CN205418104U

CN205418104U - Disk -type aircraft

Info

Publication number: CN205418104U
Application number: CN201620197604.4U
Authority: CN
Inventors: 樊民革; 张丽香
Original assignee: Shanxi University
Current assignee: Shanxi University
Priority date: 2016-03-15
Filing date: 2016-03-15
Publication date: 2016-08-03
Anticipated expiration: 2026-03-15

Abstract

The utility model belongs to the technical field of the aircraft, concretely relates to disk -type aircraft. The utility model discloses it exists unable VTOL, the flying speed is slow and the noise is big technical problem mainly to have solved current aircraft. The utility model discloses a disk -type aircraft, including base, dish form rotor, motor, internal frame, internal frame coil, interior frame shaft, vertical magnetic field coil, outer frame, frame overhead line circle, outer frame shaft, supporting seat and horizontal field coil. The utility model discloses a pivot of the precession nature regulation dish form screw of dish aircraft rational utilization top is directional, can realize VTOL and hover in air, through the adjustment to dish form screw rotational speed and inclination, can the convenience realization flying fast or at a slow speed aloft, use the precession normal running fit of inside and outside frame, possible 360 degrees all -roundly turn to wantonly fast, have good mobility, the utility model discloses a dish form rotor replaces traditional helicopter screw, has avoided traditional helicopter screw to rotate the noise that brings.

Description

A kind of saucer-like air vehicle

Technical field

This utility model belongs to vehicle technology field, is specifically related to a kind of saucer-like air vehicle.

Background technology

At present practical aircraft is nothing more than two kinds of forms: a kind of is the most common aircraft of Fixed Wing AirVehicle, the thrust utilizing propeller or engine to produce drives body to slide a segment distance, after reaching certain speed, the air force lift-off flight that the pressure reduction utilizing fixing aerofoil upper and lower produces, its advantage is that flight speed is fast, and load capacity is big；Shortcoming is to have plane track, it is impossible to VTOL.The helicopter that another kind of rotary aircraft is the most common, its advantage be can VTOL, realize hovering；Shortcoming is that flight speed is slow, noise is big.

Summary of the invention

The purpose of this utility model be solve that existing aircraft exists cannot VTOL, flight speed is slow and noise is big technical problem, it is provided that a kind of saucer-like air vehicle.

For solving above-mentioned technical problem, the technical solution adopted in the utility model is:

nullA kind of saucer-like air vehicle，Including base、Disk like rotor、Motor、Inner frame、Inner frame coil、Input axis、Vertical magnetic field coil、Outside framework、Outside framework coil、Outside framework axle、Support seat and horizontal magnetic field coil，Said two outside framework axle is located at the middle part of two sides before and after outside framework，Outside framework is arranged on two support seats of base by two outside framework axles，And make outside framework axle outside framework can be driven to rotate supporting rotation on seat，Two input axis are located at the bottom of the inner frame left and right sides，Inner frame is arranged on outside framework by two input axis，And make two input axis can rotate on outside framework thus drive inner frame to rotate，Motor is arranged in inner frame，Vertical magnetic field coil is arranged on base，And it is positioned at the lower section of two input axis，Horizontal magnetic field coil is arranged on base，And it is positioned at the lower section of outside framework left and right sides，Inner frame coil is vertically wrapped in the outer surface of inner frame，Outside framework previous level is wrapped in the outer surface of outside framework，Disk like rotor cover is on base，And make that the end of disk like rotor top and the rotating shaft of motor is fixing to be connected，Thus driven disk like rotor relative to base rotation by the rotating shaft of motor.

The rotating shaft of described motor is the tubular structure of hollow, in order to the holding wire of gps antenna introduces internal body controller.

Described outside framework axle and input axis are the tubular structure of hollow, in order to outside framework coil and inner frame coil are drawn and be connected with internal body controller.

Gather a circle hairbrush for isolating the air inside and outside body in the junction of the side of base Yu disk like rotor.

Outer surface at described disk like rotor gathers and is provided with the vacuum raising air force that when circular pit is beneficial at high speed rotating, generation is bigger.

The rotating shaft of the precession regulation disk like propeller of disc-shaped flying craft Appropriate application gyro of the present utility model is pointed to, VTOL and hovering can be realized, by the adjustment to disk like revolution speed of propeller and angle of inclination, can conveniently realize skyborne quick or slower flight；Be rotatably assorted application by the precession of inter and outer gimbal, can accomplish that 360 degree comprehensive quickly arbitrarily turn to, and have good mobility；This utility model uses disk like rotor to replace conventional helicopters propeller, it is to avoid the noise that conventional helicopters propeller rotational brings, thus solves the technical problem that noise is big.Therefore, compared with background technology, the advantage that this utility model has energy VTOL, flight maneuver is flexible and noise is little.

Accompanying drawing explanation

Accompanying drawing is structural representation of the present utility model.

Detailed description of the invention

nullAs shown in drawings，A kind of saucer-like air vehicle in the present embodiment，Including base 1、Disk like rotor 2、Motor 4、Inner frame 5、Inner frame coil 6、Input axis 7、Vertical magnetic field coil 8、Outside framework 9、Outside framework coil 10、Outside framework axle 11、Support seat 13 and horizontal magnetic field coil 12，Said two outside framework axle 11 is located at the middle part of outside framework 9 two sides front and back，Outside framework 9 is arranged on two support seats 13 of base 1 by two outside framework axles 11，And make outside framework axle 11 outside framework 9 can be driven to rotate supporting rotation on seat 13，Two input axis 7 are located at the bottom of inner frame 5 left and right sides，Inner frame 5 is arranged on outside framework 9 by two input axis 7，And make two input axis 7 can rotate on outside framework 9 thus drive inner frame 5 to rotate，Motor 4 is arranged in inner frame 5，Vertical magnetic field coil 8 is arranged on base 1，And it is positioned at the lower section of two input axis 7，Horizontal magnetic field coil 12 is arranged on base 1，And it is positioned at the lower section of outside framework 9 left and right sides，Inner frame coil 6 is vertically wrapped in the outer surface of inner frame 5，Outside framework coil 10 horizontal wrap is at the outer surface of outside framework 9，Disk like rotor 2 covers on base 1，And make that the end of disk like rotor 2 top and the rotating shaft 3 of motor 4 is fixing to be connected，Thus driven disk like rotor 2 to rotate relative to base 1 by the rotating shaft 3 of motor 4.

The rotating shaft 3 of described motor 4 is the tubular structure of hollow, in order to the holding wire of gps antenna introduces internal body controller.

Described outside framework axle 11 and input axis 7 are the tubular structure of hollow, in order to outside framework coil 10 and inner frame coil 6 are drawn and be connected with internal body controller.

Gather a circle hairbrush for isolating the air inside and outside body in the junction of the side of base 1 Yu disk like rotor 2.

Outer surface at described disk like rotor 2 gathers and is provided with the vacuum raising air force that when circular pit is beneficial at high speed rotating, generation is bigger.

Operation principle of the present utility model: utilize the precession of gyro to change rotating shaft and point to.Take off front motor rotating shaft 3 and disk like rotor 2 keeps vertical with horizontal plane, accelerate to rotate after motor 4 energising, driving disk like rotor 2 high speed rotating, on the upside of disk like rotor 2, air produces rotational flow field, and air pressure reduces and forms relative vacuum, and underpart non-moving air, air pressure is constant, and whole aircraft is under the effect of barometric pressure difference, and lift-off achieves and takes off vertically rapidly, gyroscopic effect makes the disk like rotor of high speed rotating have gyroscopic inertia, and the axle of the precession regulation disk like rotor of application gyro points to；Go up to the air after certain altitude, it is energized to horizontal magnetic field coil 12 and outside framework coil 10 simultaneously, the electrical conductor of outside framework 9 left and right sides is horizontally oriented in uniform magnetic field, the moment making outside framework 9 rotate will be produced by Ampere force effect, this moment will cause gyroscopic procession effect between outside framework 9 and inner frame 5, make outside framework 9 keep not then inner frame 5 turn an angle, disk like rotor 2 is driven to tilt, by rotor produce air force be decomposed into lift straight up and disk like rotorshaft tendency front horizontally advance power, after lift component balances with body weight, aircraft maintains the steady flight forward of certain altitude；If be energized to vertical magnetic field coil 8 and inner frame coil 6 simultaneously, in the electrical conductor vertically uniform magnetic field of inner frame 5 upper and lower sides, the moment making inner frame 5 rotate will be produced by Ampere force effect, this moment will cause gyroscopic procession effect between inner frame 5 and outside framework 9, make inner frame 5 keep not then outside framework 9 turn an angle, drive disk like rotor 2 to tilt, the air force that rotor produces is decomposed into lift and horizontal power；Utilizing precession to recover machine shaft 3 before landing and disk like rotor 2 is vertical with horizontal plane, aircraft loses the component of forward direction, the most before flies, and slow down gradually after being in floating state motor speed, makes aircraft slowly decline, completes descent.

Claims

null1. a saucer-like air vehicle，It is characterized in that: include base (1)、Disk like rotor (2)、Motor (4)、Inner frame (5)、Inner frame coil (6)、Input axis (7)、Vertical magnetic field coil (8)、Outside framework (9)、Outside framework coil (10)、Outside framework axle (11)、Support seat (13) and horizontal magnetic field coil (12)，Said two outside framework axle (11) is located at the middle part of outside framework (9) two sides front and back，Outside framework (9) is arranged on two supports seat (13) of base (1) by two outside framework axles (11)，And make outside framework axle (11) outside framework (9) can be driven to rotate supporting the upper rotation of seat (13)，Two input axis (7) are located at the bottom of inner frame (5) left and right sides，Inner frame (5) is arranged on outside framework (9) by two input axis (7)，And make two input axis (7) can rotate thus drive inner frame (5) to rotate outside framework (9) is upper，Motor (4) is arranged in inner frame (5)，Vertical magnetic field coil (8) is arranged on base (1)，And it is positioned at the lower section of two input axis (7)，Horizontal magnetic field coil (12) is arranged on base (1)，And it is positioned at the lower section of outside framework (9) left and right sides，Inner frame coil (6) is vertically wrapped in the outer surface of inner frame (5)，Outside framework coil (10) horizontal wrap outer surface in outside framework (9)，Disk like rotor (2) covers on base (1)，And make that the end of disk like rotor (2) top and the rotating shaft (3) of motor (4) is fixing to be connected，Thus driven disk like rotor (2) to rotate relative to base (1) by the rotating shaft (3) of motor (4).
A kind of saucer-like air vehicle the most according to claim 1, it is characterised in that: the rotating shaft (3) of described motor (4) is the tubular structure of hollow, in order to the holding wire of gps antenna introduces internal body controller.
A kind of saucer-like air vehicle the most according to claim 1, it is characterized in that: described outside framework axle (11) and input axis (7) are the tubular structure of hollow, in order to outside framework coil (10) and inner frame coil (6) are drawn and be connected with internal body controller.
A kind of saucer-like air vehicle the most according to claim 1, it is characterised in that: the circle hairbrush that gathers in the junction of the side of base (1) Yu disk like rotor (2) is for isolating the air inside and outside body.
A kind of saucer-like air vehicle the most according to claim 1, it is characterised in that: the outer surface described disk like rotor (2) gathers and is provided with the vacuum raising air force that when circular pit is beneficial at high speed rotating, generation is bigger.