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公开(公告)号：US11820528B2
公开(公告)日：2023-11-21
申请号：US17705528
申请日：2022-03-28
CPC分类号： B64D41/007 , B64C13/40 , F03D9/28 , F03D9/32 , F05B2220/31 , F05B2220/7068 , F05B2260/406
摘要： An aircraft hydraulic control system includes a pump system, a fluid circuit, and a controller. The pump system includes a hydraulic pump and a ram air turbine assembly. The fluid circuit delivers hydraulic fluid to the hydraulic pump and receives the hydraulic fluid output from the hydraulic pump. The controller is in signal communication with the hydraulic pump. The controller determines a rotational frequency of a ram air turbine included in the ram air turbine assembly, and controls the hydraulic pump so as to control the flow of hydraulic fluid in the fluid circuit. The flow of hydraulic fluid in the fluid circuit controls a fluid pressure of the aircraft.
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2.发明公开公开(公告)号：US20230303265A1
公开(公告)日：2023-09-28
申请号：US17705528
申请日：2022-03-28
CPC分类号： B64D41/007 , B64C13/40 , F03D9/32 , F03D9/28 , F05B2260/406 , F05B2220/31 , F05B2220/7068
摘要： An aircraft hydraulic control system includes a pump system, a fluid circuit, and a controller. The pump system includes a hydraulic pump and a ram air turbine assembly. The fluid circuit delivers hydraulic fluid to the hydraulic pump and receives the hydraulic fluid output from the hydraulic pump. The controller is in signal communication with the hydraulic pump. The controller determines a rotational frequency of a ram air turbine included in the ram air turbine assembly, and controls the hydraulic pump so as to control the flow of hydraulic fluid in the fluid circuit. The flow of hydraulic fluid in the fluid circuit controls a fluid pressure of the aircraft.
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