CN206885333U - Wing rudder face action control mechanism - Google Patents
Wing rudder face action control mechanism Download PDFInfo
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- CN206885333U CN206885333U CN201720512092.0U CN201720512092U CN206885333U CN 206885333 U CN206885333 U CN 206885333U CN 201720512092 U CN201720512092 U CN 201720512092U CN 206885333 U CN206885333 U CN 206885333U
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- wing
- rudder face
- steering wheel
- control mechanism
- action control
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Abstract
The utility model proposes a kind of wing rudder face action control mechanism, including：Wing, it has rotatable movable rudder face portion；Steering wheel, wing is arranged at, to drive the movable rudder face portion to rotate；Transmission mechanism, first end connect the movable rudder face portion, and the second end connects the steering wheel, the movable rudder face action is driven under the drive force of the steering wheel.Wing rudder face action control mechanism of the present utility model, it is ensured that be electrically connected with more stable.
Description
Technical field
It the utility model is related to unmanned vehicle rudder face technology, more particularly to a kind of wing rudder face action control machine
Structure.
Background technology
Fixed-wing model plane, it is in flight course, wing is fixed on fuselage and will not moved with respect to fuselage, by air to wing
Upper and lower active force is poor and produces the aircraft of lift, and in general, wing can include empennage, main wing.All it is generally to pass through rudder
Machine controls the rudder face action to adjust flight attitude.In existing wing, in order that rudder face can directly be driven by obtaining steering wheel rocking arm
Steering wheel, is typically all arranged on the middle part of rudder face, is usually located at wing apical location, rocking arm is fixed with rudder face position by action
Or be relatively fixed and driven to realize, but this structure, because steering wheel is distant from aircraft axis, steering wheel cabling can be compared with
Long (signal wire, power line etc.), easily occur electrically unstable.In the case of especially dismountable in wing tip, connecting portion
It is electrically extremely unstable and require higher.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of wing rudder face action control mechanism, it is ensured that electrically
Connect more stable.
To solve the above problems, the utility model proposes a kind of wing rudder face action control mechanism, including：Wing, it has
There is rotatable movable rudder face portion；Steering wheel, wing is arranged at, to drive the movable rudder face portion to rotate；Transmission mechanism, first
End connects the movable rudder face portion, and the second end connects the steering wheel, the activity is driven under the drive force of the steering wheel
Rudder face action.
According to one embodiment of the present utility model, rocking arm, the transmission mechanism are connected with the output shaft of the steering wheel
The second end pass through the rocking arm and connect the steering wheel；The rocking arm shakes under the driving of the output shaft of the steering wheel, and leads to
Cross the transmission mechanism and drive the movable rudder face portion corresponding actions.
According to one embodiment of the present utility model, the transmission mechanism includes drive link, the first end of the drive link
Be rotatably connected the rocking arm, and the second end of the drive link is rotatably connected the connecting portion in activity rudder face portion；The transmission
The pivot center of the first end of bar is parallel with the pivot center at the second end, and is each perpendicular to the shake plane of the rocking arm.
According to one embodiment of the present utility model, the wing includes airfoil root and wing tip, the wing root
It is detachably connected between portion and the wing tip.
According to one embodiment of the present utility model, the steering wheel is arranged on the airfoil root；The movable rudder face portion
A part be arranged on the airfoil root, another part is arranged on the wing tip；The first end of the transmission mechanism with
The part for being arranged on the airfoil root connection in the movable rudder face portion.
According to one embodiment of the present utility model, in connection shape between the airfoil root and the wing tip
During state, the part for being arranged on the airfoil root and the part for being arranged on the wing tip in the movable rudder face portion are relative solid
It is fixed.
According to one embodiment of the present utility model, electric connection structure, electrical structure are not provided with the wing tip.
According to one embodiment of the present utility model, steering wheel groove is offered on the airfoil root, to accommodate the rudder
Machine.
According to one embodiment of the present utility model, the groove lid covered can be opened by being provided with the steering wheel groove.
According to one embodiment of the present utility model, it is further opened with being used for steering wheel connection line cabling on the airfoil root
Cable tray.
According to one embodiment of the present utility model, the wing is the main wing or empennage of fixed-wing model plane.
After adopting the above technical scheme, the utility model has the advantages that compared with prior art：
Movable rudder face portion is driven by transmission mechanism, the stress point and steering wheel output shaft distance in movable rudder face portion are remote, power
Caused influence is bigger, no matter can be driven in the end position in movable rudder face portion or centre position；Steering wheel is arranged on machine
Wing root portion rather than wing tip, the steering wheel cable run distance between steering wheel such as governor circuit or power supply can be shortened so that electrically
It is more stable, in the case that airfoil root detachably separates with wing tip, still do not interfere with electric connection stability；
Steering wheel is arranged on airfoil root, also may be such that wing tip thickness accomplish it is thinner.
Brief description of the drawings
Fig. 1 is that the structure of the complete machine wing rudder face action control mechanism of the unmanned vehicle of the embodiment of the utility model one is shown
It is intended to；
Fig. 2 is the A partial enlargement structural representations of the main wing rudder face action control mechanism in Fig. 1；
Fig. 3 is the structural representation of the transmission mechanism 16 of the embodiment of the utility model one；
Fig. 4 is the B partial structural diagrams of Fig. 1 empennage rudder face action control mechanism.
Description of symbols in figure：
1- main wings, 11- main wings root, 12- main wings tip, 13- activity rudder faces portion, 14- groove lids, 15- rocking arms, 16- transmissions
Mechanism, the connecting portion in 131- activity rudder faces portion, 161- drive links, 162- ball head structures, 163- fixture blocks, 2- empennages, 21- empennages
Root, 22- empennages tip, 23- activity rudder faces portion, 24- steering wheels, 25- rocking arms, 26- transmission mechanisms, the company in 231- activity rudder faces portion
Socket part position, 3- foot pieces.
Embodiment
To enable above-mentioned purpose of the present utility model, feature and advantage more obvious understandable, below in conjunction with the accompanying drawings to this
The embodiment of utility model is described in detail.
Many details are elaborated in the following description in order to fully understand the utility model.But this practicality is new
Type can be to be much different from other manner described here to implement, and those skilled in the art can be new without prejudice to this practicality
Similar popularization is done in the case of type intension, therefore the utility model is not limited by following public specific implementation.
Referring to Fig. 1, the wing rudder face action control mechanism of the utility model embodiment is applied to the main wing 1 of fixed-wing model plane
Or empennage 2, it is of course also apply to the wings of other unmanned vehicles.Illustrated below with specific embodiment.
Embodiment one
Referring to Fig. 1 and Fig. 2, the wing rudder face action control mechanism of the present embodiment, including：Main wing 1, steering wheel (is hidden in figure
The inner side of groove lid 14), transmission mechanism 16.The wing of the present embodiment is the main wing 1 of unmanned vehicle, and main wing root 11 is fixed on fuselage
On, it can be fixed by connector, can be also integrally formed on fuselage.Main wing tip 12 is to be arranged on the both sides of main wing root 11
Tip, including left tip and right tip, the specific real-time mode in example below are applicable for left tip and right tip.Tool
The division proportion of body root and tip is unlimited, and depending on as needed, tip is located at side of the root away from body side.
There is movable rudder face portion 13 on main wing 1.Set-up mode of the movable rudder face portion 13 on main wing 1 can be with showing with position
There is the setting on wing identical.Movable rudder face portion 13 is arranged on the length direction of main wing 1, and positioned at the margin location of main wing 1
Put.The length direction in movable rudder face portion 13 is consistent with the length direction of main wing 1.Movable rudder face portion 13 can be relative by the driving of steering wheel
Main wing 1 stirs.
Steering wheel is arranged on main wing root 11, the driving force acted to output control activity rudder face portion 13.Steering wheel can be
The steering wheel of existing unmanned vehicle, there is output shaft, output shaft is connected with transmission mechanism, so as to pass through the band of transmission mechanism 6
Movable rudder face portion 13 is moved to move.
The first end connection activity rudder face portion 13 of transmission mechanism 16, the second end connection of the relative first end of transmission mechanism 16
Steering wheel.The structure type of transmission mechanism 16 is specifically unlimited, as long as movable rudder face portion 13 be able to can be driven under the driving of steering wheel
Corresponding action is made, can be transformed as needed.
Movable rudder face portion 13, stress point and the steering wheel output shaft distance in movable rudder face portion 13 are driven by transmission mechanism 16
Far, influence is bigger caused by power, no matter can be driven in the end position in movable rudder face portion 13 or centre position；Steering wheel is set
Put in main wing root 11 rather than main wing tip 12, the steering wheel between steering wheel such as governor circuit or power supply can be shortened and walk line-spacing
From so that it is electrically more stable, in the case of detachably being separated with main wing tip 12 even in main wing root 11, still do not interfere with
It is electrically connected with stability；Steering wheel is arranged on main wing root 11, also may be such that main wing tip 12 thickness accomplish it is thinner.
In preferred embodiment, steering wheel and transmission mechanism 16 are arranged on main wing root 11 close to the position of main wing tip 12
Place, it is easier to drive drive activity rudder face portion 13.
Preferably, being connected with rocking arm 15 on the output shaft of steering wheel, the second end of transmission mechanism 16 connects rudder by rocking arm 15
Machine.Rocking arm 15 shakes under the driving of the output shaft of steering wheel, i.e., reciprocally swinging occurs around axle, due to the second end of drive mechanism 16
It is connected on rocking arm 15, thus the end is also accordingly shaken, so as to the corresponding actions of drive activity rudder face portion 13.Existing steering wheel is direct
Movable rudder face portion is driven to act by rocking arm, shorter yet with rocking arm, stress point and output shaft distance are near, and power is to activity
The influence in rudder face portion is smaller, and the position that can be only positioned among movable rudder face portion just can driven drive.And in this implementation
In, steering wheel drives transmission mechanism 16 by rocking arm 15, and movable rudder face portion 13, stress point and output are driven by transmission mechanism 16
Wheelbase influences bigger from remote, caused by power, no matter can be driven in the end position in movable rudder face portion 13 or centre position.
Preferably, referring to Fig. 2 and Fig. 3, transmission mechanism 16 includes drive link 161.The first end of drive link 161 rotatably connects
Connect rocking arm 15, the second end of drive link 161 is rotatably connected the connecting portion 131 in activity rudder face portion.The first end of drive link 161
Pivot center it is parallel with the pivot center at the second end, and be each perpendicular to the shake plane of rocking arm 15.Rocking arm 15 is when shaking, meeting
Drive link 161 is pushed or pull on, meanwhile, certain rotation occurs for drive link first end and the second end so that drive link 161 moves
During keep it is parallel with aerofoil.
Optionally, such as Fig. 2, the attachment structure between the first end and rocking arm 15 of drive link 161 is chuck structure, chuck knot
Structure includes the vertical bending part of fixture block 163 and drive link 161.Axis hole is opened up on rocking arm 15, the first end of drive link 161 is vertically curved
Rolling over and extending into axis hole can be rotated relative to axis hole, also have fixture block 163 in the first end of drive link 161, and the one end of fixture block 163 is fixed
In the main body section of drive link 161, the position for the stretching axis hole that the connection of the other end of fixture block 162 is vertically bent is vertical for limiting
The axial movement of bending part.Attachment structure between the connecting portion 131 in the second end of drive link 161 and movable rudder face portion is
Ball head structure 162, the connecting portion 131 in movable rudder face portion is bulb, and the structure at the end of drive link second is the ball coordinated with bulb
Shell or part spherical shell.Certainly, the attachment structure at the both ends of drive link can exchange, or the attachment structure at both ends is bulb knot
Structure or chuck structure, or can be other attachment structures.
Preferably, main wing 1 can include main wing root 11 and main wing tip 12, between main wing root 11 and main wing tip 12
It is detachably connected.It can realize that Quick Release connects between main wing root 11 and main wing tip 12 by buckle structure, or can lead to
Cross the connection of other Detachable connection structures.
Steering wheel is arranged on main wing root 11.The part in movable rudder face portion 13 is arranged on main wing root 11, another part is set
Put in main wing tip 12；In other words, the division limits of main wing root 11 and main wing tip 12 are located at and split movable rudder face portion 13
For two halves.The first end of transmission mechanism 16 is connected with the part for being arranged on main wing root 11 in movable rudder face portion 13.
When connection status is between main wing root 11 and main wing tip 12, movable rudder face portion 13 is arranged on main wing root
The part in portion 11 is relatively fixed with being arranged on the part of main wing tip 12.Due to having led between main wing root 11 and main wing tip 12
Buckle structure or other structures connection are crossed, thus phase only can be limited by position limiting structure between two half parts in movable rudder face portion 13
To movement, e.g. concave-convex fit structure, attachment structure can not had to.
Preferably, electric connection structure, electrical structure are not provided with main wing tip 12.By steering wheel need electric connection structure and
Electrical structure is provided entirely on main wing root 11 so that when main wing tip 12 dismounts with main wing root 11, can avoid fuselage
Electrically isolated or reclosing between governor circuit and these electric connection structures, electrical structure and caused electrically unstable ask
Topic.
Preferably, steering wheel groove (in figure under groove lid 14) is offered on main wing root 11, to accommodate steering wheel.Steering wheel
It can be fixed on by bond or spiro connecting piece etc. in steering wheel groove.Steering wheel groove can reduce the height of steering wheel and transmission mechanism 16,
It is easy to be driven, beneficial to cabling, also makes outward appearance more complete attractive in appearance.
More preferably, the groove lid 14 covered can be opened by being provided with steering wheel groove.Certainly in the limited feelings of the wall thickness of main wing root 11
Under condition, groove lid can also be not provided with.Groove lid 14 can play certain protective effect and fixation to steering wheel, in appearance
It is more complete attractive in appearance.Groove lid 14 can be fixed on main wing root 11 by spiro connecting piece, or can be by snapping connection.
The cable tray (not shown) for steering wheel connection line cabling is further opened with main wing root 11.Cabling leads to
Road can be channel-shaped or pipe-like, specific unlimited.Line arrangement can be unified, avoid cabling mixed and disorderly and exposed etc.
The problem of.
Embodiment two
Referring to Fig. 1 and Fig. 3, the present embodiment in place of the difference of embodiment one with being, the wing rudder face action of the present embodiment
Controlling organization includes：Empennage 2, steering wheel 24, transmission mechanism 26.The wing of the present embodiment be unmanned vehicle empennage 2, empennage 2
Including empennage root 21 and empennage tip 22, empennage root 21 is fixed in the distal portion of foot piece 3, can be fixed by connector
Fuselage is connected in the distal portion of foot piece 3, and by foot piece 3, empennage tip 22 is connected in the both sides of empennage root 21.Movable rudder face portion
23 are arranged on empennage 2.
Steering wheel 24 is similarly disposed on empennage root 21, and steering wheel 24 is accommodated because empennage 2 is relatively thin, thus opening up steering wheel groove
When, on steering wheel groove can not grooved lid, steering wheel 24 is fixed in steering wheel groove.
Also rocking arm 25 can be connected with the output shaft of the steering wheel 24 of the present embodiment, the second end of transmission mechanism 26 rotatably connects
Rocking arm 25 is connect, rocking arm 25 is connected between the end of steering wheel transmission mechanism 26 second.Rocking arm 25 is under the driving of the output shaft of steering wheel 24
Shake, because the second end of drive mechanism 26 is connected on rocking arm 25, thus the end is also accordingly shaken, so as to drive activity rudder face
The corresponding actions of portion 23.The first end of transmission mechanism 26 is rotatably connected the connecting portion 231 in activity rudder face portion.Other particular contents
The description in previous embodiment one is may refer to, will not be repeated here.
Although the utility model is disclosed as above with preferred embodiment, it is not for limiting claim, Ren Heben
Art personnel are not being departed from spirit and scope of the present utility model, can make possible variation and modification, therefore
The scope of protection of the utility model should be defined by the scope that the utility model claims are defined.
Claims (11)
- A kind of 1. wing rudder face action control mechanism, it is characterised in that including：Wing, it has rotatable movable rudder face portion； Steering wheel, wing is arranged at, to drive the movable rudder face portion to rotate；Transmission mechanism, first end connect the movable rudder face portion, Second end connects the steering wheel, and the movable rudder face action is driven under the drive force of the steering wheel.
- 2. wing rudder face action control mechanism as claimed in claim 1, it is characterised in that connected on the output shaft of the steering wheel There is rocking arm, the second end of the transmission mechanism connects the steering wheel by the rocking arm；Output of the rocking arm in the steering wheel Shaken under the driving of axle, and the movable rudder face portion corresponding actions are driven by the transmission mechanism.
- 3. wing rudder face action control mechanism as claimed in claim 2, it is characterised in that the transmission mechanism includes transmission Bar, the first end of the drive link are rotatably connected the rocking arm, and the second end of the drive link is rotatably connected activity rudder face The connecting portion in portion；The pivot center of the first end of the drive link is parallel with the pivot center at the second end, and is each perpendicular to institute State the shake plane of rocking arm.
- 4. wing rudder face action control mechanism as claimed in claim 1, it is characterised in that the wing include airfoil root and Wing tip, it is detachably connected between the airfoil root and the wing tip.
- 5. wing rudder face action control mechanism as claimed in claim 4, it is characterised in that the steering wheel is arranged on the wing Root；The part in the movable rudder face portion is arranged on the airfoil root, another part is arranged on the wing tip；It is described The first end of transmission mechanism is connected with the part for being arranged on the airfoil root in the movable rudder face portion.
- 6. wing rudder face action control mechanism as claimed in claim 5, it is characterised in that in the airfoil root and the machine When connection status is between wing tip portion, the part for being arranged on the airfoil root in the movable rudder face portion is described with being arranged on The part of wing tip is relatively fixed.
- 7. wing rudder face action control mechanism as claimed in claim 5, it is characterised in that be not provided with electricity on the wing tip Attachment structure, electrical structure.
- 8. the wing rudder face action control mechanism as described in any one in claim 1-7, it is characterised in that the wing root Steering wheel groove is offered in portion, to accommodate the steering wheel.
- 9. wing rudder face action control mechanism as claimed in claim 8, it is characterised in that being provided with the steering wheel groove to beat Uncap the groove lid of conjunction.
- 10. wing rudder face action control mechanism as claimed in claim 8, it is characterised in that also opened up on the airfoil root There is the cable tray for steering wheel connection line cabling.
- 11. the wing rudder face action control mechanism as described in any one in claim 1-7, it is characterised in that the wing For the main wing or empennage of fixed-wing model plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720512092.0U CN206885333U (en) | 2017-05-09 | 2017-05-09 | Wing rudder face action control mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720512092.0U CN206885333U (en) | 2017-05-09 | 2017-05-09 | Wing rudder face action control mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206885333U true CN206885333U (en) | 2018-01-16 |
Family
ID=61340747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720512092.0U Active CN206885333U (en) | 2017-05-09 | 2017-05-09 | Wing rudder face action control mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206885333U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720564A (en) * | 2019-02-13 | 2019-05-07 | 深圳创壹通航科技有限公司 | Fixed-wing unmanned plane and its control method with VTOL function |
| CN112977802A (en) * | 2021-02-26 | 2021-06-18 | 珠海天晴航空航天科技有限公司 | Integrated control surface connecting structure, manufacturing method and unmanned aerial vehicle |
| CN114558329A (en) * | 2022-02-11 | 2022-05-31 | 东莞市飞翼电子科技有限公司 | Steering control structure of model airplane |
-
2017
- 2017-05-09 CN CN201720512092.0U patent/CN206885333U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720564A (en) * | 2019-02-13 | 2019-05-07 | 深圳创壹通航科技有限公司 | Fixed-wing unmanned plane and its control method with VTOL function |
| CN112977802A (en) * | 2021-02-26 | 2021-06-18 | 珠海天晴航空航天科技有限公司 | Integrated control surface connecting structure, manufacturing method and unmanned aerial vehicle |
| CN114558329A (en) * | 2022-02-11 | 2022-05-31 | 东莞市飞翼电子科技有限公司 | Steering control structure of model airplane |
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