发明名称 Aircraft engine bleed air flow balancing technique
摘要 A bleed flow modulator is used in conjunction with pressure regulating valves regulating bleed air pressure from each engine to a common manifold. The bleed flow modulator monitors the pressure drop across a heat exchanger, which pressure drop is proportional to flow rate of bleed air through the heat exchanger. By providing a limited authority negative feedback signal to the pressure regulating valve from the bleed flow modulator, flow rate of bleed air from each engine to the common manifold is kept near a desired uniform value, thereby achieving balanced flow extraction of bleed air from the aircraft engines.
申请公布号 US4765131(A) 申请公布日期 1988.08.23
申请号 US19860884335 申请日期 1986.07.11
申请人 ALLIED SIGNAL INC. 发明人 BENSON, PAUL A.
分类号 B64D13/00;F02C6/08;F02C9/18;(IPC1-7):F02C6/08 主分类号 B64D13/00
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