发明名称 Swashplateless active blade pitch control with a mechanical delta-3 restraint having an instantaneous blade pitch-flap coupling response
摘要 An apparatus comprising a hub (208) configured to couple to a mast (206), a grip (216) configured to couple to the hub (208) and a rotor blade (112), a pitch actuator (317) coupled to the grip (216) and configured to change a pitch of the rotor blade (112) relative to the mast (206), and a delta-3 restraint (211) coupled to the pitch actuator, wherein the delta-3 restraint (211) is fixed relative to the mast (206). An apparatus comprising a hub (208) configured to couple to a mast (206), a grip (216) configured to couple to the hub (208) and a rotor blade (112), a pitch actuator coupled to the grip (216) and configured to change a pitch of the rotor blade (112) relative to the mast (206), and a delta-3 restraint (211) coupled to the pitch actuator (317), wherein the delta-3 restraint (211) is configured to control the pitch of the blade (112) relative to the mast (206) when the pitch actuator fails, and wherein the delta-3 restraint (211) provides an instantaneous blade pitch-flap coupling response.
申请公布号 EP2778060(B1) 申请公布日期 2016.01.13
申请号 EP20130170898 申请日期 2013.06.06
申请人 BELL HELICOPTER TEXTRON INC. 发明人 FOSKEY, CHRISTOPHER E.;STAMPS, FRANK B.
分类号 B64C27/605;B64C27/72;F01D7/00 主分类号 B64C27/605
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