CN107953990A - VTOL flight instruments and fixed-wing unmanned plane - Google Patents
VTOL flight instruments and fixed-wing unmanned plane Download PDFInfo
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- CN107953990A CN107953990A CN201711418211.7A CN201711418211A CN107953990A CN 107953990 A CN107953990 A CN 107953990A CN 201711418211 A CN201711418211 A CN 201711418211A CN 107953990 A CN107953990 A CN 107953990A
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- flight instruments
- vtol flight
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- wing
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- 230000007246 mechanism Effects 0.000 claims abstract description 102
- 230000005611 electricity Effects 0.000 claims description 6
- 230000005540 biological transmission Effects 0.000 claims description 4
- 230000008878 coupling Effects 0.000 claims 1
- 238000010168 coupling process Methods 0.000 claims 1
- 238000005859 coupling reaction Methods 0.000 claims 1
- 230000005484 gravity Effects 0.000 description 4
- 238000007726 management method Methods 0.000 description 4
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 3
- 239000002390 adhesive tape Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 229910052744 lithium Inorganic materials 0.000 description 3
- 238000003032 molecular docking Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000001141 propulsive effect Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
Abstract
This application provides a kind of VTOL flight instruments and fixed-wing unmanned plane.The VTOL flight instruments includes the first rotor power mechanism and the second rotor power mechanism at horn and the both ends for being symmetrically disposed on the wing；Control mechanism, power sector and connecting line are provided with the horn, the control mechanism is of coupled connections with the first rotor power mechanism and the second rotor power mechanism, and the power sector is electrically connected with the first rotor power mechanism, the second rotor power mechanism and the control mechanism；One end of the connecting line is connected with the control mechanism telecommunications, and the other end of the connecting line is located at outside the horn and is provided with plug.The VTOL flight instruments is provided with the wing of the fixed-wing unmanned plane.The VTOL flight instruments and unmanned plane of the application, has higher efficiency, and can adapt to variously-shaped and weight the article for being suitable for transport, and easy for assembly, of low cost.
Description
Technical field
This application involves a kind of flight instruments and unmanned plane, particularly a kind of VTOL flight instruments of energy VTOL
And fixed-wing unmanned plane.
Background technology
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, using radio robot and is provided for oneself
The not manned aircraft that presetting apparatus manipulates, or fully or intermittently independently operated by car-mounted computer.Civilian
Unmanned plane in, it is most common to have fixed-wing unmanned plane and multi-rotor unmanned aerial vehicle.
Fixed-wing unmanned plane, one kind that the wing that referring to wing outer end angle of sweep can adjust with speed automatic or manual is fixed
Unmanned plane.
However, fixed-wing unmanned plane is for the more demanding of landing site.When landing site is good, fixed-wing unmanned plane
With very high efficiency.When landing site's condition is slightly insufficient, fixed-wing unmanned plane can not just carry out operation.
And traditional combined type VTOL fixed-wing unmanned plane, in flight course, its VTOL component can become
Bear a heavy burden, and produce resistance, cause the operating efficiency of combined type VTOL fixed-wing unmanned plane to reduce, air mileage has to contract
Short, even under good site condition, its efficiency is still relatively low.
Multi-rotor unmanned aerial vehicle, is a kind of special pilotless helicopter with three and above rotor shaft.It passes through
Motor rotation on each axis, drives rotor, so as to produce a liter thrust.By varying the relative rotation speed between different rotors,
The size of single shaft propulsive force can be changed, so as to control the running orbit of aircraft.
Since multi-rotor unmanned aerial vehicle is limited by own form, so the shape and weight of its article that can be transported at present
Also all it is very restricted.Shape and weight if necessary to the article of transport do not meet used multi-rotor unmanned aerial vehicle, also
Need to redesign and produce the multi-rotor unmanned aerial vehicle that can be used again, it is time-consuming and laborious, and also cost is very high.
The content of the invention
In order to solve the problems, such as current unmanned plane inefficiency and variously-shaped transport article, the application can not be adapted to
Propose a kind of VTOL flight instruments and fixed-wing unmanned plane, there is higher efficiency, and can adapt to it is variously-shaped and
The article for being suitable for transport of weight, and it is easy for assembly, it is of low cost.
Technical solution is used by the application solves its technical problem：A kind of VTOL flight instruments, it includes machine
Arm, the first rotor power mechanism and the second rotor power mechanism, the first rotor power mechanism and second rotor power
Mechanism is symmetrically disposed on the both ends of the horn；Control mechanism, power sector and connecting line are provided with the horn, it is described
Control mechanism is of coupled connections with the first rotor power mechanism and the second rotor power mechanism, the power sector with
The first rotor power mechanism, the second rotor power mechanism and the control mechanism are electrically connected；The connecting line
One end is connected with the control mechanism telecommunications, and the other end of the connecting line is located at outside the horn, and the connecting line is another
One end is provided with plug.
VTOL flight instruments as described above, wherein, the rotation axis of the first rotor power structure and described
The rotation axis of second rotor power structure is straight up.
VTOL flight instruments as described above, wherein, the structure of the first rotor power mechanism and described second
The structure of rotor power mechanism is identical.
VTOL flight instruments as described above, wherein, the first rotor power mechanism includes what is be electrically connected to each other
First brushless electric machine and the first rotor blade, the second rotor power mechanism include the second brushless electric machine for being electrically connected to each other and
Second rotor blade；First brushless electric machine and second brushless electric machine are electrically connected with the power sector.
VTOL flight instruments as described above, wherein, the first rotor power mechanism further includes the first electronics tune
Fast device, one end of first electron speed regulator are electrically connected with first brushless electric machine, first electron speed regulator it is another
One end is electrically connected with the control mechanism；The second rotor power mechanism further includes the second electron speed regulator, second electricity
One end of sub- governor is electrically connected with second brushless electric machine, the other end and the control machine of second electron speed regulator
Structure is electrically connected；The power sector is electrically connected by first electron speed regulator with first brushless electric machine, the power supply
Mechanism is electrically connected by second electron speed regulator with second brushless electric machine.
VTOL flight instruments as described above, wherein, the power sector includes the first power supply and second source, institute
State the first power supply to be electrically connected with first brushless electric machine by first electron speed regulator, the second source passes through described
Second electron speed regulator is electrically connected with second brushless electric machine；First power supply and/or the second source and the control
Mechanism processed is electrically connected.
VTOL flight instruments as described above, wherein, the control mechanism includes control unit, described control unit
Including control chip, gyroscope, accelerometer, barometer, compass and power management subelement, the control chip and the top
Spiral shell instrument, the accelerometer, the barometer, the compass and the power management subelement are of coupled connections, the control
Unit telecommunications is connected with Digital Transmission module and signal receiver.
VTOL flight instruments as described above, wherein, the control mechanism further includes GPS unit, the GPS unit
It is of coupled connections with the control chip.
VTOL flight instruments as described above, wherein, at least two screwed retaining rings are provided with the horn.
The application also proposes a kind of fixed-wing unmanned plane, it includes fuselage, and the side of the fuselage is provided with the first wing,
The opposite side of the fuselage is provided with second wing symmetrical with first wing, first wing and second machine
It is both provided with least one VTOL flight instruments as described above on the wing, the VTOL flight dress on first wing
Put and be symmetrical arranged with the VTOL flight instruments on second wing, the VTOL flight instruments on first wing
Connecting line be connected to each other with the connecting line of the VTOL flight instruments on corresponding second wing, it is multiple described vertical to rise
Center line of the center line each parallel to the fuselage of the horn of flight instruments drops.
The VTOL flight instruments and fixed-wing unmanned plane of the application, by by the first rotor power mechanism and institute
The both ends that the second rotor power mechanism is symmetrically assembled in the horn are stated, control first rotor to move by the control mechanism
Force mechanisms and the second rotor power mechanism, enable the VTOL of VTOL flight instruments and flight.Thus, institute
Stating VTOL flight instruments becomes completely self-contained modular flight part external member, its landing and flight are no longer limited by landing
Whether place is good, and has higher efficiency；The VTOL flight instruments can be loaded into respectively by connector
Kind of shape and weight, suitable on the article to be transported of transport, such as pass through chain, adhesive tape, the VTOL flight
Device can drive the article VTOL and flight to be transported, and assembling is extremely easy；If Item Weight to be transported is larger, can
, will be adjacent by the plug of the connecting line to load multiple VTOL flight instrumentses on an article to be transported
Two horns be connected to each other, can be communicated between two after the docking VTOL flight instruments, so that real
Now common flight, therefore use the VTOL flight instruments of the application, it is not necessary to according to the shape and weight of article to be transported
Unmanned plane is redesigned and produced, cost can be effectively reduced, various specifications heavy weight goods express transportation device can be used as, very
Suitable for carrying out express delivery, it is adapted to commercially be widely applied.
Brief description of the drawings
Fig. 1 is the structure diagram of the VTOL flight instruments of the application.
Description of reference numerals：
1st, horn, 11, connecting line, the 21, first brushless electric machine, the 22, first rotor blade, the 23, first electron speed regulator,
31st, the second brushless electric machine, the 32, second rotor blade, the 33, second electron speed regulator, the 41, first power supply, 42, second electricity
Source, 5, control unit, 6, Digital Transmission module, 7, signal receiver, 8, GPS unit.
Embodiment
In order to which the technical features, objects and effects of the application are more clearly understood, now control illustrates this Shen
Embodiment please.
The explanation of following embodiment is to refer to schema, the specific embodiment implemented to illustrate the present invention can be used to.This
Invent the direction term that is previously mentioned, such as " on ", " under ", "front", "rear", "left", "right", " interior ", " outer ", " side " etc., only
It is the direction with reference to schema.Therefore, the direction term used is to illustrate and understand the present invention, and is not used to limit this hair
It is bright.
As shown in Figure 1, this application provides a kind of VTOL flight instruments, it includes horn 1, the first rotor power machine
Structure and the second rotor power mechanism, the first rotor power mechanism and the second rotor power mechanism are symmetrically disposed on institute
State the both ends of horn 1；Be provided with control mechanism, power sector and connecting line 11 in the horn 1, the control mechanism with it is described
First rotor power mechanism and the second rotor power mechanism are of coupled connections, and the power sector is moved with first rotor
Force mechanisms, the second rotor power mechanism and the control mechanism are electrically connected；One end of the connecting line 11 and the control
Mechanism telecommunications connection processed, the other end of the connecting line 11 is located at outside the horn 1, and the other end of the connecting line 11 is set
There is plug.
The VTOL flight instruments of the application, by by the first rotor power mechanism and second rotor power
Mechanism is symmetrically assembled in the both ends of the horn 1, and the first rotor power mechanism and described is controlled by the control mechanism
Second rotor power mechanism, enables the VTOL of VTOL flight instruments and flight.Thus, the VTOL flies
Luggage is set to as completely self-contained modular flight part external member, and whether its landing and flight are no longer limited by landing site good
It is good, and there is higher efficiency；The VTOL flight instruments can be loaded into by connector variously-shaped and again
Amount, suitable on the article to be transported of transport, such as by chain, adhesive tape, the VTOL flight instruments can band
The article VTOL and flight to be transported are moved, assembling is extremely easy；If Item Weight to be transported is larger, can be treated at one
Multiple VTOL flight instrumentses are loaded on transport article, by the plug of the connecting line 11, by two adjacent institutes
State horn 1 to be connected to each other, can be communicated between two after the docking VTOL flight instruments, flown so as to fulfill common
OK, therefore the VTOL flight instruments of the application is used, it is not necessary to redesign according to the shape of article to be transported and weight
With production unmanned plane, can effectively reduce cost, various specifications heavy weight goods express transportation device can be used as, be highly suitable for into
Row express delivery, is adapted to commercially be widely applied.
The horn 1 can use long straight shape structure, in order to which article to be transported to be fixed on to the VTOL of the application
Flight instruments.Such as express delivery article, generally using box, either chest is packaged and is assembled in box-like or box-like express delivery
It is extremely easy in the straight shape structure of length of the horn 1.The even article of other shapes, the horn 1 with the straight shape structure of length
It is also extremely easy to carry out assembling.Furthermore the flight of the VTOL flight instruments is not only restricted to landing site, have compared with
High efficiency, it is of low cost, therefore the VTOL flight instruments is for carrying article to be transported, particularly carrying express delivery,
It is extremely effectively and convenient.Alternatively, it is also possible to select to set at least two screwed retaining rings (in figure not show on the horn 1
Go out), by the screwed retaining ring, the VTOL flight instruments is with that can set the article to be transported of bolt to be fixedly connected.
Finally, for the ease of the connection between two adjacent VTOL flight instrumentses, the connecting line 11, which can be selected, to be stretched
Contracting connecting line, for example, can folding and unfolding length of cable cable buncher, by multiple VTOL flight instrumentses and article to be transported
When mutually fixed, it just need not be limited to the length of the connecting line 11 and be inconvenient to fix the VTOL flight instruments.
In one preferred embodiment, the rotation axis of the first rotor power structure and second rotor move
The rotation axis of power structure straight up, makes the first rotor power unit and the second rotor power unit have first
There is the function of wing, so as to preferably produce upward power, to drive the horn 1 to take off vertically.
It is possible that the structure of the first rotor power mechanism is identical with the structure of the second rotor power mechanism.
Such as can be that the first rotor power mechanism includes the first brushless electric machine 21 and the first rotor blade being electrically connected to each other
22, the second rotor power mechanism includes the second brushless electric machine 31 and the second rotor blade 32 being electrically connected to each other；Described
One brushless electric machine 21 and second brushless electric machine 31 are electrically connected with the power sector.The VTOL flight instruments
The lift that takes off relies primarily on first brushless electric machine 21 and drives first rotor blade 22 and second brushless electric machine
31 drive second rotor blade 32 to produce, and when taking off, lift is more than the VTOL flight instruments and article to be transported
Gravity when, the VTOL flight instruments drives the article to be transported to rise；When taking off, lift is equal to the VTOL
During the gravity of flight instruments and article to be transported, the VTOL flight instruments drives the article to be transported to hover in the air；
When the lift that takes off is less than the gravity of the VTOL flight instruments and article to be transported, the VTOL flight instruments band
Move the article falling head to be transported.
Specifically, the first rotor power mechanism further includes the first electron speed regulator 23, first electron speed regulator
23 one end is electrically connected with first brushless electric machine 21, the other end and the control mechanism of first electron speed regulator 23
It is electrically connected；The second rotor power mechanism further includes the second electron speed regulator 33, one end of second electron speed regulator 33
It is electrically connected with second brushless electric machine 31, the other end of second electron speed regulator 33 is electrically connected with the control mechanism；
The power sector is electrically connected by first electron speed regulator 23 with first brushless electric machine 21, and the power sector leads to
Second electron speed regulator 33 is crossed to be electrically connected with second brushless electric machine 31.First electron speed regulator 23 and described
The control signal of the control mechanism can be changed into current signal, be respectively used to described in control by two electron speed regulators 33
The rotating speed of the rotating speed of first brushless electric machine 21 and second brushless electric machine 31.Because the electric current of first brushless electric machine 21 and
The electric current of second brushless electric machine 31 is very big, usual first brushless electric machine 21 or second brushless electric machine 31
In normal work, averagely there is the electric current of 3A or so, by setting first electron speed regulator 23 and the second electronics tune
Fast device 33, makes the control mechanism to bear so big electric current, and the control mechanism is conveniently driven
First brushless electric machine 21 and second brushless electric machine 31.Meanwhile first electron speed regulator 23 and second electricity
Sub- governor 33 also acts as the effect of voltage change device in the VTOL flight instruments of the application, by the power sector
Voltage become suitable for power supply to the control mechanism voltage, then supply electricity to the control mechanism.
The power sector mentioned in the VTOL flight instruments of the application, can be to be arranged at the horn 1
One block of interior power supply, such as high performance lithium battery group or the heavy-duty battery that is suitable for the application of.Can also as shown in Figure 1, institute
Stating power sector includes the first power supply 41 and second source 42, first power supply 41 by first electron speed regulator 23 with
First brushless electric machine 21 is electrically connected, and the second source 42 is brushless by second electron speed regulator 33 and described second
Motor 31 is electrically connected；First power supply 41 and/or the second source 42 are electrically connected with the control mechanism.I.e. described control
Mechanism can be only electrically connected with first power supply 41, can also be only electrically connected with the second source 42, or the control
Mechanism is electrically connected with first power supply 41 and the second source 42 at the same time, in order to first power supply 41 and described second
Power supply 42 is powered to first electron speed regulator 23 and second electron speed regulator 33 respectively.Wherein, first power supply
41 can be high performance lithium battery group or the heavy-duty battery being suitable for the application of, and the second source 42 can also be high-performance
Lithium battery group or the heavy-duty battery that is suitable for the application of.First power supply 41 can be selected identical with the second source 42
Battery, different batteries can also be selected.
In embodiment as shown in Figure 1, the control mechanism includes control unit 5, and described control unit 5 is wrapped
Include control chip, gyroscope, accelerometer, barometer, compass and power management subelement, the control chip and the gyro
Instrument, the accelerometer, the barometer, the compass and the power management subelement are of coupled connections, and the control is single
First 5 telecommunications are connected with Digital Transmission module 6 and signal receiver 7.The control mechanism further includes GPS unit 8, and the GPS is mono-
Member 8 is of coupled connections with the control chip.
Present invention also provides a kind of fixed-wing unmanned plane, it includes fuselage, and the side of the fuselage is provided with the first machine
The wing, the opposite side of the fuselage are provided with second wing symmetrical with first wing, first wing and described
It is both provided with least one VTOL flight instruments as described above on two wings, the VTOL on first wing flies
Luggage is put to be symmetrical arranged with the VTOL flight instruments on second wing, the VTOL flight on first wing
The connecting line of device is connected to each other with the connecting line of the VTOL flight instruments on corresponding second wing, multiple described vertical
Center line of the center line of the horn 1 of straight landing flight instruments each parallel to the fuselage.
The fixed-wing unmanned plane of the application, by by the first rotor power mechanism and the second rotor power mechanism
The both ends of the horn 1 are symmetrically assembled in, the first rotor power mechanism and described second are controlled by the control mechanism
Rotor power mechanism, enables the VTOL of VTOL flight instruments and flight.Thus, the VTOL flight dress
It is set to as completely self-contained modular flight part external member, whether its landing and flight are no longer limited by landing site good, and
And there is higher efficiency；Can by connector by the VTOL flight instruments be loaded into variously-shaped and weight,
Suitable on the article to be transported of transport, such as by chain, adhesive tape, the VTOL flight instruments this can be driven to treat
Article VTOL and flight are transported, assembling is extremely easy；, can be in a thing to be transported if Item Weight to be transported is larger
Multiple VTOL flight instrumentses are loaded on product, by the plug of the connecting line 11, by two adjacent horns 1
It is connected to each other, can be communicated between two after the docking VTOL flight instruments, is flown so as to fulfill common, therefore
Use the VTOL flight instruments of the application, it is not necessary to redesign and produce nothing according to the shape of article to be transported and weight
It is man-machine, cost can be effectively reduced, various specifications heavy weight goods express transportation device can be used as, is highly suitable for carrying out express delivery,
It is adapted to commercially be widely applied.
The takeoff and landing of the fixed-wing unmanned plane with it is foregoing described in VTOL flight instruments takeoff and landing
Essentially identical, details are not described herein.When the fixed-wing unmanned plane, which rises, flies to suitable position, from the foregoing it will be appreciated that when described solid
When determining the lift that takes off of wing unmanned plane and being equal to the gravity of whole the fixed-wing unmanned plane and belongings, the fixed-wing nobody
Machine can be realized under the action of the VTOL flight instruments and hovered in the air, at this time, described in the control mechanism
Control chip can receive the signal feedback of miscellaneous part in described control unit 5, so as to pass through the electron speed regulator, control
All brushless electric machines stop, to reduce resistance；At this time, the fixed-wing unmanned plane needs flight forward, increases described hang down
The rotating speed of the brushless electric machine at the rear of straight landing flight instruments, reduces the brushless electric machine in the front of the VTOL flight instruments
Rotating speed, so as to produce the power of flight forward, make the fixed-wing unmanned plane flight forward；When the fixed-wing unmanned plane needs
When changing course, if the steering of brushless electric machine is identical with the direction of course change, increase the rotating speed of the brushless electric machine, otherwise also
So, so as to carry out steering operation using the speed discrepancy of brushless electric machine.Here brushless electric machine, refers to mentioned hereinabove described hang down
First brushless electric machine 21 and second brushless electric machine 31 in straight landing flight instruments.If the fixed-wing unmanned plane goes out
Showing failure, the control mechanism can be fed back according to the signal of described control unit 5 and the GPS unit 8, be started in time, from
And the effect of parachute is served as, so that the fixed-wing unmanned plane can steadily land.
In the description of the present invention, it is necessary to illustrate, unless otherwise clearly defined and limited, term " installation ", " phase
Even ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or be integrally connected；Can
To be mechanical connection or be electrically connected；It can be directly connected, can also be indirectly connected by intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood at this
Concrete meaning in invention.
Finally it should be noted that：The above embodiments are only used to illustrate the technical solution of the present invention., rather than its limitations；To the greatest extent
Pipe is described in detail the present invention with reference to foregoing embodiments, it will be understood by those of ordinary skill in the art that：Its according to
Can so modify to the technical solution described in foregoing embodiments, either to which part or all technical characteristic into
Row equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from various embodiments of the present invention technology
The scope of scheme.
Claims (10)
1. a kind of VTOL flight instruments, it is characterised in that the VTOL flight instruments includes horn, the first rotor moves
Force mechanisms and the second rotor power mechanism, the first rotor power mechanism and the second rotor power mechanism are symmetrically arranged
In the both ends of the horn；Be provided with control mechanism, power sector and connecting line in the horn, the control mechanism with it is described
First rotor power mechanism and the second rotor power mechanism are of coupled connections, and the power sector is moved with first rotor
Force mechanisms, the second rotor power mechanism and the control mechanism are electrically connected；One end of the connecting line and the control
Mechanism telecommunications connection, the other end of the connecting line is located at outside the horn, and the other end of the connecting line is provided with plug.
2. VTOL flight instruments according to claim 1, it is characterised in that the rotation of the first rotor power structure
Shaft axis and the rotation axis of the second rotor power structure are straight up.
3. VTOL flight instruments according to claim 1 or 2, it is characterised in that the first rotor power mechanism
Structure it is identical with the structure of the second rotor power mechanism.
4. VTOL flight instruments according to claim 3, it is characterised in that the first rotor power mechanism includes
The first brushless electric machine and the first rotor blade being electrically connected to each other, the second rotor power mechanism include the be electrically connected to each other
Two brushless electric machines and the second rotor blade；First brushless electric machine and second brushless electric machine are electric with the power sector
Connection.
5. VTOL flight instruments according to claim 4, it is characterised in that the first rotor power mechanism is also wrapped
The first electron speed regulator is included, one end of first electron speed regulator is electrically connected with first brushless electric machine, first electricity
The other end of sub- governor is electrically connected with the control mechanism；The second rotor power mechanism further includes the second electronic speed regulation
Device, one end of second electron speed regulator are electrically connected with second brushless electric machine, second electron speed regulator it is another
End is electrically connected with the control mechanism；The power sector passes through first electron speed regulator and first brushless electric machine electricity
Connection, the power sector are electrically connected by second electron speed regulator with second brushless electric machine.
6. VTOL flight instruments according to claim 5, it is characterised in that the power sector includes the first power supply
And second source, first power supply are electrically connected by first electron speed regulator with first brushless electric machine, described
Two power supplys are electrically connected by second electron speed regulator with second brushless electric machine；First power supply and/or described
Two power supplys are electrically connected with the control mechanism.
7. VTOL flight instruments according to claim 5, it is characterised in that it is single that the control mechanism includes control
Member, described control unit includes control chip, gyroscope, accelerometer, barometer, compass and power management subelement, described
Control chip and the gyroscope, the accelerometer, the barometer, the compass and the equal coupling of power management subelement
Connection is closed, described control unit telecommunications is connected with Digital Transmission module and signal receiver.
8. VTOL flight instruments according to claim 7, it is characterised in that it is mono- that the control mechanism further includes GPS
Member, the GPS unit are of coupled connections with the control chip.
9. VTOL flight instruments according to claim 1, it is characterised in that be provided with least two on the horn
Screwed retaining ring.
10. a kind of fixed-wing unmanned plane, it is characterised in that the fixed-wing unmanned plane includes fuselage, and the side of the fuselage is set
The first wing is equipped with, the opposite side of the fuselage is provided with second wing symmetrical with first wing, first machine
It is both provided with least one VTOL flight instruments as described in claim 1-9 on the wing and second wing, described
VTOL flight instruments on one wing is symmetrical arranged with the VTOL flight instruments on second wing, and described first
The company of the connecting line of VTOL flight instruments on wing and the VTOL flight instruments on corresponding second wing
Wiring is connected to each other, the center line of the center line of the horn of multiple VTOL flight instrumentses each parallel to the fuselage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711418211.7A CN107953990A (en) | 2017-12-25 | 2017-12-25 | VTOL flight instruments and fixed-wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711418211.7A CN107953990A (en) | 2017-12-25 | 2017-12-25 | VTOL flight instruments and fixed-wing unmanned plane |
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| Publication Number | Publication Date |
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| CN107953990A true CN107953990A (en) | 2018-04-24 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201711418211.7A Pending CN107953990A (en) | 2017-12-25 | 2017-12-25 | VTOL flight instruments and fixed-wing unmanned plane |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108820200A (en) * | 2018-07-24 | 2018-11-16 | 南京邮电大学 | Coaxial double-rotary wing unmanned plane and its control method for movement |
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