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Licensed Unlicensed Requires Authentication Published by De Gruyter September 26, 2017

Performance Seeking Control of Propfan Engines Based on Modified Cuckoo Search

  • Yiwei Wang and Xianghua Huang EMAIL logo

Abstract

Performance seeking control benefits propfan engine by generating optimal performance in different flight status. It is based on engine model, control model and optimization model. The control scheme of propfan engine is different from those of turbofan engines, for the thrust of propfan engines is mainly produced by propfans. After analysing the control structure of propfan engines, a control scheme for the propfan engine is proposed. The control scheme works well in flight envelope and the simulation results show that the overshoot of power shaft rotation speed is less than 2 % and the settling time is less than 0.9s. Based on this, a control scheme in performance seeking mode is proposed. A Modified Cuckoo Search method, which modifies the search step size and abandonment rate, is applied in the control scheme in maximum thrust mode and minimum fuel flow mode. The control scheme in performance seeking mode can reduce 2 % fuel flow, compared with the control scheme in torque-compensation mode. Performance of the scheme is better than standard Cuckoo Search and Genetic Algorithm.

Funding statement: The authors gratefully acknowledge the financial support from the National Nature Science Foundation of China (No.51576097).

Abbreviations

CS

Cuckoo Search

EEC

Electronic Engine Controller

FCU

Fuel Control Unit

GA

Genetic Algorithm

MCS

Modified Cuckoo Search

PCM

Pitch Change Mechanism

PSC

Performance Seeking Control

SFC

Specific Fuel Consumption

sfc

specific fuel consumption of propfan engine

Nomenclature

Cp

power coefficient

m

dimension of CS solution

Nh

rotation speed of high pressure shaft (rpm)

Nl

rotation speed of low pressure shaft (rpm)

Np

rotation speed of power shaft (rpm)

n

host nests number

pa

egg abandonment rate

Q1

torque of front propfan (Nm)

Q2

torque of apt propfan (Nm)

T4

turbine inlet temperature (K)

t

generation number

u

control variables

Wf

fuel flow

X

state parameters

xt

solution at the tth generation

F

thrust (N)

Fiti

quality/fitness

α

step size of CS

β

pitch angle (°)

β1

front pitch angle (°)

β2

apt pitch angle (°)

ε

coefficient of penalty function

Subscripts
best

the best current solution

d

demand value

max

maximum

min

minimum

1

front propfan

2

apt propfan

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Received: 2017-09-02
Accepted: 2017-09-18
Published Online: 2017-09-26
Published in Print: 2020-11-18

© 2017 Walter de Gruyter GmbH, Berlin/Boston

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