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    • 53. 发明申请
    • VARIABLE GEOMETRY TURBOMACHINE
    • 可变几何涡轮机
    • US20120286066A1
    • 2012-11-15
    • US13489084
    • 2012-06-05
    • Robert L. Holroyd
    • Robert L. Holroyd
    • B64D33/04B21K3/00
    • F01D25/24F01D17/143F05D2220/40F05D2260/30Y10T29/49229Y10T29/49231
    • Variable geometry turbomachine with a bearing housing, an adjacent turbine housing, a turbine wheel rotating in the turbine housing about a turbine axis; an inlet passage upstream of the turbine wheel between inlet surfaces of first and second wall members, one wall member moveable along the turbine axis to vary the inlet passage size; vanes across the inlet passage connected to a first wall member; an array of vane slots defined by the second wall member to receive the vanes for relative movement between the wall members; the second wall member comprising a shroud defining vane slots; the second wall member supported by a support member retained by a mounting feature; the mounting feature being one of the bearing housings, the turbine housing, or the actuation element; and the shroud is fixed to the support member so axial movement of the shroud relative to the support member is substantially prevented.
    • 具有轴承壳体,相邻涡轮壳体的可变几何涡轮机,绕涡轮机壳体绕涡轮机轴线旋转的涡轮机叶轮; 涡轮机叶轮上游的入口通道在第一和第二壁构件的入口表面之间,一个壁构件可沿涡轮机轴线移动以改变入口通道的尺寸; 穿过连接到第一壁构件的入口通道的叶片; 由所述第二壁构件限定的用于接收所述叶片以用于所述壁构件之间的相对运动的叶片槽的阵列; 所述第二壁构件包括限定叶片槽的护罩; 所述第二壁构件由被安装特征保持的支撑构件支撑; 安装特征是轴承壳体,涡轮壳体或致动元件之一; 并且护罩固定到支撑构件上,因此基本上防止了护罩相对于支撑构件的轴向运动。
    • 55. 发明申请
    • METHOD OF FABRICATING A NEARWALL NOZZLE IMPINGEMENT COOLED COMPONENT FOR AN INTERNAL COMBUSTION ENGINE
    • 一种用于内燃机的近壁喷嘴冷却组件的制造方法
    • US20120272521A1
    • 2012-11-01
    • US13094966
    • 2011-04-27
    • Ching-Pang LeeJay A. Morrison
    • Ching-Pang LeeJay A. Morrison
    • B21K3/00F02C3/00
    • B21K3/00F01D9/023F05D2260/201F23R3/425F23R3/46
    • A method of forming an internal combustion engine component having a multi-panel outer wall. The multi-panel outer wall has an inner panel (16) with an inner surface (18) and an outer surface (37). The inner panel outer surface (37) has discrete pockets (23) formed by integral structural ribs (38). Each pocket (23) has a film cooling hole (31) between the pocket (23) and the plenum (20). The method includes: forming dimples (40) in the intermediate panel (22), at least one dimple (40) having a nozzle (29); securing the intermediate panel (22) to the inner panel outer surface (37), thereby enclosing at least one pocket (23); and ensuring a respective dimple (40) having a nozzle (29) protrudes into a respective enclosed pocket (24) and a respective nozzle (29) is configured to direct a respective jet (35) of cooling fluid onto the inner panel outer surface within the respective enclosed pocket (23).
    • 一种形成具有多面板外壁的内燃机部件的方法。 多面板外壁具有带有内表面(18)和外表面(37)的内板(16)。 内板外表面(37)具有由整体结构肋(38)形成的分立的袋(23)。 每个袋(23)在袋(23)和集气室(20)之间具有膜冷却孔(31)。 该方法包括:在中间板(22)中形成凹坑(40),至少一个具有喷嘴(29)的凹坑(40); 将所述中间板(22)固定到所述内板外表面(37)上,从而封闭至少一个凹槽(23); 并且确保具有喷嘴(29)的相应的凹坑(40)突出到相应的封闭的袋(24)中,并且相应的喷嘴(29)构造成将相应的冷却流体喷射(35)引导到内板的外表面 相应的封闭口袋(23)。
    • 56. 发明申请
    • CYLINDER BLOCK ASSEMBLY FOR X-ENGINES
    • 用于X发动机的气缸组件
    • US20120255516A1
    • 2012-10-11
    • US13517485
    • 2011-09-06
    • Matthew Byrne Diggs
    • Matthew Byrne Diggs
    • F02F7/00B21K3/00
    • F02F7/0017F01B9/026F02F7/0046
    • A cylinder block assembly (300) for an X-engine includes a first block half (302) having two cylinder banks (453, 454) and valley openings (361, 362) between the two cylinder banks (453, 454); and a second block half (304) fastened to the first block half (302), the second block half (304) having two cylinder banks (451, 452) and valley openings (361, 362) between the two cylinder banks (451, 452). The valley openings (361, 362) in the first and second block halves (302, 304) allow an X-engine crank train assembly (10, 100) to be assembled within the cylinder block assembly (300).
    • 用于X发动机的气缸体组件(300)包括在两个气缸组(453,454)之间具有两个气缸组(453,454)和凹槽开口(361,362)的第一块半体(302)。 以及紧固到所述第一块半部(302)的第二块半部(304),所述第二块半部(304)在所述两个气缸组(451,452)之间具有两个气缸组(451,452)和所述凹部开口(361,362) 452)。 第一和第二半块(302,304)中的谷部开口(361,362)允许将X发动机曲柄组件(10,100)组装在气缸体组件(300)内。