CN206734629U - A kind of disk aircraft - Google Patents
A kind of disk aircraft Download PDFInfo
- Publication number
- CN206734629U CN206734629U CN201720079890.9U CN201720079890U CN206734629U CN 206734629 U CN206734629 U CN 206734629U CN 201720079890 U CN201720079890 U CN 201720079890U CN 206734629 U CN206734629 U CN 206734629U
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- fuselage
- aircraft
- disk
- ducted
- ducted fan
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Abstract
A kind of disk aircraft, include the fuselage of flat, the fuselage vertical direction is provided with more than one ducted fan, and fuselage is arranged to reduce windage when flat preceding can fly, and keeps the higher speed of a ship or plane.Less windage can be improved the wind loading rating of disk aircraft.Some ducted fans are provided with aircraft, can be by controlling the rotating speeds of different ducted fans, so as to provide the power of flight and can control flight attitude, this roudnel aircraft flies before can possessing and spot hover ability, and can also improve wind loading rating when hovering.
Description
Technical field
Airmanship field is the utility model is related to, more particularly to a kind of disk aircraft.
Background technology
At present, what vehicle technology was more ripe mainly has fixed wing aircraft, rotary wings class helicopter, rocket and hot gas
The aircraft such as ball, existing aircraft can not mostly ensure spot hover, determine although multi-rotor aerocraft can provide
Point hovering, but more rotor unmanned aircrafts are because have larger windage, therefore when wind speed is more than 5 meter per second, be not easy to ensure just
Normal spot hover, carry out wind resistance in order to which spot hover must tilt fuselage, and inclined result makes its wind area just bigger, i.e., more
It is not easy to keep spot hover.
Utility model content
The purpose of this utility model be to provide it is a kind of can fly in the past and the disk aircraft of spot hover, there is wind resistance energy
Power is strong and the characteristics of can stablizing spot hover.
Above-mentioned purpose of the present utility model technical scheme is that：
A kind of disk aircraft, includes the fuselage of flat, and the fuselage vertical direction is provided with some ducted fans；
The quantity of the ducted fan and Ye Shan is 6；
Deflectable leaf coral is provided with below the ducted fan；
The body upper is provided with least one empennage；
The upper and lower part of the fuselage is raised to be set, and the height of projection of bottom is less than the height of projection on top.
As improvement of the present utility model, undercarriage is provided with below the fuselage.
As improvement of the present utility model, the undercarriage can be retracted into fuselage.
In summary, fuselage is arranged to reduce windage when flat can move ahead, and keeps the higher speed of a ship or plane, less windage
It can be improved the wind loading rating of disk aircraft, some ducted fans are provided with aircraft, can be by controlling not
With the rotating speed of ducted fan, wind resistance can also be improved so as to provide the power of flight and flight attitude can be controlled, during hovering
Ability.
Brief description of the drawings
Fig. 1 is aircraft shaft side figure one；
Fig. 2 is aircraft shaft side figure two；
Fig. 3 is aircraft upward view；
Fig. 4 is Fig. 3 A-A diagrammatic cross-sections.
In figure, 1, fuselage；2nd, ducted fan；3rd, empennage；4th, undercarriage；5th, deflectable leaf coral.
Embodiment
The utility model is described in further detail below in conjunction with accompanying drawing.
Shown in reference picture 1-4, a kind of disk aircraft includes the fuselage 1 of flat, and the upper and lower part of fuselage 1 is respectively provided with
For convex, and the height of the convex of bottom is less than the height of top convex, and the vertical direction of fuselage 1 is provided with 6 ducted fans 2,
The lower section of ducted fan 2 is provided with deflectable leaf coral 5, and the lower section of fuselage 1 is provided with some retractable undercarriages 4（It can refer to
The undercarriage 4 of aircraft）.
The upper and lower part of aircraft is disposed as convex, in-flight this shape will produce lift in the air, this part
Lift is to confirm that this is one and changed with flying speed through theoretical calculation and wind-tunnel flyoff according to designed cross sectional shape
And the amount changed.The lift that this power provides will provide contribution to flying power system, reduce the consumption of fuel oil and electric power, due to
Its streamlined design can keep the higher speed of a ship or plane, increase voyage.
The controllable deflection palisade blade in deflectable direction is housed in the bottom of each ducted fan 2, deflection leaf coral is to inclined
Turn the direction that ducted fan 2 discharges downwards gas.
The ducted fan 2 that roudnel aircraft is equipped not only provides power when hovering, landing, is also preceding winged offer flight
Power.
Also disk flying instrument can also be arranged to folding and unfolding at least one empennage 3 for adjustment direction, certain empennage 3
Formula, when flying before needs, empennage 3 is automatic spring, and the aerodynamic force caused by the flexible empennage 3 controls flying saucer heading.
When disk aircraft is as hovering flight device, flexible empennage 3 will can be packed up, flying saucer own rotation now and move left and right
Leaf grating is deflected by ducted fan 2 to provide.
This specific embodiment is only that it is not to limitation of the present utility model, ability to explanation of the present utility model
Field technique personnel can make the modification of no creative contribution to the present embodiment as needed after this specification is read, but
As long as all protected in right of the present utility model by Patent Law.
Claims (3)
- A kind of 1. disk aircraft, it is characterised in that：Fuselage (1) including flat, fuselage (1) vertical direction are provided with Some ducted fans (2)；The quantity of the ducted fan (2) and leaf coral (5) is 6；Deflectable leaf coral (5) is provided with below the ducted fan (2)；At least one empennage (3) is provided with above the fuselage (1)；The upper and lower part of the fuselage (1) is raised to be set, and the height of projection of bottom is less than the height of projection on top.
- A kind of 2. disk aircraft according to claim 1, it is characterised in that：It has been provided with below the fuselage (1) Fall frame (4).
- A kind of 3. disk aircraft according to claim 2, it is characterised in that：The undercarriage (4) can be retracted into machine In body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720079890.9U CN206734629U (en) | 2017-01-21 | 2017-01-21 | A kind of disk aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720079890.9U CN206734629U (en) | 2017-01-21 | 2017-01-21 | A kind of disk aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206734629U true CN206734629U (en) | 2017-12-12 |
Family
ID=60554724
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720079890.9U Active CN206734629U (en) | 2017-01-21 | 2017-01-21 | A kind of disk aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206734629U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108995808A (en) * | 2018-08-31 | 2018-12-14 | 耿天侃 | It can the annular wing disc-shaped flying craft that can hover of VTOL |
| CN113581475A (en) * | 2021-08-31 | 2021-11-02 | 王智强 | Circular disc wing solar electric airplane |
-
2017
- 2017-01-21 CN CN201720079890.9U patent/CN206734629U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108995808A (en) * | 2018-08-31 | 2018-12-14 | 耿天侃 | It can the annular wing disc-shaped flying craft that can hover of VTOL |
| CN113581475A (en) * | 2021-08-31 | 2021-11-02 | 王智强 | Circular disc wing solar electric airplane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20181122 Address after: 100020 No. 1901, 39th floor, Zhongzhili, Chaoyang District, Beijing Patentee after: Shen Guanqing Address before: 102300 room 2-3, 154 Cheng Zi street, Mentougou District, Beijing. Patentee before: BEIJING ZHENGXING HONGYE METAL MATERIAL CO., LTD. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190131 Address after: 102300 room 2-3, 154 Cheng Zi street, Mentougou District, Beijing. Patentee after: BEIJING ZHENGXING HONGYE METAL MATERIAL CO., LTD. Address before: 100020 No. 1901, 39th floor, Zhongzhili, Chaoyang District, Beijing Patentee before: Shen Guanqing |
|
| TR01 | Transfer of patent right |