发明名称 Aircraft engine bleed air flow balancing technique.
摘要 <p>@ A bleed flow modulator is used in conjunction with pressure regulating valves regulatng 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 single 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 aircraft engines.</p>
申请公布号 EP0190943(A2) 申请公布日期 1986.08.13
申请号 EP19860300849 申请日期 1986.02.07
申请人 THE GARRETT CORPORATION 发明人 BENSON, PAUL A.
分类号 F02C6/02;B64D13/00;F02C6/06;F02C6/08;F02C7/12;F02C9/18 主分类号 F02C6/02
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