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Rotary aircraft

A technology for an aircraft and a rotating machine, applied in the field of aviation aircraft, can solve the problems of not being able to stay in the air, the speed limit of the aircraft, etc., and achieve the effect of increasing stability

Inactive Publication Date: 2014-12-17
韩俊
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The current aircraft itself is relatively stable and will not rotate. The speed of such an aircraft will be limited, and it cannot stay in the air

Method used

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  • Rotary aircraft
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Examples

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Embodiment Construction

[0011] exist figure 1 , figure 2 and image 3 In the shown embodiment, be provided with circular wing (1), fuselage (2), cockpit (3), fuel tank (4), right elevator (5), right steering gear (6), right rudder ( 7), left rudder (8), left elevator (9), left steering gear (10), left weak rotary machine (11), right weak rotary machine (12), left middle rotary machine (13), right middle rotary machine (14), left strong rotary machine (15), right strong rotary machine (16), forward main engine (17), forward auxiliary machine (18), front landing gear (19), rear left landing gear (20), rear right Landing gear (21).

[0012] Implement the rotating aircraft of the present invention, comprise circular wing (1) and fuselage (2), circular wing (1) middle part installs fuselage (2), fuselage (2) head installs cockpit (3) , the fuel tank (4) is installed at the rear of the cockpit (3), and the right steering gear (6) is installed on the rear right side of the fuselage (2), and the right s...

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PUM

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Abstract

A rotary aircraft includes a circular wing and a fuselage, the central portion of the circular wing is provided with the fuselage, the head of the fuselage is provided with a cockpit, the rear portion of the cockpit is provided with a fuel bunker, the right side of the rear portion of the fuselage is provided with a right steering machine, the right steering machine is connected with a right rudder, the left side of the rear portion of the fuselage is provided with a left rudder, the left steering machine is connected with the left rudder, the right side of the rear portion of the circular wing is provided with a right elevating rudder, the left side of the rear portion of the circular wing is provided with a left elevating rudder, the front of the circular wing is provided with a forward auxiliary engine, a forward host is arranged behind the forward auxiliary engine, the left side of the circular wing is provided with a left strong rotating machine, a left middle rotating machine and a left weak rotating machine, the right side of the circular wing is provided with a right strong rotating machine, a right middle rotating machine and a right weak rotating machine, the bottom of the rear portion of the circular wing is provided with a front undercarriage, the left bottom of the rear portion of the circular wing is provided with a left undercarriage, and the right bottom of the rear portion of the circular wing is provided with a right undercarriage. The rotary aircraft can increase the flight stability, can exceed the speeds of present aircrafts, and can realize stay, tumbling and other high-difficulty aerobatic flights in air.

Description

1. Technical field [0001] The invention relates to an aircraft, in particular to a rotating aircraft similar to a flying saucer. 2. Background technology [0002] The current aircraft itself is relatively stable and does not rotate. The speed of such an aircraft will be limited, and it cannot stay in the air. 3. Contents of the invention [0003] The purpose of the invention is to overcome the deficiencies of the prior art and provide a rotary aircraft similar to a flying saucer. [0004] The technical solution adopted by the present invention to solve the technical problem is: a rotary aircraft, including a circular wing and a fuselage. cabin, the right steering gear is installed on the rear right side of the fuselage, and the right steering gear is connected to the right rudder; the left steering gear is installed on the rear left side of the fuselage, and the left steering gear is connected to the left rudder; Elevators, the left elevator is installed on the left side...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/06
Inventor 韩俊
Owner 韩俊