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    • 3. 发明授权
    • Turbine nozzle phasing device
    • 涡轮喷嘴定相装置
    • US5178513A
    • 1993-01-12
    • US774520
    • 1991-10-08
    • William C. TrommerGary D. Nohr
    • William C. TrommerGary D. Nohr
    • F01D17/18F42B19/18
    • F42B19/18F01D17/18
    • Turbine nozzle phasing device for controlling a flow of gasses to a plurality of nozzles in response to a control signal. The turbine nozzle phasing device includes a housing having a lower portion which includes a first plenum for receiving the flow of hot gasses and an upper portion which includes a second plenum integral with the first plenum, a detachable partition for separating the first plenum from the second plenum and a first nozzle which communicates with the first plenum. Hot gasses flowing into the first plenum flows through the first nozzle. A set of second nozzles is provided which communicates with the second plenum. Partition detaching apparatus is also included for detaching the detachable partition in response to the control signal to permit a portion of the hot gasses flowing into the first plenum to flow into the second plenum and through the set of second nozzles.
    • 涡轮喷嘴定相装置,用于响应控制信号控制气体流向多个喷嘴。 涡轮喷嘴定相装置包括壳体,其具有下部,该下部包括用于接收热气体流的第一增压室和包括与第一增压室成一体的第二增压室的上部,用于将第一增压室与第二增压室分开的可拆卸隔板 气室和与第一增压室连通的第一喷嘴。 流入第一增压室的热气体流经第一喷嘴。 提供一组第二喷嘴,其与第二增压室连通。 还包括隔离分离装置,用于响应于控制信号分离可拆卸隔板,以允许流入第一增压室的热气体的一部分流入第二增压室并通过该组第二喷嘴。
    • 5. 发明授权
    • Unidirectional no-back device
    • 单向无背装置
    • US4909363A
    • 1990-03-20
    • US061713
    • 1987-06-15
    • William C. Trommer
    • William C. Trommer
    • B64C13/28F16D43/02F16D65/14F16D67/00F16H31/00
    • B64C13/28F16D43/02F16D67/00F16H31/00F16D2121/16F16D2125/38
    • A unidirectional no-back device having an input shaft and an output shaft and grounded releasable brake structure for holding the output shaft against rotation. A drive train between the input and output shafts has first and second ball and ramp structures. The first ball and ramp structure is operable upon rotation of the input shaft in either direction by a prime mover to release the brake structure and enable driving of the output shaft by the input shaft. The second ball and ramp structure is responsive to torque flow from rotation of the output shaft in one direction to release the brake structure to permit backdriving of the input shaft and prime mover from the output shaft and is inoperative in response to torque flowing in an opposite direction of rotation of the output shaft so as to not release the brake structure and thus preclude rotation of the output shaft.
    • 具有输入轴和输出轴以及用于保持输出轴抵抗旋转的接地可释放制动结构的单向无背装置。 输入轴和输出轴之间的传动系具有第一和第二球和斜坡结构。 第一球和斜坡结构可在原动机沿任一方向旋转输入轴时操作,以释放制动结构并且能够通过输入轴驱动输出轴。 第二球和斜坡结构响应于在一个方向上从输出轴的旋转引起的扭矩流动以释放制动结构,以允许输入轴和原动机从输出轴反向驱动,并且响应于相反的扭矩流动而不起作用 输出轴的旋转方向,以便不释放制动结构,从而排除输出轴的旋转。
    • 6. 发明授权
    • Anti-rotation feature for air turbine starter
    • 空转涡轮起动器的防旋转功能
    • US08475116B2
    • 2013-07-02
    • US12842094
    • 2010-07-23
    • William C. TrommerJeffrey M. Makulec
    • William C. TrommerJeffrey M. Makulec
    • F01D15/12
    • F01D25/16F05D2270/116Y10T29/53
    • A turbine balance assembly has a turbine rotor and shaft. Bearings are positioned radially outwardly of the shaft. A bearing sleeve is positioned radially outwardly of the bearings, and supports the bearings. The bearing sleeve extends along an axial length defined by a rotational axis of the shaft, and has a turbine rotor end adjacent to the turbine rotor, and a remote end. A radially outwardly extending flange on the bearing sleeve extends radially outwardly of a support portion of the bearing sleeve at the turbine rotor end. The flange has a nominal outer diameter, and includes a slot for receiving an anti-rotation tab from a gear cage over a first circumferential extent. A bearing sleeve incorporates the anti-rotation feature, and a gear cage incorporates its portion of the anti-rotation feature. An air turbine starter, and a method of installing components of a turbine balance assembly are also disclosed.
    • 涡轮平衡组件具有涡轮转子和轴。 轴承位于轴的径向外侧。 轴承套定位在轴承的径向外侧,并支承轴承。 轴承套筒沿着由轴的旋转轴线限定的轴向长度延伸,并且具有与涡轮转子相邻的涡轮机转子端和远端。 在轴承套筒上的径向向外延伸的凸缘在涡轮转子端处径向向外延伸到轴承套筒的支撑部分。 凸缘具有标称外径,并且包括用于在第一圆周范围上从齿轮箱接收抗旋转凸片的狭槽。 轴承套筒包含防旋转特征,齿轮箱结合其抗旋转特征部分。 还公开了一种空气涡轮起动器和安装涡轮平衡组件的部件的方法。
    • 7. 发明授权
    • Manual connect-disconnect coupling
    • 手动连接断开连接
    • US5040654A
    • 1991-08-20
    • US431397
    • 1989-11-03
    • William C. Trommer
    • William C. Trommer
    • F16D11/10
    • F16D11/10
    • Difficulties in interrupting a mechanical power transmission path may be minimized in a manual connect-disconnect operator which includes a coupling shaft (38) and a translatable carrier (28) journalling the coupling shaft (38) for rotation about an axis and mounting the coupling shaft (38) for axial movement along the axis between connect and disconnect positions. A yoke (52) is mounted on a pivot (54) and is connected to the carrier (28) for translating the carrier (28) to move the coupling shaft (38) upon pivotal movement of the yoke (52). A manual actuator (78) is mounted for reciprocating movement and a detent mechanism (92), (94), (100), (102), (104), (106), (108) is operable to maintain the carrier (28) in either of the positions.
    • 中断机械动力传递路径的困难可以在手动连接断开操作器中被最小化,手动连接断开操作器包括连接轴(38)和可平移的联接轴(38)的平移载体(28),用于围绕轴线旋转并安装联接轴 (38),用于沿着连接和断开位置之间的轴线轴向运动。 轭架(52)安装在枢轴(54)上,并连接到托架(28)上,用于平移托架(28),以便在轭架(52)枢转运动时移动联轴器(38)。 安装手动致动器(78)用于往复运动,并且止动机构(92),(94),(100),(102),(104),(106),(108)可操作以维持载体 )在任一位置。
    • 8. 发明申请
    • ANTI-ROTATION FEATURE FOR AIR TURBINE STARTER
    • 空气涡轮起动器的抗旋转特性
    • US20120020784A1
    • 2012-01-26
    • US12842094
    • 2010-07-23
    • William C. TrommerJeffrey M. Makulec
    • William C. TrommerJeffrey M. Makulec
    • F04D29/04B23P19/00
    • F01D25/16F05D2270/116Y10T29/53
    • A turbine balance assembly has a turbine rotor and shaft. Bearings are positioned radially outwardly of the shaft. A bearing sleeve is positioned radially outwardly of the bearings, and supports the bearings. The bearing sleeve extends along an axial length defined by a rotational axis of the shaft, and has a turbine rotor end adjacent to the turbine rotor, and a remote end. A radially outwardly extending flange on the bearing sleeve extends radially outwardly of a support portion of the bearing sleeve at the turbine rotor end. The flange has a nominal outer diameter, and includes a slot for receiving an anti-rotation tab from a gear cage over a first circumferential extent. A bearing sleeve incorporates the anti-rotation feature, and a gear cage incorporates its portion of the anti-rotation feature. An air turbine starter, and a method of installing components of a turbine balance assembly are also disclosed.
    • 涡轮平衡组件具有涡轮转子和轴。 轴承位于轴的径向外侧。 轴承套定位在轴承的径向外侧,并支承轴承。 轴承套筒沿着由轴的旋转轴线限定的轴向长度延伸,并且具有与涡轮转子相邻的涡轮机转子端和远端。 在轴承套筒上的径向向外延伸的凸缘在涡轮转子端处径向向外延伸到轴承套筒的支撑部分。 凸缘具有标称外径,并且包括用于在第一圆周范围上从齿轮箱接收抗旋转凸片的狭槽。 轴承套筒包含防旋转特征,齿轮箱结合其抗旋转特征部分。 还公开了一种空气涡轮起动器和安装涡轮平衡组件的部件的方法。