CN109774946A - A kind of isomery VTOL system - Google Patents
A kind of isomery VTOL system Download PDFInfo
- Publication number
- CN109774946A CN109774946A CN201910051082.5A CN201910051082A CN109774946A CN 109774946 A CN109774946 A CN 109774946A CN 201910051082 A CN201910051082 A CN 201910051082A CN 109774946 A CN109774946 A CN 109774946A
- Authority
- CN
- China
- Prior art keywords
- fixed wing
- wing airvehicle
- rotor aerocraft
- recycling
- isomery
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
The invention discloses a kind of isomery VTOL systems, including multi-rotor aerocraft and Fixed Wing AirVehicle, the multi-rotor aerocraft includes first motor, the first propeller, undercarriage, recycling network is fixed on the undercarriage, the Fixed Wing AirVehicle includes the second motor and the second propeller, and the Fixed Wing AirVehicle further includes head hooking device.Multi-rotor aerocraft of the invention carries Fixed Wing AirVehicle and takes off vertically, aerial release Fixed Wing AirVehicle, Fixed Wing AirVehicle independently completes flat winged task, multi-rotor aerocraft carries recycling network and takes off when recycling Fixed Wing AirVehicle, Fixed Wing AirVehicle head recyclable device flicks, hook recycling network, multi-rotor aerocraft carries Fixed Wing AirVehicle landing, realize recycling, the flat winged stage guarantees the excellent VTOL of Fixed Wing AirVehicle and the flat winged performance of high speed, realize the aerial recycling of Fixed Wing AirVehicle, hit the entirely autonomous progress of network process, it can be applied to the aircraft landing of extreme landform.
Description
Technical field
The present invention relates to aviation aircraft master-plan, structure design and pneumatic design fields, more specifically, it relates to
A kind of isomery VTOL system.
Background technique
Pure helicopter fuselage and adjusts rotor output and realizes flat fly by verting, so that preceding winged maximum speed by
To the limitation of motor output and trimming moment, maximum cruise is far smaller than Fixed Wing AirVehicle；Normal fixed wing aircraft is then
It is unable to complete VTOL, hovering and low-speed operations.And isomery landing system combines multi-rotor aerocraft and fixed-wing flight
The flight characteristic of device, to have both the two ability, application prospect is very broad, and economic prospect is good.
Summary of the invention
In view of the deficiencies of the prior art, the present invention intends to provide a kind of isomery VTOL system, realize
Aircraft VTOL under complicated landform.
To achieve the above object, the present invention provides the following technical scheme that
A kind of isomery VTOL system, including multi-rotor aerocraft and Fixed Wing AirVehicle, the multi-rotor aerocraft
Including first motor, the first propeller, undercarriage, recycling network is fixed on the undercarriage, the Fixed Wing AirVehicle includes
Second motor and the second propeller, the Fixed Wing AirVehicle further include head hooking device.
Further, the head hooking device includes hook, guide wheel and pull rod, the top of the guide wheel and pull rod one end
It is fixedly connected, the guide wheel and hook transmission cooperate.
It further, include robust control in the control system of multi-rotor aerocraft.
Further, the control system of Fixed Wing AirVehicle includes self-contained guidance system, and the self-contained guidance system includes
Pattern recognition device.
Multi-rotor aerocraft carries Fixed Wing AirVehicle and takes off vertically, and discharges Fixed Wing AirVehicle, fixed-wing flight in the air
Device independently completes flat winged task, and multi-rotor aerocraft carries recycling network and takes off when recycling Fixed Wing AirVehicle, Fixed Wing AirVehicle
Head recyclable device flicks, and hooks recycling network, and multi-rotor aerocraft carries Fixed Wing AirVehicle landing, realizes recycling, Ping Feijie
Section guarantees the excellent VTOL of Fixed Wing AirVehicle and the flat winged performance of high speed.
By using above-mentioned technical proposal, realize the aerial recycling of Fixed Wing AirVehicle, hit network process it is entirely autonomous into
Row can be applied to the aircraft landing of extreme landform.
Detailed description of the invention
Fig. 1 is multi-rotor aerocraft structural schematic diagram of the invention；
Fig. 2 is Fixed Wing AirVehicle structural schematic diagram of the invention；
Fig. 3 is head hooking device (closed state) structural schematic diagram of the invention；
Fig. 4 is head hooking device (opening state) structural schematic diagram of the invention；
Appended drawing reference in figure: 1, multi-rotor aerocraft；2, Fixed Wing AirVehicle；3, first motor；4, the first propeller；5,
Undercarriage；6, recycling network；7, the second motor；8, the second propeller；9, head hooking device；10, it links up with；11, guide wheel；12, it draws
Bar.
Specific embodiment
In order to make those skilled in the art that the present invention may be better understood, with reference to the accompanying drawings and examples to this hair
Bright technical solution further illustrates.
- 4 pairs of embodiment of the present invention are described further referring to Fig.1.
A kind of isomery VTOL system, including multi-rotor aerocraft 1 and Fixed Wing AirVehicle 2, more rotor flyings
Device 1 includes first motor 3, the first propeller 4, undercarriage 5, and recycling network 6 is fixed on the undercarriage 5, and the fixed-wing flies
Row device 2 includes the second motor 7 and the second propeller 8, and the Fixed Wing AirVehicle 2 further includes head hooking device 9.
Further, the head hooking device 9 includes hook 10, guide wheel 11 and pull rod 12, the guide wheel 11 and pull rod
It is fixedly connected above 12 one end, the guide wheel 11 cooperates with 10 transmission of hook.
It further, include robust control in the control system of multi-rotor aerocraft 1.
Further, the control system of Fixed Wing AirVehicle 2 includes self-contained guidance system, and the self-contained guidance system includes
Pattern recognition device.
The present invention is suitable for the landing of Fixed Wing AirVehicle under complicated landform, when taking off, with common multi-rotor unmanned aerial vehicle
It is similar, it is taken off vertically by the lift that rotor generates, after reaching certain altitude, opens Fixed Wing AirVehicle dynamical system, release later
Fixed Wing AirVehicle is put, Fixed Wing AirVehicle voluntarily executes flat winged task；Into recovery stage, the first of multi-rotor aerocraft 1
Motor 3 drives the rotation of the first propeller 4 to generate lift, carries recycling network 6 and takes off, the head hooking device 9 of Fixed Wing AirVehicle 2
It flicks, process are as follows: artificial control steering engine pulls pull rod 12, and pull rod 12 drives the guide wheel 11 above it, due to linking up with 10 shapes
Matching design, so that hook 10 is driven and flicked by guide wheel 11, and keep flicking state, self-contained guidance system is opened, makes to fix
Rotor aircraft 2 can be completed independently to hit net, due to 1 control system of multi-rotor aerocraft when hitting net by image recognition recycling network 6
Robust control, so impact is cancelled in a short time, 2 head of Fixed Wing AirVehicle hook 10 hooks recycling network 6 after hitting net, from
And combined with multi-rotor aerocraft 1, multi-rotor aerocraft 1 carries Fixed Wing AirVehicle 2 and completes vertical landing.
The preferred embodiment of the present invention above described embodiment only expresses, the description thereof is more specific and detailed, but simultaneously
Limitations on the scope of the patent of the present invention therefore cannot be interpreted as.It should be pointed out that for those of ordinary skill in the art
For, without departing from the inventive concept of the premise, several deformations can also be made, improves and substitutes, these belong to this hair
Bright protection scope.Therefore, the scope of protection of the patent of the invention shall be subject to the appended claims.
Claims (4)
1. a kind of isomery VTOL system, which is characterized in that including multi-rotor aerocraft (1) and Fixed Wing AirVehicle (2), institute
Stating multi-rotor aerocraft (1) includes first motor (3), the first propeller (4), undercarriage (5), is fixed on the undercarriage (5)
Have recycling network (6), the Fixed Wing AirVehicle (2) includes the second motor (7) and the second propeller (8), the fixed-wing flight
Device (2) further includes head hooking device (9).
2. a kind of isomery VTOL system according to claim 1, which is characterized in that the head hooking device (9)
Including hook (10), guide wheel (11) and pull rod (12), it is fixedly connected above the guide wheel (11) and pull rod (12) one end, it is described
Guide wheel (11) and the hook (10) transmission cooperate.
3. a kind of isomery VTOL system according to claim 1, which is characterized in that the control of multi-rotor aerocraft (1)
It include robust control in system processed.
4. a kind of isomery VTOL system according to claim 1, which is characterized in that the control of Fixed Wing AirVehicle (2)
System processed includes self-contained guidance system, and the self-contained guidance system includes pattern recognition device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910051082.5A CN109774946A (en) | 2019-01-17 | 2019-01-17 | A kind of isomery VTOL system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910051082.5A CN109774946A (en) | 2019-01-17 | 2019-01-17 | A kind of isomery VTOL system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109774946A true CN109774946A (en) | 2019-05-21 |
Family
ID=66501591
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910051082.5A Withdrawn CN109774946A (en) | 2019-01-17 | 2019-01-17 | A kind of isomery VTOL system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109774946A (en) |
-
2019
- 2019-01-17 CN CN201910051082.5A patent/CN109774946A/en not_active Withdrawn
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190521 |
|
| WW01 | Invention patent application withdrawn after publication |