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A self-sustaining fluid oscillator and rocket-based combined cycle engine

An oscillator and self-sustaining technology, which is applied in the fields of mixing enhancement devices, self-sustaining fluid oscillators and rocket-based combined cycle engines, can solve the problems of single excitation frequency, poor mixing effect, and low adaptability, and achieve a wide range of working scenarios , simple structure, high mixing efficiency

Active Publication Date: 2021-08-06
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The invention provides a self-sustaining fluid oscillator and a rocket-based combined cycle engine, which are used to overcome the defects in the prior art such as complex structure, difficult installation, single excitation frequency, poor mixing effect, and low adaptability, and utilize supersonic concave cavity flow It can generate self-sustaining high-frequency pressure pulsation, combined with the slope configuration to induce flow direction vortex structure, and achieve the purpose of mixing enhancement through the energy of supersonic air flow itself; it has the advantages of both active mixing technology and passive mixing enhancement technology, and has obtained more good mix enhancement

Method used

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  • A self-sustaining fluid oscillator and rocket-based combined cycle engine
  • A self-sustaining fluid oscillator and rocket-based combined cycle engine
  • A self-sustaining fluid oscillator and rocket-based combined cycle engine

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Embodiment 1

[0033] Such as Figure 4-9 As shown, the embodiment of the present invention provides a self-sustained fluid oscillator for supersonic mixing enhancement, including a partition plate 10, on the same surface (in this embodiment, the upper surface) of the partition plate 10 along the length direction A concave cavity 20 and a slope structure are arranged side by side; the concave cavity 20 penetrates along the width direction of the partition plate 10; the slope structure includes a plurality of slopes 30 arranged at intervals along the width direction of the partition plate 10; each slope 30 One end of each communicates with the concave cavity 20 , and the other end gradually slopes upwards to the upper surface of the partition plate 10 along the length direction of the partition plate 10 .

[0034]In this scheme, the partition plate 10 is a plate structure, which is connected with the main structure of the engine, and is used to separate two supersonic airflows of fuel-rich ga...

Embodiment 2

[0053] On the basis of Embodiment 1, the embodiment of the present invention provides a rocket-based combined cycle engine, including an engine body and a fluid oscillator installed on the engine body, and the fluid oscillator is any of the first embodiments. Self-sustaining fluid oscillator; the end of the partition plate of the self-sustaining fluid oscillator away from the slope is connected to the main body of the engine, and the length direction of the partition plate 10 is consistent with the flow direction of the incoming flow. The end surface of the partition plate 10 away from the slope 30 is fixed between the engine main body intake passage and the gas passage. Above the partition plate 10 of the fluid oscillator is an air inlet for supersonic incoming air 1 to flow through, and below the partition plate 10 is a channel for fuel-rich gas 2 to flow through. The technical effect is the same as that of Embodiment 1, and will not be repeated here.

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Abstract

The invention discloses a self-supporting fluid oscillator and a rocket-based combined cycle engine. The oscillator includes a partition plate, and on the same surface of the partition plate along the length direction, there are: concave cavities, along which the partition plate through the width direction of the partition plate; the slope structure includes a plurality of slopes arranged at intervals along the width direction of the partition plate; one end of each slope communicates with the concave cavity, and the other end is along the length direction of the partition plate Gradually slope upwards to the upper surface of the divider. It is used to solve the problems of complex structure, difficult installation, single excitation frequency, poor mixing effect, and low adaptability in the prior art. It can use supersonic concave cavity flow to self-sustain high-frequency pressure pulsation, and combine with slope configuration to induce flow direction vortex The structure, through the energy of the supersonic airflow itself, achieves the purpose of mixing enhancement.

Description

technical field [0001] The invention relates to the field of flow control technology, in particular to a self-sustained fluid oscillator and a rocket-based combined cycle engine for supersonic mixing enhancement, and in particular to a mixing enhancement device capable of producing obvious three-dimensional effects and high-frequency disturbances. Background technique [0002] In aerospace engines, the problem of mixing two air streams is widely involved. Taking the rocket-based combined cycle engine as an example, the rapid mixing of fuel and air is the core technology of the engine design, which is directly related to the working performance of the engine. According to the difference in the mode of action, the hybrid enhancement technology can be divided into two aspects: active hybrid enhancement and passive hybrid enhancement. [0003] Active mixing enhancement technology actively applies external excitation through the exciter to stimulate the growth of unstable waves ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F23R3/28
CPCF23R3/286
Inventor 谭建国李浩张冬冬姚宵刘瑶高政旺肖犇
Owner NAT UNIV OF DEFENSE TECH
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