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    • 1. 发明授权
    • Stall protector system for a gas turbine engine
    • 用于气体涡轮发动机的保护器系统
    • US3852958A
    • 1974-12-10
    • US40165073
    • 1973-09-28
    • GEN ELECTRIC
    • ADAMS MDUNCAN V
    • F02C9/28F02C9/32F04D27/02F02C3/06F02C9/04
    • F04D27/0207F02C9/32
    • A stall protector system is provided for a gas turbine engine wherein the compressor pressure is measured, differentiated, and compared with a reference indicative of the maximum rate at which the compressor pressure decreases during normal operation. When the actual rate of decrease of compressor pressure exceeds the reference rate, then the signal is integrated and compared with a second reference indicative of the minimum change in compressor pressure before a stall occurs. If the second reference is exceeded, the fuel flow to the combustor is automatically restricted.
    • 提供了一种用于燃气涡轮发动机的失速保护器系统,其中压缩机压力被测量,微分,并且与在正常操作期间压缩机压力降低的最大速率的参考值进行比较。 当压缩机压力的实际降低速率超过参考速率时,信号被积分,并与第二个参考值进行比较,表示压缩机压力发生前的最小变化。 如果超过第二个参考值,则自动限制燃烧到燃烧器的燃料。