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    • 5. 发明公开
    • Modified gear tooth profile for an aircraft transmission and producing method
    • Modifiziertes Zahnprofilfürein Flugzeuggetriebe und Herstellverfahren
    • EP1939493A1
    • 2008-07-02
    • EP06425878.3
    • 2006-12-29
    • Agusta S.p.A.
    • Gasparini, GiuseppeSartori, Sergio, c/o Agusta S.p.A.Nihat, Yildirim, c/o University of Gaziantep
    • F16H55/08B64C27/12
    • F16H55/0806F16H55/088Y10T74/19656Y10T74/19972Y10T74/19977
    • There is described a helicopter (1) having a transmission (5) for transmitting motion from a driving member to a driven member; the transmission (5) has at least a first gear (8; 10) driven by the driving member, and a second gear (10; 12) meshing with the first gear (8) and in turn driving the driven member; the first and second gear (8, 10; 10, 12) have teeth (16, 17, 18) shaped so that the gears (8, 10) mesh with one another at at least two pairs of respective simultaneously meshing teeth (16, 17; 17, 18); the teeth (16, 17, 18) of at least one of the gears (8, 10, 12) have a profile (19) having an end portion (21) relieved with respect to a starting theoretical involute (E); and the pattern (G) of the distance between the points of the end portion (21) and the starting involute (E) along an axis (A, H) of the tooth (16, 17, 18) has at least a first and a second segment (B, C) sloping with respect to each other.
    • 描述了具有用于将运动从驱动构件传递到从动构件的变速器(5)的直升机(1) 所述变速器(5)至少具有由所述驱动构件驱动的第一齿轮(8; 10)和与所述第一齿轮(8)啮合的第二齿轮(10; 12),从而驱动所述从动构件; 第一和第二齿轮(8,10; 10,12)具有齿形(16,17,18),其形状使得齿轮(8,10)在至少两对相应的同时啮合的齿(16, 17; 17,18); 至少一个齿轮(8,10,12)的齿(16,17,18)具有轮廓(19),其具有相对于起始理论渐开线(E)缓和的端部(21); 并且沿齿(16,17,18)的轴线(A,H)的端部(21)和起始渐开线(E)的点之间的距离的图案(G)至少具有第一和第 相对于彼此倾斜的第二段(B,C)。