CN106986029A - Disc-shaped flying craft - Google Patents
Disc-shaped flying craft Download PDFInfo
- Publication number
- CN106986029A CN106986029A CN201710209314.6A CN201710209314A CN106986029A CN 106986029 A CN106986029 A CN 106986029A CN 201710209314 A CN201710209314 A CN 201710209314A CN 106986029 A CN106986029 A CN 106986029A
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- CN
- China
- Prior art keywords
- wing
- shaped
- disc
- flying craft
- dish
- 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.)
- Granted
Links
- 230000007246 mechanism Effects 0.000 claims description 18
- 230000001154 acute effect Effects 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims 1
- 230000001133 acceleration Effects 0.000 abstract description 5
- 238000005516 engineering process Methods 0.000 abstract description 3
- 108010066278 cabin-4 Proteins 0.000 description 10
- 230000008450 motivation Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000009194 climbing Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 210000003361 heart septum Anatomy 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
- B64C39/062—Aircraft not otherwise provided for having disc- or ring-shaped wings having annular wings
-
- 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
- B64C27/28—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The present invention is applied to vehicle technology field, disclose a kind of disc-shaped flying craft, including frame and be fixedly connected on the frame and in case shape the dish-shaped wing, the outer rim of the dish-shaped wing is provided with the flap of ring-type, the frame is connected with lifting system, and the lifting system is provided with the wing that climbs below the lower section of the dish-shaped wing, the dish-shaped wing.A kind of disc-shaped flying craft provided by the present invention, the wing that climbs with the dish-shaped wing and below the dish-shaped wing, lift can be provided when disc-shaped flying craft has horizontal velocity, the horizontal velocity of disc-shaped flying craft is higher, the lift that it is obtained is bigger, make the energy resource consumption of disc-shaped flying craft smaller under square one, the acceleration of disc-shaped flying craft is relatively higher, the mobility of disc-shaped flying craft is high.
Description
Technical field
The invention belongs to vehicle technology field, more particularly to a kind of disc-shaped flying craft.
Background technology
Current disc-shaped flying craft, it is general using overall saucer-like configuration, and it generally is equipped with lift drive device and pushed away
Force driving device, its energy resource consumption is big and mobility is not good enough.
The content of the invention
It is an object of the invention to overcome above-mentioned the deficiencies in the prior art, there is provided a kind of disc-shaped flying craft, its its energy
Consumption is small and mobility is good.
The technical scheme is that：A kind of disc-shaped flying craft, including frame and be fixedly connected on the frame and in cover
The dish-shaped wing of shelly, the outer rim of the dish-shaped wing is provided with the flap of ring-type, and the frame is connected with lifting system, and
The lifting system, which is located at below the lower section of the dish-shaped wing, the dish-shaped wing, is provided with the wing that climbs.
Alternatively, the trailing edge of the wing that climbs is provided with trailing edge flap, and the frame is connected with cabin, and the wing that climbs is set
The cabin front or behind is placed in, or, the wing that climbs respectively symmetrically is arranged at the both sides of the cabin.
Alternatively, the leading edge of the wing that climbs is provided with droope snoot.
Alternatively, the frame is connected with the lift angular adjustment machine of the angle for adjusting the lifting system
Structure.
Alternatively, the lifting system includes engine or motor, and the lifting system is provided with least two
Individual, Central Symmetry of each lifting system along the dish-shaped wing is set.
Alternatively, the symmetrical both sides of the flap are fixedly connected with the direction wing, and two direction wings are located at respectively
Outside the both sides of the wing that climbs, the rear end of the direction wing is provided with direction rudder plate, and the direction rudder plate is connected with direction controlling
Mechanism.
Alternatively, the lower section of the dish-shaped wing sets at least two horizontal thrust devices, and each horizontal thrust device
Set with the dish-shaped wing Central Symmetry, the horizontal thrust device is connected to the machine by horizontal thrust angle adjusting mechanism
Frame.
Alternatively, kuppe is provided with below the flap, two direction wings are centered on the kuppe
It is symmetrical arranged, the front end shape at an acute angle or arc of the kuppe.
Alternatively, the flap is away from above one end of the kuppe and is provided with empennage.
Alternatively, it is characterised in that the dish-shaped wing, which corresponds to above the lifting system, is provided with through hole, institute
State through hole and be connected with removable cover, the removable cover is connected with what is rotated or move for driving the removable cover
Open-close driving mechanism.
A kind of disc-shaped flying craft provided by the present invention, the wing that climbs with the dish-shaped wing and below the dish-shaped wing, climbs
The wing and trailing edge flap can provide lift when disc-shaped flying craft has horizontal velocity, and the horizontal velocity of disc-shaped flying craft is higher,
The lift that it is obtained is bigger, makes the energy resource consumption of disc-shaped flying craft smaller under square one, the acceleration phase of disc-shaped flying craft
To higher, the mobility height of disc-shaped flying craft.
Brief description of the drawings
Technical scheme in order to illustrate the embodiments of the present invention more clearly, below by using required in embodiment
Accompanying drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the present invention, for ability
For the those of ordinary skill of domain, on the premise of not paying creative work, it can also be obtained according to these accompanying drawings other attached
Figure.
Fig. 1 is a kind of front view of disc-shaped flying craft provided in an embodiment of the present invention；
Fig. 2 is a kind of right view of disc-shaped flying craft provided in an embodiment of the present invention；
Fig. 3 is a kind of plan view of disc-shaped flying craft provided in an embodiment of the present invention；
Fig. 4 is a kind of top view of disc-shaped flying craft provided in an embodiment of the present invention；
Fig. 5 is a kind of upward view of disc-shaped flying craft provided in an embodiment of the present invention.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
It should be noted that when element is referred to as " being fixed on " or " being arranged at " another element, it can be directly another
On one element or it may be simultaneously present centering elements.When an element is known as " being connected to " another element, it can
To be directly to another element or may be simultaneously present centering elements.
Only it is relative concept each other it should also be noted that, the orientation term such as left and right, upper and lower in the embodiment of the present invention
Or using the normal operating condition of product as reference, and should not be regarded as restrictive.
As shown in Figures 1 to 5, a kind of disc-shaped flying craft provided in an embodiment of the present invention, including frame 16 be fixedly connected
In the dish-shaped wing 1 of the frame 16, the dish-shaped wing 1 is in the case shape (UFO-like) that upward arc arches upward, and the frame 16 connects
Lifting system 2 is connected to, the lifting system 2 is located at the lower section of the dish-shaped wing 1, and the lower section of the dish-shaped wing 1 is set
The wing 3 that climbs is equipped with, the wing 3 that climbs provides lift when disc-shaped flying craft has horizontal velocity, the horizontal velocity of disc-shaped flying craft is got over
Height, the lift that it is obtained is bigger, makes the energy resource consumption of disc-shaped flying craft smaller under square one, the acceleration of disc-shaped flying craft
Relatively higher, the mobility of disc-shaped flying craft is high, may be used as unmanned plane or manned vehicle.
Specifically, the wing 3 that climbs can be connected to the frame 16 or the dish-shaped wing 1；The trailing edge of the wing 3 that climbs
Be provided with trailing edge flap 15, the frame 16 is connected with cabin 4, the wing 3 that climbs be arranged at the front of the cabin 4 or after
Side, or, the wing 3 that climbs respectively symmetrically is arranged at the both sides of the cabin 4, and the mobility of disc-shaped flying craft is high.
Specifically, the leading edge for climbing the wing 3 is provided with droope snoot (not shown), is flown with further improving dish
The mobility of row device.
Specifically, the edge of the dish-shaped wing 1 sets flap 5, and the flap 5 is in a ring.Outside the flap 5
Along being in tooth shape, in the present embodiment, the bottom of the flap 5 is provided with the inclined-plane being downwardly inclined from outer rim, the flap 5
The ramp structure for reducing the thickness of flap 5 is provided with lower surface and the close periphery of flap 5, is led by setting
The wing 5 is flowed, the flight stability of disc-shaped flying craft had both been improved, flight resistance is reduced again, and optimized the air of disc-shaped flying craft
Energy resource consumption is reduced under dynamic performance, square one.
Specifically, the top of the cabin 4 is piercing in the center of the dish-shaped wing 1, the frame 16 or the cabin 4
Bottom is connected with folding undercarriage 6, and the lower end of the undercarriage 6 is provided with tire 7.Cabin 4 can be provided with multilayer, with
Accommodate equipment, occupant etc..In concrete application, the upper strata of cabin 4 can be crew module, and middle level or lower floor can be equipment compartment, goods
Cabin etc..The top of cabin 4 can be spherical structure, and its resistance is small.The bottom of cabin 4 can also be spherical structure, with further
Reduce resistance.
Specifically, the lifting system 2 can include engine or/and motor, and the lifting system 2 is set
Have at least two, each lifting system 2 is set along the dish-shaped Central Symmetry of the wing 1.In the present embodiment, lift produces dress
Put 2 and be provided with 4, it is uniform with 90 degree of heart septum in the dish-shaped wing 1.Lifting system 2 can be entirely that engine (send out by jet
Motivation), can also be entirely motor, can also half be engine, half is motor, and engine and motor are alternated and set
Put.
Specifically, the frame 16 is connected with the lift angular adjustment of the angle for adjusting the lifting system 2
Mechanism (not shown), makes the adjustable angle of lifting system 2.Lifting system 2 can be adjusted to longitudinally perpendicular shape
State, transverse horizontal state or 45 degree of oblique angularly states.When lifting system 2 is adjusted to longitudinally perpendicular state, it can make
Disc-shaped flying craft quickly goes up to the air, and the landing time is short.It when lifting system 2 is adjusted to transverse horizontal state, can fly dish
Row device obtains bigger horizontal thrust, and level speed is fast, and horizontal acceleration is high.Lifting system 2 is adjusted to 45 degree of oblique shapes
During state, can improve the standard speed when taking off, with suitable for different use occasion and requirement.
Specifically, the lower section of the dish-shaped wing 1 sets at least two horizontal thrust devices 8, and each horizontal thrust dress
8 are put to set with the dish-shaped Central Symmetry of the wing 1.Horizontal thrust device 8 is located between the both direction wing.In the present embodiment, level
Thrust device 8 is provided with two, and is respectively symmetrically arranged at the both sides of cabin 4.Horizontal thrust device 8 can for jet engine or
It is connected with the motor of propeller.
Specifically, the horizontal thrust device 8 is connected to the frame 16, level by horizontal thrust angle adjusting mechanism
Thrust device 8 can horizontally rotate, and can also vertically rotate.
Specifically, lift angle adjusting mechanism can use mechanical rotation device or hydraulic gear.Horizontal thrust angle
Governor motion can use mechanical rotation device or hydraulic gear.
Specifically, the symmetrical both sides of the flap 5 are provided with the direction wing 9, and two direction wings 9 are located at institute respectively
Outside the both sides for stating the wing 3 that climbs, i.e., the direction wing 9 is identical with the direction of the front end for the wing 3 that climbs (facing forward), the rear end of the direction wing 9
Direction rudder plate 10 is provided with, the direction rudder plate 10 is connected with direction control mechanism, and direction control mechanism can be driven using hydraulic pressure
Motivation structure or mechanical driving structure, to control the course of disc-shaped flying craft, mobility is good.With quick regulation disc-shaped flying craft
Heading, the horizontal thrust direction without changing horizontal thrust device 8, can also make disc-shaped flying craft change of flight direction.
If coordinating the horizontal thrust direction for changing the direction of horizontal thrust device 8, disc-shaped flying craft more maneuverability can be made.
Specifically, the lower section of the flap 5 is provided with kuppe 11, and kuppe 11 is located in the front end of disc-shaped flying craft
Centre, two direction wings 9 symmetrical longitudinally disposed, front end shape at an acute angle of the kuppe 11 centered on the kuppe 11
Or arc, to reduce gas-flow resistance, it is to avoid form turbulent flow.Kuppe 11 can be monolithic construction, it can also be provided that liftable
After the lift-off of expansion, i.e. disc-shaped flying craft, the drops down of kuppe 11, water conservancy diversion area is big, and water conservancy diversion is better.
Specifically, the flap 5 is away from above one end of the kuppe 11 and is provided with empennage 12, winged to improve
Capable stability.I.e. kuppe 11 is located at the front end of disc-shaped flying craft, and empennage 12 is located at rear end, and the both direction wing 9 is set respectively
In the left and right sides.
Specifically, the dish-shaped wing 1 is provided with through hole 13, the through hole corresponding to the top of the lifting system 2
Removable cover 14 is connected with 13, the removable cover 14 is connected with for driving the removable cover 14 to rotate or mobile
Open-close driving mechanism.When rising etc. needs lift, open-close driving mechanism can drive removable cover 14 to protect through hole 13
It is held in opening.When flat winged grade does not need lift in the air, open-close driving mechanism can drive removable cover 14 to make through hole
13 are held in closed state, it is to avoid form turbulent flow, to reduce air drag, energy resource consumption is small, may be used as unmanned plane or manned
Aircraft.
Specifically, the removable cover 14 can be rotationally connected with the dish-shaped wing 1, the open-close driving mechanism by bearing pin
Including the biography for being connected to the motor or motor of the removable cover 14 and being connected between the motor and the removable cover 14
Dynamic component.Removable cover 14 can open or close through hole 13 along the surface pivots of the dish-shaped wing 1, can also be opened by upset
Or close through hole 13.
Or, removable cover 14 can also be connected to the dish-shaped wing 1 by line slide rail, and the open-close driving mechanism can
For straight-line motion mechanism, such as linear electric motors, hydraulic component, rack-and-pinion, screw body.Certainly, removable cover 14 can be with
It is designed as the structure types such as shutter.
The disc-shaped flying craft that the embodiment of the present invention is provided, it has the dish-shaped wing 1 and the wing that climbs positioned at the dish-shaped lower section of the wing 1
3, climb the wing 3 and trailing edge flap can provide lift, the level speed of disc-shaped flying craft when disc-shaped flying craft has horizontal velocity
Degree is higher, and the lift that it is obtained is bigger, makes the energy resource consumption of disc-shaped flying craft smaller under square one, the acceleration of disc-shaped flying craft
Performance is relatively higher, and the mobility of disc-shaped flying craft is high.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
Any modification, equivalent substitution or improvement made within refreshing and principle etc., should be included in the scope of the protection.
Claims (10)
1. a kind of disc-shaped flying craft, it is characterised in that including frame and be fixedly connected on the frame and in the dish of case shape
The wing, the outer rim of the dish-shaped wing is provided with the flap of ring-type, and the frame is connected with lifting system, and the lift is produced
Generating apparatus, which is located at below the lower section of the dish-shaped wing, the dish-shaped wing, is provided with the wing that climbs.
2. disc-shaped flying craft as claimed in claim 1, it is characterised in that the trailing edge of the wing that climbs is provided with trailing edge flap,
The frame is connected with cabin, and the wing that climbs is arranged at the cabin front or behind, or, it is described to climb the wing respectively symmetrically
It is arranged at the both sides of the cabin.
3. disc-shaped flying craft as claimed in claim 1, it is characterised in that the leading edge of the wing that climbs is provided with droope snoot.
4. disc-shaped flying craft as claimed in claim 1, it is characterised in that the frame is connected with for adjusting the lift production
The lift angle adjusting mechanism of the angle of generating apparatus.
5. disc-shaped flying craft as claimed in claim 1, it is characterised in that the lifting system includes engine or electricity
Machine, the lifting system is provided with least two, and Central Symmetry of each lifting system along the dish-shaped wing is set
Put.
6. disc-shaped flying craft as claimed in claim 1, it is characterised in that the symmetrical both sides side of being fixedly connected with of flap
Guide vane, and two direction wings are located at outside the both sides of the wing that climbs respectively, the rear end of the direction wing is provided with rudder
Plate, the direction rudder plate is connected with direction control mechanism.
7. the disc-shaped flying craft as any one of claim 1 to 6, it is characterised in that the lower section of the dish-shaped wing is set
At least two horizontal thrust devices, and each horizontal thrust device, with the dish-shaped wing Central Symmetry setting, the level is pushed away
Power apparatus is connected to the frame by horizontal thrust angle adjusting mechanism.
8. the disc-shaped flying craft as any one of claim 1 to 6, it is characterised in that the lower section of the flap is set
Have kuppe, two direction wings are symmetrical arranged centered on the kuppe, the front end shape at an acute angle of the kuppe or
Arc.
9. disc-shaped flying craft as claimed in claim 8, it is characterised in that the flap is away from one end of the kuppe
Top be provided with empennage.
10. the disc-shaped flying craft as any one of Claims 1-4, it is characterised in that the dish-shaped wing corresponds to described
Through hole is provided with above lifting system, the through hole is connected with removable cover, and the removable cover is connected with
For driving the removable cover rotation or mobile open-close driving mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710209314.6A CN106986029B (en) | 2017-03-31 | 2017-03-31 | Dish-shaped aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710209314.6A CN106986029B (en) | 2017-03-31 | 2017-03-31 | Dish-shaped aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106986029A true CN106986029A (en) | 2017-07-28 |
| CN106986029B CN106986029B (en) | 2024-01-12 |
Family
ID=59416354
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710209314.6A Active CN106986029B (en) | 2017-03-31 | 2017-03-31 | Dish-shaped aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106986029B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111409820A (en) * | 2020-03-31 | 2020-07-14 | 兰安德 | Propelling device in air and propelling method thereof |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1997012805A1 (en) * | 1995-10-04 | 1997-04-10 | Amorim Gagliardi Madeira Jonat | Aerodisk - atmospheric aeronautical vehicle |
| CN102582834A (en) * | 2012-03-09 | 2012-07-18 | 北京工业大学 | Saucer-shaped aircraft |
| CN202703888U (en) * | 2012-05-28 | 2013-01-30 | 严云北 | Fly ball with dish-shaped wing |
| CN204507260U (en) * | 2015-03-30 | 2015-07-29 | 河南金原碟科技有限公司 | A kind of dish-shaped manned quadrotor |
| CN106005402A (en) * | 2016-06-18 | 2016-10-12 | 夏建国 | Flying saucer type hypersonic stealth jet aircraft capable of realizing vertical take-off and landing |
| CN207015584U (en) * | 2017-03-31 | 2018-02-16 | 郭应辉 | Disc-shaped flying craft |
-
2017
- 2017-03-31 CN CN201710209314.6A patent/CN106986029B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1997012805A1 (en) * | 1995-10-04 | 1997-04-10 | Amorim Gagliardi Madeira Jonat | Aerodisk - atmospheric aeronautical vehicle |
| CN102582834A (en) * | 2012-03-09 | 2012-07-18 | 北京工业大学 | Saucer-shaped aircraft |
| CN202703888U (en) * | 2012-05-28 | 2013-01-30 | 严云北 | Fly ball with dish-shaped wing |
| CN204507260U (en) * | 2015-03-30 | 2015-07-29 | 河南金原碟科技有限公司 | A kind of dish-shaped manned quadrotor |
| CN106005402A (en) * | 2016-06-18 | 2016-10-12 | 夏建国 | Flying saucer type hypersonic stealth jet aircraft capable of realizing vertical take-off and landing |
| CN207015584U (en) * | 2017-03-31 | 2018-02-16 | 郭应辉 | Disc-shaped flying craft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111409820A (en) * | 2020-03-31 | 2020-07-14 | 兰安德 | Propelling device in air and propelling method thereof |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106986029B (en) | 2024-01-12 |
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