CN207374658U - Both sides have the disc-shaped flying craft of the direction wing - Google Patents
Both sides have the disc-shaped flying craft of the direction wing Download PDFInfo
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- CN207374658U CN207374658U CN201720332990.8U CN201720332990U CN207374658U CN 207374658 U CN207374658 U CN 207374658U CN 201720332990 U CN201720332990 U CN 201720332990U CN 207374658 U CN207374658 U CN 207374658U
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Abstract
The utility model is suitable for vehicle technology field, disclosing a kind of both sides has the disc-shaped flying craft of the direction wing, including rack and be fixedly connected on the rack and in case shape the dish-shaped wing, the rack is connected with lifting system, and the lifting system is located at the lower section of the dish-shaped wing, the outer rim of the dish wing is provided with cricoid flap, the symmetrical both sides of flap are fixedly connected with the direction wing, the direction wing is longitudinally disposed, the rear end of the direction wing is provided with direction rudder plate, and the direction rudder plate is connected with direction control mechanism.A kind of both sides provided by the utility model have the disc-shaped flying craft of the direction wing, and the rear end of the direction wing of both sides is provided with direction rudder plate, and the direction rudder plate is connected with direction control mechanism, and to control the course of disc-shaped flying craft, mobility is good.
Description
Technical field
The utility model, which belongs to vehicle technology field more particularly to a kind of both sides, has the disc-shaped flying craft of the direction wing.
Background technology
Current disc-shaped flying craft, it is general using whole saucer-like configuration, it generally is equipped with lift driving device and pushes away
Force driving device, mobility is not good enough.
Utility model content
The purpose of the utility model is to overcome above-mentioned the deficiencies in the prior art, and providing a kind of both sides has the direction wing
Disc-shaped flying craft, mobility are good.
The technical solution of the utility model is:A kind of both sides have the disc-shaped flying craft of the direction wing, including rack and fixation
It is connected to the rack and in the dish-shaped wing of case shape, the rack is connected with lifting system, and the lift generates dress
Setting in the lower section of the dish-shaped wing, the outer rim of the dish wing is provided with cricoid flap, the flap symmetrical two
Side is fixedly connected with the direction wing, and the direction wing is longitudinally disposed, and the rear end of the direction wing is provided with direction rudder plate, the direction
Rudder plate is connected with direction control mechanism;The direction control mechanism uses hydraulic drive mechanism or mechanical driving structure, the dish
The shape wing, which corresponds to above the lifting system, is provided with through hole, and the through hole is provided with for described in opening and closing of fault
The mechanism for opening/closing of through hole.
Optionally, the wing that climbs is provided with below the dish-shaped wing, the wing that climbs is connected to the rack or the dish
The shape wing;The trailing edge of the wing that climbs is provided with trailing edge flap, and the rack is connected with cabin, and the wing that climbs is arranged at the machine
Cabin front or behind, alternatively, the wing that climbs is symmetrically arranged in the both sides of the cabin.
Optionally, the leading edge of the wing that climbs is provided with droope snoot.
Optionally, the lifting system includes engine or motor, and the lifting system is provided at least two
It is a, center symmetric setting of each lifting system along the dish-shaped wing.
Optionally, the rack is connected with to adjust the lift angular adjustment machine of the angle of the lifting system
Structure.
Optionally, the lower section of the dish-shaped wing sets at least two horizontal thrust devices, and each horizontal thrust device
With the dish-shaped wing center symmetric setting, the horizontal thrust device is connected to the machine by horizontal thrust angle adjusting mechanism
Frame.
Optionally, 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.
Optionally, the flap is away from above one end of the kuppe and is provided with empennage.
Optionally, the rack is connected with cabin, and the top of the cabin is passed through in the dish-shaped wing, the bottom of the cabin
Portion is connected with folding undercarriage, and the lower end of the undercarriage is provided with tire.
A kind of both sides provided by the utility model have the disc-shaped flying craft of the direction wing, the rear end of the direction wing of both sides
Direction rudder plate is provided with, the direction rudder plate is connected with direction control mechanism, to control the course of disc-shaped flying craft, mobility
It is good.
Description of the drawings
In order to illustrate more clearly of the technical scheme in the embodiment of the utility model, will make below to required in embodiment
Attached drawing is briefly described, it should be apparent that, the accompanying drawings in the following description is only some embodiments of the utility model,
For those of ordinary skill in the art, without creative efforts, can also be obtained according to these attached drawings
Other attached drawings.
Fig. 1 is the front view for the disc-shaped flying craft that a kind of both sides that the utility model embodiment provides have the direction wing;
Fig. 2 is the right view for the disc-shaped flying craft that a kind of both sides that the utility model embodiment provides have the direction wing;
Fig. 3 is the plan view for the disc-shaped flying craft that a kind of both sides that the utility model embodiment provides have the direction wing;
Fig. 4 is the top view for the disc-shaped flying craft that a kind of both sides that the utility model embodiment provides have the direction wing;
Fig. 5 is the bottom view for the disc-shaped flying craft that a kind of both sides that the utility model embodiment provides have the direction wing.
Specific embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, is further elaborated the utility model.It should be appreciated that specific embodiment described herein is only used to explain
The utility model is not used to limit the utility model.
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.
It should also be noted that, the orientation term such as left and right, upper and lower in the utility model embodiment, is only opposite each other
Concept or using the normal operating condition of product as reference, and should not be regarded as restrictive.
As depicted in figs. 1 and 2, a kind of both sides that the utility model embodiment provides have the disc-shaped flying craft of the direction wing,
Including rack 16 and the dish-shaped wing 1 for being fixedly connected on the rack 16, the dish wing 1 arches upward in case shape and upward arc,
The rack 16 is connected with lifting system 2, and the lifting system 2 is located at the lower section of the dish-shaped wing 1, the dish
The outer rim of the wing 1 is provided with cricoid flap 5, and the 5 symmetrical both sides of flap are fixedly connected with the direction wing 9, the direction
The wing 9 is longitudinally disposed, and the rear end of the direction wing 9 is provided with direction rudder plate 10, and the direction rudder plate 10 is connected with direction controlling machine
Hydraulic drive mechanism or mechanical driving structure may be employed in structure, direction control mechanism, motor-driven to control the course of disc-shaped flying craft
Excellent performance may be used as unmanned plane or manned vehicle.
Specifically, the lower section of the dish-shaped wing 1 is provided with the wing 3 that climbs, and the wing 3 that climbs is connected to the rack 16 or institute
State the dish-shaped wing 1;The trailing edge for climbing the wing 3 is provided with trailing edge flap 15, and the rack 16 is connected with cabin 4, the wing that climbs
3 are arranged at 4 front or behind of cabin, alternatively, the wing 3 that climbs is symmetrically arranged in the both sides of the cabin 4, climb
The wing 3 and trailing edge flap 15 can provide lift when disc-shaped flying craft has horizontal velocity, and the horizontal velocity of disc-shaped flying craft is got over
Height, the lift obtained is bigger, and the energy consumption smaller of disc-shaped flying craft, the accelerating ability of disc-shaped flying craft are made under square one
With respect to higher, the mobility of disc-shaped flying craft is high.
Specifically, the leading edge for climbing the wing 3 is provided with droope snoot, to further improve the mobility of disc-shaped flying craft
Energy.
Specifically, the flap 5 is in a ring.The outer of the flap 5 is in tooth shape, in the present embodiment, the water conservancy diversion
The bottom of the wing 5 is provided with from the inclined-plane that outer rim is downwardly inclined, i.e., the lower face of described flap 5 and at 5 periphery of flap
The ramp structure for reducing 5 thickness of flap is provided with, by setting flap 5, both improves disc-shaped flying craft
Flight stability, and reduce flight resistance, optimize the aerodynamic performance of disc-shaped flying craft, reduced under square one
Energy consumption.
Specifically, the top of the cabin 4 is piercing in the center of the dish-shaped wing 1, the rack 16 or the cabin 4
Bottom is connected with undercarriage 6, and undercarriage 6 is connected with tire 7.Cabin 4 can be provided with multilayer, to accommodate equipment, occupant etc..Tool
In body application, the upper strata of cabin 4 can be crew module, and middle level or lower floor can be equipment compartment, cargo hold etc..The top of cabin 4 can
Think spherical structure, resistance is small.The bottom of cabin 4 or spherical structure, further to reduce resistance.
Specifically, the lifting system 2 can include engine or motor, and the lifting system 2 is provided with
At least two, each lifting system 2 is along dish-shaped 1 center symmetric setting of the wing.In the present embodiment, lifting system
2 are provided with 4, uniformly distributed with 90 degree of heart septum in the dish-shaped wing 1.Lifting system 2 can be entirely engine, can also be complete
Portion is motor, can also half be engine, half is motor, and engine and motor alternate setting.
Specifically, the rack 16 is connected with to adjust the lift angular adjustment of the angle of the lifting system 2
Mechanism.Lifting system 2 can be adjusted to longitudinally perpendicular state, transverse horizontal state or 45 degree of oblique angularly states.It rises
When force generating apparatus 2 is adjusted to longitudinally perpendicular state, disc-shaped flying craft can be made quickly to go up to the air, the landing time is short.Lift generates
When device 2 is adjusted to transverse horizontal state, disc-shaped flying craft can be made to obtain the horizontal thrust of bigger, level speed is fast, horizontal
Acceleration is high.When lifting system 2 is adjusted to 45 degree of oblique states, can improve the standard speed when taking off, to be suitable for
Different use occasions and requirement.Mechanical rotation device or hydraulic gear can be used in lift angle adjusting mechanism.
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 with 1 center symmetric setting of the dish-shaped wing.Horizontal thrust device 8 is between the both direction wing 9.In the present embodiment, water
There are two flat-pushing power apparatus 8 is set, and positioned at the both sides of cabin 4.
Specifically, the horizontal thrust device 8 is connected to the rack 16, water by horizontal thrust angle adjusting mechanism
Flat-pushing power apparatus 8 can horizontally rotate, and can also vertically rotate.Mechanical rotation device can be used in horizontal thrust angle adjusting mechanism
Or hydraulic gear.
In the present embodiment, two direction wings 9 are located at respectively outside the both sides of the wing 3 that climbs, i.e., the direction wing 9 with climb
The direction of the front end of the wing 3 is identical (facing forward), without changing the horizontal thrust direction of horizontal thrust device 8, can also fly dish
Row device change of flight direction.If cooperation changes the horizontal thrust direction in 8 direction of horizontal thrust device, disc-shaped flying craft can be made more
Add maneuverability.
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, avoid the formation of turbulent flow.Kuppe 11 can be monolithic construction, may be set to be liftable
After the lift-off of expansion, i.e. disc-shaped flying craft, 11 drops down of kuppe, 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, is flown with improving
Capable stability.I.e. kuppe 11 is located at front end, and empennage 12 is located at rear end, and the both direction wing 9 is respectively arranged at the left and right sides.
Specifically, the top that the dish-shaped wing 1 corresponds to the lifting system 2 is provided with through hole 13, the through hole
The mechanism for opening/closing 14 for through hole described in opening and closing of fault 13 is provided at 13.Rising when needing lift, mechanism for opening/closing
14 can make through hole 13 be held in opening.It puts down and flies when lift is not required in the air, mechanism for opening/closing 14 can make through hole
13 are held in closed state, avoid the formation of turbulent flow, to reduce air drag.
The disc-shaped flying craft that the utility model embodiment is provided, the rear end of the direction wing 9 of 5 both sides of flap are provided with
Direction rudder plate 10, the direction rudder plate 10 are connected with direction control mechanism, to control the course of disc-shaped flying craft, mobility
It is good.
The above is only the preferred embodiment of the utility model only, is not intended to limit the utility model, all at this
Any modification, equivalent substitution or improvement made within the spirit and principle of utility model etc., should be included in the utility model
Protection domain within.
Claims (9)
1. a kind of both sides have the disc-shaped flying craft of the direction wing, which is characterized in that including rack and are fixedly connected on the rack
And in the dish-shaped wing of case shape, the rack is connected with lifting system, and the lifting system is located at the dish
The lower section of the wing, the outer rim of the dish wing are provided with cricoid flap, the symmetrical both sides side of being fixedly connected with of flap
Guide vane, the direction wing is longitudinally disposed, and the rear end of the direction wing is provided with direction rudder plate, and the direction rudder plate is connected with direction
Control mechanism;The direction control mechanism uses hydraulic drive mechanism or mechanical driving structure, and the dish wing corresponds to described
Through hole is provided with above lifting system, the through hole is provided with for the headstock gear of through hole described in opening and closing of fault
Structure.
2. both sides as described in claim 1 have the disc-shaped flying craft of the direction wing, which is characterized in that the lower section of the dish wing
The wing that climbs is provided with, the wing that climbs is connected to the rack or the dish-shaped wing;The trailing edge of the wing that climbs is provided with trailing edge
Wing flap, the rack are connected with cabin, and the wing that climbs is arranged at the cabin front or behind, alternatively, the wing point that climbs
The both sides of the cabin are not symmetrically disposed on.
3. both sides as claimed in claim 2 have the disc-shaped flying craft of the direction wing, which is characterized in that the leading edge of the wing that climbs
It is provided with droope snoot.
4. both sides as described in claim 1 have the disc-shaped flying craft of the direction wing, which is characterized in that the lifting system
Including engine or motor, the lifting system is provided at least two, and each lifting system is along the dish
The center symmetric setting of the wing.
5. both sides as described in claim 1 have the disc-shaped flying craft of the direction wing, which is characterized in that the rack connection is useful
In the lift angle adjusting mechanism for the angle for adjusting the lifting system.
6. both sides have the disc-shaped flying craft of the direction wing according to any one of claims 1 to 4, which is characterized in that described
The lower section of the dish-shaped wing sets at least two horizontal thrust devices, and each horizontal thrust device is with the dish-shaped wing central symmetry
It sets, the horizontal thrust device is connected to the rack by horizontal thrust angle adjusting mechanism.
7. both sides have the disc-shaped flying craft of the direction wing according to any one of claims 1 to 4, which is characterized in that described
Kuppe is provided with below flap, two direction wings are symmetrical arranged centered on the kuppe, the kuppe
Front end shape at an acute angle or arc.
8. both sides as claimed in claim 7 have the disc-shaped flying craft of the direction wing, which is characterized in that the flap is away from
Empennage is provided with above one end of the kuppe.
9. both sides have the disc-shaped flying craft of the direction wing according to any one of claims 1 to 4, which is characterized in that described
Rack is connected with cabin, and the top of the cabin is passed through in the dish-shaped wing, and the bottom of the cabin is connected with folding
Fall frame, the lower end of the undercarriage is provided with tire.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201720332990.8U CN207374658U (en) | 2017-03-31 | 2017-03-31 | Both sides have the disc-shaped flying craft of the direction wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201720332990.8U CN207374658U (en) | 2017-03-31 | 2017-03-31 | Both sides have the disc-shaped flying craft of the direction wing |
Publications (1)
Publication Number | Publication Date |
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CN207374658U true CN207374658U (en) | 2018-05-18 |
Family
ID=62297461
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201720332990.8U Active CN207374658U (en) | 2017-03-31 | 2017-03-31 | Both sides have the disc-shaped flying craft of the direction wing |
Country Status (1)
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CN (1) | CN207374658U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109250110A (en) * | 2018-07-26 | 2019-01-22 | 合肥学院 | A kind of scenic spot flying robot |
-
2017
- 2017-03-31 CN CN201720332990.8U patent/CN207374658U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109250110A (en) * | 2018-07-26 | 2019-01-22 | 合肥学院 | A kind of scenic spot flying robot |
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Legal Events
Date | Code | Title | Description |
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GR01 | Patent grant | ||
GR01 | Patent grant | ||
TR01 | Transfer of patent right |
Effective date of registration: 20211231 Address after: 518000 floor 1, building 30, chentian Industrial Zone, chentian community, Xixiang street, Bao'an District, Shenzhen, Guangdong Province Patentee after: BITEMAN TECHNOLOGY Co.,Ltd. Address before: 518000 Haifeng Pavilion 1-4C, Baocheng West Coast Garden, Bao'an District, Shenzhen City, Guangdong Province Patentee before: Guo Yinghui |
|
TR01 | Transfer of patent right |