CN208102306U - A kind of dynamic trapezoidal VTOL equipment of circle of oil - Google Patents
A kind of dynamic trapezoidal VTOL equipment of circle of oil Download PDFInfo
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- CN208102306U CN208102306U CN201820057882.9U CN201820057882U CN208102306U CN 208102306 U CN208102306 U CN 208102306U CN 201820057882 U CN201820057882 U CN 201820057882U CN 208102306 U CN208102306 U CN 208102306U
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Abstract
The utility model provides a kind of dynamic trapezoidal VTOL equipment of circle of oil, including body, electricity generation system, self-starting system, dynamical system, flight control system, kinetic control system, undercarriage.Body is the circle trapezoidal shape of all round closure, and bottomless no top, the upper body of body, lower body are all made of carbon fibre composite；Electricity generation system includes generator, rectifier；Self-starting system includes starting motor, starter receiver, electronic switch；Dynamical system includes petrol engine, propeller；Flight control system is mounted on body position of centre of gravity；Kinetic control system includes the first moving cell, the second moving cell, third moving cell, the 4th moving cell；Undercarriage is carbon fibre material, is mounted on body lower body.The utility model VTOL equipment can complete narrow space, and the industrial application in complex environment, cruise duration is long, highly-safe.
Description
Technical field
The utility model relates to flight machinery fields, the in particular to dynamic trapezoidal VTOL equipment of circle of oil.
Background technique
Conventional flight equipment（Fixed-wing, more rotors, helicopter）Due to the restriction of aerodynamic arrangement, it is unable to complete some spaces
It is narrow, the industrial application in complex environment.Most of flight equipment currently on the market is all made of lithium battery as power source, by
Energy density limitation causes cruise duration shorter, and average flight 15-30 minutes.Most of flight equipment is during take-off and landing to race simultaneously
Road is more demanding, it is difficult to realize VTOL；And because blade is exposed, safety is poor, and equipment is easily damaged, and leads to making for equipment
It is greatly shortened with the service life.
Summary of the invention
The purpose of the utility model is to overcome above-mentioned prior art Shortcomings, provide a kind of the dynamic circle of oil trapezoidal vertical
Equipment drops, and cruise duration is long, security performance is high, suitable for executing task under complex environment.
What the purpose of this utility model was realized in：
A kind of dynamic trapezoidal VTOL equipment of circle of oil, including body, flight control system, dynamical system, motion control system
System, self-starting system, electricity generation system, undercarriage.
The body includes upper body, lower body；The flight control system is mounted on body position of centre of gravity, including flight control
Device and inertial navigation measuring unit；The dynamical system includes petrol engine, propeller；The kinetic control system includes
First moving cell, the second moving cell, third moving cell, the 4th moving cell；The self-starting system includes starting electricity
Machine, starter receiver, electronic switch；The electricity generation system includes generator, rectifier；The undercarriage is carbon fibre material, peace
Mounted in body lower body, resilient cushion is mounted on undercarriage bottom.
The turbulent flow of blade tip is eliminated in circle trapezoidal shape of the body for all round closure, bottomless no top, this configuration design,
Stability and efficiency are improved, 15% or so lift is increased, the upper body of the body, lower body are all made of carbon fiber composite
Material.
The flight control system and first moving cell of kinetic control system, the second moving cell, third move
Unit, the 4th moving cell are all connected with；
The inertial navigation measuring unit includes three axis accelerometer, three-axis gyroscope, three axle magnetometer, barometer, GPS
Module is installed in internal body, and flight attitude and position can be monitored in real time.
The petrol engine is mounted on internal body；The propeller is two leaf spacing paddles, is directly driven by engine.
First moving cell is connect with the first rudder beam of the body；
Second moving cell is connect with the second rudder beam of the body；
The third moving cell is connect with the third rudder beam of the body；
4th moving cell is connect with the 4th rudder beam of the body, wherein first moving cell and third fortune
Moving cell is located at the machine main body symmetric position, and the second moving cell and the 4th moving cell are located at the symmetrical position of machine main body
It sets.
The starting motor is connected with starter receiver, electronic switch, and the electronic switch is connect with flight control system.
The generator connects rectifier, is that body and device battery charge after the rectifier rectification pressure stabilizing.
First moving cell is provided with the first rudder piece and drives the first steering engine of the first rudder piece rotation,
Second moving cell is provided with the second rudder piece and drives the second steering engine of the second rudder piece rotation,
The third moving cell is provided with third rudder piece and drives the third steering engine of third rudder piece rotation,
4th moving cell is provided with the 4th rudder piece and drives the 4th steering engine of the 4th rudder piece rotation.
Flight control system controls the first moving cell steering engine, the second moving cell steering engine, the by kinetic control system
The rotation of three moving cell steering engines, the 4th moving cell steering engine, to control corresponding first moving cell rudder piece, the second movement
The rotation of unit rudder piece, third moving cell rudder piece, the 4th moving cell rudder piece, and then flight attitude is controlled, rudder piece
Rotational angle is -45o~45o。
Three smooth gondolas of addition can be selected as needed（Laser range finder, infrared imaging, it is seen that light）, task module and rescue
It helps, explore, spraying, the industrial applications module such as forestry.
Compared with prior art, the utility model has the beneficial effects that：
1, since special aerodynamic arrangement designs, narrow space, the industrial application in complex environment can be completed.
2, completely new aerodynamic arrangement's shape, improves stability and efficiency, increases 15% or so lift.
3, complete machine 95% is carbon-fiber composite material, and structural strength is big, itself take-off weight is small.
4, cruise duration is long, can be flight 1-2 hours according to task needs.
5, the larger raising of safety, while with good stability and maneuverability.
6, very low to ground requirement due to VTOL, flexibly, controllability is very high for movement.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment
Needed in attached drawing be briefly described, it should be apparent that, the accompanying drawings in the following description is only of the invention some
Example for those of ordinary skill in the art without creative efforts, can also be according to these attached drawings
Obtain other attached drawings.
Fig. 1 is the dynamic trapezoidal VTOL device structure schematic diagram of circle of the utility model oil.
Fig. 2 is the utility model embodiment kinetic control system structural schematic diagram.
Fig. 3 is the utility model embodiment self-starting system structural schematic diagram.
Fig. 4 is the utility model embodiment power generation system structure schematic diagram.
Fig. 5 is the utility model embodiment flight control system and kinetic control system structural schematic diagram.
Appended drawing reference is in figure：10 bodies, 101 be the first rudder beam, 102 be the second rudder beam, 103 be third rudder beam, 104
It is upper body for the 4th rudder beam, 11,12 be lower body, and 13 be undercarriage, and 131 be resilient cushion, and 20 be flight control system, and 201 be winged
Line control unit, 202 be inertial navigation measuring unit, and 30 be dynamical system, and 301 be petrol engine, and 302 be propeller, and 40 are
Kinetic control system, 41 be the first moving cell, and 42 be the second moving cell, and 43 be third moving cell, and 44 be the 4th movement
Unit, 411 be the first steering engine, and 412 be the first rudder piece, and 421 be the second steering engine, and 422 be the second rudder piece, and 431 be third steering engine,
432 be third rudder piece, and 441 be the 4th steering engine, and 442 be the 4th rudder piece, and 50 be self-starting system, and 501 be electronic switch, and 502 are
Start motor, 503 be starter receiver, and 60 be electricity generation system, and 601 be generator, and 602 be rectifier, and 603 be battery.
Specific embodiment
Below in conjunction with the attached drawing in the example of the utility model, the technical scheme in the embodiment of the utility model is carried out clear
Chu is fully described by.
Obviously, the described embodiments are only a part of the embodiments of the utility model, instead of all the embodiments.Base
In the embodiments of the present invention, those of ordinary skill in the art's every other embodiment obtained is belonged to practical new
The range of type protection.
Term " first " used in the disclosure " second " etc. is that do not have to distinguish an element and another element
Succession and importance.
A kind of dynamic trapezoidal VTOL equipment of circle of oil of the embodiments of the present invention flies as shown in Figure 1, including body 10
Row control system 20, dynamical system 30, kinetic control system 40, self-starting system 50, electricity generation system 60, undercarriage 13.
Body 10 is the circle trapezoidal shape of all round closure, bottomless no top.The turbulent flow of blade tip is eliminated in this configuration design, is improved
Stability and efficiency, increase 15% or so lift.
Body includes upper body 11, lower body 12, is all made of carbon fibre composite, and structural strength is big.
Petrol engine 301 is mounted on internal body in dynamical system 30, provides power source for VTOL equipment.
Propeller 302 is two leaf spacing paddles, is directly driven by petrol engine 301.
Undercarriage 13 is mounted on body lower body 12, and undercarriage 13 uses carbon fibre material, and resilient cushion 131 is mounted on undercarriage
13 bottoms.
As shown in Fig. 2, in the utility model embodiment, 40 first moving cell 41 of kinetic control system and the first rudder of body
Beam 101 connects, and the second moving cell 42 is connect with the second rudder of body beam 102, third moving cell 43 and body third rudder beam 103
Connection, the 4th moving cell 44 are connect with the 4th rudder beam 104 of body, wherein first moving cell 41 and third moving cell
43 are located at the 10 main body symmetric position of body, and it is main that second moving cell 42 and the 4th moving cell 44 are located at body 10
Body symmetric position.
As shown in figure 3, being equipped with self-starting system 50, starting in the utility model embodiment in the utility model embodiment
Motor 502 is connected with starter receiver 503, electronic switch 501, and the electronic switch 501 is connect with flight control system 20.It rises
When flying, flight control system 20 controls electronic switch 501, and then controls starting motor 502 and rotate, and passes through 503 band of starter receiver
Dynamic petrol engine 301 starts.
As shown in figure 4,60 generator 601 of electricity generation system connects rectifier 602, rectified in the utility model embodiment
It is that body and device battery 603 charge after 602 rectifying and voltage-stabilizing of device.
In the utility model embodiment, flight control system 20 can stabilized flight posture, be mounted on 10 center of gravity position of body
It sets, is all connected with first moving cell 41, the second moving cell 42, third moving cell 43, the 4th moving cell 44；
As shown in figure 5, the first moving cell 41 is provided with the first steering engine 411 and the first rudder piece 412；
Second moving cell 42 is provided with the second steering engine 421 and the second rudder piece 422；
Third moving cell 43 is provided with third steering engine 431 and third rudder piece 432；
4th moving cell 44 is provided with the 4th steering engine 441 and the 4th rudder piece 442.
Inertial navigation measuring unit 202 includes three axis accelerometer, three-axis gyroscope, three axle magnetometer, barometer, GPS
Module is installed in inside body 10, and flight attitude and position can be monitored in real time.
In the utility model embodiment, flight control system 20 passes through control 40 first moving cell 41 of kinetic control system
First steering engine 411,42 second steering engine 421 of the second moving cell, 43 third steering engine 431 of third moving cell, the 4th moving cell
The rotation of 44 the 4th steering engines 441, to control corresponding the first rudder of first moving cell piece 412, second the second rudder of moving cell
The rotation of piece 422, third moving cell third rudder piece 432, the 4th rudder piece 442 of the 4th moving cell.
First rudder piece 412, the second rudder piece 422, third rudder piece 432,442 rotational angle of the 4th rudder piece are -45 degree ~ 45
Degree.
In the utility model embodiment, by the control of control and rudder piece angle, speed to engine output,
To realize the gesture stability to equipment rolling, pitching, yaw, hovering and flight.
Vertical displacement movement in this example is realized by adjusting petrol engine 301 revolving speed.
In the utility model embodiment, when equipment is taken off, is taken off first by control instruction control, pass through calculating
Roll angle, pitch angle, the numerical value of yaw angle, flight control system 20 control the control signal of steering engine, and steering engine drives rudder
Piece rotation, makes body keep statokinetic.
According to task needs, three smooth gondolas of addition can be selected in equipment（Laser range finder, infrared imaging, it is seen that
Light）, the industrial applications module such as task module and rescue, exploration, spraying, forestry provides solution for industrial application.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for
For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this
In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter
From the point of view of which point, embodiment should all be regarded as exemplary, and be non-limiting, the scope of the utility model is by appended
Claim rather than above description limit, it is intended that the institute that will be fallen within the meaning and scope of the equivalent elements of the claims
It changes and is embraced therein.
Claims (10)
1. a kind of dynamic trapezoidal VTOL equipment of circle of oil, it is characterised in that：Including body, flight control system, dynamical system, fortune
Autocontrol system, self-starting system, electricity generation system, undercarriage；The body includes upper body, lower body；The flight control system
It is mounted on body position of centre of gravity, including flight controller and inertial navigation measuring unit；The dynamical system includes gasoline hair
Motivation, propeller；The kinetic control system includes the first moving cell, the second moving cell, third moving cell, the 4th fortune
Moving cell；The self-starting system includes starting motor, starter receiver, electronic switch；The electricity generation system includes generator, whole
Flow device；The undercarriage is carbon fibre material, is mounted on body lower body, resilient cushion is mounted on undercarriage bottom.
2. the dynamic trapezoidal VTOL equipment of circle of a kind of oil according to claim 1, it is characterised in that：
The body is the circle trapezoidal shape of all round closure, and bottomless no top, the upper body of the body, lower body are all made of carbon fiber
Composite material.
3. the dynamic trapezoidal VTOL equipment of circle of a kind of oil according to claim 1, it is characterised in that：
The flight control system and first moving cell of kinetic control system, the second moving cell, third moving cell,
4th moving cell is all connected with；The inertial navigation measuring unit includes three axis accelerometer, three-axis gyroscope, three axis magnetic force
Meter, barometer, GPS module, are installed in internal body, and flight attitude and position can be monitored in real time.
4. the dynamic trapezoidal VTOL equipment of circle of a kind of oil according to claim 1, it is characterised in that：
The petrol engine is mounted on internal body；The propeller is two leaf spacing paddles, is directly driven by engine.
5. the dynamic trapezoidal VTOL equipment of circle of a kind of oil according to claim 1, it is characterised in that：
First moving cell is connect with the first rudder beam of the body；
Second moving cell is connect with the second rudder beam of the body；
The third moving cell is connect with the third rudder beam of the body；
4th moving cell is connect with the 4th rudder beam of the body；Wherein first moving cell and third movement are single
Member is located at the main body symmetric position of the body, and the main body that second moving cell and the 4th moving cell are located at body is symmetrical
Position.
6. the dynamic trapezoidal VTOL equipment of circle of a kind of oil according to claim 1, it is characterised in that：
The starting motor is connected with starter receiver, electronic switch, and the electronic switch is connect with flight control system.
7. the dynamic trapezoidal VTOL equipment of circle of a kind of oil according to claim 1, it is characterised in that：
The generator connects rectifier, is that body and device battery charge after rectified device rectifying and voltage-stabilizing.
8. a kind of dynamic trapezoidal VTOL equipment of circle of oil described according to claim 1 or 3 or 5, it is characterised in that：
First moving cell is provided with the first rudder piece and drives the first steering engine of the first rudder piece rotation,
Second moving cell is provided with the second rudder piece and drives the second steering engine of the second rudder piece rotation,
The third moving cell is provided with third rudder piece and drives the third steering engine of third rudder piece rotation,
4th moving cell is provided with the 4th rudder piece and drives the 4th steering engine of the 4th rudder piece rotation.
9. the dynamic trapezoidal VTOL equipment of circle of a kind of oil according to claim 1 or 3, it is characterised in that：
Flight control system controls the first moving cell steering engine, the second moving cell steering engine, third by kinetic control system and transports
The rotation of moving cell steering engine, the 4th moving cell steering engine, to control corresponding first moving cell rudder piece, the second moving cell
The rotation of rudder piece, third moving cell rudder piece, the 4th moving cell rudder piece, and then flight attitude is controlled, the rotation of rudder piece
Angle is -45 °~45 °.
10. the dynamic trapezoidal VTOL equipment of circle of a kind of oil according to claim 1-7, it is characterised in that：
Three smooth gondolas of addition, task module and rescue, exploration, spraying, forestry industry application module can be selected as needed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820057882.9U CN208102306U (en) | 2018-01-16 | 2018-01-16 | A kind of dynamic trapezoidal VTOL equipment of circle of oil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820057882.9U CN208102306U (en) | 2018-01-16 | 2018-01-16 | A kind of dynamic trapezoidal VTOL equipment of circle of oil |
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| Publication Number | Publication Date |
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| CN208102306U true CN208102306U (en) | 2018-11-16 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108128438A (en) * | 2018-01-16 | 2018-06-08 | 沈阳朗峰科技有限公司 | A kind of dynamic trapezoidal VTOL equipment of circle of oil |
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2018
- 2018-01-16 CN CN201820057882.9U patent/CN208102306U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108128438A (en) * | 2018-01-16 | 2018-06-08 | 沈阳朗峰科技有限公司 | A kind of dynamic trapezoidal VTOL equipment of circle of oil |
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