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Modeling and control schedule design of a two-dimensional thrust-vectoring nozzle and aeroengine

Published online by Cambridge University Press:  11 December 2020

Y. Liu Open the ORCID record for Y. Liu [Opens in a new window] ,
M. Chen Open the ORCID record for M. Chen [Opens in a new window]  and
H. Tang
Y. Liu
Affiliation:
School of Energy and Power Engineering, Beihang University, Beijing, China
M. Chen*
Affiliation:
School of Energy and Power Engineering, Beihang University, Beijing, China
H. Tang
Affiliation:
School of Energy and Power Engineering, Beihang University, Beijing, China
*
08585@buaa.edu.cn
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Abstract

For advanced operational aircraft, the two-dimensional (2-D) thrust-vectoring (TV) nozzle effectively improves the flight mobility and post-stall manoevrability. However, its flow capacity decreases when deflecting and cooling air is injected, which impacts the engine’s operating state, including decreasing the fan surge margin and increasing the turbine inlet temperature. Therefore, in order to improve engine performance in the whole flight envelope, this paper studies the matching mechanism of the engine and the cooled 2-D TV nozzle, performance characterisation and control schedule of the nozzle, and an integrated aeroengine/nozzle modeling method is put forward. Based on these, an engine performance simulation model is modified to include a cooled 2-D TV nozzle. The testing results show that applying the nozzle control schedules recommended in this paper avoids the performance degradation when the nozzle deflects. This work advances the field of engine/nozzle integrated modeling, and helps to instruct the simulation and experimentation to better fit the needs of engine modeling and engineering applications.

Keywords

thrust-vectoring nozzleengine control scheduleaeroengine matching mechanismaeroengine/nozzle integrated modeling
Type
Research Article
Information
The Aeronautical Journal , Volume 125 , Issue 1287 , May 2021 , pp. 879 - 915
Copyright
© The Author(s), 2020. Published by Cambridge University Press on behalf of Royal Aeronautical Society

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References

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