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1. 发明授权

US08291715B2 Bi-modal turbine assembly and starter / drive turbine system employing the same 有权
标题翻译：双模涡轮机组件和起动/驱动涡轮机系统采用它
公开(公告)号：US08291715B2
公开(公告)日：2012-10-23
申请号：US12137303
申请日：2008-06-11
申请人： Tony Libera , Peter Zeiner
发明人： Tony Libera , Peter Zeiner
IPC分类号： F02C7/277 , F02C7/32 , F02C6/08
CPC分类号： F02C7/277 , F02C6/08 , F02C7/32 , F05D2260/85 , Y02T50/671
摘要： A bi-modal turbine assembly is provided for use in conjunction with a gas turbine engine. In one embodiment, the bi-modal turbine assembly includes a housing assembly having a flow passage therethrough, a turbine wheel rotatably mounted in the housing assembly and positioned so as to be driven by pressurized air flowing through the flow passage, an output shaft rotatably mounted in the housing assembly, and first and second gear trains disposed in the housing assembly. A switching device is also disposed in the housing assembly and configured to mechanically couple: (i) the first gear train between the turbine wheel and the output shaft in a first operational mode, and (ii) the second gear train between the turbine wheel and the output shaft in a second operational mode.
摘要翻译：提供了与燃气涡轮发动机结合使用的双模式涡轮组件。在一个实施例中，双模涡轮组件包括具有穿过其中的流动通道的壳体组件，涡轮机叶轮可旋转地安装在壳体组件中并且定位成由流过流动通道的加压空气驱动，输出轴可旋转地安装在壳体组件中，以及设置在壳体组件中的第一和第二齿轮系。开关装置还设置在壳体组件中并且构造成在第一操作模式下机械地联接：（i）在涡轮机叶轮和输出轴之间的第一齿轮系，以及（ii）涡轮机叶轮和输出轴处于第二操作模式。

2. 发明申请

US20110296812A1 THRUST REVERSER ACTUATION SYSTEM ARCHITECTURE 审中-公开
标题翻译：逆向转换器启动系统架构
公开(公告)号：US20110296812A1
公开(公告)日：2011-12-08
申请号：US12796418
申请日：2010-06-08
申请人： Steve Abel , Tony Libera
发明人： Steve Abel , Tony Libera
IPC分类号： F02K1/54 , H02K7/116 , H02K7/102 , F16H57/00
CPC分类号： F02K1/763 , F05D2260/4031 , Y02T50/671 , Y10T74/19
摘要： A thrust reverser actuation system includes a plurality of actuators, a power drive unit, and a gear set. Each actuator is coupled to receive an actuator input torque and is configured, upon receipt of the actuator input torque, to move between a stowed position and a deployed position. The power drive unit has only one output shaft, and is configured to supply a drive torque via the output shaft. The gear set is connected to the output shaft and is coupled to each of the actuators. The gear set is configured to receive the drive torque via the output shaft and to supply the actuator input torque to each of the actuators.
摘要翻译：推力反向器致动系统包括多个致动器，动力驱动单元和齿轮组。每个致动器被联接以接收致动器输入扭矩，并且在接收到致动器输入扭矩时被配置为在收起位置和展开位置之间移动。动力驱动单元仅具有一个输出轴，并且经配置以通过输出轴提供驱动扭矩。齿轮组连接到输出轴并联接到每个致动器。齿轮组构造成经由输出轴接收驱动扭矩，并将致动器输入扭矩提供给每个致动器。

3. 发明申请

US20090314002A1 BI-MODAL TURBINE ASSEMBLY AND STARTER / DRIVE TURBINE SYSTEM EMPLOYING THE SAME 有权
标题翻译：双模式涡轮组件和启动器/驱动器涡轮机系统
公开(公告)号：US20090314002A1
公开(公告)日：2009-12-24
申请号：US12137303
申请日：2008-06-11
申请人： Tony Libera , Peter Zeiner
发明人： Tony Libera , Peter Zeiner
IPC分类号： F02C7/277 , F01D15/12
CPC分类号： F02C7/277 , F02C6/08 , F02C7/32 , F05D2260/85 , Y02T50/671
摘要： A bi-modal turbine assembly is provided for use in conjunction with a gas turbine engine. In one embodiment, the bi-modal turbine assembly includes a housing assembly having a flow passage therethrough, a turbine wheel rotatably mounted in the housing assembly and positioned so as to be driven by pressurized air flowing through the flow passage, an output shaft rotatably mounted in the housing assembly, and first and second gear trains disposed in the housing assembly. A switching device is also disposed in the housing assembly and configured to mechanically couple: (i) the first gear train between the turbine wheel and the output shaft in a first operational mode, and (ii) the second gear train between the turbine wheel and the output shaft in a second operational mode.
摘要翻译：提供了与燃气涡轮发动机结合使用的双模式涡轮组件。在一个实施例中，双模涡轮组件包括具有穿过其中的流动通道的壳体组件，涡轮机叶轮可旋转地安装在壳体组件中并且定位成由流过流动通道的加压空气驱动，输出轴可旋转地安装在壳体组件中，以及设置在壳体组件中的第一和第二齿轮系。开关装置还设置在壳体组件中并且构造成在第一操作模式下机械地联接：（i）在涡轮机叶轮和输出轴之间的第一齿轮系，以及（ii）涡轮机叶轮和输出轴处于第二操作模式。

4. 发明授权

US08146370B2 Turbine drive system with lock-up clutch and method 有权
标题翻译：具有锁止离合器和方法的涡轮驱动系统
公开(公告)号：US08146370B2
公开(公告)日：2012-04-03
申请号：US12124362
申请日：2008-05-21
申请人： Peter Kenneth Zeiner , Tony Libera , Todd Langston
发明人： Peter Kenneth Zeiner , Tony Libera , Todd Langston
IPC分类号： F02C3/10 , F02C6/00
CPC分类号： F02C3/10 , F02C7/32 , F02C9/18 , Y02T50/671
摘要： A pneumatically driven turbine drive system is coupled to a gas turbine engine that includes low and high pressure compressors, low and high pressure turbines, a lock-up clutch, and at least one engine accessory driven by the high pressure compressor. The pneumatically driven turbine drive system selectively bleeds air discharged from the high pressure compressor and supplies it to an air turbine that is coupled to the at least one engine accessory. Thus, the system selectively reduces the power extracted from the high pressure compressor and is capable of supplying power back to the engine core. This, coupled with the bleed air that is diverted from the high pressure turbine and the low pressure turbine, allows the high pressure spool and the low pressure spool to run at lower speeds when high engine thrust is not needed or desired, but when the at least one engine accessory is still needed.
摘要翻译：气动涡轮机驱动系统耦合到包括低压和高压压缩机，低压和高压涡轮机，锁止离合器和由高压压缩机驱动的至少一个发动机附件的燃气涡轮发动机。气动驱动的涡轮驱动系统选择性地将从高压压缩机排出的空气排出并将其提供到联接到至少一个发动机附件的空气涡轮机。因此，系统选择性地降低从高压压缩机提取的功率，并且能够将功率返回到发动机芯。这与从高压涡轮机和低压涡轮机转向的排出空气相结合，允许高压阀芯和低压阀芯在不需要或期望的高发动机推力时以较低的速度运行，但是当at 仍然需要至少一个发动机附件。

5. 发明申请

US20090288421A1 TURBINE DRIVE SYSTEM WITH LOCK-UP CLUTCH AND METHOD 有权
标题翻译：具有锁定离合器和方法的涡轮驱动系统
公开(公告)号：US20090288421A1
公开(公告)日：2009-11-26
申请号：US12124362
申请日：2008-05-21
申请人： Peter Kenneth Zeiner , Tony Libera , Todd Langston
发明人： Peter Kenneth Zeiner , Tony Libera , Todd Langston
IPC分类号： F02C3/10 , F02C9/18 , F02C6/00 , F02C7/275
CPC分类号： F02C3/10 , F02C7/32 , F02C9/18 , Y02T50/671
摘要： A pneumatically driven turbine drive system is coupled to a gas turbine engine that includes low and high pressure compressors, low and high pressure turbines, a lock-up clutch, and at least one engine accessory driven by the high pressure compressor. The pneumatically driven turbine drive system selectively bleeds air discharged from the high pressure compressor and supplies it to an air turbine that is coupled to the at least one engine accessory. Thus, the system selectively reduces the power extracted from the high pressure compressor and is capable of supplying power back to the engine core. This, coupled with the bleed air that is diverted from the high pressure turbine and the low pressure turbine, allows the high pressure spool and the low pressure spool to run at lower speeds when high engine thrust is not needed or desired, but when the at least one engine accessory is still needed.
摘要翻译：气动涡轮机驱动系统耦合到包括低压和高压压缩机，低压和高压涡轮机，锁止离合器和由高压压缩机驱动的至少一个发动机附件的燃气涡轮发动机。气动驱动的涡轮驱动系统选择性地将从高压压缩机排出的空气排出并将其提供到联接到至少一个发动机附件的空气涡轮机。因此，系统选择性地降低从高压压缩机提取的功率，并且能够将功率返回到发动机芯。这与从高压涡轮机和低压涡轮机转向的排出空气相结合，允许高压阀芯和低压阀芯在不需要或期望的高发动机推力时以较低的速度运行，但是当at 仍然需要至少一个发动机附件。

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