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
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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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