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    • 1. 发明公开
    • DISPOSITIF DE PRECONTRAINTE A ACTION RADIALE
    • VORSPANNUNGSVORRICHTUNG MIT RADIALERAKTIVITÄT
    • EP2462361A1
    • 2012-06-13
    • EP10737040.5
    • 2010-07-23
    • Snecma
    • BOSTON, Eric, JacquesBOURU, Michel, AndréJABLONSKI, LaurentJOLY, Philippe, Gérard, Edmond
    • F16F1/32F16F3/02
    • F16F1/324F16C25/083F16C2360/00F16F3/02
    • The invention relates to a prestressing device (10) extending about an axis (A) between a first plane that is substantially perpendicular to the axis (A) and a second plane that is substantially parallel to the first plane and axially offset relative to the latter. The device includes a first annular body (13) extending in the first plane, and a first series of at least three tabs (15), each of which is connected to the first body and extending in an essentially radial direction, each of the tabs of the first series including a planar surface (17) extending in the second plane. This arrangement ensures surface contact between the parts of the elements to be subjected to prestressing. The device can be used in particular for a rotor, and especially for a rotor of an unducted propeller for a turbine engine.
    • 预应力装置,其围绕基本上垂直于所述轴线的第一平面之间的轴线延伸,以及基本上平行于所述第一平面并相对于所述第一平面轴向偏移的第二平面。 该装置包括在第一平面中延伸的第一环形主体和至少三个突出部的第一系列,每个突出部分连接到第一主体并沿基本上径向方向延伸,第一系列的每个突片包括一个 平面在第二平面中延伸。 这种布置确保要进行预应力的元件的部分之间的表面接触。 该装置可以例如用于转子,例如用于涡轮发动机的未被驱动的螺旋桨的转子。
    • 8. 发明公开
    • MOYEU D'HELICE
    • EP2449265A1
    • 2012-05-09
    • EP10726997.9
    • 2010-07-02
    • Snecma
    • BOSTON, Eric, JacquesBOURU, Michel, AndréJABLONSKI, LaurentJOLY, Philippe, Gérard, Edmond
    • F04D29/32B64C11/02F01D5/02F01D21/04
    • F04D29/321B64C11/306B64D2027/005F02K3/072Y02T50/66
    • The invention relates to a hub of a propeller with variable-pitch blades for a turbine engine, in particular for a propfan engine. The hub of the propeller comprises a polygonal ring (234) with substantially radial cylindrical recesses (236) distributed about a central axis of the ring (234) for receiving said blades, a turbine rotor element (243) of the turbine engine, and a securing flange that is attached to the ring so as to connect said ring to said rotor element (243). The hub further comprises a plurality of back-up hooks (244) inserted with clearance in openings (241), the back-up hooks (244) being connected either to the ring (234) or to the rotor element (243), and the openings (241) being connected to the other one of the two.
    • 本发明涉及用于涡轮发动机的具有可变桨距叶片的螺旋桨的桨毂,特别是用于普罗旺斯发动机的桨毂。 螺旋桨的轮毂包括多边形环(234),该多边形环具有围绕环(234)的中心轴线分布的用于接收所述叶片的大致径向圆柱形凹部(236),涡轮发动机的涡轮转子元件(243) 固定凸缘,该凸缘连接到所述环以便将所述环连接到所述转子元件(243)。 轮毂还包括多个以间隙插入开口(241)中的支撑钩(244),支撑钩(244)连接到环(234)或连接到转子元件(243),以及 开口(241)连接到两个中的另一个。