发明名称 Direct-drive control of aircraft stability augmentation
摘要 <p>According to one embodiment, a stability augmentation system 200 includes a master linkage 210, a stability augmentation motor 220, and three linkages 212, 214, 216. A first linkage 212, is coupled to the master linkage 210 and operable to receive movements representative of pilot commands from a pilot command system. A second linkage 214 is coupled between the stability augmentation motor 220 and the master linkage 210 and operable to receive movements representative of augmentation commands from the stability augmentation motor 220. A third linkage 216 is coupled to the master linkage 210 and operable to transmit movements representative of blade position commands to a blade control system 116 in response to the movements representative of pilot commands and the movements representative of augmentation commands. To be accompanied, when published, by Figure 3 of the drawings.</p>
申请公布号 EP2722277(B1) 申请公布日期 2015.03.11
申请号 EP20130171020 申请日期 2013.06.07
申请人 BELL HELICOPTER TEXTRON INC. 发明人 COVINGTON, CHARLES E.;FENNY, CARLOS A.;ATKINS, BRADY G.
分类号 B64C27/56;B64C27/00;B64C27/59;B64C27/605 主分类号 B64C27/56
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