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A binary plug-type vector nozzle with adjustable throat area and aircraft

A vector nozzle and area technology, which is applied in the directions of machines/engines, jet propulsion devices, etc., can solve the problems of large airflow loss and small area adjustment range, and achieve the effect of reducing airflow loss.

Active Publication Date: 2020-03-03
AECC SHENYANG ENGINE RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The existing pre-researched binary plug vector nozzle with adjustable throat area has a small adjustment range of throat area, and the vector adjustment can only be adjusted to a single component to achieve vector deflection, and the airflow loss is large

Method used

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  • A binary plug-type vector nozzle with adjustable throat area and aircraft
  • A binary plug-type vector nozzle with adjustable throat area and aircraft
  • A binary plug-type vector nozzle with adjustable throat area and aircraft

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Embodiment Construction

[0037] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention. Embodiments of the present invention will be described in detail below ...

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Abstract

The invention discloses a two-dimensional plug type vectoring thrust nozzle with an adjustable throat area and an aircraft. The two-dimensional plug type vectoring thrust nozzle with the adjustable throat area comprises a round-rotating square cylinder body, a first static arc wall, a second static arc wall, a first dynamic arc wall, a second dynamic arc wall, a first adjusting plate, a second adjusting plate, a cone, a first actuating cylinder, a third actuating cylinder, a second actuating cylinder, a fourth actuating cylinder and a side wall plate; and the first actuating cylinder, the second actuating cylinder, the third actuating cylinder and the fourth actuating cylinder move cooperatively, so that a synchronous motion state and an asynchronous motion state are provided. According tothe two-dimensional plug type vectoring thrust nozzle with the adjustable throat area, throat adjustment and overall deflection of a rear section of the nozzle are realized by utilizing one set of actuating system, the capacity of large-range adjustment of the throat area and the capacity of the overall deflection of the rear section of the nozzle are achieved, and the airflow loss can be reducedthrough the overall deflection of the rear section.

Description

technical field [0001] The invention relates to the technical field of nozzles, in particular to a binary plug-type vector nozzle with adjustable throat area and an aircraft. Background technique [0002] The range of the working envelope of the aero-engine is getting wider and wider, and the range of the drop pressure ratio reaches tens, so a nozzle with stronger expansion capacity is needed; [0003] The existing pre-researched binary plug vector nozzle with adjustable throat area has a small adjustment range of throat area, and the vector adjustment can only be adjusted to a single component to achieve vector deflection, resulting in a large airflow loss. [0004] Therefore, it is desirable to have a technical solution to overcome or at least alleviate at least one of the above-mentioned drawbacks of the prior art. Contents of the invention [0005] The object of the present invention is to provide a dual plug-type vector nozzle with adjustable throat area to overcome ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02K1/08F02K1/15F02K1/78
CPCF02K1/002F02K1/08F02K1/15F02K1/78
Inventor 徐速张少丽赵春生周吉利宋经远左云智商鹏程
Owner AECC SHENYANG ENGINE RES INST