CN105314111A - Large-size high-speed invisible flying saucer - Google Patents
Large-size high-speed invisible flying saucer Download PDFInfo
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- CN105314111A CN105314111A CN201410310874.7A CN201410310874A CN105314111A CN 105314111 A CN105314111 A CN 105314111A CN 201410310874 A CN201410310874 A CN 201410310874A CN 105314111 A CN105314111 A CN 105314111A
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Abstract
The invention discloses a flying saucer and two smoke- and fire-free engines. The flying saucer is composed of a cabin and a disk which rotates round the cabin. The disk includes a disk-shaped wing and a rotary engine. The cabin includes a driving cabin, a passenger cabin and a device cabin. The rotary engine sucks air which is mixed with water, and then the mixture is jetted out horizontally through jet tubes installed on the edge of the disk according to the sprayer principle, so that a generated reactive force enables the disk to rotate at a high speed, thereby generating an upward raising force on the disk. Four fixing wings are installed outside the device cabin to eliminate reverse rotation of the cabin. A vector engine and a diesel power generating set are installed in the device cabin under the disk. The vector engine sucks large amount of air through an air inlet duct in the passenger cabin to form vacuum above the passenger cabin, which enables air pressure difference between an upper surface and a lower surface of the disk to be increased, thereby generating a huge raising force. The sucked air is compressed to form high-pressure gas which is discharged into vector jet tubes and is jetted out, wherein the directions and the angles of the vector jet tubes are adjustable to generate pushing forces in different directions, thereby achieving maneuvering flight of the flying saucer.
Description
Technical field
The present invention relates to aviation field, be specifically related to the manufacturing technology field of disc-shaped flying craft.
Background technology
According to the data display disclosed in recent years, during World War II, Nazi Germany is secret development disc-shaped flying craft just, and has produced the model machine " Bie Longcai disk " that can fly.
After World War II terminates, American, according to Nazi's flying saucer manufacturing technology data of capturing, has produced multiple disc-shaped flying craft successively.More famous has V-173 screw propeller power aerial vehicle; Also has the AVROCAR adopting fanjet as power in addition.
Nineteen fifty-five, Xi Er company of the U.S. have developed one and is called that VZ-1 flies the disc-shaped flying craft of platform, and speed per hour is 24 kilometers.
1980, mole company of the U.S. have developed a kind of two-seater XM-4 flying disc of ducted fan, and 4 engine drives, 8 ducted fans are jet downwards, produced lift.
1987, the disc-shaped flying craft developing co-axial rotor was set about by Xi Kesiji company of the U.S., and two secondary rotors are coaxial, two secondary rotor contrarotations each other.Engine installation can select gas generator turbine, spark ignition engine or electrical motor.
The U.S. still further developed a kind of disc-shaped flying craft of the fixing dish type wing, and its radial section is airfoil, can produce lift.Also have a kind of disc-shaped flying craft of the swivel eye wing, its ring wing rotates, and flight can be made more stable.
In July, 2008, a unpiloted small-sized disc-shaped flying craft of Harbin Shengshi Special Type Aerocraft Co., Ltd.'s development of China.
, there is following problem in above-mentioned disc-shaped flying craft:
1, disk size is too little.Because propulsive effort derives from the centre of aircraft, rotor inertia is little, and when the size of disk increases, when load is larger, the drive efficiency exported by rotating shaft is on the low side, and excessive being easy to of moment of torsion causes rotating shaft to be ruptured.The unpiloted disc-shaped flying craft that Harbin company of China manufactures, diameter just 1.2 meters.
2, cabin volumes is little, can not load more load.
3, speed is slow, highly low.There is no any difference with helicopter, do not play the advantage of disk self, be not really disc-shaped flying craft truly.The flying speed of the disc-shaped flying craft of a company of U.S. development reaches as high as 100 miles per hour (about 161 kilometers), terrain clearance can reach about about 3 meters, its power comes from 8 the rotatable engines be arranged on fuselage, can take for 2 people at every turn.
4, up-and-down maneuver performance is poor, can not be stealthy.It is motor-driven that aircraft cannot vertically rise to, and the high-temperature gas of driving engine ejection is easily detected by infrared detector, cannot be stealthy.
Summary of the invention
For the problems referred to above existing for existing disc-shaped flying craft manufacturing technology, the invention provides the stealthy flying saucer of a kind of large high-speed and two kinds of smokeless fireless engines.
The technical scheme that the present invention is adopted for achieving the above object is:
The stealthy flying saucer of a kind of large high-speed and two kinds of smokeless fireless engines, this flying saucer forms by cabin with around the disk of cabin rotation, and the two is rotated mutually by thrust ball bearing.Cabin comprises driving compartment, crew module, equipment compartment and inlet channel part; Disk comprises circular wing, rotary engine.Rotary engine has 4, is evenly arranged on below disk border; Rotary engine sucks air, and sprayed by nozzle level after mixing with water, the recoil of generation makes disk High Rotation Speed; Disc rotary produces lift upwards, and produces the stable of gyro effect maintenance flight; The vector engine be arranged in equipment compartment sucks large quantity of air from inlet channel, causes the air pressure on crew module top sharply to decline, occurs region of no pressure, and the draught head of disk upper and lower surface increases, thus produces huge lift; The air sucked is compressed into high pressure gas, outwards sprays through vector spray; The direction of vector spray and adjustable angle, produce the thrust of different directions, realize the maneuvering flight of flying saucer.
Flying saucer as above, driving compartment is positioned at top, inner installs control desk, controls the startup of rotary engine, acceleration, deceleration and parking by infrared acquisition and receiving device; Control to be arranged on the diesel powerplant in bottom equipment cabin, vector engine and take-off and landing device by cable; Handle different control buttons and handle, realize the taking off of flying saucer, rise, flatly fly, turn to, hover and land.
Flying saucer as above, crew module is positioned at the below of driving compartment, and is fixedly connected with driving compartment, has manufactured the induction opening of a circle, connected respectively by inlet channel with the air inlet valve of the diesel powerplant in equipment compartment and 8 air suctiton ventilators at crew module's outer wall; The lower surface of crew module has manufactured annular lip, is used for being combined by thrust ball bearing with the disk of below.
Flying saucer as above, disk is positioned at the below of crew module, is arranged between crew module and equipment compartment; Circular wing is formed by connecting by wheel hub, blade and steel ring; Wheel hub hollow, its upper surface has manufactured annular groove, is used for placing thrust ball bearing; The lower circle of thrust ball bearing and groove jam-packed, upper circle is fixedly connected with the flange of crew module, and Shang Quan and lower circle are by ball contact, and ball is kept frame location; The lower surface of wheel hub has manufactured annular lip, is used for realizing being connected with the equipment compartment thrust ball bearing of below, peace and quiet when making disk high speed rotating and smooth and easy.
Flying saucer as above, equipment compartment is positioned at the below of disk, connects as one with crew module; 8 vector engines, 2 diesel generator group and 1 cover take-off and landing device are installed in equipment compartment; The upper surface of equipment compartment has manufactured annular groove, is used for placing thrust ball bearing; The lower circle of bearing and groove jam-packed, upper circle is fixedly connected with the annular lip of the wheel hub of disk, is used for realizing being connected with the thrust ball bearing of top disk; Install 4 secondary fixing aerofoils in equipment compartment external symmetry, the backspin airflow function that disc rotary produces, on fixing aerofoil, is used for eliminating the reversion in cabin; 4 infrared transmitters are installed in equipment compartment external symmetry, and the infrared receiver controller of the rotary engine be arranged on below disk is aimed in direction.
Described circular wing, can be considered the secondary rotor rotational track of a week, its blade one end is connected with hub shaft hole, the mode that the other end is connected with steel ring axis hole, and multiple blade laminates successively, and all form an elevation angle with horizontal surface, the rotation of blade is by servos control, and when circular wing rotates, blade produces downward application force to air, air is then to blade generation antagonistic force upwards, and this is identical with the aerodynamic force principle of helicopter; When after flying saucer lift-off, when the rotating speed of circular wing drops to certain numerical value, by steering wheel moving vane to level angle, seal seamless between blade, fall to ensure that flying saucer can not be fallen off.
Described rotary engine, comprises spark ignition engine, piston pump, fuel tank, water tank, infrared receiver controller and horizontal nozzles; Rotary engine is working medium with water and air, utilizes the principle of atomizing cone, sucks air, because automatic pumping appears low pressure effect, in high flow rate in exhaust process, by being arranged on the nozzle ejection of disk border after empty G&W mixing; The direction of nozzle ejection and the edge level of disk tangent, the recoil of generation forms the moment at an opposed discs center, make disk accelerate rotate.
The groundwork process of rotary engine is:
1. control desk sends the instruction of " startup rotary engine ", and the light-up plug circuit of spark ignition engine connected by infrared receiver controller, starts spark ignition engine.
2. spark ignition engine drives piston pump work, piston reciprocates, sucks air, then discharges air.
3. bleeder line from the coarse to fine, and air rate strengthens.
4., near the end of bleeder line, be connected to the suction pipe of an insertion water tank; The air flowing of bleeder line, cause air pressure to reduce, the water in water tank enters bleeder line along suction pipe, and the air of discharging mixes.
5. the fluid-mixing of water and air enters high pressure nozzle, and along the edge horizontal direction ejection of disk, the recoil of generation makes disc rotary.
6. after the lift obtained when flying saucer is greater than take-off weight, flying saucer vertical uplift; To certain altitude, control desk sends the instruction of " rotary engine deceleration " by 4 infrared transmitters, and the throttle control circuit of spark ignition engine connected by infrared receiver controller, and delivery quality reduces, and disk no longer accelerates to rotate, and rotating speed trend is stable; After control desk sends the instruction of " rotary engine parking ", disk, because having larger rotor inertia, still can keep long rotation, to ensure the stable of flight.
Rotary engine essence is a spraying driving engine.According to the computing formula of impulse force, impulse force F=MV/T, F and M is directly proportional.M is the quality of displacement fluids, is directly proportional to the density of fluid and volume.Because the density of air is much smaller than water, under the condition of identical volume, speed V and time T, the recoil of simple jet generation is also much smaller than the recoil that water spray produces.If merely spray water, then need high-capacity water tank and water pump are installed, add the load that take-off weight and disk bear.The combination of water and air can eliminate the shortcoming of the two, even if after the water of water tank exhausts, the recoil of jet generation can overcome the friction force between disk and air, keeps disk to have certain rotating speed.
Described vector engine, is made up of electrical motor, air suctiton ventilator, air compressor and vector spray, is evenly arranged on the position of equipment compartment bottom outer-edge; Vector engine, by direct motor drive, take air as working medium; The large quantity of air that air suctiton ventilator sucks from inlet channel, enters air compressor by blow off valve; Air compressor shortens air pressure into high pressure gas; High pressure gas enter vector spray with higher flow velocity by stainless steel flexible hose; Vector spray is designed to Laval nozzle shape, plays accelerating action, and high pressure gas are outwards sprayed with ultrasonic speed.
Described vector spray, its anterior and stainless steel flexible hose sealed attachment, jet pipe can carry out 0 ~ 90 degree freely rotating in a perpendicular; According to the manipulation of control desk, steering hardware can adjust direction and the angle of jet pipe at any time, both vertically downward, can produce thrust upwards; Horizontally outward, the thrust of horizontal direction can be produced, realizes the maneuvering flight of aircraft again.
Vector spray technology is a up-to-date technology of present generation aircraft development of engine, only has the U.S. and Russia to grasp in the world.Due to jet pipe ejection is high temperature, high-speed gas, and to direction, the angle of adjustment injection, difficulty is very big.What vector engine jet pipe of the present invention sprayed is cold gas, utilizes the feature that flexible pipe can arbitrarily bend, just can realize the object that appropriate spray bar technology reaches.
Described take-off and landing device, adopts the hydraulic ram system of car hosit, is made up of 4 supporting legs and hydraulic gear.4 supporting legs are evenly arranged on the outside below equipment compartment, alternate with 4 fixing aerofoils.During flight, 4 supporting legs are vertically packed up; During landing, under the promotion of hydraulic gear, supporting leg rotates, until contact perpendicular to the ground.
The groundwork process of vector engine is:
1. control desk sends the instruction of " system startup ", and diesel powerplant starts, to whole flying saucer system power supply.
2. " startup air suctiton ventilator ", 8 air suctiton ventilators work simultaneously, and a large amount of air is drawn into by inlet channel, cause the air pressure above flying saucer sharply to decline, close to vacuum; The difference of pressure of disk upper and lower surface increases, and adds the difference of pressure that disc rotary produces, and when being greater than the weight that flying saucer takes off, flying saucer vertical uplift, leaves ground.
3. " startup air compressor ", 4 air compressors compress the air that air suctiton ventilator is discharged, and after reaching certain pressure, high pressure gas wash limiting valve open, enter vector spray by stainless steel flexible hose.
4. the shape of vector spray is that head and the tail are thick, middle thin, and like the most advanced and sophisticated weld together of two cones, the thinnest middle position is called critical cross-section; Before critical cross-section, from the coarse to fine, gas is subject to further compression to pipeline in flowing, and flow velocity is accelerated; Reach velocity of sound when arriving critical cross-section, pipeline is by carefully thicker, and gas is discharged with the speed exceeding velocity of sound.
5. the bar handle of control desk, with " upwards " for reference position, all 8 vector sprays are jet straight down, and flying saucer vertically rises to; Flying saucer is raised to certain altitude, and when turning to " put down forward and fly ", the angle of the vector spray of 3 below turn 90 degrees by steering hardware, shifts horizontal direction onto; Otherwise when turning to " put down backward and fly ", the angle of the vector spray of 3 above turn 90 degrees by steering hardware, shifts horizontal direction onto; Flat fly state under, when needing " left-hand rotation ", the angle of 3 of the right side vector sprays turn 90 degrees by steering hardware, shifts horizontal direction onto; When needing " right-hand rotation ", the angle of 3 of the left side vector sprays turn 90 degrees by steering hardware, shifts horizontal direction onto; When needing " hovering ", all 8 vector sprays straight down, reduce the free air capacity of air compressor, make lift and the weight balancing of flying saucer; When needing " landing ", constantly reducing the free air capacity of air compressor, until closeall vector spray, by vacuumizing the rotation with disk, stablizing the falling state of flying saucer, until land close to ground.
Advantage of the present invention is:
(1) driving engine being working medium with water or air is used, smokeless without fire, there is hidden function.
(2) propulsive effort rotated is placed in the outer fringe position of disk, and the size of disk is larger, and the moment of rotation of generation is larger, and therefore disk can do very large, and load capacity increases thereupon greatly.
(3) flying saucer obtains raising force, large discharge that disc rotary produces in vertical direction and vacuumizes to produce and upward pressure and thrust that vector spray produces, substantially increases take-off weight and up-and-down maneuver performance.
(4) adopt vector engine, jet pipe is the jet speed and motor-driven that can promote again flight to different directions.
(5) principle of work is simple, and manufacturing technology process is ripe, practicable, can realize the object of the large scale of flying saucer, large load, high speed and stealth.
Accompanying drawing explanation
Fig. 1 is the overall structure schematic diagram of embodiments of the invention 1.
Fig. 2 is the A--A elevation profile local structure schematic diagram of Fig. 1.
Fig. 3 is the schematic top plan view of circular wing of the present invention.
Fig. 4 is the structural representation of vector spray of the present invention.
Fig. 5 is the distribution schematic diagram of vector spray of the present invention.
Fig. 6 is rotary engine of the present invention spraying principle schematic.
Detailed description of the invention
Below in conjunction with drawings and Examples, the invention will be further described:
Fig. 1 is the front elevation of flying saucer of the present invention, as shown in the figure, flying saucer be by driving compartment 1001, crew module 1002, circular wing 1003, equipment compartment 1004, fixing aerofoil 1005, infrared transmitter 1006, vector engine 1007, take-off and landing device 1008, rotary engine 1009, etc. formed.
Fig. 2 is the elevation profile local structure schematic diagram of the embodiment of the present invention, display cabin and circular wing realize the internal state of Structure deformation by thrust ball bearing, as shown in the figure, occupant's bulkhead 2001, induction opening 2002, annular lip 2003, thrust ball bearing enclose 2004, thrust ball bearing steel ball 2005, blade 2006, circle 2007, wheel hub annular lip 2008, lower thrust ball bearing 2009, equipment compartment annular groove 2010, wheel hub 2011, wheel hub annular groove 2012, inlet channel 2013 under thrust ball bearing.
In Fig. 3, circular wing 1003 is made up of wheel hub 2011, blade 2006 and steel ring 3001, and wheel hub 2011 comprises upper surface 3002, annular groove 2012, circular hole 3003.
In Fig. 4, vector spray 5001 is made up of stainless steel flexible hose 4001, contraction cone 4002, critical cross-section 4003, expansion cone 4004.
In Fig. 5,8 vector sprays 5001 are symmetrically distributed in the boundary position bottom equipment compartment 1004.
In Fig. 6, steel cylinder 6001, piston 6002, freeing pipe 6003, suction pipe 6004, nozzle 6005, water tank 6006, piston rod 6007.
Described driving compartment 1001 is positioned at the top of whole flying saucer, and outer shape is half sphere, is made up of the clear glass of high strength, has the visual-field space of 360 degree, is convenient to omnibearing observation and search, and inner installation is driven and control convenience.
Described crew module 1002 is positioned at the below of driving compartment 1001, truncated conical shape, as shown in Figure 2; Bulkhead 2001 has manufactured a circle induction opening 2002, and be connected with inlet channel 2013, the lower surface of the bilge has manufactured annular lip 2003, and with upper circle 2004 weld together of thrust ball bearing.
Described circular wing 1003 is positioned at the below of crew module 1002, as shown in Figure 2; The upper surface of wheel hub 2011 has manufactured annular groove 2012, its size matches with the annular lip 2003 of crew module 1002, annular groove 2012 is embedded in the lower circle 2007 of thrust ball bearing, and with groove jam-packed, make crew module 1002 and circular wing 1003 realize Structure deformation; The lower surface of wheel hub 2011 has manufactured annular lip 2008, connect with the upper lap welding of thrust ball bearing 2009, in the annular groove 2010 of upper surface, thrust ball bearing 2009 embedded equipment cabin, circular wing and equipment compartment is made to achieve Structure deformation, quiet and smooth and easy when making disk high speed rotating.
Described rotary engine 9 has 4, and symmetry is arranged on below circular wing edge; Rotary engine is made up of spark ignition engine, piston pump, fuel tank, water tank, infrared receiver controller and horizontal nozzles; As shown in Figure 6, spark ignition engine drives piston pump work, and piston rod 6007 promotes piston 6002 crank motion in steel cylinder 6001, sucks air, then enters freeing pipe 6003; Freeing pipe 6003 is collapsible tubes, plays accelerating action to air-flow; According to the principle of atomizing cone, because low pressure effect appears in high flow rate in exhaust process, automatically drawn water from water tank 6006 by suction pipe 6004, sprayed by the nozzle 6005 being arranged on disk border after empty G&W mixing; The direction of nozzle ejection and the edge level of disk tangent, the recoil of generation forms the moment at an opposed discs center, make circular wing 1003 accelerate rotate; Adopt wireless control mode, control rotary engine 1009 by 4 infrared transmitters 1006 be arranged on outside equipment compartment 1004, make the disk of rotation become a relatively independent operational system, to simplify manufacture, mounting process; Infrared receiver controller adopts linkage work pattern, as long as one of them receives infrared control signal, is just delivered to all the other 3 controllers by signal wire (SW), carries out synchro control to 4 spark ignition engines.
Because the system height of flying saucer is symmetrical, its center of gravity is positioned at the centre of circular wing 1003, the lift obtained at state of flight lower wing acts near the mid point of disc radius, and circular wing can be subject to one relative to center vertical moment upwards, and circular wing K/UP is out of shape.Although the weight of rotary engine adds the load of circular wing, can produce a moment downward relative to center vertical, can offset part moment upwards, what decrease circular wing upwarps distortion, adds the service life of circular wing.
Described equipment compartment 1004 is positioned at the below of circular wing 1003, as shown in Figure 2, connects as one with crew module 1002; 8 vector engines, 2 diesel generator group and 1 cover take-off and landing device are installed in equipment compartment; The upper surface of equipment compartment has manufactured annular groove 2010, and its size matches with the annular lip 2008 of circular wing 1003; Annular groove 2010 is embedded in thrust ball bearing 2009; The lower circle of bearing and groove jam-packed, upper circle is fixedly connected with the annular lip 2008 of the wheel hub of disk, is used for realizing being connected with the thrust ball bearing of top disk; In equipment compartment 1004 external symmetry, 4 secondary fixing aerofoils 1005 are installed, are used for eliminating the reversion in cabin; 4 infrared transmitters 1006 are installed in equipment compartment external symmetry, and the infrared receiver controller of the rotary engine 1009 be arranged on below disk is aimed in direction.
Described vector engine 1007, comprises electrical motor, air suctiton ventilator, air compressor and vector spray, and amount to 8, symmetry is arranged on the bottom of equipment compartment 1004, as shown in Figure 5; Air suctiton ventilator selects large discharge, high negative pressure blower fan, by direct motor drive, large quantity of air is sucked from the induction opening 2002 of crew module by inlet channel 2013, the air pressure on crew module top is caused sharply to decline, occur region of no pressure, the draught head of disk upper and lower surface is increased, below air pressure large, air pressure is little above, thus produces huge lift; The air sucked enters air compressor by the blow off valve of air suctiton ventilator; Air compressor shortens air pressure into high pressure gas, and after certain pressure, gas enters vector spray 5001 by stainless steel flexible hose; Vector spray is designed to Laval nozzle shape, plays accelerating action to high pressure gas, and gas is outwards sprayed with ultrasonic speed, increases recoil.
Described vector spray 5001, as shown in Figure 4, its anterior and stainless steel flexible hose 4001 sealed attachment, jet pipe can carry out 0 ~ 90 degree freely rotating in a perpendicular; Jet pipe adopts Laval nozzle, and front portion is one and shrinks cone 4002, and accelerate low velocity gas compression, rear portion is an expansion cone 4004, and expand to high-speed gas and accelerate, middle joint portion is critical cross-section 4003; According to the manipulation of control desk, steering hardware can adjust direction and the angle of jet pipe at any time, as shown in Figure 5, both vertically downward, can produce thrust upwards; Horizontally outward, the thrust of horizontal direction can be produced, realizes the maneuvering flight of aircraft again.
Described fixing aerofoil 1005, shape, as trapezoidal, amounts to 4; When the disk rotates, according to the law of conservation of momentum, cabin there will be opposite spin; Meanwhile, the disk of rotation can produce strong lower rotational gas flow, and its direction and cabin direction of rotation act on fixing aerofoil 1005, just can prevent the reversion in cabin.
Described take-off and landing device 1008, adopts the hydraulic ram system of car hosit, and structure is simple, is easy to operation.Supporting leg amounts to 4, and symmetry is arranged on the outside below equipment compartment, alternate with 4 fixing aerofoils 1005, to avoid influencing each other.After flying saucer takes off, 4 supporting legs are vertically packed up; During flying saucer landing, under the promotion of the hydraulic gear in cabin, supporting leg rotates, until contact perpendicular to the ground; Supporting leg hangs a treadmill, to increase the area of contact with ground, ensures aircraft lands safety.
Claims (10)
1. a flying saucer, form by cabin with around the disk of cabin rotation, cabin comprises driving compartment, crew module, equipment compartment, disk comprises rotary engine, circular wing, rotary engine has 4, they are evenly placed on 4 positions of disk following peripheral, driving compartment is positioned at the top of flying saucer, inner installation control desk, crew module is positioned at the below of driving compartment and the top of disk, bulkhead has manufactured a circle induction opening, equipment compartment is positioned at the below of disk, connect as one with crew module, in equipment compartment, 8 vector engines are installed, 2 diesel generator group and 1 cover take-off and landing device, 4 pairs of fixing aerofoils installed outward by equipment compartment, 4 infrared transmitters and 4 hydraulic rams, it is characterized in that:
(1) described rotary engine is spraying driving engine, rotary engine utilizes piston pump suction air, nozzle level by being arranged on disk border after mixing with water sprays, and the recoil of generation makes disk High Rotation Speed, produces lift upwards and gyro effect;
(2) described vector engine, is made up of electrical motor, air suctiton ventilator, air compressor and vector spray, is evenly arranged on the position of equipment compartment bottom outer-edge;
(3) described vector engine sucks large quantity of air from the inlet channel of crew module, causes the air pressure on crew module top sharply to decline, and the draught head of disk upper and lower surface increases, thus produces huge lift; The air sucked is compressed into high pressure gas, outwards sprays through vector spray; The direction of vector spray and adjustable angle, produce the thrust of different directions.
2. flying saucer as claimed in claim 1, is characterized in that:
By 2 cover thrust ball bearing Structure deformation between cabin and disk, mutually rotate.
3. flying saucer as claimed in claim 1, is characterized in that:
Driving compartment is positioned at the top of flying saucer, and outer shape is half sphere, is made up of the clear glass of high strength, and inner installation is driven and control convenience.
4. flying saucer as claimed in claim 1, is characterized in that:
Crew module is positioned at the below of driving compartment, and is fixedly connected with driving compartment, has manufactured the induction opening of a circle, connected respectively by inlet channel with the diesel powerplant in equipment compartment and 8 air suctiton ventilators at crew module's outer wall; The lower surface of crew module has manufactured annular lip, connects with the upper lap welding of thrust ball bearing.
5. flying saucer as claimed in claim 1, is characterized in that:
Circular wing is positioned at the below of crew module, is arranged between crew module and equipment compartment; Circular wing is formed by connecting by wheel hub, blade and steel ring; Wheel hub hollow, its upper surface has manufactured annular groove, with the lower circle jam-packed of thrust ball bearing; The lower surface of wheel hub has manufactured annular lip, connects with the upper lap welding of the thrust ball bearing of below.
6. flying saucer as claimed in claim 1, is characterized in that:
Equipment compartment is positioned at the below of disk, connects as one with crew module; In equipment compartment, vector engine, diesel generator group and take-off and landing device are installed; The upper surface of equipment compartment has manufactured annular groove, with the lower circle jam-packed of thrust ball bearing; 4 secondary fixing aerofoils are installed in equipment compartment external symmetry.
7. flying saucer as claimed in claim 1, is characterized in that:
Described rotary engine, symmetry is arranged on the outer fringe position below disk; Rotary engine comprises spark ignition engine, piston pump, fuel tank, water tank, infrared receiver control setup and horizontal nozzles.
8. flying saucer as claimed in claim 5, is characterized in that:
Described circular wing, shape can be considered the secondary rotor rotational track of a week, and its blade one end is connected with hub shaft hole, and the other end is connected with steel ring axis hole, and multiple blade laminates successively, and all forms an elevation angle with horizontal surface, and the rotation of blade is by servos control.
9. flying saucer as claimed in claim 1, is characterized in that:
Described vector spray, it is anterior connects with a ball valve sealing, and direction and angle can adjust at any time, both can vertically downward, again can be horizontally outward.
10. flying saucer as claimed in claim 9, is characterized in that:
Described fixing aerofoil, shape is as trapezoidal, and amount to 4, symmetry is arranged on outside the bulkhead of equipment compartment.
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| CN106152123A (en) * | 2016-08-25 | 2016-11-23 | 易瓦特科技股份公司 | It is applied to the flame device of unmanned plane |
| CN106152123B (en) * | 2016-08-25 | 2018-12-18 | 易瓦特科技股份公司 | Flame device applied to unmanned plane |
| CN107054668A (en) * | 2017-01-20 | 2017-08-18 | 成都前沿动力科技有限公司 | A kind of stealthy unmanned plane based on electronic Wo Pen VTOL Flying-wing |
| CN110914151A (en) * | 2017-03-13 | 2020-03-24 | 桑迪普·古玛·钦塔拉 | Aircraft with bladeless propeller |
| CN109283868A (en) * | 2018-08-24 | 2019-01-29 | 江西洪都航空工业集团有限责任公司 | A method of it reissues and starts bicycle and motorcycle and cutoff command |
| CN110201337A (en) * | 2019-06-28 | 2019-09-06 | 湖南工业大学 | It is a kind of can autonomous flight high-pressure nozzle and its application |
| CN110201337B (en) * | 2019-06-28 | 2023-10-13 | 湖南工业大学 | High-pressure spray head capable of independently flying and application thereof |
| CN110963035A (en) * | 2019-12-18 | 2020-04-07 | 王力丰 | Personal aircraft with compressed air as power source and operation method thereof |
| CN111204455A (en) * | 2020-03-12 | 2020-05-29 | 王略 | Disc-wing machine |
| CN112158325A (en) * | 2020-09-30 | 2021-01-01 | 浙江大学 | Tailstock type vertical take-off and landing unmanned aerial vehicle and control method thereof |
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Application publication date: 20160210 |