Aircraft

A technology for an aircraft and an aircraft tube, which is applied in the field of aircraft and can solve the problems of high cost and complex structure of the aircraft.

Inactive Publication Date: 2010-04-14
徐林波
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For this reason, additional engines must be ad

Method used

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Example Embodiment

[0026] Figure 4 The air is sucked from the lower space (3a) and upper space (3b) of the aircraft cylinder (1), and then enters from the front end into the suction and exhaust ducts (4) of each turbojet engine (7) from the rear end It ejects and generates lateral thrust on the wings (5) and (6). The thrust direction can be adjusted by rotating the angle of the wings (5) and (6).

[0027] Through the working parameters of the turbojet engine (7) and the shape and angle design of the partition (3), the airflows passing through the two internal spaces (3a) and (3b) of the aircraft cylinder (1) have different speeds, so that The partition (3) generates lateral thrust.

[0028] When the aircraft needs to turn, the tail ends of the suction and exhaust pipes (4) of the turbojet engine (7) in the reverse position are closed, and the gas is ejected from the side jet ports (4a).

[0029] When the aircraft needs lateral displacement, it can be achieved by adjusting the rotation angle of each ...

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Abstract

The invention relates to an aircraft, in particular to a vertical/short take-off and landing aircraft which is characterized in that a high-speed airflow generated when a turbojet engine works blows through airfoils to generate the required lift force when the aircraft takes off, lands and flies. The aircraft can be used as a surface ship or a submarine, and can take-off and land in water. The aircraft can be also designed into a pilotless aircraft, a cruise missile, an underground latent amphibious striking weapon, or various flying vehicles.

Description

technical field [0001] The invention relates to an aircraft, especially a vertical / short take-off and landing aircraft. Background technique [0002] At present, various vertical take-off and landing aircraft with fixed wings mostly adopt the mode of spraying fluid to the ground to achieve the purpose of vertical take-off and landing. Must increase engine additionally for this reason, make aircraft structure complicated, cost is expensive. Contents of the invention [0003] For this reason, the present invention has designed a kind of longitudinal wing vertical / STOL aircraft. Its design scheme is: [0004] 1. The high-speed airflow generated by the turbojet engine is blown over the wings to make it generate the lift required for the aircraft to take off, land and fly. [0005] 2. The wings (5) and (6) are longitudinally arranged in the air intake and exhaust duct (4) of the turbojet engine (7) and allowed to rotate axially along the duct. The airfoils (5) and (6) divid...

Claims

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Application Information

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IPC IPC(8): B64C39/00B64D27/02
Inventor 徐林波
Owner 徐林波
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