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公开(公告)号:US20150247417A1
公开(公告)日:2015-09-03
申请号:US14458770
申请日:2014-08-13
Applicant: ROLLS-ROYCE PLC
Inventor: Marko BACIC , James TOOKE
CPC classification number: F01D19/02 , F01D5/02 , F01D7/02 , F01D11/20 , F01D21/003 , F01D21/14 , F01D25/12 , F04D27/001 , F04D29/164 , F04D29/526 , F05D2220/32 , F05D2260/81 , F05D2260/821 , F05D2270/114 , F05D2270/301 , F05D2270/305 , F05D2270/44 , F05D2270/80
Abstract: A method of controlling a rotor tip clearance arrangement of a gas turbine engine and a control system configured to control rotor tip clearance. Steps include measuring at least one engine parameter; determining engine power demand from the at least one engine parameter; and calculating rotor tip clearance given the determined engine power demand. The rotor tip clearance arrangement is controlled to increase or decrease the rotor tip clearance based on the difference between the calculated clearance and a predefined target clearance.
Abstract translation: 一种控制燃气涡轮发动机的转子顶端间隙布置的方法和被配置为控制转子尖端间隙的控制系统。 步骤包括测量至少一个引擎参数; 从所述至少一个发动机参数确定发动机功率需求; 并根据确定的发动机功率需求计算转子顶端间隙。 基于计算出的间隙和预定义的目标间隙之间的差异,控制转子顶端间隙布置以增加或减小转子顶端间隙。