CN101092167A - Dished aircraft - Google Patents
Dished aircraft Download PDFInfo
- Publication number
- CN101092167A CN101092167A CN 200710012249 CN200710012249A CN101092167A CN 101092167 A CN101092167 A CN 101092167A CN 200710012249 CN200710012249 CN 200710012249 CN 200710012249 A CN200710012249 A CN 200710012249A CN 101092167 A CN101092167 A CN 101092167A
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- dish body
- dish
- rudder
- motor
- steering wheel
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Abstract
The invention relates to dish shape aircraft. It includes cowl, propeller, electric machine, diversion interlayer, dish framework, flow deflector, rudder face, dish body, shock absorber support, rudder snail machine, electrical source, electron speed regulator, direction steering gear, support disk, torsion moment steering gear, and receiver. The cowl is fixed at the upper of the dish body. The diversion interlayer is pasted on it. The invention can improve air current character to increase ascending effect, improve aerodynamic characteristics to increase boundary layer efficiency and increase lift force respectively by the cowl and dish shape design. The invention can be widely used in military affairs, agriculture, mountains research fields etc, also can be changed into toy to sell in the market.
Description
Technical field: the present invention relates to a kind of aircraft, especially a kind of Dished aircraft, the promptly usual said flying saucer of people.
Background technology: up to now, flying saucer remains a kind of " UFO " people in the eyes.Along with the reach of science, developed the Dished aircraft that can fly abroad, but because the defective on its project organization, lift-rising, the delay effect of flying saucer are not obvious, and quiet dynamic stability is not high yet, and cost is very high.
Summary of the invention: at above-mentioned the deficiencies in the prior art, the invention provides a kind of lift-rising, delay effect is obvious, the Dished aircraft that stability is high.
For achieving the above object, the technical solution used in the present invention is: Dished aircraft comprises fairing (1), screw propeller (2), motor (3), water conservancy diversion interlayer (4), dish body skeleton (5), flow deflector (6), rudder face (7), dish body (8), shock bracket (9), rudder spiral shell instrument (10), power supply (11), electronic governor (12), direction steering wheel (13), support disk (14), moment of torsion steering wheel (15), receiver (16).Fairing (1) is fixed on the upper end of dish body (8).Water conservancy diversion interlayer (4) is attached on the dish body (8).Propeller (2) links to each other with motor (3), and propeller (2) is in the fairing (1), and motor (3) is positioned at the top of dish body (8).Dish body skeleton (5) is in the dish body (8), is supporting dish body (8).Flow deflector (6) is inserted in the dish body (8), is in the middle and lower part of dish body (8).Rudder face (7) is connected the lower end of dish body (8), and evolution becomes hinges.Shock bracket (9) is fixed on the bottom of dish body (8).Support disk (14) is in the dish body (8), is fixed on the dish body skeleton (5).Rudder spiral shell instrument (10), power supply (11), electronic governor (12), receiver (16) is fixed on the support disk (14).Direction steering wheel (13) is in the dish body (8), links to each other with rudder face (7).Moment of torsion steering wheel (15) links to each other with flow deflector (6).Motor (3) is by lead and power supply (11), and electronic governor (12) links to each other.
Characteristics of the present invention are as follows:
1, streamlined reefer housing collection contraction, voltage stabilizing, the incorporate design of expansion improve flow quality, and the lift-rising effect is good.
2, attach water conservancy diversion interlayer (4) on the dish body (8), thereby improved aerodynamic characteristic, improved boundary-layer efficient, improved lift.
3, the dish-shaped physique amount distribution that is evenly distributed improves quiet, the dynamic behaviour of dish body and surely controls.
4, the dish body adopts the foam glass steel composite material to make, and guarantees that project organization is integrated, keeps the not yielding of dish face, keep pneumatic indeformable.
5, the shock bracket of Cai Yonging makes cushion characteristic, anti-bump performance and obviously improves.
The present invention can be applied in fields such as military affairs, agricultural, mountain area are searched and rescued, take photo by plane in ground widely, can also be transformed into toy and be used for market sale.
Description of drawings:
Fig. 1 is a structural representation of the present invention.
The specific embodiment:
As shown in Figure 1: Dished aircraft comprises fairing 1, screw propeller 2, motor 3, water conservancy diversion interlayer 4, dish body skeleton 5, flow deflector 6, rudder face 7, dish body 8, shock bracket 9, rudder spiral shell instrument 10, power supply 11, electronic governor 12, direction steering wheel 13, support disk 14, moment of torsion steering wheel 15, receiver 16.Fairing 1 is fixed on the upper end of dish body 8.Water conservancy diversion interlayer 4 is attached on the dish body 8.Propeller 2 links to each other with motor 3, and propeller 2 is in the fairing 1, and motor 3 is positioned at the top of dish body 8.Dish body skeleton 5 is in the dish body 8, is supporting dish body 8.Flow deflector 6 is inserted in the dish body 8, is in the middle and lower part of dish body 8.Rudder face 7 is connected the lower end of dish body 8, and evolution becomes hinges.Shock bracket 9 is fixed on the bottom of dish body 8.Support disk 14 is in the dish body 8, is fixed on the dish body skeleton 5.Rudder spiral shell instrument 10, power supply 11, electronic governor 12, receiver 16 is fixed on the support disk 14.Direction steering wheel 13 is in the dish body 8, links to each other with rudder face 7.Moment of torsion steering wheel 15 links to each other with flow deflector 6.Motor 3 is by lead and power supply 11, and electronic governor 12 links to each other.
Principle of work:
(air-flow of high-speed motion can move along plane of bending Dished aircraft on the object curved surface with Coanda effect, rather than move along a straight line, this can provide vertical lift for object) be theoretical foundation, rotate by the driven by motor propeller, fairing produces high velocity air, high velocity air produces lift by dish body and water conservancy diversion interlayer, regulates its reactive torque by flow deflector, by the path of motion of four rudder face control flying saucers.
Working process:
Motor and power supply, electronic governor, receiver is communicated with lead, sends instruction by transmitting set, makes driven by motor propeller high speed rotating, produces high velocity air by fairing, and high velocity air produces lift by dish body and water conservancy diversion interlayer, and flying saucer is risen.Because the rotation of driven by motor screw propeller certainly leads to a moment of torsion, therefore on Dished aircraft dish body flow deflector is housed, the moment of torsion steering wheel drives flow deflector and reverses certain angle, and air-flow will produce the moment of torsion that reactive torque power is offset the dish body, makes the dish body keep state of equilibrium.Send instruction by transmitting set, controlling party drives 4 rudder faces to steering wheel and rotates, thus the motion all around of control flying saucer.During landing, send instruction by transmitting set, motor speed is reduced, the dish body descends, at last by the shock bracket landing on the ground.
Claims (2)
1, Dished aircraft comprises screw propeller (2), motor (3), dish body skeleton (5), flow deflector (6), rudder face (7), dish body (8), shock bracket (9), rudder spiral shell instrument (10), power supply (11), electronic governor (12), direction steering wheel (13), support disk (14), moment of torsion steering wheel (15), receiver (16); Propeller (2) links to each other with motor (3), and propeller (2) is in the fairing (1), and motor (3) is positioned at the top of dish body (8); Dish body skeleton (5) is in the dish body (8), is supporting dish body (8); Flow deflector (6) is inserted in the dish body (8), is in the middle and lower part of dish body (8); Rudder face (7) is connected the lower end of dish body (8), and evolution becomes hinges; Support disk (14) is in the dish body (8), is fixed on the dish body skeleton (5); Rudder spiral shell instrument (10), power supply (11), electronic governor (12), receiver (16) are fixed on the support disk (14); Direction steering wheel (13) is in the dish body (8), links to each other with rudder face (7); Moment of torsion steering wheel (15) links to each other with flow deflector (6); Motor (3) is by lead and power supply (11), and electronic governor (12) links to each other, and it is characterized in that also comprise fairing (1) and water conservancy diversion interlayer (4), fairing (1) is fixed on the upper end of dish body (8); Water conservancy diversion interlayer (4) is attached on the dish body (8).
2, Dished aircraft as claimed in claim 1 is characterized in that, also comprises the shock bracket (9) of the bottom that is fixed on dish body (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200710012249 CN101092167A (en) | 2007-07-24 | 2007-07-24 | Dished aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200710012249 CN101092167A (en) | 2007-07-24 | 2007-07-24 | Dished aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101092167A true CN101092167A (en) | 2007-12-26 |
Family
ID=38990653
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200710012249 Pending CN101092167A (en) | 2007-07-24 | 2007-07-24 | Dished aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101092167A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101712377B (en) * | 2009-05-25 | 2013-10-09 | 吴新保 | Helicopter rotor wings with commutation net cover |
| CN105661785A (en) * | 2015-12-28 | 2016-06-15 | 南京航空航天大学 | Flying sunshade and control method thereof |
| CN105799927A (en) * | 2016-03-17 | 2016-07-27 | 高大勇 | Ducted ring fixed wing helicopter |
| CN111409820A (en) * | 2020-03-31 | 2020-07-14 | 兰安德 | Propelling device in air and propelling method thereof |
| CN113002773A (en) * | 2019-12-20 | 2021-06-22 | 刘甫庆 | Novel flight mode and novel aircraft |
-
2007
- 2007-07-24 CN CN 200710012249 patent/CN101092167A/en active Pending
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101712377B (en) * | 2009-05-25 | 2013-10-09 | 吴新保 | Helicopter rotor wings with commutation net cover |
| CN105661785A (en) * | 2015-12-28 | 2016-06-15 | 南京航空航天大学 | Flying sunshade and control method thereof |
| CN105661785B (en) * | 2015-12-28 | 2018-01-19 | 南京航空航天大学 | A kind of flight parasols and its control method |
| CN105799927A (en) * | 2016-03-17 | 2016-07-27 | 高大勇 | Ducted ring fixed wing helicopter |
| CN113002773A (en) * | 2019-12-20 | 2021-06-22 | 刘甫庆 | Novel flight mode and novel aircraft |
| CN111409820A (en) * | 2020-03-31 | 2020-07-14 | 兰安德 | Propelling device in air and propelling method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |