WO2013004070A1

WO2013004070A1 - Spherical saucer-shaped aviation aircraft

Info

Publication number: WO2013004070A1
Application number: PCT/CN2012/000353
Authority: WO
Inventors: 刘刚
Original assignee: Liu Gang
Priority date: 2011-07-04
Filing date: 2012-03-21
Publication date: 2013-01-10
Also published as: CN102862680A

Abstract

A spherical saucer-shaped aviation aircraft, capable of rapid vertical takeoff and flight, differs from the takeoff and flight principle of all aviation aircrafts, comprising vertical power system devices, a transverse power system device, a circular saucer, a main cabin, an upper circular track, an upper wheel, a stabilizing and control device, a lower circular track, a lower wheel, landing gear and the like. The spherical saucer-shaped aviation aircraft of the present invention can vertically and rotationally take off, levitate and land at a high speed, and can transversely and rapidly change directions in 360 degrees in flight, with the following advantages: high speed, safe and low takeoff and landing site condition requirements.

Description

Spherical aircraft

Technical field

The spheroidal aircraft is an aerospace vehicle that can be quickly and vertically escaping from all aerospace aircraft. Background technique

The existing aviation aircraft has high requirements for take-off and landing, and the air steering is slow. There are several types of aircraft that can be lifted vertically and the airlifting speed is slow and there are safety hazards. There is a kind of fireworks called a rotating disc that can rotate at high speed even if there is only one nozzle with a certain angle to the vertical (horizontal). The spheroidal aircraft has three vertical (horizontal) angled powertrain devices, and a laterally moving powertrain device that allows the aircraft to be vertically lifted at high speed, suspended, landed, and 360° laterally tuned. The aircraft can be safely landed even in the event of a sudden failure of a longitudinal power system unit. Summary of the invention

― A spherical aerospace vehicle: capable of vertical high-speed rotary lift, .360° horizontal quick-tuning flight, which can be applied in many fields such as civil aviation, military, and aerospace. It is mainly composed of a longitudinal power system device, a lateral power system device, a circular disk, a main cabin, an upper ring type rail, an upper wheel, a fixed steering device, a lower ring type track, a lower wheel, a landing gear, and the like (see the attached drawings). DRAWINGS

BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 is a schematic view showing the appearance of an aircraft of the present invention. Figure 2 is a front view. Figure 3 is a plan view. Figure 4 is a right side view. Figure 5 is a cross-sectional view taken along line A - A of Figure 2; B is a partial section. (1) Power system devices for vertical lift, suspension, and landing of aircraft, power system devices (1) at an angle to vertical (horizontal) direction (Fig. 5), (2) power system devices for lateral movement of aircraft, (3) The annular disk of the power system unit is installed, (4) the main compartment is composed of driving, manned, cargo, etc., (5) upper ring type track, (6) upper wheel, (7) is the fixed steering device of the aircraft , (8) lower wheel, (9) lower ring type track, (10) is landing gear.

detailed description

The spheroidal aircraft is a simple and easy-to-flight aircraft, and the current level of science and technology can be easily implemented and achieved. The specific embodiment is as follows: In FIG. 2, the upper ring type track (5), the upper wheel (6), the lower wheel (8), and the lower ring type track (9) adopt a train wheel track structure to make a ring disk (3). ) Rotating around the main compartment (4), magnetic suspension technology can also be used to achieve its purpose. The power generated by the N (N 3 ) power system units (1 ) at an angle to the vertical (horizontal) direction is decomposed into vertical and horizontal forces. During the initial operation of the powertrain unit (1), the horizontal force causes the annular disc (3) to rotate around the main compartment (4). When the power exceeds a certain value, the vertical force causes the annular disc to lift off and lift it up. The upper ring (5) acts on the upper wheel (6) to drive the main compartment (4) to rotate together at high speed. The force between the lower rear wheel (8) and the lower ring track (9) is zero. Because the circular disc (3) rotates at a high speed, the power point is continuously distributed on the trajectory of its circular motion, which solves the problem of difficult power balance control, so the driving area in the main compartment (4) is remotely controlled by a fixed distance. It is only necessary to control the power of the N (N 3) power system devices (1) for simultaneous increase, decrease, and reduction to achieve the purpose of aircraft lifting, suspension, and lowering. The power system unit (1) uses a ducted fan and a turboprop engine. (2) The power system unit (Fig. 3) only needs to bear the lateral flight power, which makes it easy for the aircraft to fly at high speed, using ducted fans and turbofan engines. The fixed steering device (7) interacts with the lower ring type track (9) on the annular disk to make the main compartment (4) rotate in the opposite direction to the rotation direction of the annular disk, and the steering device (7) and the lower ring type The rail (9) adopts the gear (inner ring gear) method or the friction method, so as to achieve the purpose of making the circular motion of the main cabin (4) static with respect to the ground and 360° to determine the flight direction of the aircraft. The aircraft instantaneously flies in the opposite direction).

Claims

Essentials

A spherical dish aircraft characterized by: a large spheroid (1) and a circular disk (3) rotating around it.

2. (1) on the circular disc is the power system device for the vertical lift, suspension and landing of the aircraft. Features: N (N 3) power system devices (1) are at an angle to the vertical (horizontal) direction. The power generated by it is decomposed into forces in the vertical direction and forces in the horizontal direction. The vertical force lifts the ring disk and lifts its lift force through the upper ring track (5) to the upper wheel (6) to drive the main compartment (4) to take off. The horizontal force causes the ring disc (3) to rotate around the main compartment (4). One

3. (2) A powertrain device that moves the aircraft laterally.

4. (7) is the fixed steering device of the aircraft, characterized by: The device (7) interacts with the lower ring type track (9) on the annular disk to rotate the main compartment (4) and the circular disk In the opposite direction, the circular motion of the main compartment (4) is stationary relative to the ground and can be adjusted 360° to determine the flight direction of the aircraft.

5. The aircraft is lowered before lifting, and the ring plate is supported by the lower ring (8) on the main compartment (4) through the lower ring type track (9).