CN112124592B

CN112124592B - Disk type flying device capable of vertically lifting

Info

Publication number: CN112124592B
Application number: CN202011046699.7A
Authority: CN
Inventors: 张京生
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-09-29
Filing date: 2020-09-29
Publication date: 2022-04-12
Anticipated expiration: 2040-09-29
Also published as: CN112124592A

Abstract

The invention relates to the technical field of aircrafts, and particularly discloses a disk type flying device capable of vertically lifting, which comprises a shell, wherein three electric lifting undercarriages are hinged to the lower end face of each electric lifting undercarriage in an array mode, a cockpit is rotatably mounted above the center of the shell, a control console is fixed inside the cockpit through screws, a fixing frame is fixed in the center of the shell through screws, an energy module is fixed inside the fixing frame through a clamping groove, a rotating motor is fixed in the center of the upper end of the fixing frame through screws, the upper rotating key of the rotating motor is connected with the cockpit, and a second power device is fixed in the center of the lower end of the fixing frame through screws. Has the advantages that: 1. the jet power, the rotary wing power and the thermal power are combined for use, so that the lifting effect is good, and the energy is saved; 2. the vertical take-off and landing saves the area of an airport; 3. the disk type modeling has streamlined appearance, good stability of resisting crosswind and small air resistance.

Description

Disk type flying device capable of vertically lifting

Technical Field

The invention relates to the technical field of aircrafts, in particular to a disk type flying device capable of vertically lifting.

Background

An aircraft is an instrumental flying object made by humans, capable of flying off the ground, flying in space and controlled by humans, flying in the atmosphere or in the extraterrestrial space (space). Flying in the atmosphere is called aircraft and flying in space is called spacecraft.

Although current jet propulsion technology in the aerospace field allows aircraft to fly at speeds in excess of sonic speeds and even up to third cosmic speeds, these designs suffer from the following problems and disadvantages: if the jet propulsion technology is applied to an aircraft with a flying saucer shape, the direction of an air jet opening of the jet propulsion technology needs to be arranged at a position (the side surface of a shell) opposite to the horizontal advancing direction of an aircraft body, so that the optimal shape of the aircraft on the horizontal plane can only be the streamline shape similar to that of the current jet aircraft in order to reduce the air resistance during advancing, however, the aircraft without a perfect circular plane structure is not in the category of structural modeling of a disc aircraft.

If the past "artificial flying saucer" used a standard perfect circle shape and the helicopter "rotorcraft" to generate vertical power. When the horizontal direction flight is needed, the prior art method of changing the rotor angle can be adopted to generate horizontal thrust. The problem is that the disc surface of the artificial flying disc needs to be hollow up and down, the disc body loses the capability of utilizing the lifting force of the hot air rising from the ground, and a large amount of fuel is used in the process of hovering and horizontal flight in the air. Therefore, the "artificial flying saucer" manufactured by the "rotor method" in the past is actually a "disc-type helicopter". Because of the extra weight of the disc structure support, the fuel consumption of the disc structure support is larger than that of a helicopter, and the effective volume of a cabin is smaller than that of the helicopter. Has no practical application value.

Disclosure of Invention

The invention provides a disk type flying device capable of vertically lifting in order to solve the problems.

The technical scheme of the invention is realized as follows:

a disk type flying device capable of vertically lifting comprises a shell, wherein three electric lifting undercarriages are hinged on the lower end face of the shell in an array mode, a cockpit is rotatably installed above the center of the shell, a control console is fixed inside the cockpit through screws, a fixing frame is fixed in the center of the shell through screws, an energy module is fixed inside the fixing frame through a clamping groove, a rotating motor is fixed in the center of the upper end of the fixing frame through screws, the cockpit is connected with the rotating upper key of the rotating motor, a second power device is fixed in the center of the lower end of the fixing frame through screws, a navigation gyroscope is fixed inside the cockpit through screws, the electric lifting undercarriages, the control console, the rotating motor, the navigation gyroscope, the second power device and the first power device are all electrically connected with the energy module, the control console is connected with the electric lifting landing gear, the rotating motor, the navigation gyroscope, the second power device and the first power device through wireless signals.

Furthermore, four ventilation windows are arranged on the upper surface of the shell in an annular array mode, sealing doors are arranged on the lower surfaces of the ventilation windows, one ends of the sealing doors are fixed to the inner wall of the shell through hinge pins, door opening motors are connected to fixed hinge pins of the sealing doors in a transmission mode, the door opening motors are electrically connected with the energy module, and the door opening motors are connected with the console through wireless signals.

Furthermore, 3-8 first power devices are fixed on the periphery of the second power device in an annular array mode, the first power devices are jet engines, the first power devices are fixed on the fixing frame through rotation, the jet angle of the first power devices can be adjusted, the first power devices are electrically connected with the energy module, and the first power devices are connected with the control console through wireless signals.

Further, the second power device comprises a fixed seat, the fixed seat is fixed to the center of the lower surface of the fixed frame through screws, a transmission shaft is fixed to the inside of the fixed seat through a bearing, a lifting motor is connected to the upper end of the transmission shaft in a transmission mode, a paddle fixing disc is installed at the lower end of the transmission shaft in a rotating mode, four propeller blades are fixed to the paddle fixing disc through a pin shaft annular array, the lifting motor is electrically connected with the energy module, and the lifting motor is connected with the control console through wireless signals.

Further, paddle fixed disk upper surface edge has inclination adjustment rod through round pin hub fixation, inclination adjustment rod is close to propeller blade's stiff end sets up, the inclination adjustment rod other end is fixed on the carousel through the round pin axle, the carousel passes through the bearing and rotates and install on the fixing base outer wall, inclination adjustment rod is electronic pole, inclination adjustment rod with the energy module electricity is connected, inclination adjustment rod pass through radio signal with the control cabinet is connected.

Further, a plurality of illuminating lamps are embedded in the annular arrays at the lower end edge and the lower surface edge of the shell, the illuminating lamps are electrically connected with the energy module, and the illuminating lamps are connected with the console through wireless signals.

Furthermore, the cockpit is fixed on the fixing frame through a bearing, two bidirectional thrust bearings are arranged on the upper surface and the lower surface of the fixed position of the cockpit and the fixing frame, and a radial rotating bearing is arranged on the fixed position rotating shaft side of the cockpit and the fixing frame.

Further, the rotation direction of the cab is opposite to the rotation direction of the second power device.

By adopting the technical scheme, the invention has the beneficial effects that: 1. the jet power, the rotary wing power and the thermal power are combined for use, so that the lifting effect is good, and the energy is saved; 2. the vertical take-off and landing saves the area of an airport; 3. the disc type modeling has streamlined appearance, good stability of resisting cross wind and small air resistance; 4. the rotating shafts of the main large-mass components such as the fixed frame, the second power device and the like are positioned at the circle center of the shell (vertical to the horizontal plane), and the generated integral gyro effect has a good stabilizing effect on the flying of the disk type flying device in the air; 5. first power device and second power device all set up in the casing, reducible accident that causes with birds collision when aerial horizontal flight.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

FIG. 1 is a front cross-sectional view of the present invention;

FIG. 2 is a front view of the present invention;

FIG. 3 is a schematic structural view of a second power plant of the present invention;

FIG. 4 is a top view of the present invention;

FIG. 5 is a bottom view of the present invention;

FIG. 6 is a schematic view of the horizontal movement of the present invention;

fig. 7 is a block diagram of the circuit configuration of the present invention.

The reference numerals are explained below:

1. an electric lifting undercarriage; 2. a housing; 3. a sealing door; 4. a ventilation window; 5. a door opening motor; 6. an energy module; 7. a console; 8. a cockpit; 9. a rotating electric machine; 10. a navigation gyroscope; 11. a fixed mount; 12. a second power unit; 13. a first power unit; 14. a hoisting motor; 15. a drive shaft; 16. a fixed seat; 17. a paddle fixing tray; 18. a propeller blade; 19. an inclination angle adjusting rod; 20. a turntable; 21. an illuminating lamp.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The first embodiment is as follows:

as shown in fig. 1-7, a disk type flying device capable of vertically lifting comprises a casing 2, three electric lifting undercarriages 1 are hinged on the lower end face of the casing 2 in an array manner, the structure of the disk type flying device is like that of an airplane undercarriage, the disk type flying device can be folded when not in use and can be put down when in use, a cockpit 8 is rotatably arranged above the center of the casing 2, a control console 7 is fixed inside the cockpit 8 through screws, a flight control system is arranged in the control console 7, a fixing frame 11 is fixed in the center of the casing 2 through screws, an energy module 6 is fixed inside the fixing frame 11 through a clamping groove, the energy module 6 is a battery or an internal combustion generator capable of storing electric energy and used for providing energy, a rotating motor 9 is fixed in the center of the upper end of the fixing frame 11 through screws, a rotating upper key of the rotating motor 9 is connected with the cockpit 8 and can control the rotation of the cockpit 8, the utility model discloses a control system, including mount 11, power module 6, SCC1300, electric lift undercarriage 1, control cabinet 7, rotating electrical machines 9, navigation gyroscope 10, second power device 12, first power device 13 all is connected with energy module 6 electricity, control cabinet 7 passes through radio signal and electric lift undercarriage 1, rotating electrical machines 9, navigation gyroscope 10, second power device 12, first power device 13 is connected, control cabinet 7 is connected with energy module 6 electricity through rotatory brush, realize that the electric energy lasts the supply, realize the signal connection of control cabinet 7 and electrical equipment through radio signal, can avoid the trouble of wiring, avoid simultaneously influencing the use of signal transmission cable because cockpit 8 is rotatory indefinite.

In this embodiment, four ventilation windows 4 have been seted up to casing 2 upper surface annular array, the 4 lower surfaces of ventilation windows are provided with sealing

door

3, 3 one end of sealing door is fixed on the casing 2 inner wall through the round pin axle, sealing door 3's fixed round pin axle transmission is connected with door opening motor 5, door opening motor 5 is connected with energy module 6 electricity, door opening motor 5 passes through radio signal and is connected with control cabinet 7, when sealing door 3 blocks up in ventilation window 4 department, casing 2 forms a lower extreme open-ended enclosed construction (the structure is similar to the kongming lantern), the heat that produces in the during operation of second power device 12 can make the inside temperature of casing 2 rise, thereby produce certain thermodynamic, supplementary disc flying device flies.

In this embodiment, second power device 12 includes fixing base 16, fixing base 16 passes through fix with screw at 11 lower surface centers of mount, be fixed with transmission shaft 15 through the bearing in the fixing base 16, the transmission of 15 upper ends of transmission shaft is connected with lift motor 14, the 15 lower extremes of transmission shaft are rotated and are installed paddle fixed disk 17, be fixed with four propeller blades 18 through round pin axle annular array on the paddle fixed disk 17, lift motor 14 is connected with energy module 6 electricity, lift motor 14 passes through radio signal and is connected with control cabinet 7.

In this embodiment, paddle fixed disk 17 upper surface edge has inclination adjustment rod 19 through round pin hub fixation, inclination adjustment rod 19 is close to the stiff end setting of propeller blade 18, the 19 other end of inclination adjustment rod is fixed on carousel 20 through the round pin axle, carousel 20 passes through the bearing and rotates and install on the 16 outer walls of fixing base, inclination adjustment rod 19 is electronic pole, inclination adjustment rod 19 is connected with energy module 6 electricity, inclination adjustment rod 19 passes through radio signal and is connected with control cabinet 7, inclination adjustment rod 19 can drive paddle fixed disk 17 and take place the slope of certain angle, thereby change the direction of power.

In this embodiment, a plurality of illuminating lamps 21 are embedded in the annular arrays on the lower end edge and the lower surface edge of the shell 2 for illumination, the illuminating lamps 21 are electrically connected with the energy module 6, and the illuminating lamps 21 are connected with the console 7 through wireless signals.

In this embodiment, the cockpit 8 is fixed on the fixing frame 11 through a bearing, two bidirectional thrust bearings are mounted on the upper and lower surfaces of the fixed position of the cockpit 8 and the fixing frame 11, and a radial rotating bearing is mounted on the rotating shaft side of the fixed position of the cockpit 8 and the fixing frame 11, so that the torque (M1) of the bottom fixing frame 11 is reduced as much as possible and is transmitted to the cockpit 8 through contact friction to generate additional torque, and the rotating speed ω 1 of the "random rotation" of the cockpit 8 caused by the additional torque is reduced.

Since the friction cannot be completely removed, even if the rotation speed ω 1 is small, the cockpit 8 can cause the visual confusion of the cockpit driver, the unclear visibility of the stationary reference objects on the ground, and even the dizzy accident of the human body when the "random rotation" occurs, therefore, in the aspect of stable design of the cockpit 8, the "random rotation" of the cockpit 1 must be completely eliminated, and the rotation speed "ω 1 ≡ 0" of the random rotation is ensured.

To achieve the above object, the present invention adopts a "method of neutralizing the rotation speed", in which a rotating electrical machine 9 is provided on a floor of a cab 8 to rotate the cab 8 in the direction opposite to ω 1 (the rotation speed is ω 2), and ω 2 is opposite to ω 1, so that Σ ω is 0 as long as the absolute values of ω 2| ═ ω 1|, are equal. The actual effect of "ω 1 equals 0" can be achieved, the "random rotation" is eliminated, and the stability of the cockpit 8 is ensured.

Since M1, the friction force, and ω 1 change at any time during ascent and descent and acceleration/deceleration of the disk flight device, "the rotation speed ω 2 supplied to the cabin 8 by the rotating electrical machine 9 must also change while following the change described above, so as to ensure that | ω 2| ═ ω 1|, and Σ ω ═ 0, and eliminate the disturbance of ω 1 to the stability of the cabin 1 at any time.

The navigation gyroscope 10 is arranged to detect the rotation speed omega 1 of the cockpit 8 which generates the random rotation and the stable state of the cockpit 8, transmit the detected information to the console 7 with an automatic control system, automatically regulate and control the rotation speed (and the output torque) of the rotating motor 9 by the control system in the console 7, push (and adjust) the cockpit 8 to generate the rotation speed omega 2, keep | omega 2| ═ omega 1|, Σ omega ═ 0 at any time, and completely eliminate the random rotation to ensure the stability of the cockpit 8.

In this embodiment, the direction of rotation of the cabin 8 is opposite to the direction of rotation of the second power means 12.

Spiral power and thermal power are adopted for lifting and translating, and flying of the aircraft is achieved.

When taking off, the door opening motor 5 controls the top 4 sealing doors 3 of the shell 2 to be completely opened, the second power device 12 rotates to generate the maximum vertical lift force, the flying disc rises into the air, after the flying disc reaches a certain height of the ground, the door opening motor 5 controls the top 4 sealing doors 3 of the shell 2 to simultaneously and horizontally rotate, the ventilation window 4 of the ventilation part of the closed shell 2 during taking off is used for sealing the top surface of the shell 2, the inner cavity can store hot air caused by the work of an engine, therefore, the effect of 'hot air balloon lift force' is generated, meanwhile, the area of the fully-sealed shell 2 can effectively utilize the thrust generated when the ground hot air rises to generate the lift force, a driver can properly reduce the rotating speed of the second power device 12 according to the strength of the hot air, so as to save energy and prolong the suspension time of the disc type flying device.

When the disc type flying device rises to a certain height, when horizontal flying is needed, the inclination angle of the wing surface of the second power device 12 is changed (realized by controlling the extension and contraction of the inclination angle adjusting rod 19), so that the shell 2 (and the whole disc type flying device) inclines towards the advancing direction, then the rotating speed of the second power device 12 is reduced by a proper amount, the disc type flying device slightly falls, and then under the combined action of the gravity acceleration of the earth and the air resistance at the lower part of the disc body, the disc type flying device can dive towards the inclined direction to generate the needed horizontal flying speed.

When the second power device 12 rotates, the fixed frame 11 and the casing 2 rigidly connected with the fixed frame rotate in the direction opposite to the moving direction of air under the reaction of air resistance, so as to form a high-mass 'integral gyro rotor', thereby generating 'integral gyro effect', and effectively ensuring the aerial stability of the disk type flying device.

Example two:

the content of this embodiment is substantially the same as that of the first embodiment, except that:

in this embodiment, mount 11 lower surface does not have second power device 12, mount 11 lower surface annular array all around is fixed with 3-8 first power device 13, first power device 13 is jet engine, first power device 13 is fixed on mount 11 through rotating, the jet angle of first power device 13 is adjustable, first power device 13 is connected with energy module 6 electricity, first power device 13 passes through radio signal and is connected with control cabinet 7, adopt jet engine to produce the promotion power alone, realize the promotion flight of aircraft.

When the aircraft takes off, the gas nozzles of the first power device 13 are vertically downward, the ejected gas obtains the maximum upward thrust by utilizing the ground effect, after the aircraft is lifted to a certain height in the air, when the aircraft needs to fly in the horizontal direction, the directions of the gas nozzles of all the first power devices 13 are simultaneously changed to form a small angle opposite to the advancing direction, so that the shell 2 (and the whole disk type flying device) is inclined towards the advancing direction, then the flow of the gas ejected by the first power device 13 is properly reduced, so that the disk type flying device slightly falls, and then under the combined action of the gravity acceleration of the earth and the air resistance at the lower part of the disk body, the disk type flying device can dive towards the inclined direction to generate the required horizontal flying speed.

When the frisbee flies to a certain height from the ground, for keeping stable, preventing to take place to rock and the accident of turning on one's side in the air: two first power devices 13 are symmetrically changed by a small angle towards different directions at the same time, and the component of horizontal thrust in the ejected gas can cause the fixed frame 11 connected with the first power devices 13 and the shell 2 connected with the fixed frame to rotate towards the direction opposite to the air injection direction while keeping the thrust in the vertical direction, so that the fixed frame 11 (and the shell 2 rigidly connected with the fixed frame) is changed into a 'high-mass integral gyro rotor', and the 'integral gyro effect' generated by the rotation can provide effective guarantee for the aerial stability of the disk type flying device.

Example three:

in this embodiment, the lower surface of the fixing frame 11 is provided with the second power device 12 and the

first power device

13, 3 to 8 first power devices 13 are fixed on the periphery of the second power device 12 in an annular array, the first power device 13 is a jet engine, the first power device 13 is fixed on the fixing frame 11 through rotation, the jet angle of the first power device 13 is adjustable, the first power device 13 is electrically connected with the energy module 6, the first power device 13 is connected with the control console 7 through a wireless signal, three types of thermal power, jet power and rotary wing power are combined for use, the power is strong, and the lifting efficiency is improved.

When the flying disc type flying device is lifted vertically and moved horizontally, the first power device 13 or the second power device 12 can be selected to be started to generate power automatically, and flying of the flying disc type flying device is achieved.

As shown in fig. 6, the horizontal power of the disk-type flying device adopts "dip-dive method", after the disk-type flying device is raised to a certain height, the front part of the housing 2 (together with the bottom plane of the disk-type flying device) is tilted to the direction to be reached by an angle Φ about 20 ° away from the horizontal plane (the angle may not be too large to prevent instability), then the lift force of the power device is reduced by a proper amount to cause the disk-type flying device to slightly fall, the acceleration caused by the earth gravitational field and the upward resistance of the air at the bottom of the housing 2 are utilized to synthesize "power for accelerating and diving obliquely and downwards with offset" on the inclined plane at the bottom of the disk body ", so that the disk-type flying device obtains the sliding (linear) speed V0 (like the oblique downward diving of an aerial bird) consistent with the tilt angle Φ, and the speed V0 is increased along with the increase of the diving time t, and after the usage requirement of the pilot that V0 has a horizontal speed component Vx, the housing 2 (together with the disk flying device) can be horizontally pulled up and continues to glide forward by the inertial force.

If the departure point is far from the destination and the disc type flying device cannot arrive after one horizontal acceleration flight, the height of the disc type flying device can be lifted again before the horizontal speed Vx of the disc type flying device is reduced to the required lower limit by the air resistance, the horizontal acceleration action program of inclining, falling, diving and leveling is repeated, and the disc type flying device can arrive at the remote destination by continuously flying forwards.

In the flight, upwards rise a small angle to the dead ahead of casing 2, the resistance that increases the place ahead air just can slow down, if want scram, when the preliminary speed reduction of the front end that rises casing 2, reduce some vertical lift again, cause the aircraft to descend slightly, utilize "inclination dive method", make disk flying device produce backward (and below) dive acceleration, the speed that flies before the fast speed reduction, reach the mesh of scram, when beginning to slow down in flying fast, the angle that casing 2 front end rises can not be too big, prevent to take place the turn-buckle accident.

The horizontal turning is convenient, if the disk type flying device needs to turn to the right east for flying in the north-ward flight, the front end of the shell 2 can be lifted by a small angle to cause deceleration, then the console 7 is utilized to send a turning instruction of turning right by 90 degrees (the orientation is modified and corrected by combining the navigation gyroscope 10), the rotating motor 9 is controlled to change the direction of the cockpit 8 facing the north-ward from the original direction to the direction facing the right east, so that the cockpit and the body are facing the east (the cockpit and the base of the cockpit 8 are fixed into a whole), then the shell 2 is slightly inclined downwards by about 20 degrees (reference value) in the direction of the east-ward direction, meanwhile, the lift force is reduced by a proper amount, the disk type flying device slightly falls down, and then the disk type flying device can turn to the right east for diving under the action of the inclination angle diving method and then is leveled for flying.

When the horizontal state of the housing 2 needs to be automatically maintained, a key of an automatic horizontal state program can be started, and a computer system in the console 7 automatically adjusts the working angle of the first power device 13 or the second power device 12 by combining with the horizontal state information provided by the navigation gyroscope 10, so that the horizontal state of the disk type flying device in the air is automatically maintained.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.

Claims

1. A disk flying device capable of vertically lifting is characterized in that: including casing (2), the terminal surface goes up the array and articulates under casing (2) has three electric lift undercarriage (1), casing (2) central authorities top is rotated and is installed cockpit (8), cockpit (8) are inside to have control cabinet (7) through the fix with screw, casing (2) central authorities have mount (11) through the fix with screw, mount (11) are inside to be fixed with energy module (6) through the draw-in groove, mount (11) upper end central authorities have rotating electrical machines (9) through the fix with screw, the key connection is gone up in the rotation of rotating electrical machines (9) has cockpit (8), mount (11) lower extreme central authorities have second power device (12) through the fix with screw, there are navigation gyroscope (10) through the fix with screw in cockpit (8), electric lift undercarriage (1) control cabinet (7), The rotary motor (9), the navigation gyroscope (10) and the second power device (12) are electrically connected with the energy module (6), the console (7) is connected with the electric lifting undercarriage (1), the rotary motor (9), the navigation gyroscope (10) and the second power device (12) through wireless signals, the second power device (12) comprises a fixed seat (16), the fixed seat (16) is fixed in the center of the lower surface of the fixed frame (11) through screws, a transmission shaft (15) is fixed in the fixed seat (16) through a bearing, the upper end of the transmission shaft (15) is in transmission connection with a lifting motor (14), a blade fixed disc (17) is rotatably installed at the lower end of the transmission shaft (15), and four spiral blades (18) are fixed on the blade fixed disc (17) through a pin shaft annular array, promote motor (14) with energy module (6) electricity is connected, promote motor (14) pass through radio signal with control cabinet (7) are connected, paddle fixed disk (17) upper surface edge has inclination adjustment pole (19) through the round pin hub fixation, inclination adjustment pole (19) are close to the stiff end setting of propeller blade (18), inclination adjustment pole (19) other end is fixed on carousel (20) through the round pin axle, carousel (20) rotate through the bearing and install on fixing base (16) outer wall, inclination adjustment pole (19) are electronic pole, inclination adjustment pole (19) with energy module (6) electricity is connected, inclination adjustment pole (19) pass through radio signal with control cabinet (7) are connected.

2. A vertically liftable disk flying device according to claim 1, wherein: four ventilation windows (4) are arranged on the upper surface of the shell (2) in an annular array, sealing doors (3) are arranged on the lower surfaces of the ventilation windows (4), one ends of the sealing doors (3) are fixed on the inner wall of the shell (2) through pin shafts, a door opening motor (5) is connected to the fixing pin shafts of the sealing doors (3) in a transmission mode, the door opening motor (5) is electrically connected with the energy module (6), and the door opening motor (5) is connected with the control console (7) through wireless signals.

3. A vertically liftable disk flying device according to claim 1, wherein: the utility model discloses an energy module, including second power device (12), second power device (12) annular array all around is fixed with 3-8 first power device (13), first power device (13) are jet engine, first power device (13) are fixed through rotating on mount (11), the jet-propelled angle of first power device (13) is adjustable, first power device (13) with energy module (6) electricity is connected, first power device (13) through radio signal with control cabinet (7) are connected.

4. A vertically liftable disk flying device according to claim 1, wherein: casing (2) lower extreme edge and lower surface edge annular array inlay and have a plurality of light (21), light (21) with energy module (6) electricity is connected, light (21) pass through radio signal with console (7) are connected.

5. A vertically liftable disk flying device according to claim 1, wherein: the cockpit (8) are fixed on the fixing frame (11) through bearings, the surface mounting has two-way thrust bearings about the cockpit (8) with the fixed position of fixing frame (11), cockpit (8) with a radial rotating bearing is installed to the fixed position pivot side of fixing frame (11).

6. A vertically liftable disk flying device according to claim 1, wherein: the rotation direction of the cab (8) is opposite to the rotation direction of the second power device (12).