发明名称 Turboprop for controlling pitch of blade, has groups of planet gearwheels, where one group is interposed between toothed rings of support and casing and other group is interposed between toothed rings of actuator annulus and control annulus
摘要 <p>The turboprop (11) has a set of propellers (13a, 13b) formed by a blade (20) secured to a pair of annular rotary supports (19a, 19b). An epicyclic mechanism (27a) carries a planet-carrier ring (30a) mounted on the support. The ring carries two groups (33b, 34b) of planet gearwheels (35). The gearwheels of the group (33b) is interposed between a toothed ring (39) of the support and a toothed ring (40) of a stationary casing (14), and the gearwheels of the group (34b) is interposed between a toothed ring (42) of an actuator annulus (21a) and a toothed ring (44) of a control annulus (25a).</p>
申请公布号 FR2911930(A1) 申请公布日期 2008.08.01
申请号 FR20070052910 申请日期 2007.01.26
申请人 SNECMA SOCIETE ANONYME 发明人 GALLET FRANCOIS
分类号 F04D29/36;F02K3/02 主分类号 F04D29/36
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