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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 added, making the aircraft complex and expensive

Method used

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Examples

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Embodiment Construction

[0026] Figure 4 In the process, after the air is inhaled from the lower space (3a) and the upper space (3b) in the aircraft barrel (1), it enters the air intake and exhaust ducts (4) of each turbojet engine (7) from the front end and from the tail end Eject, and produce lateral thrust to wing (5) and (6). Thrust direction can be adjusted by rotating the angle of 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 air-flows passing through the two parts of the inner space (3a) and (3b) of the aircraft barrel (1) have different speeds, so that The partition (3) generates lateral thrust.

[0028] When the aircraft needs to turn, the tail end of the air intake and exhaust pipeline (4) of the turbojet engine (7) in the reverse position is closed, and the gas is ejected from its side jet port (4a).

[0029] When the aircraft needs lateral displacement, it can be realized by adjusting the r...

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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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