CN104648671A - Manned flying saucer - Google Patents
Manned flying saucer Download PDFInfo
- Publication number
- CN104648671A CN104648671A CN201310577215.5A CN201310577215A CN104648671A CN 104648671 A CN104648671 A CN 104648671A CN 201310577215 A CN201310577215 A CN 201310577215A CN 104648671 A CN104648671 A CN 104648671A
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- Prior art keywords
- vacuum chamber
- flying saucer
- rotor
- air
- leading engine
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- 240000002836 Ipomoea tricolor Species 0.000 title claims abstract description 53
- 238000007789 sealing Methods 0.000 claims description 24
- 229910052751 metal Inorganic materials 0.000 claims description 20
- 239000002184 metal Substances 0.000 claims description 20
- 239000007788 liquid Substances 0.000 claims description 17
- 230000001419 dependent effect Effects 0.000 claims description 6
- 229920000642 polymer Polymers 0.000 claims description 6
- 230000003014 reinforcing effect Effects 0.000 claims description 6
- 238000007599 discharging Methods 0.000 claims description 5
- 230000006698 induction Effects 0.000 claims description 5
- 229910001069 Ti alloy Inorganic materials 0.000 claims description 3
- 229910045601 alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 230000005672 electromagnetic field Effects 0.000 claims description 3
- 238000004804 winding Methods 0.000 claims description 3
- 108010066114 cabin-2 Proteins 0.000 description 8
- 238000010586 diagram Methods 0.000 description 6
- 239000000463 material Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 239000000284 extract Substances 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 235000001674 Agaricus brunnescens Nutrition 0.000 description 1
- 241000242583 Scyphozoa Species 0.000 description 1
- 230000003042 antagnostic effect Effects 0.000 description 1
- 230000000740 bleeding effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000001186 cumulative effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000013505 freshwater Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000013535 sea water Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
The invention provides a manned flying saucer, relating to the technical field of aircrafts. The manned flying saucer comprises an electric automatic control system, a first-grade vacuum chamber and a second-grade vacuum chamber. A solar cell panel is installed on the top of the first-grade vacuum chamber; the second-grade vacuum chamber is arranged outside the first-grade vacuum chamber; a direct-current motor system is mounted on the bottom of the first-grade vacuum chamber and comprises a main engine rotor and stators locating at both sides of the main engine rotor; a storage battery pack is arranged around the direct-current motor system; a personnel cabin and a magazine are arranged at the periphery of the direct-current motor system; an auxiliary engine is arranged at the bottom of the second-grade vacuum chamber; air suction windows are arranged along the outer edge of the manned flying saucer; an atmospheric pressure highly-sensitive sensor is arranged at the lower end of the second-grade vacuum chamber and between the personnel cabin and the magazine; and a vertical-lift air suction window is arranged at the connection place of the second-grade vacuum chamber and the first-grade vacuum chamber. The manned flying saucer provided by the invention takes off and lands steadily, can stay in air for a long time and fly at a fast speed, is exempt from interference of electric waves and influence of road and weather conditions, is safe in flight, occupies a small area when landing and is especially applicable to aerial surveillance, command and urgent repair in the industries like the power supply industry, traffic and marine accident rescue, anti-terrorism and antiriot action and police enforcement.
Description
Technical field
The present invention relates to vehicle technology field, specifically a kind of manned flying saucer.
Background technology
Existing manned craft, mainly contains spacecraft, autogyro, aircraft etc.Autogyro is mainly used in the low-latitude flying performing special duty, and adopt screw propeller as flying power, speed is slow, and energy consumption is large, and flight environment of vehicle requires high, but is then difficult to be used widely as aerial manned vehicle.And existing all kinds of aircraft, landing environment limits by multiple condition, airflight complicated operation, cannot vertical takeoff and landing, and manipulation is inconvenient.Society, along with the development of material science and computer autocontrol technique and high dependent sensor, the folding of the air-breathing window of the novel high-elastic smooth material required for front suction flying method is made to be easy to control, air tight, and adjustment controls precisely, high dependent sensor makes every data messages such as the use of the draught head of flying saucer, dish body tilt vector, electric energy more easily collect grasp.The breakthrough of large engine technique, the appearance of high-effect battery, more solid foundation has been established in the real realization developing into flying saucer of field of solar energy utilization.Also have prior be exactly electromagnetism mechanics, the research of the magneto-mechanical principle of physics to manned flying saucer provides theoretical basis.
Summary of the invention
For overcoming the deficiencies in the prior art, goal of the invention of the present invention is to provide a kind of manned flying saucer, to realize the fast and pulsation-free object of ride comfort safety and flying speed.
For achieving the above object, the present invention includes automatic electrical control system, secondary vacuum cabin is set outside one-level vacuum chamber, solar panel is equipped with on the top of one-level vacuum chamber, direct current motor system is contained in the bottom of one-level vacuum chamber, direct current motor system comprises the leading engine stator of leading engine rotor and leading engine rotor both sides, and battery pack is arranged around direct current motor system, and the outer of direct current motor system is arranged with personnel's passenger cabin and magazine; Secondary engine is arranged on the bottom in secondary vacuum cabin; The level and smooth continuous arrangement of air-breathing window encloses in the disc outer one of flying saucer; Air pressure height dependent sensor is arranged on one-level vacuum chamber lower end and between personnel's passenger cabin and magazine; Go straight up to the joining place that air-breathing window is arranged on secondary vacuum cabin and one-level vacuum chamber.
Described leading engine rotor is made up of with the spiral fashion Polymer screw propeller spoke be attached thereto the rotor wheel rim of its periphery, rotor wheel rim is permanent magnet, the top of leading engine rotor is provided with arch support, the below of leading engine rotor is provided with lower arch support, and the center of leading engine rotor is the eccentric axial connecting rod of fixing leading engine rotor; The winding of leading engine stator has four groups, two groups of cws around, two groups of conter clockwises around, form electromagnetic field N pole and the S pole of leading engine stator.
Described upper arch support is made up of the titanium alloy reinforcing bar one that many are connected with axle center.
Described lower arch support is made up of the alloy reinforcing bar two that many are connected with axle center, and the bottom of lower arch support is provided with sealing hatch door.
Described sealing hatch door is with discharging gas or liquid dielectric and the elasticity folding rubber hole that gas or liquid dielectric can not be made to enter, elasticity folding rubber pore area has soft rubber air valve, the middle part of soft rubber air valve is provided with hard tracheae, hard tracheae, on have induction opening, deflation hole, hard tracheae with sealing hatch door be connected.
The stators and rotators of described secondary engine links together, with axle center draw-in groove on rotor, one end of kinematic link is connected with axle center draw-in groove, the other end is connected with propeller, stators and rotators is equipped with N pole and S pole, sealing hatch door is provided with below each secondary engine, the elasticity folding rubber hole that sealing hatch door can not make gas or liquid dielectric enter with discharging gas or liquid dielectric, elasticity folding rubber pore area has soft rubber air valve, the middle part of soft rubber air valve is provided with hard tracheae, hard tracheae there is induction opening, deflation hole, hard tracheae is connected with sealing hatch door.
Described secondary vacuum cabin is with multiple air-breathing windows that flying saucer can be made to carry out turn to, be can the trapezoidal outer side window frame of fixing metal curtain outside air-breathing window, inner side is for padding the trapezoidal inside window frame of metal curtain, metal curtain is with openwork part, the upper and lower edge of metal curtain is respectively equipped with a line engaging hole, and two turning cylinders are fixed between trapezoidal outer side window frame, trapezoidal inside window frame, with engaging tooth on turning cylinder, turning cylinder rotates, and drives the positive and negative movement of metal curtain.
The lift-off of manned flying saucer adopts most of air of top one-level vacuum chamber of finding time, and with the screw propeller of time image helicopter like that to below forces air, makes flying saucer increase by antagonistic force.Because air in cabin is pumped, vacuum chamber body is huge simultaneously, flying saucer global density is less than the density of equal-volume air, flying saucer is made to be gone up to the air as fire balloon and suspend completely, thus break away from the impact that gravity flies on flying saucer, not only overcome the impact of gravity but also lift can be provided for inhaling flight before next step.Before utilizing secondary vacuum cabin and the secondary engine implementation of the high speed below it during flying saucer flight, air-breathing is flown and the motor-driven adjustment of height.
Lift-off mode of the present invention, for going straight up to, is widely used in tourism, goes sightseeing, takes the fields such as inspection, exploration, power supply, rescue, tracking, Construction of High-rise, have the following advantages:
1, landing is steady, can do aerial stop for a long time, and flying speed is fast, and F-Zero can reach 1500km/h;
2, not by wave interference, not by road and weather effect;
3, be particularly suitable for the industry air surveillances such as power supply, commander and repairing, traffic and casualty rescue, fight against terrorism and violence and police execution;
4, airflight safety, landing floor area is little.
Accompanying drawing explanation
Fig. 1 is structural representation sketch of the present invention.
Fig. 2 is leading engine stator and the rotator model figure of Fig. 1.
Fig. 3 is the leading engine rotor arch support structures schematic diagram of Fig. 1.
Fig. 4 is the lower arch support structures schematic diagram of Fig. 3.
Fig. 5 is the upper arch support structures schematic diagram of Fig. 3.
Fig. 6 is the sealed module door system structural representation of Fig. 3.
Fig. 7 is the secondary engine structure schematic diagram of Fig. 1.
Fig. 8 is the sealed module door system schematic diagram of Fig. 6.
Fig. 9 is the longitudinal diagram of the air-breathing window in Fig. 1 secondary vacuum cabin.
Figure 10 is air-breathing window roller shutter structure figure.
Figure 11 is the distribution graph of air-breathing window.
Detailed description of the invention
As shown in Figure 1, the present invention includes automatic electrical control system, secondary vacuum cabin 2 is set outside one-level vacuum chamber 1, two vacuum chamber upper part form the arch of a continuously smooth, ensure that two vacuum chambers are not subject to air pressure crimp to greatest extent, one-level vacuum chamber 1 accounts for 85% of flying saucer cumulative volume, secondary vacuum cabin 2 can be flight or submerge provides motive power, and quick adjusting can be carried out to flying saucer attitude, ensure that flying saucer can out of control, manipulation error, carry out adjustment rapidly when breaking down and face a danger to dodge at a high speed, solar panel 3 top of one-level vacuum chamber 1 is equipped with, direct current motor system is contained in the bottom of one-level vacuum chamber 1, direct current motor system comprises the leading engine stator 6 of leading engine rotor 5 and leading engine rotor 5 both sides, battery pack 8 is arranged on around direct current motor system, the outer of direct current motor system is arranged with personnel's passenger cabin and magazine 7, can be manned, also cannon can be installed additional, radar, electronics, laser equipment, even hang bomb, Airforce Missile, secondary engine 4 is arranged on the bottom in secondary vacuum cabin 2, the level and smooth continuous arrangement of air-breathing window 9 encloses in the disc outer one of flying saucer, air pressure height dependent sensor 10 is arranged on one-level vacuum chamber 1 lower end and between personnel's passenger cabin and magazine 7, go straight up to the joining place that air-breathing window 11 is arranged on secondary vacuum cabin 2 and one-level vacuum chamber 1.
The upper surface of the whole mushroom umbrella one-level vacuum chamber 1 of flying saucer sticks solar panel 3, for battery pack 8 provides electric energy, for the rotating shaft of the air-breathing window 9 in leading engine, secondary engine 4, secondary vacuum cabin 2 and automatic electrical control system provide stable sufficient electric energy after battery pack 8 is full of electric energy.
Flying saucer can go up to the air, fly and the key of the motor-driven adjustment of height be exactly by vacuum chamber and ambient pressure poor.So, the material of one-level vacuum chamber 1 and secondary vacuum cabin 2 shell must very strongly can not be shriveled by draught head, when leading engine rotor 5 rotates and bleeds, air pressure height dependent sensor 10 record the inner and outer air pressure difference of one-level vacuum chamber 1 suitable time (draught head namely in ambient pressure and one-level vacuum chamber 1 reaches standard value P(according to formula quality=density * volume, can calculate density of air in one-level vacuum chamber=with the quality of the isopyknic air of whole flying saucer (according to seawer quality during submerge) quality-flying saucer betal can) volume of/whole flying saucer, density-atmospheric envelope gas density in one-level vacuum chamber inner and outer air pressure difference P=(vacuum chamber) * constant) time, automatic electrical control system gives leading engine power-off automatically, the soft rubber air valve of the female shape of each pouring of lower arch support base is when ambient pressure is much larger than interior boundary's air pressure, be squeezed tightly between and be adjacent on elasticity folding rubber hole, gas or liquid all cannot enter in one-level vacuum chamber 1.Gas in one-level vacuum chamber 1 is thin, reduces the global density of flying saucer, and flying saucer can be made to float.Then, medium constantly sucks and extracts out by ten secondary engines 4 under the control of automatic electrical control system, drives flying saucer to move ahead, and ensures to inhale navigation and adjustment at a high speed before flying saucer rapidly.Flying saucer also can realize suspending in water by taking part water away and closing vacuum chamber in seawater, fresh water.
As shown in Fig. 2, Fig. 3, Fig. 4, Fig. 5, Fig. 6, Fig. 8, leading engine is the maximum power source of flying saucer, and diameter is close to 10 meters.Leading engine rotor 5 is made up of with the spiral fashion Polymer screw propeller spoke 13 be attached thereto the rotor wheel rim 12 of its periphery, rotor wheel rim 12 is permanent magnet, the top of leading engine rotor 5 is provided with arch support 14, the below of leading engine rotor 5 is provided with lower arch support 15, the center of leading engine rotor 5 is the eccentric axial connecting rod 16 of fixing leading engine rotor 5, and eccentric axial connecting rod 16 is connected with direct current motor system; The winding of leading engine stator 6 has four groups, two groups of cws around, two groups of conter clockwises around, form electromagnetic field N pole and the S pole of leading engine stator 6; Described upper arch support 14 is made up of the titanium alloy reinforcing bar 1 that nine are connected with axle center 22; Described lower arch support 15 is made up of the alloy reinforcing bar 2 19 that three are connected with axle center 20, and the bottom of lower arch support 15 is provided with sealing hatch door 17; Described sealing hatch door 17 is with discharging gas or liquid dielectric and the elasticity folding rubber hole 18 that gas or liquid dielectric can not be made to enter.
The spiral fashion Polymer screw propeller spoke 12 of flying saucer leading engine rotor 5, all by the battery pack driven rotary of direct current motor system, because DC motor speed-regulating performance is good, starts braking torque large, is easy to control.And the electric energy of flying saucer is mainly by solar cell, battery directly supplies direct current (DC), so be more not suitable for adopting alternating current dynamo.
Leading engine rotor 5 can be subject to powerful atmospheric pressure from bottom to top after taking most of air of one-level vacuum chamber away.So, above and below leading engine rotor 5, be all provided with the support of arch.Leading engine rotor 5 self is exactly one and is made up of with the gossamery screw propeller spoke 13 of a lot of bar spiral fashion Polymers be attached thereto the permanent magnet rotor wheel rim 12 of periphery, rotor wheel rim 12 is under the magnetic field that the rotation of leading engine stator changes, be subject to the promotion of magnetic torque and High Rotation Speed, spiral fashion spoke 13 is the high speed rotating along with the rotation of rotor wheel rim 12 just, screw propeller spoke 13 constantly cuts the air of top and shift below onto among rotation, thus the air molecule constantly taken away above leading engine also pushes away fiercely immediately below flying saucer.Because leading engine rotor 5 is very large, power is also very large, there is very large draft, when the air pressure above leading engine rotor 5 too low and turn motionless time, the inner and outer air pressure difference of one-level vacuum chamber may cause lower air to pour in down a chimney one-level vacuum chamber above rotor, so, very large on the one hand to the power designs of leading engine, on the one hand when one-level vacuum chamber gas is thin in flying saucer can be made to float, the sealed module door system below leading engine rotor 5 closes sealing at once.
The bleeding point of flying saucer---sealed module door system can only discharge gas or liquid dielectric and gas liquid medium can not be made to enter the elasticity folding rubber hole 18 of one-level vacuum chamber.
Under the pushing that gas rotates at the spiral fashion Polymer screw propeller spoke 13 of leading engine rotor 5, enter lower arch support 15 and elasticity folding rubber hole 18, the soft rubber air valve 29 in elasticity folding rubber hole 18 large upside down, elasticity folding rubber hole 18 is with soft rubber air valve 29, the middle part of soft rubber air valve 29 is provided with hard tracheae 28, hard tracheae 28 has induction opening, deflation hole, hard tracheae 28 is connected with sealing hatch door 17.After air-flow is pushed hard tracheae 28, the air flow line as indication in Fig. 8 is flowed out from the gap at edge, if the gas pressure difference of outer bound pair one-level vacuum chamber, be not sufficient to the soft rubber air valve 29 of jellyfish shape to be pressed on sealing hatch door 17, so gas medium still can from one-level vacuum chamber wash open soft rubber air valve 29 spray, if one-level vacuum chamber gas is enough thin, external pressure will compress and kills soft rubber air valve 29 thus seal up sealing hatch door 17, in any case gas can not flow out from one-level vacuum chamber.Like this, just ensure that the sealing of one-level vacuum chamber.
By the time, time flying saucer floats slightly, automatic electrical control system is to leading engine power-off, and sealed module door system closes sealing at once, internal gas no longer flows out, now under external atmosphere pressure, elasticity folding rubber hole 18 is shut, and extraneous gas still can not enter in cabin.
As shown in Figure 7, stator 23 and the rotor 24 of described secondary engine 4 link together, with axle center draw-in groove 27 on rotor 24, one end of kinematic link 25 is connected with axle center draw-in groove 27, the other end is connected with propeller 26, stator 23 and rotor 24 are equipped with N pole and S pole, sealing hatch door is provided with below each secondary engine 4, sealing hatch door is the elasticity folding rubber hole 18 that secondary vacuum cabin 2 can be made can only to discharge gas or liquid dielectric and gas or liquid dielectric can not be made to enter, and elasticity folding rubber hole 18 is with soft rubber air valve 29.
As shown in Fig. 9, Figure 10, Figure 11, Fig. 9 is also the drawing in side sectional elevation of flying saucer along air-breathing window aspect, secondary vacuum cabin 2 with six air-breathing windows that flying saucer can be made to carry out turning to, every 30 degree, central angle have a fan be the air-breathing window 9 of 30 degree to central angle.Be can the trapezoidal outer side window frame 31 of fixing metal curtain 30 outside air-breathing window 9, inner side is for padding the trapezoidal inside window frame 32 of metal curtain 30, metal curtain 30 is with openwork part 34, the lower edges of metal curtain 30 is respectively equipped with a line engaging hole 35, two, air-breathing window 9 both sides of the edge turning cylinder 33 is fixed between trapezoidal outer side window frame 31, trapezoidal inside window frame 32, with engaging tooth on turning cylinder 33, turning cylinder 33 rotates, and drives the positive and negative movement of metal curtain 30.Secondary vacuum cabin is the passage of gas or liquid dielectric.Medium constantly sucks and extracts out by secondary engine, drives flying saucer to move ahead.Also under air-breathing window 9 sealing state, constantly can finding time or be charged into air in cabin in secondary vacuum cabin, strengthens inner and outer air pressure poor, then open air-breathing window, and flying saucer is adjusted and accelerates flight suddenly.Air-breathing window is evenly distributed on disc edge, has one section of opening portion accounting for 30 degree of camber lines, as air-breathing window 9 every 30 degree.Such flying saucer can carry out 360 degree and turn to arbitrarily.Air-breathing window 9 has three, upper, middle and lower district, goes straight up to air-breathing window and flying saucer can also be made to go straight up to rapidly.Roller shutter structure is taked in the folding of air-breathing window 9, at air-breathing window one, two, 3rd district are respectively equipped with a respective scroll bar 33, the volume above of scroll bar 33 posts shape as film and with the high-molecule metal curtain 30 of openwork part 34, metal curtain 30 is pulled to aim at the opening portion of air-breathing window 9 housing with openwork part 34 by engaging tooth on scroll bar 33 and being engaged in engaging hole scrolling on curtain, realize the control to folding air intake window mouth 9, because the pressure of ambient atmos liquid dielectric is always greater than secondary vacuum cabin, so high-molecule metal curtain 30 is tightly attached on air-breathing window by the pressure in the external world completely to the sealing in secondary vacuum cabin, as long as the trapezoidal outer side window frame 31 of window fixes metal curtain 30, trapezoidal inside window frame 32 make metal curtain 30 pad be pressed on, just can ensure the leak tightness in secondary vacuum cabin.
Claims (7)
1. a manned flying saucer, it is characterized in that: comprise automatic electrical control system, secondary vacuum cabin (2) is set outside one-level vacuum chamber (1), solar panel (3) top of one-level vacuum chamber (1) is equipped with, direct current motor system is contained in the bottom of one-level vacuum chamber (1), direct current motor system comprises the leading engine stator (6) of leading engine rotor (5) and leading engine rotor (5) both sides, battery pack (8) is arranged on around direct current motor system, and the outer of direct current motor system is arranged with personnel's passenger cabin and magazine (7); Secondary engine (4) is arranged on the bottom of secondary vacuum cabin (2); The level and smooth continuous arrangement of air-breathing window (9) encloses in the disc outer one of flying saucer; Air pressure height dependent sensor (10) is arranged on one-level vacuum chamber (1) lower end and between personnel's passenger cabin and magazine (7); Go straight up to the joining place that air-breathing window (11) is arranged on secondary vacuum cabin (2) and one-level vacuum chamber (1).
2. manned flying saucer according to claim 1, it is characterized in that: described leading engine rotor (5) is made up of the rotor wheel rim (12) of its periphery and spiral fashion Polymer screw propeller spoke (13) that is attached thereto, rotor wheel rim (12) is permanent magnet, the top of leading engine rotor (5) is provided with arch support (14), the below of leading engine rotor (5) is provided with lower arch support (15), and the center of leading engine rotor (5) is the eccentric axial connecting rod (16) of fixing leading engine rotor (5); The winding of leading engine stator (6) has four groups, two groups of cws around, two groups of conter clockwises around, form electromagnetic field N pole and the S pole of leading engine stator (6).
3. manned flying saucer according to claim 2, is characterized in that: described upper arch support (14) is made up of the titanium alloy reinforcing bar one (21) that many are connected with axle center (22).
4. manned flying saucer according to claim 2, is characterized in that: described lower arch support (15) is made up of the alloy reinforcing bar two (19) that many are connected with axle center (20), and the bottom of lower arch support (15) is provided with sealing hatch door (17).
5. manned flying saucer according to claim 4, it is characterized in that: described sealing hatch door (17) is with discharging gas or liquid dielectric and the elasticity folding rubber hole (18) that gas or liquid dielectric can not be made to enter, elasticity folding rubber hole (18) is with soft rubber air valve (29), the middle part of soft rubber air valve (29) is provided with hard tracheae (28), (28) have induction opening, deflation hole to hard tracheae, and hard tracheae (28) is connected with sealing hatch door (17).
6. manned flying saucer according to claim 1, it is characterized in that: stator (23) and the rotor (24) of described secondary engine (4) link together, with axle center draw-in groove (27) on rotor (24), one end of kinematic link (25) is connected with axle center draw-in groove (27), the other end is connected with propeller (26), stator (23) and rotor (24) are equipped with N pole and S pole, sealing hatch door (17) is provided with below each secondary engine (4), the elasticity folding rubber hole (18) that sealing hatch door (17) can not make gas or liquid dielectric enter with discharging gas or liquid dielectric, elasticity folding rubber hole (18) is with soft rubber air valve (29), the middle part of soft rubber air valve (29) is provided with hard tracheae (28), (28) have induction opening to hard tracheae, deflation hole, hard tracheae (28) is connected with sealing hatch door (17).
7. manned flying saucer according to claim 1, it is characterized in that: described secondary vacuum cabin (2) is with multiple air-breathing windows (9) that flying saucer can be made to carry out turn to, air-breathing window (9) outside is can the trapezoidal outer side window frame (31) of fixing metal curtain (30), inner side is for padding the trapezoidal inside window frame (32) of metal curtain (30), metal curtain (30) is with openwork part (34), metal curtain (30) upper, lower edge is respectively equipped with a line engaging hole (35), two turning cylinders (33) are fixed on trapezoidal outer side window frame (31), between trapezoidal inside window frame (32), with engaging tooth on turning cylinder (33), turning cylinder (33) rotates, drive metal curtain (30) positive and negative movement.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310577215.5A CN104648671A (en) | 2013-11-19 | 2013-11-19 | Manned flying saucer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310577215.5A CN104648671A (en) | 2013-11-19 | 2013-11-19 | Manned flying saucer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104648671A true CN104648671A (en) | 2015-05-27 |
Family
ID=53240405
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310577215.5A Pending CN104648671A (en) | 2013-11-19 | 2013-11-19 | Manned flying saucer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104648671A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109319114A (en) * | 2018-09-06 | 2019-02-12 | 武汉豪岩照明电子有限公司 | A kind of dish gas curtain aeromodelling aerocraft |
| CN109462345A (en) * | 2018-12-14 | 2019-03-12 | 华北水利水电大学 | A kind of magnetic suspension mixing engine |
| EP3418193A4 (en) * | 2016-02-16 | 2019-10-02 | Shandong Natergy Energy Technology Co., Ltd. | Aircraft |
-
2013
- 2013-11-19 CN CN201310577215.5A patent/CN104648671A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3418193A4 (en) * | 2016-02-16 | 2019-10-02 | Shandong Natergy Energy Technology Co., Ltd. | Aircraft |
| CN109319114A (en) * | 2018-09-06 | 2019-02-12 | 武汉豪岩照明电子有限公司 | A kind of dish gas curtain aeromodelling aerocraft |
| CN109462345A (en) * | 2018-12-14 | 2019-03-12 | 华北水利水电大学 | A kind of magnetic suspension mixing engine |
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Application publication date: 20150527 |