CN102085914A - Flying saucer - Google Patents
Flying saucer Download PDFInfo
- Publication number
- CN102085914A CN102085914A CN2010106239893A CN201010623989A CN102085914A CN 102085914 A CN102085914 A CN 102085914A CN 2010106239893 A CN2010106239893 A CN 2010106239893A CN 201010623989 A CN201010623989 A CN 201010623989A CN 102085914 A CN102085914 A CN 102085914A
- Authority
- CN
- China
- Prior art keywords
- shell
- rudder
- lower house
- internal layer
- layer shell
- 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
Images
Abstract
The invention relates to a flying saucer which comprises a shell and is characterized in that the shell comprises an upper shell and a lower shell, wherein the upper shell is in a hemispherical shape; the lower shell is in a turbinate shape; the diameter of the upper shell is the same to the diameter of the upper circular surface of the lower shell; the lower shell comprises an inner layer shell and an outer layer shell; the inner layer shell is divided into an upper part and a lower part; a propeller is installed between the upper part and the lower part of the inner layer shell of the lower shell; more than one fan rudder is installed between the upper shell and the outer layer of the lower shell; an upper fan blade is arranged between the upper part of the inner layer shell and the outer layer shell; a lower fan blade is arranged between the lower part of the inner layer shell and the outer layer shell; a disc rudder is arranged in the lower shell; a balanced fan blade is installed at the lower part of the inner layer shell; and a balanced rudder is arranged at the lower part of the inner layer shell of the lower shell. The flying saucer can perpendicularly take off or land and does not need to rotate a machine body to rapidly change a flight direction when flying in the air.
Description
Technical field
The present invention relates to a kind of flying saucer, belong to the aircraft field.
Background technology
Existing aircraft mainly is an aircraft, and aircraft flight has a lot of limiting conditions, as: need special-purpose runway, can only be in land landing flight etc.Existing aircraft is not a centrosymmetric structure, and this their ability of bearing external powerful fluid impact in flight course that make descends greatly.When turning to, owing to limit by its dynamic structure, can only change by rotating fuselage, this makes them very easily out of control in high-speed motion.And the navigation of can not diving beneath the water of existing aircraft, the landing field there is certain requirement, more impossiblely between building, fly, can not in thick forest, land.Known flying saucer, be " UFO " promptly: UFO, butterfly aircraft are not used for practice in actual life yet.
Summary of the invention
The purpose of this invention is to provide when can aloft fly, not needing to rotate fuselage just can quick change of flight direction, aircraft--the flying saucer of the landing and the navigation of diving beneath the water on the water.
The objective of the invention is to realize in the following manner:
The present invention includes housing, it is characterized in that: housing is by last, following two parts constitute, upper shell is a segment shape, lower house is a turbination, the equal diameters of disc on the diameter of upper shell and the lower house, lower house is by interior, outer two-layer housing constitutes, internal layer shell is divided into again, following two parts, there is base plate the lower part of internal layer shell, the upper limb on internal layer shell top and the inwall of upper shell are connected and fixed, on the lower house internal layer shell, between following two parts screw propeller is installed, screw propeller is by interior, outer two-layer ring combines, interior, be connected with blade equally spacedly along circumference between the outer two-layer ring, on the inwall of inner layer ring, be provided with circle teeth, be provided with the columnar oar skirt of a circle in the lower edge of outer layer ring, on screw propeller and the internal layer shell, following two parts all connect by rolling bearing, and on screw propeller and lower house internal layer shell, be provided with fixed type bearing between following two parts, the bottom of the outer casing of lower house is circular vent; The more than one wind rudder that can be free to slide along circumference is installed between the upper limb of the edge of upper shell and the outer casing of lower house, the surface of wind rudder is an arc surface, on the inwall of wind rudder, be provided with teeth, between the outer casing of the top of the internal layer shell of lower house and lower house, be provided with fan blade equidistantly, between the outer casing of the lower part of the internal layer shell of lower house and lower house, be provided with fan blade down equidistantly by circumference by circumference; On the inwall of the housing of the lower part of the internal layer shell of lower house driving engine is installed, the output shaft of driving engine is by the teeth engagement of transmission device and screw propeller inner layer ring; The circumference equal intervals of the submarginal inwall of upper shell be provided with counter gear, teeth engagement on counter gear and the wind rudder inwall, in lower house, be provided with manual dish rudder, on the dish rudder, be provided with teeth, the teeth number of dish rudder equates with the teeth number of wind rudder, be provided with link rod between dish rudder and wind rudder, the two ends of link rod all are equipped with gear, and two gears mesh with the teeth of dish rudder and the teeth of wind rudder respectively; At the lower edge of the lower part of the internal layer shell of lower house and each corresponding balance fan blade that is equipped with of fan blade down, between per two the balance fan blades of lower edge of the lower part of the internal layer shell of lower house, Connection Block is arranged, adjacent Connection Block is height arrangement straggly, be connected with a balanced rudder with bearing on each Connection Block, the surface of balanced rudder is an arc, has a hydraulic stem to be connected with the base plate of the lower part of internal layer shell at the middle part of balanced rudder.
Advantage of the present invention is: landing does not need private track, can vertical takeoff and landing, when can aloft fly, do not need to rotate the just quick change of flight direction of energy of fuselage, the landing and the navigation of diving beneath the water on the water, any attitude that fixed wing aircraft aloft can be done, this aircraft all can be accomplished.
Description of drawings
Fig. 1 is that the installation site of the housing of flying saucer concerns scheme drawing;
Fig. 2 is structural representation of the present invention (the part signal of vertical profile);
Fig. 3 is the structural representation of upper shell;
Fig. 4 is that the installation site concerns scheme drawing between upper and lower two parts of screw propeller and lower house internal layer shell;
Fig. 5 is the structural representation of lower part of the internal layer shell of lower house;
Fig. 6 is the structural representation of the outer casing of lower house;
Fig. 7 is the structural representation of screw propeller;
Fig. 8 is rolling bearing distribution schematic diagram on screw propeller;
Fig. 9 is the scheme drawing that the wind rudder is installed on the outer casing of lower house;
Figure 10 is the partial longitudinal section of the distribution of upper and lower fan blade on the outer casing of lower house;
Figure 11 goes up the distribution schematic diagram of fan blade between the outer casing of the top of lower house internal layer shell and lower house;
Figure 12 is the distribution schematic diagram of fixed type bearing;
Figure 13 is the scheme of installation of balanced rudder;
Figure 14 is the partial longitudinal section of upper shell;
Figure 15 is the partial longitudinal section of wind rudder;
Figure 16 is a structural representation of going up fan blade;
Figure 17 is the structural representation of following fan blade;
Figure 18 is the structural representation of balance fan blade;
Figure 19 is the structural representation of balanced rudder;
Figure 20 is the structural representation of dish rudder;
Figure 21 is the upward view of dish rudder;
Figure 22 is the structural representation of link rod.
Among the figure: 1--upper shell, the top of the internal layer shell of 2--lower house, 3-screw propeller, the lower part of the internal layer shell of 4--lower house, the outer casing of 5--lower house, 6-wind rudder, the 7--counter gear, the 8--link rod, 9--coils rudder, the 10-fixed type bearing, 11--transmission device, 12-driving engine, 13--balance fan blade, 14--balanced rudder, fan blade under the 15-, the last fan blade of 16-, the 17-hydraulic stem, the 18-rolling bearing, 19--hydraulic stem oil pipe passes through the hole, 20--balance fan blade fixed connecting piece, 21--screw propeller inner layer ring, 22--screw propeller inner layer ring teeth, 23--screw propeller outer layer ring, the 24--propeller blade, 25--screw propeller oar skirt.
The specific embodiment
The present invention includes housing, housing is by last, following two parts constitute, upper shell 1 is a segment shape, lower house is a turbination, the equal diameters of disc on the diameter of upper shell 1 and the lower house, lower house is by interior, outer two-layer housing constitutes, internal layer shell is divided into again, following two parts 2,4, there is base plate the lower part 4 of internal layer shell, it (can be riveted joint that the inwall of the upper limb on internal layer shell top 2 and upper shell 1 is connected and fixed, modes such as welding), on the lower house internal layer shell, between following two parts screw propeller 3 is installed, screw propeller 3 is by interior, outer two- layer ring 21,23 combine, interior, outer two-layer ring 21, be connected with blade 24 equally spacedly along circumference between 23, on the inwall of inner layer ring 21, be provided with circle teeth 22, be provided with the columnar oar skirt 25 of a circle in the lower edge of outer layer ring 23, on screw propeller 3 and the internal layer shell, following two parts 2,4 all connect by rolling bearing 18, and on screw propeller 3 and lower house internal layer shell, following two parts 2, be provided with fixed type bearing 10 between 4, the bottom of the outer casing 5 of lower house is circular vent; Four wind rudders 6 that can be free to slide along circumference are installed between the upper limb of the edge of upper shell 1 and the outer casing of lower house 5, the surface of wind rudder 6 is an arc surface, on the inwall of wind rudder 6, be provided with teeth, be provided with fan blade 16 equidistantly by circumference 5 of the outer casings of the top 2 of the internal layer shell of lower house and lower house, be provided with fan blade 15 down equidistantly by circumference 5 of the outer casings of the lower part 4 of the internal layer shell of lower house and lower house; On the inwall of the housing of the lower part 4 of the internal layer shell of lower house driving engine 12 is installed, the output shaft of driving engine 12 is by teeth 22 engagements of transmission device 11 with the screw propeller inner layer ring; The circumference equal intervals of the submarginal inwall of upper shell 1 be provided with counter gear 7, teeth engagement on counter gear 7 and wind rudder 6 inwalls, in lower house, be provided with manual dish rudder 9, on dish rudder 9, be provided with teeth, the teeth number of dish rudder 9 equates with the teeth number of wind rudder 6, be provided with link rod 8 at dish rudder 9 and 6 of wind rudders, the two ends of link rod 8 all are equipped with gear, and two gears mesh with the teeth of dish rudder 9 and the teeth of wind rudder 6 respectively; Fan blade 15 is corresponding down by balance fan blade fixed connecting piece 20 balance fan blade 13 is installed with each at the lower edge of the lower part 4 of the internal layer shell of lower house, between per two the balance fan blades of lower edge of the lower part 4 of the internal layer shell of lower house, Connection Block is arranged, adjacent Connection Block is height arrangement straggly, be connected with a balanced rudder 14 with bearing on each Connection Block, the surface of balanced rudder 14 is an arc, have a hydraulic stem 17 to be connected with the base plate of the lower part 4 of internal layer shell at the middle part of balanced rudder 14, the oil pipe of hydraulic stem is connected with hydraulic stem 17 by hole 19 by the hydraulic stem oil pipe of opening on the base plate of the lower part 4 of internal layer shell.
Monnolithic case of the present invention is a dish, when driving engine drives the screw propeller rotation, the air-flow of horizontal direction enters the housing of flying saucer from the interval between the wind rudder, the air-flow under oblique is changed in the effect of fan blade on the process, the downward air-flow of rotation is changed in effect through screw propeller, change into air-flow under oblique through following fan blade effect, change into vertically downward air-flow, flying saucer is suspended in the air through the balanced rudder effect.By changing the relative position between the wind rudder, can change the orientation that enters of air-flow, and then change the heading of machine.Can make not rotation of flying saucer by the adjustment fan blade.Can change the force-bearing situation of flying saucer bottom by the up and down balance system rudder, and then change the skyborne attitude of flying saucer.The antagonistic force of suffered air-flow and air-flow offseted the application force of following fan blade when screw propeller rotated, and the balance fan blade is used to finely tune balance.
Claims (1)
1. flying saucer, comprise housing, it is characterized in that: housing is by last, following two parts constitute, upper shell is a segment shape, lower house is a turbination, the equal diameters of disc on the diameter of upper shell and the lower house, lower house is by interior, outer two-layer housing constitutes, internal layer shell is divided into again, following two parts, there is base plate the lower part of internal layer shell, the upper limb on internal layer shell top and the inwall of upper shell are connected and fixed, on the lower house internal layer shell, between following two parts screw propeller is installed, screw propeller is by interior, outer two-layer ring combines, interior, be connected with blade equally spacedly along circumference between the outer two-layer ring, on the inwall of inner layer ring, be provided with circle teeth, be provided with the columnar oar skirt of a circle in the lower edge of outer layer ring, on screw propeller and the internal layer shell, following two parts all connect by rolling bearing, and on screw propeller and lower house internal layer shell, be provided with fixed type bearing between following two parts, the bottom of the outer casing of lower house is circular vent; The more than one wind rudder that can be free to slide along circumference is installed between the upper limb of the edge of upper shell and the outer casing of lower house, the surface of wind rudder is an arc surface, on the inwall of wind rudder, be provided with teeth, between the outer casing of the top of the internal layer shell of lower house and lower house, be provided with fan blade equidistantly, between the outer casing of the lower part of the internal layer shell of lower house and lower house, be provided with fan blade down equidistantly by circumference by circumference; On the inwall of the housing of the lower part of the internal layer shell of lower house driving engine is installed, the output shaft of driving engine is by the teeth engagement of transmission device and screw propeller inner layer ring; The circumference equal intervals of the submarginal inwall of upper shell be provided with counter gear, teeth engagement on counter gear and the wind rudder inwall, in lower house, be provided with manual dish rudder, on the dish rudder, be provided with teeth, the teeth number of dish rudder equates with the teeth number of wind rudder, be provided with link rod between dish rudder and wind rudder, the two ends of link rod all are equipped with gear, and two gears mesh with the teeth of dish rudder and the teeth of wind rudder respectively; At the lower edge of the lower part of the internal layer shell of lower house and each corresponding balance fan blade that is equipped with of fan blade down, between per two the balance fan blades of lower edge of the lower part of the internal layer shell of lower house, Connection Block is arranged, adjacent Connection Block is height arrangement straggly, be connected with a balanced rudder with bearing on each Connection Block, the surface of balanced rudder is an arc, has a hydraulic stem to be connected with the base plate of the lower part of internal layer shell at the middle part of balanced rudder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010623989 CN102085914B (en) | 2010-12-30 | 2010-12-30 | Flying saucer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201010623989 CN102085914B (en) | 2010-12-30 | 2010-12-30 | Flying saucer |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102085914A true CN102085914A (en) | 2011-06-08 |
| CN102085914B CN102085914B (en) | 2012-12-05 |
Family
ID=44097955
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201010623989 Expired - Fee Related CN102085914B (en) | 2010-12-30 | 2010-12-30 | Flying saucer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102085914B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103803082A (en) * | 2014-03-04 | 2014-05-21 | 黄坤祥 | Novel flying saucer |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB883634A (en) * | 1958-08-15 | 1961-12-06 | Rolls Royce | Improved gas turbine engine |
| DE3639899A1 (en) * | 1986-11-21 | 1988-01-14 | Erwin Glaser | Magnetically driven flying object |
| CN1081984A (en) * | 1992-08-13 | 1994-02-16 | 迟宇光 | Flying saucer |
| US6892980B2 (en) * | 2001-10-31 | 2005-05-17 | Mitsubishi Heavy Industries, Ltd. | Vertical takeoff and landing aircraft |
| CN2799401Y (en) * | 2005-05-13 | 2006-07-26 | 沙庆军 | Dish shaped aircraft |
| CN101381001A (en) * | 2007-09-04 | 2009-03-11 | 刘新广 | Magneto-flying saucer |
| CN101633408A (en) * | 2008-07-23 | 2010-01-27 | 刘新广 | Flying disk |
-
2010
- 2010-12-30 CN CN 201010623989 patent/CN102085914B/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB883634A (en) * | 1958-08-15 | 1961-12-06 | Rolls Royce | Improved gas turbine engine |
| DE3639899A1 (en) * | 1986-11-21 | 1988-01-14 | Erwin Glaser | Magnetically driven flying object |
| CN1081984A (en) * | 1992-08-13 | 1994-02-16 | 迟宇光 | Flying saucer |
| US6892980B2 (en) * | 2001-10-31 | 2005-05-17 | Mitsubishi Heavy Industries, Ltd. | Vertical takeoff and landing aircraft |
| CN2799401Y (en) * | 2005-05-13 | 2006-07-26 | 沙庆军 | Dish shaped aircraft |
| CN101381001A (en) * | 2007-09-04 | 2009-03-11 | 刘新广 | Magneto-flying saucer |
| CN101633408A (en) * | 2008-07-23 | 2010-01-27 | 刘新广 | Flying disk |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103803082A (en) * | 2014-03-04 | 2014-05-21 | 黄坤祥 | Novel flying saucer |
| CN103803082B (en) * | 2014-03-04 | 2016-05-18 | 黄坤祥 | A kind of flying saucer machine |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102085914B (en) | 2012-12-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN1200702A (en) | Aircraft | |
| CN102119102A (en) | Rotational bottom blade type flight vehicle | |
| CN103803078A (en) | Flying saucer type helicopter utilizing active airflow to generate lifting power | |
| CN201457738U (en) | Dishing aircraft | |
| CN103935517A (en) | Aircraft | |
| WO2011041991A2 (en) | Aircraft using ducted fan for lift | |
| CN102085914B (en) | Flying saucer | |
| CN104875875B (en) | A kind of gas wing-type air-flow orients load transportation aircraft | |
| CN108263594A (en) | A kind of bladeless fan power vertical take-off and landing drone | |
| CN205022860U (en) | Coaxial pair changes duct aircraft | |
| CN101985310A (en) | Rotor head structure of gyroplane | |
| CN104787328A (en) | Rotor wing folding and unfolding mechanism for composite aircraft | |
| CN203996896U (en) | A kind of vertical Lift type plate-shape aircraft | |
| CN208021716U (en) | Adjustable rotary wing mechanism for fixed-wing unmanned plane | |
| RU2664851C1 (en) | Vertical take-off and landing aircraft | |
| CN208021740U (en) | Adjustable rotor fuselage device for fixed-wing unmanned plane | |
| CN101905747A (en) | Design method of UFO (Unidentified Flying Object)-shaped helicopter | |
| CN202022300U (en) | Winged helicopter with propeller capable of deflecting by 10-110 degrees | |
| RU2641399C1 (en) | Aircraft | |
| RU2365522C1 (en) | Flying source | |
| RU2012143742A (en) | VERTICAL TAKEOFF AND LANDING DEVICE | |
| CN106143905A (en) | Universe flyball | |
| CN205034345U (en) | Aircraft | |
| CN103231803A (en) | Small unmanned aircraft configuration | |
| CN203255356U (en) | Annular-wing aircraft |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20121205 Termination date: 20151230 |
|
| EXPY | Termination of patent right or utility model |