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Jetting system on tailpipe nozzle of jet airplane

A jet aircraft and tail nozzle technology, applied in the field of aircraft, can solve problems such as inability to retreat, inability to lift vertically, poor performance at low altitude and low speed, etc., and achieve the effect of increasing stability and safety

Inactive Publication Date: 2015-08-12
李彦征
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Jet planes are fast, have a large payload, and can fly at high altitudes, but they can’t lift vertically, can only move forward, can’t retreat, can’t fly left or right, have poor low-altitude and low-speed performance, and can’t spin and stop in the air
This shortcoming limits its scope of application

Method used

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  • Jetting system on tailpipe nozzle of jet airplane
  • Jetting system on tailpipe nozzle of jet airplane
  • Jetting system on tailpipe nozzle of jet airplane

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0011] figure 1 , figure 2 , image 3 It is a forward jet system installed on the tail nozzle of a jet aircraft, and consists of a gas switch 2, a high-temperature-resistant soft air pipe 3, a hard air pipe, and a direction controller. The front end of the main air pipe of the system is connected with the tail nozzle of the jet aircraft, and then the front jet pipe 8 and its direction controller are installed in sequence, the left and right jet pipes 10, 11 and their direction controllers, and the down jet pipe 12 and its direction control device, followed by the jet pipeline 9 and its direction controller. figure 1 , figure 2 , image 3 The three jet systems are identical except for the direction controller. The gas switch 2 controls the size of the airflow, and the direction controller controls the direction of the airflow.

[0012] Figure 4 , Figure 5 , Image 6 It is the back-jet system installed on the tail nozzle of jet aircraft, and figure 1 , figure 2 ,...

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PUM

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Abstract

The invention discloses a jetting system on a tailpipe nozzle of a jet airplane. The jetting system capable of jetting gas toward various directions at any time according to demands is installed on the tailpipe nozzle of the jet airplane, and the sizes and directions of gas flows in the various directions can be continuously adjusted; the jetting system is composed of a high-temperature-resistant hard gas pipe, a soft gas pipe, a gas switch and a direction controller; the gas switch is used for controlling the sizes of the gas flows, the direction controller is used for controlling the directions of the gas flows. After the jetting system is installed on the jet airplane, the jet airplane can realize vertical takeoff and landing, slanting takeoff and landing, and runway takeoff and landing, and is capable of flying front, back, left and right, the balance performance in the air is good, and the security of the jet airplane is improved.

Description

technical field [0001] The invention belongs to the field of aircraft, in particular to an air jet system on the tail nozzle of a jet aircraft. Background technique [0002] Jet planes are fast, have a large load capacity, and can fly at high altitudes, but they cannot vertically lift, can only move forward, cannot retreat, cannot fly left or right, have poor low-altitude and low-speed performance, and cannot spin and stop in the air. This shortcoming limits its scope of application. Contents of the invention [0003] The present invention is exactly under above-mentioned situation, provides the jet system on a kind of jet aircraft tail nozzle. [0004] In order to overcome the shortcoming of jet aircraft, enlarging its scope of application, increase its safety, the present invention has done following improvement: on the tail nozzle pipe of jet aircraft, install a jet system that can spray to each direction at any time as required, And the size and direction of the airf...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C15/00B64C15/02
Inventor 李彦征
Owner 李彦征
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