发明名称 A conical rotary actuator and its application to control an aircraft hinge
摘要 <p>The cylinder consists of coaxially inner (32) and outer (34) housings enclosing at least one annular space containing two sets of vanes (40,44) one fixed to each housing and located alternately inside the space(s) to form variable-volume control chambers. At least one of the two housings has a variable cross-section, so that the vanes' width decreases from one end to the other. The other housing has a constant cross-section, while the inner one has truncated conical and cylindrical sections (38a,38b), meeting at the smaller end of the truncated conical section. The inner and outer housings form, respectively, a rotor and stator, with the inner housing linked to a heating fluid circuit.</p>
申请公布号 EP0715084(A1) 申请公布日期 1996.06.05
申请号 EP19950402648 申请日期 1995.11.23
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 DURAND, YVES
分类号 B64C13/40;F15B15/12;(IPC1-7):F15B15/12 主分类号 B64C13/40
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