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    • 1. 发明申请
    • INTERSHAFT SEAL WITH ASYMMETRIC SEALING RING AND CENTRIFUGAL RETAINING PLATES
    • INTERSHAFT密封不对称密封圈和离心保持板
    • WO2016168870A3
    • 2017-02-23
    • PCT/US2016044615
    • 2016-07-29
    • STEIN SEAL CO
    • GARRISON GLENN M
    • F01D11/00F01D25/16F16J15/44
    • F01D11/003F01D11/02F05D2240/58F05D2250/73
    • An intershaft seal assembly (30) for use between an inner shaft (32) and an outer shaft (31) within a turbine engine is presented. The seal assembly (30) includes a sealing ring (33), centrifugal retaining plates (102), and end rings (37, 38). The sealing ring (33) further includes a plurality of asymmetric ring segments (34) whereby each asymmetric ring segment (34) further includes a vertical flange (46) and horizontal flanges (47) extending from the vertical flange (46) in a non-symmetric arrangement. At least one slot (104) is disposed along each horizontal flange (47). The sealing ring (33) is interposed between the centrifugal retaining plates (102). Each centrifugal retaining plate (102) includes a plurality of tabs (103) extending therefrom. Each tab (103) is engaged by one slot (104). The sealing ring (33) and the centrifugal retaining plates (102) are interposed between the end rings (37, 38). Each centrifugal retaining plate (102) is directly interposed between one horizontal flange (47) and one end ring (37, 38). The vertical flange (46) extends from between the end rings (37, 38) in the direction of the outer shaft (31). A non-contact seal is formed between an outer sealing surface (62) along the vertical flange (46) and an inner sealing surface (63) along the outer shaft (31).
    • 提出了一种在涡轮发动机内的内轴(32)和外轴(31)之间使用的轴间密封组件(30)。 密封组件(30)包括密封环(33),离心保持板(102)和端环(37,38)。 所述密封环(33)还包括多个不对称环段(34),由此每个不对称环段(34)还包括垂直凸缘(46)和水平凸缘(47),所述凸缘以垂直凸缘(46) 对称排列。 至少一个槽(104)沿着每个水平凸缘(47)设置。 密封环(33)介于离心保持板(102)之间。 每个离心保持板(102)包括从其延伸的多个突片(103)。 每个接片(103)由一个槽(104)接合。 密封环(33)和离心保持板(102)插在端环(37,38)之间。 每个离心保持板(102)直接插入在一个水平凸缘(47)和一个端环(37,38)之间。 垂直凸缘46在端轴(37,38)之间沿外轴(31)的方向延伸。 在沿着垂直凸缘(46)的外密封表面(62)和沿着外轴(31)的内密封表面(63)之间形成非接触式密封。
    • 2. 发明申请
    • INTERSHAFT SEAL WITH ASYMMETRIC SEALING RING
    • INTERSHAFT密封与不对称密封圈
    • WO2016179608A3
    • 2017-02-23
    • PCT/US2016033165
    • 2016-05-19
    • STEIN SEAL CO
    • GARRISON GLENN M
    • F01D11/00F01D25/16F16J15/44
    • F01D11/003F01D25/16F05D2240/55F05D2240/60F16J15/441F16J15/442F16J15/443
    • An intershaft seal assembly (30) for use between an inner shaft (32) and an outer shaft (31) rotatable within a turbine engine is presented. The seal assembly (30) includes a sealing ring (33), an inner ring (39), and a pair of end rings (37, 38). The sealing ring (33) further includes a plurality of asymmetric ring segments (34) whereby each asymmetric ring segment (34) further includes a vertical flange (46) and a pair of horizontal flanges (47) extending from the vertical flange (46) in a non-symmetric arrangement. The non- symmetric seal geometry provides an axial force balance thereby reducing wear and increasing seal life. The sealing ring (33) is disposed about the inner ring (39). The inner ring (39) includes a plurality of ridges (43) that engage the asymmetric ring segments (34) so as to prevent rotation of the asymmetric ring segments (34) with respect to the inner shaft (32). The end rings (37, 38) are disposed about the sealing ring (33) and the inner ring (39). The horizontal flanges (47) separately contact the end rings (37, 38) so that the vertical flange (46) extends from and between the end rings (37, 38) in the direction of the outer shaft (31). A non-contact seal is formed between an outer sealing surface (62) along the vertical flange (46) and an inner sealing surface (63) along the outer shaft (31).
    • 提出了一种用于在涡轮发动机内旋转的内轴(32)和外轴(31)之间的轴间密封组件(30)。 密封组件(30)包括密封环(33),内环(39)和一对端环(37,38)。 密封环(33)还包括多个不对称环段(34),由此每个不对称环段(34)还包括垂直凸缘(46)和从垂直凸缘(46)延伸的一对水平凸缘(47) 在非对称的布置。 非对称密封几何形状提供轴向力平衡,从而减少磨损并增加密封寿命。 密封环(33)围绕内圈(39)设置。 内环(39)包括与不对称环段(34)接合以便防止不对称环段(34)相对于内轴(32)旋转的多个脊(43)。 端环(37,38)围绕密封环(33)和内环(39)设置。 水平凸缘(47)分别接触端环(37,38),使得垂直凸缘(46)沿着外轴(31)的方向从端环(37,38)中和之间延伸。 在沿着垂直凸缘(46)的外密封表面(62)和沿着外轴(31)的内密封表面(63)之间形成非接触式密封。
    • 3. 发明申请
    • IMPROVED AIR RIDING SEAL
    • 改进的空气密封
    • WO2010099193A3
    • 2011-01-06
    • PCT/US2010025220
    • 2010-02-24
    • STEIN SEAL COGARRISON GLENN M
    • GARRISON GLENN M
    • F02C7/28F01D11/02F16J15/24F16J15/34F16J15/46F16J15/50
    • F01D11/001F01D11/02F16J15/164F16J15/3448F16J15/3476F16J15/4472Y02T50/671
    • An improved air-riding seal system (1) for turbine engines is presented. The seal system (1) includes a movable primary seal assembly (2), a stationary secondary seal assembly, and at least one structure to increase the stiffness of a thin film between the primary seal and a rotating component. The primary seal assembly (2) includes an annular seal ring (23) and an arcuate support arm (25). The annular seal ring (23) has a cross section that is substantially L-shaped and a surface with a step face (4) and a circumferential dam (3). The arcuate support arm (25) has a tooth (27) at one end adjacent to an outermost circumferential surface (26) along the seal runner (19), which could include an optional notch (37). The tooth (27) and outermost circumferential surface (26) are separated by a gap (28). The secondary seal ring (6) is disposed between and contacts the primary seal assembly (2) and housing structure (5) so as to form a bore seal and a face seal therewith. A plurality of radial dams (35) disposed along the surface in an outward radial arrangement from the circumferential dam (3) are provided to improve the stiffness of the thin film. Features of the invention allow for higher operating speeds.
    • 提出了一种用于涡轮发动机的改进的气垫密封系统(1)。 密封系统(1)包括可移动主密封组件(2),固定二次密封组件以及至少一个结构,以增加主密封件和旋转部件之间的薄膜的刚度。 主密封组件(2)包括环形密封环(23)和弓形支撑臂(25)。 环形密封环(23)具有大致L形的横截面和具有台阶面(4)和周向坝(3)的表面。 弧形支撑臂(25)在与密封流道(19)的最外周表面(26)相邻的一端处具有齿(27),其可包括任选的凹口(37)。 齿(27)和最外圆周表面(26)被间隙(28)隔开。 二次密封环(6)设置在主密封组件(2)和壳体结构(5)之间并与之接触,以便与其形成孔密封和面密封。 为了提高薄膜的刚度,提供了多个从周向坝(3)沿着表面设置的向外径向布置的径向坝(35)。 本发明的特征允许更高的操作速度。