CN108750097A - Rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing and additional fin - Google Patents
Rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing and additional fin Download PDFInfo
- Publication number
- CN108750097A CN108750097A CN201810550677.0A CN201810550677A CN108750097A CN 108750097 A CN108750097 A CN 108750097A CN 201810550677 A CN201810550677 A CN 201810550677A CN 108750097 A CN108750097 A CN 108750097A
- Authority
- CN
- China
- Prior art keywords
- wing
- additional fin
- compound auxiliary
- lift
- rear single
- 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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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/12—Adjustable control surfaces or members, e.g. rudders surfaces of different type or function being simultaneously adjusted
Abstract
The present invention is a kind of rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin, including rear single-screw paddle composite wing aircraft, be assemblied in its wing both sides without the compound auxiliary wing of thrust self energizing, additional fin and manned storehouse；Wherein, additional fin is folding on the outside of the compound auxiliary wing of no thrust self energizing by wing hinge, and manned storehouse is mounted on mounted on the lower section of body.The present invention not only has landing apart from short, flying speed is fast, wing structure intensity is high, wing can with energy storage, flight low energy consumption, the hang time is long the features such as, the hybrid lift wing of large area, it can play the role of aerodone under case of emergency, greatly improve the safety of aircraft, the safety of support personnel and goods and materials.
Description
Technical field
The present invention relates to a kind of aircraft, the rear single-screw paddle of the compound auxiliary wing of specifically a kind of band and additional fin is compound
Wing manned vehicle belongs to aircraft equipment technology field.
Background technology
Existing aircraft is broadly divided into fixed-wing and vertically taking off and landing flyer（Such as helicopter and more rotors）Two major classes.When
So also there is this product of VTOL fixed-wing.Traditional fixed-wing have the advantages that flying speed is fast, low energy consumption, but have
It is not connected to before and after main wing and tailplane, wing structure intensity is not high, is easily damaged, and landing requires high, landing distance disadvantage；
Traditional vertically taking off and landing flyer has the advantages that landing is convenient, but has that energy consumption is big, safety coefficient is low, and load capacity is poor, water
Flat flying speed is slow, is easy the shortcomings of air crash；Although current VTOL fixed-wing has the characteristics that landing is convenient, but in water
The shortcomings of controllability when flat flight is not satisfactory, and that there is flight resistances is big, and energy consumption is high, and safety coefficient is not still high.
Invention content
In view of the above-mentioned problems of the prior art, the present invention not only has landing apart from short, flying speed is fast, wing knot
Structure intensity height, wing can be with energy storage, the features such as low energy consumption, the hang time is long of flying, the hybrid lift wing of large area, feelings of meeting an urgent need
It can play the role of aerodone under condition, greatly improve the safety of aircraft, the safety of support personnel.
To achieve the goals above, the present invention includes rear single-screw paddle composite wing aircraft, is movably arranged on compound liter
Power aircraft both sides without the compound auxiliary wing of thrust self energizing, additional fin and manned storehouse；Wherein, rear single-screw paddle composite wing flies
Row device includes body, is fixedly mounted on body both sides hybrid lift wing, screw propeller；Wherein, body is set as deck
Platform；Self-enclosed ducted fan built in hybrid lift wing, hybrid lift wing outside are designed with wing hinge；No thrust confession
It can be provided with self-enclosed ducted fan in the compound auxiliary wing, the one or both sides of the no compound auxiliary wing of thrust self energizing are provided with electro-hydraulic gas
Interface and wing hinge, and be flexibly connected with hybrid lift wing by wing hinge, additional fin is foldable by wing hinge
On the outside of the compound auxiliary wing of no thrust self energizing.Additional fin internal battery/fuel, manned storehouse are mounted on the lower section of body.
Further, propeller be electric propeller, the dynamic propeller of oil, etc. various ways.
Further, hybrid lift wing can be divided into two parts of lift main wing and balance empennage, be separately positioned on compound
The front and back of lifting wing；It is reserved with space between lift main wing and balance empennage, the horizontal lifting rudder wing is provided in space；Its
In, at least there are one self-enclosed ducted fans for installation inside lift main wing.
Further, further include vertical tail, the vertical tail is arranged above or below body；The vertical tail is set
It sets in wing both sides；The vertical tail may be implemented to fold；Mobilizable vertical rudder wing is installed behind the vertical tail.
Further, body is set as deck platform；The mounting hole of the regular arrangement in deck platform both sides；The first
It is designed with socket on plate platform；The socket is female or male.
Further, electro-hydraulic gas interface carries lid.
Further, the compound auxiliary wing of no thrust self energizing can be divided into lift additional fin and auxiliary two parts of empennage of balance, point
It is not arranged in the front and back of the compound auxiliary wing of no thrust self energizing；It is reserved with space between lift additional fin and the auxiliary empennage of balance, it is empty
It is interior to be provided with the horizontal lifting rudder wing；Wherein, at least there are one self-enclosed ducted fans for installation inside lift additional fin.
Further, engine installation position, engine installation position are additionally provided on the compound auxiliary wing of no thrust self energizing（111）It is interior
It is provided with power plant.
Further, it is provided with battery/fuel on the compound auxiliary wing of no thrust self energizing.
The prior art is compared, the main feature having is invented：
1, the present invention has landing apart from short, and flying speed is fast, maneuverability, avoidance ability are strong, wing structure intensity is high, wing
It can be with energy storage, the features such as low energy consumption of flying.It relies on self-enclosed vertical ducted fan, aircraft can be provided in horizontal flight
Additional maneuverability realizes the super maneuver ability of moment change of flight posture and track.
2, additional fin is also added on the outside of the compound auxiliary wing of no thrust self energizing in the present invention, improves aircraft level
Lift when flight also increases the energy of energy device.
3, the very large Waverider wing of the present invention, can play the role of certain paraglider, substantially reduce acceleration of gravity,
Safety coefficient is greatly improved, the control function of the hydroplane wing and the vertical rudder wing and the aerofoil closing of self-enclosed ducted fan are coordinated
Function greatly improves winged even if lift ducted fan and horizontal propeller can realize that aerodone formula is force-landed if damage simultaneously
The safety of row device has ensured the safety of personnel and goods and materials.
4, the present invention can realize multiple functions using hardware and software platform, modularized design,
5, the present invention using both sides wing can Expanding design, wing area can be expanded when necessary, improve the standard flight when
Lift, improve load capacity.
6, the present invention also has successive socket, and the cluster of aircraft is facilitated to fly, and further decreases cluster flight
When power consumption.In front and back serial connection, the aircraft at rear only needs a small amount of energy expenditure, can be achieved with flying for long range
Row, not the cluster flight of only aircraft provide the low-power consumption scheme of clustering, it might even be possible to realize the sky between aircraft
Middle rescue, i.e., before aircraft the dragging of faulty aircraft below is taken off, realize and mutually come to sb.'s rescue between aircraft not seen before
Help phenomenon.
7. can lead between the modularization ducted fan drive-in hybrid lift additional fin and hybrid lift aircraft of invention
Cross wing hinge and electro-hydraulic gas interface be attached, by hybrid lift aircraft main control unit control, and can by the battery of aerofoil/
The energy transmissions such as fuel give aircraft host, improve the flight time.Performance may be implemented by superimposion lift additional fin
Multiplication.Modular design reduces the disposable input of client, reduces buying and operation cost.
8. the modularization ducted fan drive-in hybrid lift additional fin of the present invention with other hybrid lifts additional fins phases simultaneously
Connection, and be attached by wing hinge and electro-hydraulic gas interface, it is synchronous to be controlled by hybrid lift aircraft main control unit, it opens up again
Zhan Bingke gives the energy transmissions such as battery/fuel of aerofoil to aircraft host, improves the flight time.
9. thrust device modularization can very easily realize that repair is replaced.
10. in the present invention, additional fin side is provided with electro-hydraulic gas interface, realizes additional fin and hybrid lift aircraft
Energy intercommunication between main plane, and action is controlled by hybrid lift aircraft, improves the flexibility of complete machine.
11. additional fin is also built-in with the horizontal lifting rudder wing, improves complete machine and manipulate agility！
12. aerofoil type energy device, efficiently uses space.
13. the present invention uses modularized design, compound different types of machines to use, cost has been saved.
Description of the drawings
Fig. 1 is the structural schematic diagram of the present invention；
Fig. 2 is the side view of the present invention；
Fig. 3 is the rearview of the present invention；
Fig. 4 is the plan view of the present invention；
Fig. 5 is the oblique view of the present invention；
In figure：101：Body；102：Hybrid lift wing；104：Self-enclosed ducted fan；105：Vertical tail；1051. vertical
The rudder wing；106：Propeller；107：Energy Management System；1021：Lift main wing；1022：The horizontal lifting rudder wing；1023：Balance tail
The wing；1028：Wing hinge；1001：Socket；1002：Cavity；1003：Mounting hole；1006：Battery/fuel；108：Video camera；
1026：Convex series connection head；1027：Spill series connection seat；1031, without the compound auxiliary wing of thrust self energizing；10311, lift additional fin；
10312, auxiliary empennage is balanced；1026, electro-hydraulic gas interface；10261, lid；111, engine installation position；112, manned storehouse；114,
Additional fin.
Specific implementation mode
The present invention will be further described below in conjunction with the accompanying drawings.
As shown in Figures 1 to 5, the rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing and additional fin, packet
Include rear single-screw paddle composite wing aircraft, be movably arranged on hybrid lift aircraft both sides without the compound auxiliary wing of thrust self energizing
1031 compositions；111, engine installation position.
Wherein, the rear single-screw paddle composite wing aircraft includes body 101, is fixedly mounted on 101 both sides of body
Hybrid lift wing 102, propeller 106；Wherein, the body 101 is set as deck platform；The hybrid lift wing
Self-enclosed ducted fan 104 built in 102,102 outside of hybrid lift wing are designed with wing hinge 1028；
It is described without self-enclosed ducted fan 104 is provided in the compound auxiliary wing of thrust self energizing 1031, no thrust self energizing is compound
The one or both sides of the auxiliary wing 1031 are provided with electro-hydraulic gas interface 1026 and wing hinge 1028, and by wing hinge 1028 and again
Lifting wing 102 is closed to be flexibly connected.
Additional fin 114 is folding on the outside of the compound auxiliary wing of no thrust self energizing by wing hinge 1028.
114 internal batteries of additional fin/fuel 1006,
Manned 112 storehouse is mounted on the lower section of body 101.
As further improvement of the invention, propeller 106 is the various ways such as electric propeller, the dynamic propeller of oil.
As further improvement of the invention, hybrid lift wing 102 can be divided into lift main wing 1021 and balance empennage
1023 two parts, are separately positioned on the front and back of hybrid lift wing 102；Between lift main wing 1021 and balance empennage 1023
It is reserved with space, the horizontal lifting rudder wing 1022 is provided in space；Wherein, at least there are one certainly for installation inside lift main wing 1021
Close ducted fan 104.
Improved as of the invention further, vertical tail 105, vertical tail 105 be arranged above body 101 or under
Side；The vertical tail 105 is arranged in wing both sides；The vertical tail 105 may be implemented to fold；The vertical tail 105
Mobilizable vertical rudder wing 1051 is installed below.
As further improvement of the invention, body 101 is set as deck platform；The deck platform both sides are regular
The mounting hole 1003 of arrangement；Socket 1001 is designed in the deck platform；The socket 1001 is female or male.
As further improvement of the invention, electro-hydraulic gas interface 1026 carries lid 10261.
Improved as of the invention further, can be divided into lift additional fin without the compound auxiliary wing of thrust self energizing 1031
10311 and auxiliary 10,312 two parts of empennage of balance, it is separately positioned on the front and back of the compound auxiliary wing of no thrust self energizing 1031；
It is reserved with space between lift additional fin 10311 and the auxiliary empennage of balance 10312, the horizontal lifting rudder wing 1022 is provided in space；
Wherein, at least there are one self-enclosed ducted fans 104 for installation inside lift additional fin 10311.
It is improved as of the invention further, engine installation position is additionally provided on the compound auxiliary wing of no thrust self energizing 1031
111, power plant is provided in engine installation position 111.
It is improved as of the invention further, battery/fuel 1006 is provided on the compound auxiliary wing of no thrust self energizing 1031.
The prior art is compared, the main feature having is invented：
3,1, the present invention has landing apart from short, and flying speed is fast, maneuverability, avoidance ability are strong, wing structure intensity is high, machine
The wing can be with energy storage, the features such as low energy consumption of flying.Self-enclosed vertical ducted fan is relied on, aircraft can be provided in horizontal flight
Additional maneuverability, realize moment change of flight posture and track super maneuver ability.
4, additional fin is also added on the outside of the compound auxiliary wing of no thrust self energizing in the present invention, improves aircraft level
Lift when flight also increases the energy of energy device.
3, the very large Waverider wing of the present invention, can play the role of certain paraglider, substantially reduce acceleration of gravity,
Safety coefficient is greatly improved, the control function of the hydroplane wing and the vertical rudder wing and the aerofoil closing of self-enclosed ducted fan are coordinated
Function greatly improves winged even if lift ducted fan and horizontal propeller can realize that aerodone formula is force-landed if damage simultaneously
The safety of row device has ensured the safety of personnel and goods and materials.
4, the present invention can realize multiple functions using hardware and software platform, modularized design,
5, the present invention using both sides wing can Expanding design, wing area can be expanded when necessary, improve the standard flight when
Lift, improve load capacity.
6, the present invention also has successive socket, and the cluster of aircraft is facilitated to fly, and further decreases cluster flight
When power consumption.In front and back serial connection, the aircraft at rear only needs a small amount of energy expenditure, can be achieved with flying for long range
Row, not the cluster flight of only aircraft provide the low-power consumption scheme of clustering, it might even be possible to realize the sky between aircraft
Middle rescue, i.e., before aircraft the dragging of faulty aircraft below is taken off, realize and mutually come to sb.'s rescue between aircraft not seen before
Help phenomenon.
7. can lead between the modularization ducted fan drive-in hybrid lift additional fin and hybrid lift aircraft of invention
Cross wing hinge and electro-hydraulic gas interface be attached, by hybrid lift aircraft main control unit control, and can by the battery of aerofoil/
The energy transmissions such as fuel give aircraft host, improve the flight time.Performance may be implemented by superimposion lift additional fin
Multiplication.Modular design reduces the disposable input of client, reduces buying and operation cost.
8. the modularization ducted fan drive-in hybrid lift additional fin of the present invention with other hybrid lifts additional fins phases simultaneously
Connection, and be attached by wing hinge and electro-hydraulic gas interface, it is synchronous to be controlled by hybrid lift aircraft main control unit, it opens up again
Zhan Bingke gives the energy transmissions such as battery/fuel of aerofoil to aircraft host, improves the flight time.
9. thrust device modularization can very easily realize that repair is replaced.
10. in the present invention, additional fin side is provided with electro-hydraulic gas interface, realizes additional fin and hybrid lift aircraft
Energy intercommunication between main plane, and action is controlled by hybrid lift aircraft, improves the flexibility of complete machine.
11. additional fin is also built-in with the horizontal lifting rudder wing, improves complete machine and manipulate agility！
12. aerofoil type energy device, efficiently uses space.
13. the present invention uses modularized design, compound different types of machines to use, cost has been saved.
Schematically the present invention and embodiments thereof are described above, description is not limiting, institute in attached drawing
What is shown is also one of embodiments of the present invention, and actual structure is not limited to this.So if the common skill of this field
Art personnel are enlightened by it, without departing from the spirit of the invention, are not inventively designed and the technical solution
Similar frame mode and embodiment, are within the scope of protection of the invention.
Claims (10)
1. the rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing and additional fin, which is characterized in that including rear list
The compound rotor aircraft of propeller type, be assemblied in its wing both sides without the compound auxiliary wing of thrust self energizing, additional fin（114）And it carries
People storehouse（112）；
Wherein, the rear single-screw paddle composite wing aircraft includes body（101）, be fixedly mounted on body（101）Both sides
Hybrid lift wing（102）, propeller（106）；Wherein, the body（101）It is set as deck platform；The compound liter
Power wing（102）Built-in self-enclosed ducted fan（104）, hybrid lift wing（102）Outside is designed with wing hinge (1028)；
Propeller（106）For screw propeller；
It is described without being provided with self-enclosed ducted fan in the compound auxiliary wing of thrust self energizing（104）, no thrust self energizing is compound auxiliary
The one or both sides of the wing are provided with electro-hydraulic gas interface（1026）With wing hinge (1028), and by wing hinge (1028) with it is multiple
Close lifting wing（102）Flexible connection；
The additional fin（114）It is folding outside the compound auxiliary wing of no thrust self energizing by wing hinge (1028)
Side；The additional fin（114）Internal battery/fuel（1006）.
Manned storehouse described in 2.（112）Mounted on body（101）Lower section.
3. the rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin according to claim 1,
It is characterized in that, the propeller（106）For a variety of power modes such as electric propeller, the dynamic propellers of oil.
4. the rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin according to claim 1,
It is characterized in that, the hybrid lift wing（102）Lift main wing can be divided into（1021）And balance empennage（1023）Two
Part is separately positioned on hybrid lift wing（102）Front and back；Lift main wing（1021）With balance empennage（1023）Between it is pre-
There are space, the horizontal lifting rudder wing is provided in space（1022）；Wherein, lift main wing（1021）There are one internal at least installations
Self-enclosed ducted fan（104）.
5. the rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin according to claim 1,
It is characterized in that, further including vertical tail（105）, the vertical tail（105）It is arranged in body（101）Above or below；Institute
State vertical tail（105）It is arranged in wing both sides；The vertical tail（105）It may be implemented to fold；The vertical tail（105）
Mobilizable vertical rudder wing is installed below（1051）.
6. the rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin according to claim 1,
It is characterized in that, the body（101）It is set as deck platform；The mounting hole of the regular arrangement in deck platform both sides
（1003）；It is designed with socket in the deck platform（1001）；The socket（1001）For female or male.
7. the rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin according to claim 1,
It is characterized in that, the electro-hydraulic gas interface（1026）With lid（10261）.
8. the rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin according to claim 1,
It is characterized in that, the compound auxiliary wing of no thrust self energizing can be divided into lift additional fin（10311）And the auxiliary empennage of balance
（10312）Two parts are separately positioned on the front and back of the compound auxiliary wing of no thrust self energizing；Lift additional fin（10311）With it is flat
Weigh auxiliary empennage（10312）Between be reserved with space, the horizontal lifting rudder wing is provided in space（1022）；Wherein, lift additional fin
（10311）There are one self-enclosed ducted fans for internal at least installation（104）.
9. the rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin according to claim 1,
It is characterized in that, being additionally provided with engine installation position on the compound auxiliary wing of no thrust self energizing（111）, engine installation position
（111）Inside it is provided with power plant.
10. the rear single-screw paddle composite wing manned vehicle of the band compound auxiliary wing and additional fin according to claim 1,
It is characterized in that, being provided with battery/fuel on the compound auxiliary wing of no thrust self energizing（1006）.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810550677.0A CN108750097A (en) | 2018-05-31 | 2018-05-31 | Rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing and additional fin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810550677.0A CN108750097A (en) | 2018-05-31 | 2018-05-31 | Rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing and additional fin |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108750097A true CN108750097A (en) | 2018-11-06 |
Family
ID=64001532
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810550677.0A Withdrawn CN108750097A (en) | 2018-05-31 | 2018-05-31 | Rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing and additional fin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108750097A (en) |
-
2018
- 2018-05-31 CN CN201810550677.0A patent/CN108750097A/en not_active Withdrawn
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| 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 | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20181106 |