首页> 外国专利> 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

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

机译:用于控制叶片俯仰的涡轮螺旋桨发动机具有多组行星齿轮,其中一组插在支撑件和壳体的齿环之间,另一组插在致动器环和控制环的齿环之间

摘要

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).
机译:涡轮螺旋桨发动机(11)具有一组螺旋桨(13a,13b),由一组固定在一对环形旋转支架(19a,19b)上的叶片(20)形成。周转机构(27a)带有安装在支架上的行星架环(30a)。该环承载两组(33b,34b)行星齿轮(35)。组(33b)的齿轮插入在支撑件的齿环(39)和固定壳体(14)的齿环(40)之间,组(34b)的齿轮插入在齿环之间致动器环(21a)(42)和控制环(25a)的齿环(44)。

著录项

  • 公开/公告号FR2911930A1

    专利类型

  • 公开/公告日2008-08-01

    原文格式PDF

  • 申请/专利权人 SNECMA SOCIETE ANONYME;

    申请/专利号FR20070052910

  • 发明设计人 GALLET FRANCOIS;

    申请日2007-01-26

  • 分类号F04D29/36;F02K3/02;

  • 国家 FR

  • 入库时间 2022-08-21 19:47:03

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