带加力燃烧室的引射式涡喷发动机增推力研究

2022 International Conference on Dynamics and Vibroacoustics of Machines (DVM) Pub Date : 2022-09-21 DOI:10.1109/DVM55487.2022.9930931

Khaliulin R.R., Sychenkov V.A., Stepicheva N.V.

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摘要

本文对带加力燃烧室的引射式涡喷发动机方案的应用可能性进行了分析。确定了在飞机起飞模式中使用喷射器的有效性。在发动机推力获取装置上进行了ETJEA的实验研究。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

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Research of Thrust Increase on the Ejector Turbojet Engine with the Afterburner

In this paper the using possibility of the scheme of an ejector turbojet engine with an afterburner (ETJEA) was carried out. The effectiveness of using of an ejector nozzle during a takeoff aircraft mode is determined. Experimental research of ETJEA were carried out on a unit with obtaining of engine thrust.

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2022 International Conference on Dynamics and Vibroacoustics of Machines (DVM)

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