CN104417752A - Saucer-shaped aircraft - Google Patents
Saucer-shaped aircraft Download PDFInfo
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- CN104417752A CN104417752A CN201310375873.6A CN201310375873A CN104417752A CN 104417752 A CN104417752 A CN 104417752A CN 201310375873 A CN201310375873 A CN 201310375873A CN 104417752 A CN104417752 A CN 104417752A
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Abstract
A saucer-shaped aircraft belongs to an advanced multiangular-direction saucer-shaped aircraft. The design thought is that: based on the multiangular-direction rapid steering function of a saucer shape, the saucer-shaped aircraft can steer arbitrarily in 360 degrees; powerful air flow is formed by air compression through a propeller or a turbofan, and acts on the upper surface of the saucer-shaped aircraft, so as to reduce the atmospheric pressure of the upper surface, and to enable the aircraft to taking off and landing vertically and to hover in the sky; the flying direction of the aircraft can be controlled by adjusting the density of the compressed air flow above the saucer-shaped aircraft, and thus multiangular-direction steering can be accomplished. The saucer-shaped aircraft mainly comprises three main parts: a power system, a control system, and a body composition system. The saucer-shaped aircraft can take off and land safely both on land and in water, and can run in a high speed or a low speed in water. The saucer-shaped aircraft can be further designed to dive and run underwater, and when a automatic control system is equipped, the saucer-shaped aircraft can be designed into a water-land-air triphibian unmanned aircraft. The saucer-shaped aircraft can land safely under a condition that power is lost completely. The saucer-shaped aircraft used as an aircraft for military use can realize 360-degree multiangular-direction attack and 360-degree omnibearing early warning, and can take charge of the early warning task for aircraft carrier formation or fighter air fleet.
Description
Technical field
This invention belongs to a kind of very advanced polygonal to butterfly aircraft.
Background technology
Now, no matter be military or civil aircraft nothing more than two kinds of forms: one is Fixed Wing AirVehicle, it is exactly seen aircraft at ordinary times, utilize the powerful thrust that propeller or engine produce, promote body and slide a segment distance, after reaching certain speed, the aerodynamic force principle lift-off flight utilizing fixed-wing to produce.Its advantage is that flying speed is fast, and load capacity is large, and military secret fighting capacity is strong; Shortcoming to have plane track, can not vertical takeoff and landing.Another kind is rotary aircraft, is exactly seen helicopter at ordinary times.Its advantage is can vertical takeoff and landing, realizes hovering; Shortcoming is that flying speed is slow, and load capacity is little, and military secret fighting capacity is weak.Other forms of aircraft is all be in science fiction or imagination stage, lacks strong theory support.
Summary of the invention
For the deficiency of the above two kinds of aircraft, spy devises this butterfly aircraft.Its mentality of designing is: 1 utilizes the polygonal to rapid turning function of butterfly, can 360 degree turn to arbitrarily.2 utilize screw propeller or turbofan pressurized air to form airflow, act on butterfly aircraft upper surface, thus reduce the atmospheric pressure of upper surface, make aircraft can vertical takeoff and landing and hovering.3, by regulating the heading of the compressed air stream density domination aircraft above butterfly aircraft, can complete polygonal to turning to.
Solution of the present invention is: butterfly aircraft is made up of main three parts, is power system, control system, organization system respectively.Power system comprises driving engine, transmission shaft, turbofan, turbofan streamlined reefer housing.Control system comprises chaufeur operation bench, motor speed controller, turbofan streamlined reefer housing angle adjustable column, turbofan streamlined reefer housing angle controller.Organization system comprises butterfly body, power cabin, driving compartment, upper egress hatch, lower egress hatch, hold-down arm hatch, guiding screw propeller hatch, illuminating lamp.
Its basic structure is: arrange power cabin in the lower central of butterfly body, power cabin internal fixtion driving engine, the outputting power of driving engine passes to the turbofan at butterfly body top by transmission shaft, turbofan surrounding has turbofan streamlined reefer housing, turbofan streamlined reefer housing is connected with butterfly-type body by turbofan streamlined reefer housing angle adjustable column, turbofan streamlined reefer housing angle adjustable column can slide up and down, in order to the size of the angle and air gap that regulate turbofan streamlined reefer housing.The top of butterfly body arranges egress hatch, and bottom arranges lower egress hatch and hold-down arm hatch, and lead screw propeller hatch and illuminating lamp.In guiding screw propeller hatch, guiding screw propeller is set; In hold-down arm hatch, hold-down arm is set, supporting & stablizing butterfly body during for landing.At butterfly internal body side assembling chaufeur operation bench, chaufeur operation bench is arranged motor speed controller, turbofan streamlined reefer housing angle controller and automatic control device and instrument.Chaufeur operation bench is arranged on a side relative with the screw propeller hatch that leads and is advisable.If used as military secret, bottom, power cabin can arrange warhead hanger; Can arrange 360 degree of angle radars in bottom, comprehensive is fighter group or aircraft carrier fleet's early warning simultaneously.
This butterfly aircraft also can covering surface solar panel thereon, and turbofan changes electronic turbofan into.
Its basic functional principle is: along with driving engine accelerates gradually, and turbofan is along with acceleration rotation, and the air of butterfly body upper will be siphoned away rapidly by turbofan, and air becomes relatively thin, thus forms relative vacuum, reduces the air resistance that butterfly body rises; The compressed air stream that turbofan produces simultaneously is discharged at a high speed by the air gap between turbofan streamlined reefer housing and butterfly body, annular high speed compression air-flow is formed at butterfly block upper surface, because butterfly block upper surface is subject to the impact of high velocity air, the bar pressure of butterfly body upper is diminished relatively, the bar pressure of bottom is constant, whole like this butterfly aircraft under the effect of bar pressure difference, will rise rapidly, has accomplished to take off vertically.Certain height is raised to when butterfly aircraft rises, turbofan streamlined reefer housing angle controller can be utilized to regulate the angle of turbofan streamlined reefer housing by turbofan streamlined reefer housing angle adjustable column, its front is made to sink to the upper surface of butterfly body, such high pressure draft will spray backward, after making butterfly body, upper surface bar pressure reduces thus whole butterfly body is turned forward, simultaneously, the antagonistic force of jet-stream wind promotes butterfly aircraft flight forward backward, now butterfly body front upper place produces by moving air flow, same generation lift upwards, maintain butterfly aircraft smooth flight.This butterfly aircraft can do random angle to turning to by regulating the angle of turbofan streamlined reefer housing, and also can climb rapidly by improving turbofan rotating speed, its spaceflight alerting ability is better than any current flight device.Can be balanced by the airslide below turbofan because turbofan rotates the deflection moment of torsion produced, also can open guiding screw propeller hatch and stretch out guiding screw propeller auxiliary balance deflection moment of torsion.
Butterfly aircraft needs only need slowly slow down turbofan speed during landing, and butterfly aircraft will slowly decline, and selects suitable landing point, completes descent.This butterfly aircraft can land on land, also can take the water; When landing on land, need slowly close to ground, slowly open hold-down arm hatch and put down hold-down arm, the butterfly aircraft that comes to a complete stop completes landing; When taking the water, do not need to open any hatch, only need slowly adjoined water surface to complete landing.This butterfly aircraft on the water can fast and microinching; Open guiding screw propeller hatch, stretch out guiding screw propeller, regulate angle, start guiding screw propeller, butterfly aircraft will on the water surface microinching the same as ship; If regain guiding screw propeller, close guiding screw propeller hatch, start turbofan, turbofan streamlined reefer housing is leaned forward, butterfly aircraft will on the water surface as without going into it deeply rapid movement.
This butterfly aircraft is extensible to be designed and developed, motion of diving beneath the water; Can also be equipped with robot control system(RCS), utilize satellite positioning, automatically go up to the air, automatically select optimal path, the water, land and air three of landing voluntarily is dwelt unmanned vehicle.Even if this butterfly aircraft is when power loses entirely, utilize its glide principle also can not cause large accident, particularly have the place of the water surface, can glide safe falling.
If this butterfly aircraft is as military spacecraft, can in its bottom, power cabin, 360 degree are polygonal to suspension missile launcher, and realize polygonal to strike, 3 cover, 120 degree of angle radars can be mated in bottom, realize 360 degree of early warning on a large scale; Exactly solve China aircraft carrier fleet's early warning plane can not a difficult problem for warship.
This beneficial effect of the invention is: 1 butterfly aircraft can realize vertical takeoff and landing and hovering, and aloft rapid flight.2 these butterfly aircrafts can do 360 degree of random angles to turning to and climbing fast.3 these butterfly aircrafts can on land with safe landing in water, and can on the water surface fast or slow running.The extensible design of 4 this butterfly aircraft is dived beneath the water motion, is equipped with robot control system(RCS) and can be designed to water, land and air three and dwells unmanned vehicle.5 these butterfly aircrafts can safe falling when power loses entirely.6 these butterfly aircrafts as military spacecraft, can realize 360 degree polygonal to strike and 360 degree of comprehensive early warning, serve as the early warning task of aircraft carrier fleet or fighter group.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, this invention is further illustrated
Accompanying drawing 1 is that this invention is taken off vertically schematic diagram.
Accompanying drawing 2 is this invention structure schematic diagrams above.
Accompanying drawing 3 is this invention structure schematic diagrams below.
Accompanying drawing 4 is these invention horizontal flight schematic diagrams
In figure, 1 power cabin 2 butterfly body 3 transmission shaft 4 airflow direction indicates 5 turbofan streamlined reefer housing 6 turbofan streamlined reefer housing angle adjustable column 7 compressed air stream direction 8 butterfly aircraft service directions to indicate egress hatch 15 in 9 turbofan 10 illuminating lamp, 11 times egress hatch 12 hold-down arm hatch 13 passive air flow line instruction 14 to lead screw propeller hatch
Detailed description of the invention
Butterfly aircraft is made up of main three parts, is power system, control system, organization system respectively.Power system comprises driving engine, transmission shaft (3), turbofan (9), turbofan streamlined reefer housing (5).Control system comprises chaufeur operation bench, motor speed controller, turbofan streamlined reefer housing angle adjustable column (6), turbofan streamlined reefer housing angle controller.Organization system comprises butterfly body (2), power cabin (1), driving compartment, upper egress hatch (14), lower egress hatch (11), hold-down arm hatch (12), guiding screw propeller hatch (15), illuminating lamp (10).
Its basic structure is: arrange power cabin (1) in the lower central of butterfly body (2), power cabin (1) internal fixtion driving engine, the outputting power of driving engine passes to the turbofan (9) at butterfly body (2) top by transmission shaft (3), turbofan (9) surrounding has turbofan streamlined reefer housing (5), turbofan streamlined reefer housing (5) is connected with butterfly-type body (2) by turbofan streamlined reefer housing angle adjustable column (6), turbofan streamlined reefer housing angle adjustable column (6) can slide up and down, in order to the size of the angle and air gap that regulate turbofan streamlined reefer housing (5).The top of butterfly body (2) arranges egress hatch (14), bottom arranges lower egress hatch (11) and hold-down arm hatch (12), and lead screw propeller hatch (15) and illuminating lamp (10).In guiding screw propeller hatch (15), guiding screw propeller is set; Hold-down arm hatch arranges hold-down arm in (12), supporting & stablizing butterfly body (2) during for landing.At butterfly body (2) inner side assembling chaufeur operation bench, chaufeur operation bench is arranged motor speed controller, turbofan streamlined reefer housing angle controller and automatic control device and instrument.The side that chaufeur operation bench is arranged on guiding screw propeller hatch (15) relative is advisable.If used as military secret, power cabin (1) bottom can arrange warhead hanger; Can arrange 360 degree of angle radars in bottom, comprehensive is fighter group or aircraft carrier fleet's early warning simultaneously.
This butterfly aircraft also can covering surface solar panel thereon, and turbofan (9) changes electronic turbofan into.
Claims (8)
1. butterfly aircraft forms primarily of three parts, is power system, control system, organization system respectively; It is characterized in that: power system comprises driving engine, transmission shaft, turbofan, turbofan streamlined reefer housing; Control system comprises chaufeur operation bench, motor speed controller, turbofan streamlined reefer housing angle adjustable column, turbofan streamlined reefer housing angle controller; Organization system comprises butterfly body, power cabin, driving compartment, upper egress hatch, lower egress hatch, hold-down arm hatch, guiding screw propeller hatch, illuminating lamp; In the lower central of butterfly body, power cabin is set, power cabin internal fixtion driving engine, the outputting power of driving engine passes to the turbofan at butterfly body top by transmission shaft, turbofan surrounding has turbofan streamlined reefer housing, turbofan streamlined reefer housing is connected with butterfly-type body by turbofan streamlined reefer housing angle adjustable column, turbofan streamlined reefer housing angle adjustable column can slide up and down, in order to the size of the angle and air gap that regulate turbofan streamlined reefer housing; The top of butterfly body arranges egress hatch, and bottom arranges lower egress hatch and hold-down arm hatch, and lead screw propeller hatch and illuminating lamp; In guiding screw propeller hatch, guiding screw propeller is set; In hold-down arm hatch, hold-down arm is set, supporting & stablizing butterfly body during for landing; At butterfly internal body side assembling chaufeur operation bench, chaufeur operation bench is arranged motor speed controller, turbofan streamlined reefer housing angle controller and automatic control device and instrument.
2. butterfly aircraft according to claim 1, is characterized in that: chaufeur operation bench is arranged on a side relative with the screw propeller hatch that leads and is advisable, and is convenient to manipulation and aquatic sports like this.
3. butterfly aircraft according to claim 1, is characterized in that: use as military secret, bottom, power cabin can arrange warhead hanger; Can arrange 360 degree of angle radars in bottom, comprehensive is fighter group or aircraft carrier fleet's early warning simultaneously.
4. butterfly aircraft according to claim 1, is characterized in that: butterfly aircraft also can covering surface solar panel thereon, and turbofan changes electronic turbofan into.
5. butterfly aircraft according to claim 1, is characterized in that: butterfly aircraft can vertical takeoff and landing, and hovering, smooth flight, 360 degree of random angles are to turning to.
6. butterfly aircraft according to claim 1, is characterized in that: butterfly aircraft can landing on land and the water surface, and can on the water surface fast or microinching.
7. butterfly aircraft according to claim 1, is characterized in that: butterfly aircraft is extensible to be designed and developed, motion of diving beneath the water; Can also be equipped with robot control system(RCS), utilize satellite positioning, automatically go up to the air, automatically select optimal path, dwell unmanned vehicle in the land, water and air three of landing voluntarily.
8. butterfly aircraft according to claim 1, is characterized in that: even if butterfly aircraft is when power loses entirely, and utilize its glide principle also can not cause large accident, particularly have the place of the water surface, can glide safe falling.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310375873.6A CN104417752A (en) | 2013-08-26 | 2013-08-26 | Saucer-shaped aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310375873.6A CN104417752A (en) | 2013-08-26 | 2013-08-26 | Saucer-shaped aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104417752A true CN104417752A (en) | 2015-03-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310375873.6A Pending CN104417752A (en) | 2013-08-26 | 2013-08-26 | Saucer-shaped aircraft |
Country Status (1)
| Country | Link |
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| CN (1) | CN104417752A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947199A (en) * | 2016-05-03 | 2016-09-21 | 王西银 | Autoroatation self-flinging antigravity butterfly-shaped aircraft |
| CN106516108A (en) * | 2016-05-12 | 2017-03-22 | 王金海 | Atmospheric pressure anti-gravity device |
| CN106672182A (en) * | 2016-10-28 | 2017-05-17 | 湖南科技大学 | Underwater submerged plate |
| CN113650775A (en) * | 2021-08-25 | 2021-11-16 | 东莞市利芯智能科技有限公司 | Unmanned aerial vehicle's flight structure |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3592413A (en) * | 1969-06-25 | 1971-07-13 | Chandler Evans Inc | Vertical lift machine |
| WO2011010155A2 (en) * | 2009-07-21 | 2011-01-27 | Aesir Limited | Steering vehicles through control of aerofoils |
| CN102548842A (en) * | 2009-07-06 | 2012-07-04 | 艾希尔有限公司 | Craft and method for assembling craft with controlled spin |
| CN102556350A (en) * | 2012-02-10 | 2012-07-11 | 杜云鹏飞 | Solar electromagnetic power disc-shaped aircraft |
-
2013
- 2013-08-26 CN CN201310375873.6A patent/CN104417752A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3592413A (en) * | 1969-06-25 | 1971-07-13 | Chandler Evans Inc | Vertical lift machine |
| CN102548842A (en) * | 2009-07-06 | 2012-07-04 | 艾希尔有限公司 | Craft and method for assembling craft with controlled spin |
| WO2011010155A2 (en) * | 2009-07-21 | 2011-01-27 | Aesir Limited | Steering vehicles through control of aerofoils |
| CN102556350A (en) * | 2012-02-10 | 2012-07-11 | 杜云鹏飞 | Solar electromagnetic power disc-shaped aircraft |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947199A (en) * | 2016-05-03 | 2016-09-21 | 王西银 | Autoroatation self-flinging antigravity butterfly-shaped aircraft |
| CN106516108A (en) * | 2016-05-12 | 2017-03-22 | 王金海 | Atmospheric pressure anti-gravity device |
| CN106672182A (en) * | 2016-10-28 | 2017-05-17 | 湖南科技大学 | Underwater submerged plate |
| CN113650775A (en) * | 2021-08-25 | 2021-11-16 | 东莞市利芯智能科技有限公司 | Unmanned aerial vehicle's flight structure |
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|---|---|---|---|
| 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 |
Application publication date: 20150318 |