CN107813929A - Combined type dalta wing duct aircraft - Google Patents
Combined type dalta wing duct aircraft Download PDFInfo
- Publication number
- CN107813929A CN107813929A CN201610813544.9A CN201610813544A CN107813929A CN 107813929 A CN107813929 A CN 107813929A CN 201610813544 A CN201610813544 A CN 201610813544A CN 107813929 A CN107813929 A CN 107813929A
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- China
- Prior art keywords
- wing
- aircraft
- dalta
- combined type
- duct aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
A kind of combined type dalta wing duct aircraft, by multiple dalta wings coaxially to turning duct aircraft monomer, it is combined into pyramid stepped-style, and the overall shape after combination is maintained as triangle；Described dalta wing is main with coaxially to turning duct aircraft, dalta wing, accelerating propulsive wing coaxially to turning duct aircraft monomer；The bindiny mechanism on wing tip that each dalta wing coaxially passes through dalta wing to turning duct aircraft monomer connects, and forms combined type dalta wing duct aircraft.
Description
Technical field
The present invention relates to a kind of aircraft, more particularly, to a kind of combined type dalta wing duct aircraft.
Background technology
Possess the aircraft of hovering and VTOL investigate, take photo by plane, search and rescue, atmospheric seeing, the technical field such as communication
Demand is increasing, and application field also constantly expands to security, the disaster relief and transport etc..Hovering and VTOL can be completed at present
The structure of aircraft mainly have single-rotor helicopter, twin-rotor helicopter, tiltrotor, Multi-axis aircraft etc..It is but small-sized
Aircraft can not meet the task of heavy load, Large Scale Space Vehicle is, it is necessary to pilot driver, and endurance is held by fuel tank
The limitation of amount.There is also certain hidden danger for the flight stability of Multi-axis aircraft.According to the development of society, existing fixed-wing flies
Row device, helicopter and some small aircrafts can not meet to require.
The content of the invention
It is an object of the present invention to overcome the above-mentioned drawbacks of the prior art and provide one kind extend the flight time,
The loading capacity of aircraft parent can be according to the combined type dalta wing duct aircraft that application purpose is changed.
The purpose of the present invention can be achieved through the following technical solutions.
A kind of combined type dalta wing duct aircraft, by multiple dalta wings coaxially to turning duct aircraft monomer, with golden word
Tower stepped-style is combined into, and the overall shape after combination is maintained as triangle；Described dalta wing is coaxially to turning
Duct aircraft monomer, it is main with coaxially to turning duct aircraft, dalta wing, accelerating propulsive wing.Each dalta wing is coaxially right
The bindiny mechanism turned on the wing tip that duct aircraft monomer passes through dalta wing connects, and forms the flight of combined type dalta wing duct
Device（Coaxially see the patent No. to turning duct aircraft data：ZL2015 2 0741312.8 ）.
Aircraft monomer of the present invention be dalta wing coaxially to turning duct aircraft, i.e., each monomer aircraft it is outer
Shape is all triangle or class triangle.
Dalta wing of the present invention is coaxially designed with bindiny mechanism to the triangle wing tip for turning duct aircraft monomer, is used for
Each aircraft is combined connection.
Combined type dalta wing of the present invention is coaxially to turning duct aircraft, with pyramid when the aircraft of monomer combines
Stepped-style combines, and such aircraft number of combinations requires after combination that general shape is remained in that as triangle, after ensuring combination
Remain in that most stable of structure.So minimum number during a number of monomer aircraft combination is three, and it is group
General shape remains in that the quantity for triangle after conjunction, to ensure that it is most stable of that combined type dalta wing duct aircraft remains
Structure.
Combined type dalta wing duct aircraft of the present invention, combined with pyramid step-wise manner, it is ensured that each
The dead astern of unit aircraft maintains a triangular space, it is ensured that accelerate the working space of propulsive wing, meanwhile, dalta wing is fixed
It is each coaxially to turning the distance of duct aircraft, it is ensured that the working air current of each aircraft do not interfere with each other.
Combined type dalta wing duct aircraft of the present invention, and in flight course, it can use wherein a part of
Aircraft after reaching certain voyage, reuses another part aircraft as the second stage of power, so analogizes behaviour as a phase power
Work goes down, it is possible to greatly improves the course continuation mileage of aircraft.
Compared with prior art, the technology of the present invention is by combining aircraft, can make aircraft combine after rock-steady structure not
Increase lifting area, high load ability and endurance in the case of change greatly.
Brief description of the drawings
Fig. 1 is dalta wing of the present invention coaxially to turning duct Flight Vehicle Structure schematic diagram；Include coaxially to turning to contain
Road aircraft 01, dalta wing 02, accelerate propulsive wing 03.
Fig. 2 is dalta wing of the present invention coaxially to turning duct aircraft top view；Include coaxially to turning
Duct aircraft 01, dalta wing 02, accelerate propulsive wing 03, wing tip bindiny mechanism.
Fig. 3 is combined type dalta wing duct Flight Vehicle Structure schematic diagram of the present invention.
Specific embodiment
The present invention is described in detail with specific embodiment below in conjunction with the accompanying drawings.
As shown in figure 3, a kind of combined type dalta wing duct aircraft of the present invention, by multiple dalta wings coaxially to turning
Duct aircraft monomer, is combined into pyramid stepped-style, and the overall shape after combination is maintained as triangle；
Described dalta wing coaxially to turning duct aircraft monomer, it is main include coaxially to turn duct aircraft 01, dalta wing 02,
Accelerate propulsive wing 03；Coaxially be placed in turning duct aircraft 01 in dalta wing 02, accelerate propulsive wing 03 be arranged on
The dead astern of the relative dalta wing 02 of aircraft direction of advance；Wing tip bindiny mechanism is designed with the wing tip of dalta wing 02
04 ；The wing tip bindiny mechanism 04 on wing tip that each dalta wing coaxially passes through dalta wing 02 to turning duct aircraft monomer
Connect, constitute combined type dalta wing duct aircraft.
For dalta wing of the present invention coaxially to turning duct aircraft monomer, profile is all triangle or class triangle, when
A number of dalta wing is coaxially combined into combined type dalta wing duct to turning duct aircraft monomer with pyramid stepped-style
During aircraft, the number of combinations is at least 3, and is the quantity that general shape remains in that as triangle after combining, with true
Protect combined type dalta wing duct aircraft and remain most stable of structure.
Combined type dalta wing duct aircraft of the present invention, by multiple dalta wings coaxially to turning duct aircraft monomer
After being combined with pyramid step-wise manner, a triangular space is maintained in the dead astern of each aircraft, as acceleration propulsive wing
03 working space, meanwhile, dalta wing 02 secures each coaxially to turning the distance of duct aircraft 01, it can be ensured that
The working air current of each aircraft is not interfere with each other.
Combined type dalta wing duct aircraft of the present invention, can be first using wherein a part of in flight course
Aircraft after reaching certain voyage, reuses another part aircraft as the second stage of power, so analogized as first phase power
Operation is gone down, it is possible to realizes the course continuation mileage target for improving aircraft.
Claims (4)
1. a kind of combined type dalta wing duct aircraft, it is characterised in that the aircraft is coaxially flown by multiple dalta wings to turning duct
Row device monomer is combined into pyramid stepped-style, and the overall shape after combination remains triangle.
2. a kind of combined type dalta wing duct aircraft as claimed in claim 1, it is characterised in that on the wing tip of dalta wing all
Provided with wing tip bindiny mechanism；Wing tip connection on the wing tip that each dalta wing coaxially passes through dalta wing to turning duct aircraft monomer
Mechanism connects, and constitutes combined type dalta wing duct aircraft.
3. a kind of combined type dalta wing duct aircraft as claimed in claim 1, it is characterised in that when a number of triangle
When the wing is coaxially combined into combined type dalta wing duct aircraft to turning duct aircraft monomer with pyramid stepped-style, the combination
Minimum number is 3, and is the quantity that general shape remains in that as triangle after combining.
4. a kind of combined type dalta wing duct aircraft as claimed in claim 1, it is characterised in that coaxial by multiple dalta wings
After turning duct aircraft monomer with the combination of pyramid step-wise manner, the dead astern of each aircraft maintains a triangle sky
Between, as the working space for accelerating propulsive wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610813544.9A CN107813929A (en) | 2016-09-11 | 2016-09-11 | Combined type dalta wing duct aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610813544.9A CN107813929A (en) | 2016-09-11 | 2016-09-11 | Combined type dalta wing duct aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107813929A true CN107813929A (en) | 2018-03-20 |
Family
ID=61600390
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610813544.9A Pending CN107813929A (en) | 2016-09-11 | 2016-09-11 | Combined type dalta wing duct aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107813929A (en) |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482663A (en) * | 2018-05-31 | 2018-09-04 | 江苏常探机器人有限公司 | The rear single-blade formula combined wing aircraft of the double duct thrusts of the band compound auxiliary wing and additional fin |
| CN108502168A (en) * | 2018-05-31 | 2018-09-07 | 江苏常探机器人有限公司 | The rear compound rotor aircraft of single-blade folding with the compound auxiliary wing of airscrew thrust |
| CN108502164A (en) * | 2018-05-31 | 2018-09-07 | 江苏常探机器人有限公司 | A kind of rear single-screw paddle composite wing aircraft with the compound auxiliary wing of airscrew thrust |
| CN108528699A (en) * | 2018-05-31 | 2018-09-14 | 江苏常探机器人有限公司 | Rear single screw folding composite wing manned vehicle with the compound auxiliary wing of thrust |
| CN108545179A (en) * | 2018-05-31 | 2018-09-18 | 江苏常探机器人有限公司 | Single ducted fan formula composite wing manned vehicle afterwards |
| CN108639327A (en) * | 2018-05-31 | 2018-10-12 | 江苏常探机器人有限公司 | A kind of rear single-blade formula combined wing aircraft of the compound auxiliary wing of double duct thrusts |
| CN108750095A (en) * | 2018-05-31 | 2018-11-06 | 江苏常探机器人有限公司 | A kind of rear single-blade formula composite wing airfreighter of the compound auxiliary wing of double duct thrusts |
| CN108750099A (en) * | 2018-05-31 | 2018-11-06 | 江苏常探机器人有限公司 | A kind of band is without the rear compound rotor aircraft of single screw folding for pushing away the compound auxiliary wing |
| CN108750088A (en) * | 2018-05-31 | 2018-11-06 | 江苏常探机器人有限公司 | Rear single screw folding composite wing cargo aircraft with the compound auxiliary wing of thrust |
| CN108773487A (en) * | 2018-05-31 | 2018-11-09 | 江苏常探机器人有限公司 | Rear single-screw paddle composite wing cargo aircraft with the compound auxiliary wing and additional fin |
| CN108773485A (en) * | 2018-05-31 | 2018-11-09 | 江苏常探机器人有限公司 | The foldable composite wing manned vehicle of single vortex-spraying type afterwards |
| CN108791862A (en) * | 2018-05-31 | 2018-11-13 | 江苏常探机器人有限公司 | Double culverts push away the compound auxiliary wing and rear single culvert pushing-type composite wing manned vehicle of additional fin |
| CN108791869A (en) * | 2018-05-31 | 2018-11-13 | 江苏常探机器人有限公司 | With turbofan push away the compound auxiliary wing without back pressure formula composite wing manned vehicle |
| CN108820201A (en) * | 2018-05-31 | 2018-11-16 | 江苏常探机器人有限公司 | Rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing of airscrew thrust |
| CN108820202A (en) * | 2018-05-31 | 2018-11-16 | 江苏常探机器人有限公司 | It is a kind of with the compound auxiliary wing of ducted fan without the compound rotor aircraft of back pressure formula |
| CN108839796A (en) * | 2018-05-31 | 2018-11-20 | 江苏常探机器人有限公司 | A kind of composite wing cargo aircraft of the compound auxiliary wing of twin screw thrust |
| CN108860593A (en) * | 2018-05-31 | 2018-11-23 | 江苏常探机器人有限公司 | Rear single ducted fan formula composite wing manned vehicle with solar energy additional fin |
| CN108928473A (en) * | 2018-05-31 | 2018-12-04 | 江苏常探机器人有限公司 | A kind of folding composite wing manned vehicle of the compound auxiliary wing of twin screw thrust |
| CN108945422A (en) * | 2018-05-31 | 2018-12-07 | 江苏常探机器人有限公司 | A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away composite wing airfreighter |
| CN113525680A (en) * | 2021-07-20 | 2021-10-22 | 中国空气动力研究与发展中心空天技术研究所 | Reconfigurable combined type unmanned aerial vehicle |
-
2016
- 2016-09-11 CN CN201610813544.9A patent/CN107813929A/en active Pending
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108482663A (en) * | 2018-05-31 | 2018-09-04 | 江苏常探机器人有限公司 | The rear single-blade formula combined wing aircraft of the double duct thrusts of the band compound auxiliary wing and additional fin |
| CN108502168A (en) * | 2018-05-31 | 2018-09-07 | 江苏常探机器人有限公司 | The rear compound rotor aircraft of single-blade folding with the compound auxiliary wing of airscrew thrust |
| CN108502164A (en) * | 2018-05-31 | 2018-09-07 | 江苏常探机器人有限公司 | A kind of rear single-screw paddle composite wing aircraft with the compound auxiliary wing of airscrew thrust |
| CN108528699A (en) * | 2018-05-31 | 2018-09-14 | 江苏常探机器人有限公司 | Rear single screw folding composite wing manned vehicle with the compound auxiliary wing of thrust |
| CN108545179A (en) * | 2018-05-31 | 2018-09-18 | 江苏常探机器人有限公司 | Single ducted fan formula composite wing manned vehicle afterwards |
| CN108639327A (en) * | 2018-05-31 | 2018-10-12 | 江苏常探机器人有限公司 | A kind of rear single-blade formula combined wing aircraft of the compound auxiliary wing of double duct thrusts |
| CN108750095A (en) * | 2018-05-31 | 2018-11-06 | 江苏常探机器人有限公司 | A kind of rear single-blade formula composite wing airfreighter of the compound auxiliary wing of double duct thrusts |
| CN108750099A (en) * | 2018-05-31 | 2018-11-06 | 江苏常探机器人有限公司 | A kind of band is without the rear compound rotor aircraft of single screw folding for pushing away the compound auxiliary wing |
| CN108750088A (en) * | 2018-05-31 | 2018-11-06 | 江苏常探机器人有限公司 | Rear single screw folding composite wing cargo aircraft with the compound auxiliary wing of thrust |
| CN108773487A (en) * | 2018-05-31 | 2018-11-09 | 江苏常探机器人有限公司 | Rear single-screw paddle composite wing cargo aircraft with the compound auxiliary wing and additional fin |
| CN108773485A (en) * | 2018-05-31 | 2018-11-09 | 江苏常探机器人有限公司 | The foldable composite wing manned vehicle of single vortex-spraying type afterwards |
| CN108791862A (en) * | 2018-05-31 | 2018-11-13 | 江苏常探机器人有限公司 | Double culverts push away the compound auxiliary wing and rear single culvert pushing-type composite wing manned vehicle of additional fin |
| CN108791869A (en) * | 2018-05-31 | 2018-11-13 | 江苏常探机器人有限公司 | With turbofan push away the compound auxiliary wing without back pressure formula composite wing manned vehicle |
| CN108820201A (en) * | 2018-05-31 | 2018-11-16 | 江苏常探机器人有限公司 | Rear single-screw paddle composite wing manned vehicle with the compound auxiliary wing of airscrew thrust |
| CN108820202A (en) * | 2018-05-31 | 2018-11-16 | 江苏常探机器人有限公司 | It is a kind of with the compound auxiliary wing of ducted fan without the compound rotor aircraft of back pressure formula |
| CN108839796A (en) * | 2018-05-31 | 2018-11-20 | 江苏常探机器人有限公司 | A kind of composite wing cargo aircraft of the compound auxiliary wing of twin screw thrust |
| CN108860593A (en) * | 2018-05-31 | 2018-11-23 | 江苏常探机器人有限公司 | Rear single ducted fan formula composite wing manned vehicle with solar energy additional fin |
| CN108928473A (en) * | 2018-05-31 | 2018-12-04 | 江苏常探机器人有限公司 | A kind of folding composite wing manned vehicle of the compound auxiliary wing of twin screw thrust |
| CN108945422A (en) * | 2018-05-31 | 2018-12-07 | 江苏常探机器人有限公司 | A kind of spiral shell with the auxiliary wing of twin screw and the attached wing pushes away composite wing airfreighter |
| CN113525680A (en) * | 2021-07-20 | 2021-10-22 | 中国空气动力研究与发展中心空天技术研究所 | Reconfigurable combined type unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180320 |
|
| WD01 | Invention patent application deemed withdrawn after publication |