CN206202663U - A kind of propeller twin shaft vector servo deviator and VTOL fixed-wing unmanned plane - Google Patents
A kind of propeller twin shaft vector servo deviator and VTOL fixed-wing unmanned plane Download PDFInfo
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- CN206202663U CN206202663U CN201621305940.2U CN201621305940U CN206202663U CN 206202663 U CN206202663 U CN 206202663U CN 201621305940 U CN201621305940 U CN 201621305940U CN 206202663 U CN206202663 U CN 206202663U
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Abstract
The utility model is related to unmanned air vehicle technique field, especially a kind of propeller twin shaft vector servo deviator and VTOL fixed-wing unmanned plane.It includes the rotation steering wheel that the fixed steering wheel that is regularly installed on the tail end of unmanned plane, axle be connected on fixed steering wheel, the airscrew engine that axle is connected on rotation steering wheel and the propeller being set on the output shaft of airscrew engine；Fixed servo driving rotates steering wheel and makees upper and lower rotary motion, rotates servo driving airscrew engine and makees left-right rotation, and airscrew engine drives propeller to rotate.The utility model is using fixed steering wheel, rotation steering wheel, the driving between airscrew engine and propeller and structural relation, the universal driving effect of twin shaft can be formed, carried out in multiple directions and plane with the rotary state for finally enabling propeller, hover for the high-altitude for realizing aircraft, level is pushed, the steering of various angles etc. provides condition, the scope of unmanned plane deflecting is effectively expanded, for the conversion of the flight attitude of unmanned plane provides sound assurance.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, especially a kind of propeller twin shaft vector servo deviator and
Based on the VTOL fixed-wing unmanned plane that this deviator is formed.
Background technology
Unmanned plane is the not manned vehicle of a kind of utilization radio robot and the presetting apparatus manipulation provided for oneself,
Be widely used in taking photo by plane because its maneuverability, reaction quick, unmanned flight and operation require low advantage,
The numerous areas such as agricultural plant protection, disaster relief, geological mapping, news report, electric inspection process, movies-making, military surveillance.
At present, thrust deflecting technology unmanned plane flight attitude adjust and flying height adjust during play to
Close important effect.Traditional thrust deflecting technology generally refers to deflection of the motor power by jet pipe or tail jet
The thrust component of generation substitutes the control surface of former aircraft or the operating function of enhancing aircraft, and the flight to aircraft controlled in real time
The technology of system, can effectively improve the maneuvering capability of aircraft, and so as to reduce the pneumatic rudder face of aircraft, the synthesis for strengthening aircraft flies
Row performance；But in view of unmanned plane structural and feature in itself, existing unmanned plane is mainly by the control to propeller
To realize the deflecting function of thrust, i.e.,：Its thrust is set to produce vertical or horizontal deflection by controlling engine, so as to nobody
Machine produces additional thrust component and additional thrust torque, and to realize that the thrust to aircraft is deflected, and then it is extra to obtain aircraft
Control ability, realize the adjustment control of flight attitude and flying height.However, due to existing airscrew thrust side steering
Certain deficiency is still present in the design of structure, flexibility is poor, direction change scope to cause propeller deflecting to exist
The problems such as small, deflecting process stability difference；Meanwhile, it is relatively multiple also to there is this body structure in existing propeller side steering
Miscellaneous, structure member arrangement is unreasonable, realize difficulty etc. defect.
Furthermore, existing unmanned plane is generally divided into two kinds of fixed-wing unmanned plane and rotary wings unmanned plane；Wherein, rotate
Wing unmanned plane relies primarily on engine makes rotary wings around own axes rotation, produces relative motion to obtain with air during rotary wings rotation
Lift, but it is mainly lift due to what rotary wings were provided, and the level parallel to fuselage axis that rotary wings unmanned plane is obtained is pushed away
Power is smaller, so horizontal flight speed is slower.And fixed-wing unmanned plane is then mainly promoted by engine, engine drives generation flat
Row allows unmanned plane high-speed flight in the air in the horizontal thrust of fuselage axis, but due to engine can not produce perpendicular to
The lift of fuselage axis, so fixed-wing unmanned plane can only obtain lift by the relative motion between fixed-wing and air, with
The gravity of fixed-wing unmanned plane, the speed of related movement between the size and fixed-wing and air of lift is overcome to there is positive correlation pass
System, speed of related movement is bigger, and the lift that fixed-wing unmanned plane is obtained is also bigger；So that fixed-wing unmanned plane is mainly deposited
In following two shortcomings：Runway more long is needed when the first, taking off can just make fixed-wing unmanned plane obtain enough horizontal velocities,
So that fixed-wing unmanned plane obtains enough lift and takes off；2nd, fixed-wing unmanned plane needs to keep after take off enough flight
Speed could obtain enough lift to overcome the gravity of itself.Based on this, or current unmanned plane horizontal flight speed compared with
Slowly, or needing to rely on long runway and needing to keep enough flying speeds after taking off.
Utility model content
For the deficiency that above-mentioned prior art is present, a purpose of the present utility model is to provide a kind of propeller twin shaft
Vector servo deviator；Another purpose of the present utility model be provide it is a kind of based on this deviator formed it is vertical
Landing fixed-wing unmanned plane.
To achieve these goals, first technical scheme that the utility model is used for：
A kind of propeller twin shaft vector servo deviator, it includes the fixation being regularly installed on the tail end of unmanned plane
Rotation steering wheel that steering wheel, axle are connected on fixed steering wheel, axle are connected in the airscrew engine that rotates on steering wheel and are set in spiral
Propeller on the output shaft of paddle motor；The fixed servo driving rotates steering wheel relative to fixed steering wheel in Y-Z axial planes
Inside make upper and lower rotary motion, the rotation servo driving airscrew engine is made relative to steering wheel is rotated in upper X-Y axial planes
Left-right rotation, the airscrew engine drives propeller to make rotation fortune by axis of the central shaft of airscrew engine
It is dynamic.
Preferably, the fixed steering wheel includes the first base of steering gear and the fixation that are regularly installed on the tail end of unmanned plane
Be installed in the first vector motor on the first base of steering gear, the output shaft of the first vector motor is arranged along X-direction, and
The center line of the output shaft of the first vector motor is located in the central region of the first base of steering gear；
Two the first spiral arms, two described first are symmetrically provided with the bottom surface for rotating steering wheel and along X-direction
The equal axle in end of spiral arm is connected in the first base of steering gear lower area and respectively positioned at the left side and right side of the first vector motor, institute
The first active swing arm is socketed with the output shaft for stating the first vector motor, the central region axle of the rotation steering wheel is connected with the first rank
Swing arm is connect, the end phase axle that the head end of the first active swing arm is connected swing arm with first connects；
The first vector motor rotates steering wheel with two first by the first active swing arm and the first linking swing arm driving
Connecting line between the end of spiral arm for rotation axis in Y-Z axial planes relative to the first base of steering gear make from top to bottom or by
Under supreme rotary motion.
Preferably, first base of steering gear is " u "-shaped along the cross sectional shape of X-direction, and the first vector motor is consolidated
Surely it is installed on the base plate of the first base of steering gear, two first spiral arms are located at two relative side plates of the first base of steering gear
Between and each described first spiral arm be connected by the side plate of a pivotal axis and corresponding first base of steering gear.
Preferably, ring is all on the set hole inwall of the first active swing arm and is equably provided with some anti-skid racks.
Preferably, the head end of the first active swing arm is formed with two the first axillares of Relative distribution, first rank
The end for connecing swing arm is held between two the first axillares and is connected with the first axillare by a connecting shaft.
Preferably, the rotation steering wheel includes the second base of steering gear and is regularly installed on the bottom surface of the second base of steering gear
The second vector motor, two first spiral arms by the second base of steering gear bottom surface the left and right sides towards the first base of steering gear
Extension aftershaping is made in direction, and the output shaft of the second vector motor is arranged along Y direction, the bottom of second base of steering gear
Region and a positive stop strip mouthful is offered along X-direction, the output shaft of the second vector motor is located at the middle region of positive stop strip mouthful
In domain；
Two second are symmetrically provided with the bottom surface of the airscrew engine and positioned at the both sides up and down of positive stop strip mouthful
Spiral arm, on the top surface of the second base of steering gear and position corresponding with each the second spiral arm is each formed with one with corresponding
Two spiral arm phase axles support arm even, is socketed with the second active swing arm, the propeller on the output shaft of the second vector motor
The eccentric region axle of engine is connected with the second linking swing arm, the end that the head end of the second active swing arm is connected swing arm with second
Phase axle connects；
The second vector motor is by the second active swing arm and the second linking swing arm driving airscrew engine with two
Connecting line between the end of the second spiral arm for rotation axis in X-Y plane relative to the second base of steering gear make from left to right or
Rotary motion from right to left.
Preferably, ring is all on the set hole inwall of the second active swing arm and is equably provided with some anti-skid racks.
Preferably, the head end of the second active swing arm is formed with two the second axillares of Relative distribution, second rank
The end for connecing swing arm is held between two the second axillares and is connected with the second axillare by a connecting shaft.
Preferably, the airscrew engine includes engine body and is regularly installed in the bottom surface of engine body
On engine base, two second spiral arms are both formed on the bottom surface of engine base, and the engine base
Also be symmetrically provided with bottom surface two for clamp the second linking swing arm head end and be connected the head end phase axle of swing arm with second
The second axillare even, two second axillares are triangular in shape centered on the axis of engine body with two the second spiral arms
Distribution, the propeller is set on the output shaft of engine body.
Second technical scheme that the utility model is used for：
A kind of VTOL fixed-wing unmanned plane, it includes fuselage and is fixed on fuselage and relative to the length side of fuselage
To two wings being symmetric, Vertical Dynamic propeller, the tail end dress of the fuselage are equiped with each described wing
It is provided with an above-mentioned a kind of propeller twin shaft vector servo deviator；
The Vertical Dynamic propeller is including being fixed on the overarm of the front of wing along Z-direction, being installed in overarm
The fixed seat of front end, the lift motor along Y direction seat in the fixed seat and it is installed on the output shaft of lift motor simultaneously
With the elevating screw that the central shaft of lift motor rotates as rotating shaft in X-Z axial planes.
As a result of such scheme, the utility model is using fixed steering wheel, rotation steering wheel, airscrew engine and spiral
Driving and structural relation between oar, can form the universal driving effect of twin shaft, finally to enable the rotary state of propeller
Carried out in multiple directions and plane, hovered for the high-altitude for realizing aircraft, level is pushed, the steering of various angles etc. is provided
Condition, effectively expands the scope of unmanned plane deflecting, for the conversion of the flight attitude of unmanned plane provides sound assurance；Its
Simple and compact for structure, control accuracy and stability is high, flexibility strong, with very strong actual application value and marketing valency
Value.Meanwhile, the fixed-wing unmanned plane formed by deviator then can not only realize VTOL, hovering, flight appearance
The functions such as state adjustment, and by the conversion and control to deviator and Vertical Dynamic propeller, can effectively save unmanned plane
Energy loss, to extend the cruising time of unmanned plane and reducing its mission payload and provide advantage.
Brief description of the drawings
Fig. 1 is the deviator structural representation in the mounted state of the utility model embodiment；
Fig. 2 is the Standard schematic diagram of the deviator of the utility model embodiment；
Fig. 3 is the structural decomposition diagram () of the deviator of the utility model embodiment；
Fig. 4 is the structural decomposition diagram (two) of the deviator of the utility model embodiment；
Fig. 5 is the structural decomposition diagram (three) of the deviator of the utility model embodiment；
Fig. 6 is the structural decomposition diagram (four) of the deviator of the utility model embodiment；
Fig. 7 is the dimensional structure diagram of the fixed-wing unmanned plane of the utility model embodiment；
Fig. 8 is the planar structure schematic diagram of the fixed-wing unmanned plane of the utility model embodiment.
Specific embodiment
Embodiment of the present utility model is described in detail below in conjunction with accompanying drawing, but the utility model can be by right
It is required that the multitude of different ways for limiting and covering is implemented.
As shown in Figures 1 to 6, a kind of propeller twin shaft vector servo deviator that the present embodiment is provided, it includes solid
Surely the fixed steering wheel a that is installed on the tail end of unmanned plane (such as on the tail end end face of unmanned plane), axle are connected on fixed steering wheel a
Airscrew engine c and be set on the output shaft of airscrew engine c that rotation steering wheel b, axle are connected on rotation steering wheel b
Propeller d；Wherein, fixed steering wheel a drives rotation steering wheel b to rotate fortune up and down in Y-Z axial planes relative to fixed steering wheel a
Dynamic, rotating steering wheel b can then drive airscrew engine c to make left-right rotation in upper X-Y axial planes relative to steering wheel b is rotated
(can be understood as：X-Y axial planes mentioned in this are a relative planes, i.e., when rotate steering wheel b and fixed steering wheel a it
Between when not producing relative rotation, now rotate the X-Y axles that steering wheel b drives an airscrew engine c actions tangible standard just
In plane, and when rotate relatively rotated between steering wheel b and fixed steering wheel a when, then X-Y axles now are one relative flat
Face), airscrew engine c drives propeller d to be rotated by axis of the central shaft of airscrew engine c.
In this way, driving airscrew engine to rotating the rotation driving effect of steering wheel b, rotating steering wheel b using fixed steering wheel a
C synchronizes the effect of rotation and rotates steering wheel b directly to the driving effect of airscrew engine c, forms twin shaft universal
Effect is driven, i.e.,：The rotary state of propeller d can finally be enable to be carried out in multiple directions and plane；Such as implement by this
After the device of example is installed on such as fixed-wing unmanned plane, by coordinating the propeller of other forms and by propeller d's
Course changing control, realizes high-altitude hovering, level push, steering of various angles of aircraft etc., effectively expands unmanned plane change
To scope, for the conversion of the flight attitude of unmanned plane provides sound assurance.
It is driving effects of the fixed steering wheel a of enhancing to rotation steering wheel b, the fixed steering wheel a of the present embodiment is including regularly filling
The first base of steering gear 10 on the tail end of unmanned plane and the first vector horse being regularly installed on the first base of steering gear 10
Up to 11；Wherein, the output shaft of the first vector motor 11 is in the state arranged along X-direction on the first base of steering gear 10, and the
The center line of the output shaft of one vector motor 11 is located in the central region of the first base of steering gear 10；Meanwhile, rotating steering wheel b's
Two the first spiral arms 20 are symmetrically provided with bottom surface and along X-direction, the equal axle in end of two the first spiral arms 20 is connected in first
In the lower area of base of steering gear 10 and respectively positioned at the left side and right side of the first vector motor 11, in the defeated of the first vector motor 11
The first active swing arm 12 is socketed with shaft, the first linking swing arm 21 is connected with the central region axle for rotating steering wheel b, first actively
The end phase axle that the head end of swing arm 12 is connected swing arm 21 with first connects；So as to using moving that the first vector motor 11 is provided
Power driven by the first active swing arm 12 and the first linking swing arm 21 rotate steering wheel b can be with two ends of the first spiral arm 20
Between connecting line make from top to bottom or from the bottom to top relative to the first base of steering gear 10 in Y-Z axial planes for rotation axis
Rotary motion is (i.e.：Equivalent to enabling rotation steering wheel b to be opened as axle and with certain angle fixing the lower edge of steering wheel a or
Closing motion).Using said structure and by the specific size Control to associated components, can enable rotation steering wheel b relative to
Fixed steering wheel a is rotated in the range of 90 degree, such as when the axis for rotating steering wheel b coincides with the axis of fixed steering wheel a
When relatively closed (both), propeller d can make left-right rotation at any angle in X-Y axial planes；When rotation steering wheel b's
When axis is perpendicular with the axis of fixed steering wheel a (when both relative unlatchings are to maximum angle), propeller d then can be in X-
Make left-right rotation at any angle in Z axis plane；Meanwhile, power is provided using vector motor, or rotate steering wheel b motions
Accuracy, stability and flexibility system control basis is provided.
To optimize the structure of whole fixed steering wheel a to greatest extent, structure matching reasonably is carried out to relevant components part,
It is the structure of " u "-shaped, the first vector motor 11 that first base of steering gear 10 of the present embodiment is used along the cross sectional shape of X-direction
Regularly it is installed on the base plate of the first base of steering gear 10, two the first spiral arms 20 be located at the first base of steering gear 10 two are relative
Between side plate and each first spiral arm 20 is connected by the side plate of a pivotal axis and corresponding first base of steering gear 10.With this,
Using the U-shape structure form of the first base of steering gear 10, while enough installing spaces are provided for the first vector motor 11, make
It can be that axle is smoothly rotated relative to fixed steering wheel a with the first spiral arm 20 that steering wheel b must be rotated.
Occurs the problem for slipping when driving rotation steering wheel b to be rotated to avoid the first vector motor 11, it is ensured that whole
The accuracy of device action, ring is all on the set hole inwall of the first active swing arm 12 and is equably provided with some anti-skid racks
(not shown), to be strengthened using anti-skid rack between the first active swing arm 12 and the output shaft of the first vector motor 11
Frictional force.
There is unnecessary swing during by the first linking swing arm 21 to avoid the first active swing arm 12, the
The head end of one active swing arm 12 is formed with two the first axillare e of Relative distribution, and the end of the first linking swing arm 21 is held on two
It is connected with the first axillare e between individual first axillare e and by a connecting shaft.
To optimize the structure of whole device to greatest extent, the rotation steering wheel b of the present embodiment includes the second base of steering gear 22
The second vector motor 23 on the bottom surface of the second base of steering gear 22 is regularly installed in, two the first spiral arms 20 are by the second steering wheel
Make extension aftershaping, the output of the second vector motor 23 towards the direction of the first base of steering gear 10 in the left and right sides of the bottom surface of pedestal 22
Axle arranges on the second base of steering gear 22 along Y direction, at the same the second base of steering gear 23 lower area and open along X-direction
A positive stop strip mouthful f is provided with, the output shaft of the second vector motor 23 is located in the central region of positive stop strip mouthful f；In engine-propeller
Two the second spiral arms 30 are symmetrically provided with the bottom surface of machine c and positioned at the both sides up and down of positive stop strip mouthful f, in the second base of steering gear
On the 22 top surface and position corresponding with each the second spiral arm 30 is each formed with one with the phase axle of corresponding second spiral arm 30 company
Support arm 24, is socketed with the second active swing arm 25, the eccentric region of airscrew engine c on the output shaft of the second vector motor 23
Axle is connected with the second linking swing arm 31, and the end phase axle that the head end of the second active swing arm 25 is connected swing arm 31 with second connects；With this, can
The power provided using the second vector motor 23 drives propeller by the second active swing arm 25 and the second linking swing arm 31
Engine c with the connecting line between two ends of the second spiral arm 30 as rotation axis in X-Y plane relative to the second steering wheel
Pedestal 22 makees rotary motion from left to right or from right to left (i.e.：Equivalent to when airscrew engine c can be rotating steering wheel c
The axis of Y direction be axle and make left-handed rotation or dextrad rotary motion at a certain angle)；When fixed steering wheel a and rotation
When there is not relative motion between steering wheel b, the left and right of whole device is capable of achieving to deflecting effect, in fixed steering wheel a and rotation rudder
When relative motion occurs in machine b, the superposition of deflecting effect can be also realized, so as to provide bar for the multi-direction deflecting of device is promoted
Part, advantageously ensures the functions such as lifting, hovering and the deflecting of unmanned plane.
Based on above-mentioned same principle, ring is all on the set hole inwall of the second active swing arm 25 of the present embodiment and equably sets
It is equipped with some anti-skid rack (not shown)s.Meanwhile, it is formed with two Relative distributions in the head end of the second active swing arm 25
The second axillare g, the end of the second linking swing arm 31 is held between two the second axillare g and by a connecting shaft and the second axle
Plate g is connected.
In addition, the airscrew engine c of the present embodiment includes engine body 32 and is regularly installed in engine sheet
Engine base 33 on the bottom surface of body 32, two the second spiral arms 30 are both formed on the bottom surface of engine base 33, and are started
Also be symmetrically provided with the bottom surface of machine pedestal 33 two for clamp second linking swing arm 31 head end and be connected pendulum with second
The second axillare h, two the second axillare h and two the second spiral arms 30 of the head end phase axle company of arm 31 are with the axis of engine body 32
Distribution triangular in shape centered on line, propeller d is then set on the output shaft of engine body 32.
Based on the structure of above-mentioned deviator, the utility model embodiment additionally provide a kind of VTOL fixed-wing without
Man-machine, as shown in Figure 7 and Figure 8 and in combination with Fig. 1 to Fig. 6, it includes fuselage k and is fixed on fuselage k and relative to fuselage k
Length direction (i.e.：Z-direction) two wing m being symmetric, it is equiped with Vertical Dynamic spiral on each wing m
Oar, an above-mentioned a kind of propeller twin shaft vector servo deviator is then equiped with the tail end of fuselage k；Wherein, Vertical Dynamic
Propeller include along Z-direction be fixed on wing m front overarm 40, be installed in overarm 40 front end fixed seat 41,
(its output shaft can be using the shape being arranged upwards along Y direction for lift motor 42 along Y direction seat in fixed seat 41
Formula, also can be in the form of being arranged downwards along Y direction) and be installed on the output shaft of lift motor 42 and with lift
The central shaft of motor 42 is the elevating screw 43 that rotating shaft rotates in X-Z axial planes.Thus, using Vertical Dynamic
The power (i.e. Y direction) of the vertical direction that propeller is provided realizes the landing of unmanned plane, without being fixed-wing unmanned plane
Special runway is set so that it can carry out landing in any Environment space, and deflecting can be closed in the process
Device；When in aircraft in the air flight course, using the multidirectional thrust produced by aerostatic buoyancy and deviator, can protecting
Holding aircraft has enough horizontal flight power, and realizes the steering of aircraft and the conversion of flight attitude etc., in this process
In can close Vertical Dynamic propeller；And unmanned plane can then start Vertical Dynamic propeller when hovering in the air and close deflecting dress
Put.Based on this, the functions such as VTOL, hovering and the flight attitude adjustment of fixed-wing unmanned plane can be not only realized；And
And control is opened and closed by being converted to Vertical Dynamic propeller and deviator, and the energy loss of unmanned plane has been effectively saved, have
Beneficial to the cruising time of extension unmanned plane, and reduce the mission payload of unmanned plane.
Preferred embodiment of the present utility model is the foregoing is only, the scope of the claims of the present utility model is not thereby limited,
Equivalent structure or equivalent flow conversion that every utilization the utility model specification and accompanying drawing content are made, or directly or indirectly fortune
Used in other related technical fields, similarly it is included in scope of patent protection of the present utility model.
Claims (10)
1. a kind of propeller twin shaft vector servo deviator, it is characterised in that：It includes regularly being installed in the tail of unmanned plane
Rotation steering wheel that fixed steering wheel on end, axle are connected on fixed steering wheel, axle be connected in the airscrew engine that rotates on steering wheel and
It is set in the propeller on the output shaft of airscrew engine；The fixed servo driving rotates steering wheel and exists relative to fixed steering wheel
Make upper and lower rotary motion in Y-Z axial planes, the rotation servo driving airscrew engine is relative to rotation steering wheel in upper X-Y axles
Make left-right rotation in plane, the airscrew engine drives propeller with the central shaft of airscrew engine as axis
Rotate.
2. a kind of propeller twin shaft vector servo deviator as claimed in claim 1, it is characterised in that：The fixed steering wheel
It is installed in including the first base of steering gear being regularly installed on the tail end of unmanned plane and regularly on the first base of steering gear
One vector motor, the output shaft of the first vector motor arranges along X-direction, and the output shaft of the first vector motor center
Line is located in the central region of the first base of steering gear；
Two the first spiral arms, two first spiral arms are symmetrically provided with the bottom surface for rotating steering wheel and along X-direction
The equal axle in end be connected in the first base of steering gear lower area and respectively positioned at the left side and right side of the first vector motor, described the
The first active swing arm is socketed with the output shaft of one vector motor, the central region axle of the rotation steering wheel is connected with the first linking pendulum
Arm, the end phase axle that the head end of the first active swing arm is connected swing arm with first connects；
The first vector motor rotates steering wheel with two the first spiral arms by the first active swing arm and the first linking swing arm driving
End between connecting line for rotation axis in Y-Z axial planes relative to the first base of steering gear make from top to bottom or by it is lower extremely
On rotary motion.
3. a kind of propeller twin shaft vector servo deviator as claimed in claim 2, it is characterised in that：First steering wheel
Pedestal is " u "-shaped along the cross sectional shape of X-direction, and the first vector motor is regularly installed in the base plate of the first base of steering gear
On, two first spiral arms are located between two relative side plates of the first base of steering gear and each described first spiral arm passes through
One pivotal axis is connected with the side plate of corresponding first base of steering gear.
4. a kind of propeller twin shaft vector servo deviator as claimed in claim 3, it is characterised in that：Described first actively
Ring is all on the set hole inwall of swing arm and is equably provided with some anti-skid racks.
5. a kind of propeller twin shaft vector servo deviator as claimed in claim 2, it is characterised in that：Described first actively
The head end of swing arm is formed with two the first axillares of Relative distribution, and the end of the first linking swing arm is held on two first axles
It is connected with the first axillare between plate and by a connecting shaft.
6. a kind of propeller twin shaft vector servo deviator as claimed in claim 2, it is characterised in that：The rotation steering wheel
Including the second base of steering gear and the second vector motor being regularly installed on the bottom surface of the second base of steering gear, two described first
Spiral arm makees extension aftershaping, second arrow by the left and right sides of the bottom surface of the second base of steering gear towards the direction of the first base of steering gear
The output shaft for measuring motor arranges along Y direction, the lower area of second base of steering gear and to offer along X-direction spacing
Bar mouthful, the output shaft of the second vector motor is located in the central region of positive stop strip mouthful；
Two the second spiral arms are symmetrically provided with the bottom surface of the airscrew engine and positioned at the both sides up and down of positive stop strip mouthful,
On the top surface of the second base of steering gear and position corresponding with each the second spiral arm is each formed with one with the corresponding second rotation
Arm phase axle support arm even, is socketed with the second active swing arm, the engine-propeller on the output shaft of the second vector motor
The eccentric region axle of machine is connected with the second linking swing arm, and the head end of the second active swing arm is connected the end phase axle of swing arm with second
Even；
The second vector motor is by the second active swing arm and the second linking swing arm driving airscrew engine with two second
Connecting line between the end of spiral arm is that rotation axis is made from left to right or by the right side in X-Y plane relative to the second base of steering gear
To left rotary motion.
7. a kind of propeller twin shaft vector servo deviator as claimed in claim 6, it is characterised in that：Described second actively
Ring is all on the set hole inwall of swing arm and is equably provided with some anti-skid racks.
8. a kind of propeller twin shaft vector servo deviator as claimed in claim 6, it is characterised in that：Described second actively
The head end of swing arm is formed with two the second axillares of Relative distribution, and the end of the second linking swing arm is held on two the second axles
It is connected with the second axillare between plate and by a connecting shaft.
9. a kind of propeller twin shaft vector servo deviator as claimed in claim 6, it is characterised in that：The propeller hair
Motivation includes engine body and the engine base being regularly installed on the bottom surface of engine body, two described second
Spiral arm is both formed on the bottom surface of engine base, and two are also symmetrically provided with the bottom surface of the engine base are used for
Clamping second is connected the head end of swing arm and is connected the second axillare that the head end phase axle of swing arm connects with second, two second axillares
The distribution triangular in shape centered on the axis of engine body with two the second spiral arms, the propeller is set in engine sheet
On the output shaft of body.
10. a kind of VTOL fixed-wing unmanned plane, it includes fuselage and is fixed on fuselage and relative to the length side of fuselage
To two wings being symmetric, it is characterised in that：Vertical Dynamic propeller, the machine are equiped with each described wing
The tail end of body is equiped with an a kind of propeller twin shaft vector servo deviator as claimed in any one of claims 1-9 wherein；
The Vertical Dynamic propeller is including being fixed on the overarm of the front of wing along Z-direction, being installed in the front end of overarm
Fixed seat, the lift motor along Y direction seat in the fixed seat and be installed on the output shaft of lift motor and to rise
The elevating screw that the central shaft of motor rotates for rotating shaft in X-Z axial planes drops.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621305940.2U CN206202663U (en) | 2016-11-30 | 2016-11-30 | A kind of propeller twin shaft vector servo deviator and VTOL fixed-wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621305940.2U CN206202663U (en) | 2016-11-30 | 2016-11-30 | A kind of propeller twin shaft vector servo deviator and VTOL fixed-wing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206202663U true CN206202663U (en) | 2017-05-31 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621305940.2U Withdrawn - After Issue CN206202663U (en) | 2016-11-30 | 2016-11-30 | A kind of propeller twin shaft vector servo deviator and VTOL fixed-wing unmanned plane |
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| Country | Link |
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| CN (1) | CN206202663U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428527A (en) * | 2016-11-30 | 2017-02-22 | 深圳市优鹰科技有限公司 | Dual-axis vector servo turning device with propeller and vertical take-off and landing unmanned aerial vehicle with fixed wings |
| CN109334947A (en) * | 2018-11-06 | 2019-02-15 | 西北农林科技大学 | A kind of helium balloon unmanned plane and its working method |
| CN111003172A (en) * | 2018-10-08 | 2020-04-14 | 苏郁夫 | Jet type vertical lifting pneumatic system |
-
2016
- 2016-11-30 CN CN201621305940.2U patent/CN206202663U/en not_active Withdrawn - After Issue
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428527A (en) * | 2016-11-30 | 2017-02-22 | 深圳市优鹰科技有限公司 | Dual-axis vector servo turning device with propeller and vertical take-off and landing unmanned aerial vehicle with fixed wings |
| WO2018098993A1 (en) * | 2016-11-30 | 2018-06-07 | 深圳市优鹰科技有限公司 | Dual-axis vector servo steering device for propeller and vertical take-off and landing of unmanned aerial vehicle with fixed wings |
| CN111003172A (en) * | 2018-10-08 | 2020-04-14 | 苏郁夫 | Jet type vertical lifting pneumatic system |
| CN111003172B (en) * | 2018-10-08 | 2021-07-27 | 苏郁夫 | Jet type vertical lifting pneumatic system |
| CN109334947A (en) * | 2018-11-06 | 2019-02-15 | 西北农林科技大学 | A kind of helium balloon unmanned plane and its working method |
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