motor pivoted arm clamping of the control seat and motor on the empennage rudder face connects.Pass through turning for motor
The rotation of dynamic drive motor pivoted arm, so that the empennage rudder face on control seat is swung.
Preferably, the mounting hole is interference fitted with motor pivoted arm.Effectively reduce the diastema of empennage rudder face.
Preferably, the projection extended to outside empennage is provided with the middle part of the empennage.
Preferably, the groove to fixed seat inner recess is provided with the middle part of the fixed seat.
Preferably, the projection is interference fitted with groove.By the interference fit of projection and groove, make empennage and fixation
Seat can firmly install.
Preferably, it is to tilt down in the domatic of hill-like structure with empennage rudder face junction on the empennage.Increase
Macrodome, the empennage can be made to be tailed off in flight course by resistance.
Preferably, the motor is rotatablely connected through fixed seat and with motor pivoted arm.Driven by the rotation of motor
The rotation of motor pivoted arm.
Operation principle：When directly driving control device using the unmanned airplane empennage rudder face, by starting motor, make the electricity on motor
Machine pivoted arm is rotated, and motor pivoted arm is interference fitted with the control hole on control seat, makes the volume control seat being arranged on motor pivoted arm
Rotate, so as to drive the empennage rudder face of control seat side to swing up and down, so as to reach the direction that driving unmanned plane moves left and right.
The utility model compared with prior art, the advantage is that：Empennage and fixed seat, empennage end are provided with empennage rudder
Face, fixed seat side are provided with motor, and motor pivoted arm is connected with motor, and the motor pivoted arm and empennage rudder face rotation axis are same
The heart, empennage rudder face are being provided with control seat close to fixed seat side, and the control seat is provided with the installation to match with motor pivoted arm
Hole, the unmanned airplane empennage rudder face, which directly drives control device, can reduce unmanned plane full set empennage rudder face control device volume, improve nothing
Space availability ratio in man-machine machine；The straight control accuracy driven control mode and improve empennage rudder face；The simplification of structure and institute simultaneously
The reduction of part is needed to improve reliability and maintainability.
Brief description of the drawings
The essential structure that the utility model unmanned airplane empennage rudder face directly drives control device is illustrated with reference to the accompanying drawings, its
In：
Fig. 1 is the structural representation that this practical unmanned airplane empennage rudder face directly drives control device；
Fig. 2 is the structural representation for the control seat that this practical unmanned airplane empennage rudder face directly drives control device；
Fig. 3 is that this practical unmanned airplane empennage rudder face directly drives the structural representation that the projection of control device and groove are connected；
Fig. 4 is the structural representation for another embodiment that this practical unmanned airplane empennage rudder face directly drives control device.
Embodiment
For clarity of illustration, control device is directly driven to unmanned airplane empennage rudder face in an illustrative manner with reference to the accompanying drawings to add
With explanation.It should be appreciated that the utility model is not intended to be limited thereto.
Embodiment 1
As shown in Figure 1-2, unmanned airplane empennage rudder face of the present utility model directly drives control device, including empennage 1 and fixation
Seat 2, the end of empennage 1 is provided with empennage rudder face 3, and the side of fixed seat 2 is provided with motor 4, motor is connected with the motor 4
Pivoted arm 5, the empennage rudder face 3 are being provided with control seat 6 close to the side of fixed seat 2, and the control seat 6 is provided with and motor pivoted arm 5
The mounting hole 7 to match.
The empennage 1 is detachably connected with fixed seat 2.Empennage 1 and fixed seat 2 can be installed according to actual conditions
With dismounting.
The rotating shaft of the motor pivoted arm 5 and the rotation axis of empennage rudder face 3 are concentric.
Control seat 6 on the empennage rudder face 3 is connected with the clamping of motor pivoted arm 5 of motor 4.Pass through the rotational band of motor 4
The rotation of dynamic motor pivoted arm 5, so that the empennage rudder face 3 on control seat 6 is swung.
The mounting hole 7 is interference fitted with motor pivoted arm 5.Effectively reduce the diastema of empennage rudder face 3.
With the junction of empennage rudder face 3 it is to tilt down in domatic the 10 of hill-like structure on the empennage 1.Increase domatic
10, the empennage 1 can be made to be tailed off in flight course by resistance.
The motor 4 is rotatablely connected through fixed seat 2 and with motor pivoted arm 5.Turned by the rotation drive motor of motor 4
The rotation of arm 5.
When control device is directly driven using the unmanned airplane empennage rudder face 3, by starting motor 4, make the motor pivoted arm on motor 4
5 are rotated, and motor pivoted arm 5 is interference fitted with the control hole on control seat 6, make volume 6 turns of the seat of control being arranged on motor pivoted arm 5
It is dynamic, so as to drive the empennage rudder face 3 of control seat 6 side to swing up and down, so as to reach the direction that driving unmanned plane moves left and right.
The utility model compared with prior art, the advantage is that：Empennage and fixed seat, empennage end are provided with empennage rudder
Face, fixed seat side are provided with motor, and motor pivoted arm is connected with motor, and the motor pivoted arm and empennage rudder face rotation axis are same
The heart, empennage rudder face are being provided with control seat close to fixed seat side, and the control seat is provided with the installation to match with motor pivoted arm
Hole, the unmanned airplane empennage rudder face, which directly drives control device, can reduce unmanned plane full set empennage rudder face control device volume, improve nothing
Space availability ratio in man-machine machine；The straight control accuracy driven control mode and improve empennage rudder face；The simplification of structure and institute simultaneously
The reduction of part is needed to improve reliability and maintainability.
Embodiment 2
As in Figure 2-4, unmanned airplane empennage rudder face of the present utility model directly drives control device, including empennage 1 and fixed seat
2, the end of empennage 1 is provided with empennage rudder face 3, and the side of fixed seat 2 is provided with motor 4, and motor is connected with the motor 4 and is turned
Arm 5, the empennage rudder face 3 are being provided with control seat 6 close to the side of fixed seat 2, and the control seat 6 is provided with and the phase of motor pivoted arm 5
The mounting hole 7 of matching.
The empennage 1 is detachably connected with fixed seat 2.Empennage 1 and fixed seat 2 can be installed according to actual conditions
With dismounting.
The rotating shaft of the motor pivoted arm 5 and the rotation axis of empennage rudder face 3 are concentric.
Control seat 6 on the empennage rudder face 3 is connected with the clamping of motor pivoted arm 5 of motor 4.Pass through the rotational band of motor 4
The rotation of dynamic motor pivoted arm 5, so that the empennage rudder face 3 on control seat 6 is swung.
The mounting hole 7 is interference fitted with motor pivoted arm 5.Effectively reduce the diastema of empennage rudder face 3.
The middle part of empennage 1 is provided with the projection 8 extended to outside empennage 1.
The middle part of fixed seat 2 is provided with the groove 9 to the inner recess of fixed seat 2.
The projection 8 is interference fitted with groove 9.By the interference fit of projection 8 and groove 9, make empennage 1 and fixed seat 2
It can firmly install.
With the junction of empennage rudder face 3 it is to tilt down in domatic the 10 of hill-like structure on the empennage 1.Increase domatic
10, the empennage 1 can be made to be tailed off in flight course by resistance.
The motor 4 is rotatablely connected through fixed seat 2 and with motor pivoted arm 5.Turned by the rotation drive motor of motor 4
The rotation of arm 5.
When control device is directly driven using the unmanned airplane empennage rudder face 3, by starting motor 4, make the motor pivoted arm on motor 4
5 are rotated, and motor pivoted arm 5 is interference fitted with the control hole on control seat 6, make volume 6 turns of the seat of control being arranged on motor pivoted arm 5
It is dynamic, so as to drive the empennage rudder face 3 of control seat 6 side to swing up and down, so as to reach the direction that driving unmanned plane moves left and right.
The utility model compared with prior art, the advantage is that：Empennage and fixed seat, empennage end are provided with empennage rudder
Face, fixed seat side are provided with motor, and motor pivoted arm is connected with motor, and the motor pivoted arm and empennage rudder face rotation axis are same
The heart, empennage rudder face are being provided with control seat close to fixed seat side, and the control seat is provided with the installation to match with motor pivoted arm
Hole, the unmanned airplane empennage rudder face, which directly drives control device, can reduce unmanned plane full set empennage rudder face control device volume, improve nothing
Space availability ratio in man-machine machine；The straight control accuracy driven control mode and improve empennage rudder face；The simplification of structure and institute simultaneously
Need the reduction of part to improve reliability and maintainability, the projection extended to outside empennage, fixed seat middle part are provided with the middle part of empennage
The groove to fixed seat inner recess is provided with, projection is interference fitted with groove, by the interference fit of projection and groove, makes tail
The wing can firmly install with fixed seat, difficult for drop-off in flight course.
Preferred embodiment of the present utility model is clearly stated above with reference to accompanying drawing, it is understood, however, that the utility model
It is not intended to be limited thereto.For those skilled in the art, the utility model can have various modifications and variations.It is all in this reality
Within new spirit and principle, any modification, equivalent substitution and improvements made etc., it should be included in of the present utility model
Within right.
Claims (10)
1. a kind of unmanned airplane empennage rudder face directly drives control device, it is characterised in that：Including empennage and fixed seat, the empennage end
Provided with empennage rudder face, the fixed seat side is provided with motor, is connected with motor pivoted arm on the motor, the empennage rudder face by
Nearly fixed seat side is provided with control seat, and the control seat is provided with the mounting hole to match with motor pivoted arm.
2. unmanned airplane empennage rudder face according to claim 1 directly drives control device, it is characterised in that：The empennage and fixation
Seat is detachably connected.
3. unmanned airplane empennage rudder face according to claim 1 directly drives control device, it is characterised in that：The motor pivoted arm
Rotating shaft and empennage rudder face rotation axis are concentric.
4. unmanned airplane empennage rudder face according to claim 3 directly drives control device, it is characterised in that：On the empennage rudder face
Control seat and motor motor pivoted arm clamping connect.
5. unmanned airplane empennage rudder face according to claim 1 directly drives control device, it is characterised in that：The mounting hole and electricity
Machine pivoted arm is interference fitted.
6. unmanned airplane empennage rudder face according to claim 1 directly drives control device, it is characterised in that：On in the middle part of the empennage
Provided with the projection extended to outside empennage.
7. unmanned airplane empennage rudder face according to claim 6 directly drives control device, it is characterised in that：In the middle part of the fixed seat
It is provided with the groove to fixed seat inner recess.
8. unmanned airplane empennage rudder face according to claim 7 directly drives control device, it is characterised in that：The projection and groove
Interference fit.
9. unmanned airplane empennage rudder face according to claim 1 directly drives control device, it is characterised in that：On the empennage with tail
Wing rudder face junction is to tilt down in the domatic of hill-like structure.
10. unmanned airplane empennage rudder face according to claim 1 directly drives control device, it is characterised in that：The motor runs through
It is rotatablely connected in fixed seat and with motor pivoted arm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720629084.4U CN206968964U (en) | 2017-06-02 | 2017-06-02 | A kind of unmanned airplane empennage rudder face directly drives control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720629084.4U CN206968964U (en) | 2017-06-02 | 2017-06-02 | A kind of unmanned airplane empennage rudder face directly drives control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206968964U true CN206968964U (en) | 2018-02-06 |
Family
ID=61411721
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720629084.4U Expired - Fee Related CN206968964U (en) | 2017-06-02 | 2017-06-02 | A kind of unmanned airplane empennage rudder face directly drives control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206968964U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791820A (en) * | 2018-05-08 | 2018-11-13 | 兰州空间技术物理研究所 | A kind of flat steering engine mechanism for aileron |
| CN109238634A (en) * | 2018-09-12 | 2019-01-18 | 北京空天技术研究所 | Hypersonic aircraft model in wind tunnel rudder-face device |
| WO2020000690A1 (en) * | 2018-06-25 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Fixed-wing unmanned aerial vehicle and empennage thereof |
| CN112520017A (en) * | 2020-12-14 | 2021-03-19 | 中宇航通(北京)航空集团有限公司 | Control surface driving device and method of aircraft |
-
2017
- 2017-06-02 CN CN201720629084.4U patent/CN206968964U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791820A (en) * | 2018-05-08 | 2018-11-13 | 兰州空间技术物理研究所 | A kind of flat steering engine mechanism for aileron |
| WO2020000690A1 (en) * | 2018-06-25 | 2020-01-02 | 深圳市大疆创新科技有限公司 | Fixed-wing unmanned aerial vehicle and empennage thereof |
| CN109238634A (en) * | 2018-09-12 | 2019-01-18 | 北京空天技术研究所 | Hypersonic aircraft model in wind tunnel rudder-face device |
| CN112520017A (en) * | 2020-12-14 | 2021-03-19 | 中宇航通(北京)航空集团有限公司 | Control surface driving device and method of aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180206 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |