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Low-emission optimization control method for coaxial compound helicopter/engine based on variable geometry adjustment.
- Source :
-
Aerospace Science & Technology . Aug2024, Vol. 151, pN.PAG-N.PAG. 1p. - Publication Year :
- 2024
-
Abstract
- • A multidisciplinary simulation framework integrating the CCH and turboshaft engine is constructed. • A multi-objective optimization problem is designed to evaluate and quantify the flight performance and environmental impact of the CCH. • The NSGA-II multi-objective optimization method based on entropy weight evaluation is adopted. • The goal of low-emission for CCH is achieved through variable rotor speed and variable geometry adjustment. To address compatibility issues of the operational performance and environmental impact of Coaxial Compound Helicopters (CCH), a low-emission optimization control method for coaxial compound helicopter/engine based on variable geometry adjustment is proposed. Firstly, a multidisciplinary simulation framework for CCH and turboshaft engine is deployed by integrating the power characteristics of CCH, the performance of a variable geometry turbine engine, and the emission characteristics of nitrogen oxides (NO x). Subsequently, a multivariable and multi-objective optimization problem is formulated to assess and quantify the flight performance and environmental impact of CCH through a holistic optimization strategy. On this basis, a Non-dominated Sorting Genetic Algorithm II (NSGA-II) multi-objective optimization method based on entropy weight assessment is employed to obtain the optimal control plan for variable rotor speed and adjustable mechanisms within the operation envelope, by balancing the thermodynamic losses of the engine and the aerodynamic efficiency of the CCH. Finally, the optimization control method for CCH is validated based on flight missions. The simulation results demonstrate that the combination of variable rotor speed and variable geometry adjustment of engine effectively reduces the engine NO x emission index by more than 10.7 % within the full envelope, relative to the original rotor speed plan. In the actual flight mission profile, the total NO x emissions can be reduced by 11.78 %, improving the environmental impact of CCH. [ABSTRACT FROM AUTHOR]
Details
- Language :
- English
- ISSN :
- 12709638
- Volume :
- 151
- Database :
- Academic Search Index
- Journal :
- Aerospace Science & Technology
- Publication Type :
- Academic Journal
- Accession number :
- 178463873
- Full Text :
- https://doi.org/10.1016/j.ast.2024.109263