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    • 2. 发明公开
    • Aircraft wheel
    • Flugzeugrad。
    • EP0438719A1
    • 1991-07-31
    • EP90124314.7
    • 1990-12-15
    • THE B.F. GOODRICH COMPANY
    • Russell, Donald LouisKahrs, Michael Peter
    • B60B25/04B60B25/18
    • B60B25/04B60B25/18
    • An annular locking ring for use on an aircraft wheel that has a pair of separable wheel sections (10,11) wherein the locking ring (31) has a lobe section (30) and a leg section (35). The cross-sectional shape of the leg section (35) has a pair of spaced linear portions (37,38) that are interconnected at their one ends while the cross-sectional shape of the lobe section (30) has a curvilinear portion (39) and a linearly extending portion (40) that intersects one of the linear portions (38) of the leg section (35). The curvilinear portion (39) of the lobe section (30) has one end that merges with the other one of the spaced linear portions (37). The extension of the one linear portion (38) of the leg section (35) makes an acute angle with the linear portion (40) of the lobe portion (30). Alternatively, the lobe section (56) may have two spaced linear portions (61,62) separated by the curvilinear portion (60) with one of such linear portions (62) merging with one linear portion (57) of the leg section (55) and with the other one of such linear portions (61) of the lobe section (56) intersecting the other linear portion (58) of the leg section (55).
    • 一种在具有一对可分离轮部分(10,11)的飞行器轮上使用的环形锁定环,其中所述锁定环(31)具有凸起部分(30)和腿部部分(35)。 腿段(35)的横截面形状具有一对间隔开的直线部分(37,38),它们在它们的一端互连,而叶片部分(30)的横截面形状具有曲线部分(39 )和与腿部(35)的直线部分(38)中的一个相交的线性延伸部分(40)。 凸缘部分(30)的曲线部分(39)具有与另一个间隔开的直线部分(37)合并的一端。 腿部(35)的一个直线部分(38)的延伸部与凸起部分(30)的直线部分(40)成锐角。 或者,凸角部分(56)可以具有由曲线部分(60)分开的两个间隔开的直线部分(61,62),其中一个直线部分(62)与腿部部分(55)的一个直线部分(57) ),并且与所述腿部(55)的另一直线部(58)相交的所述凸部(56)的所述直线部(61)中的另一方。