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1. 发明申请

US20050022465A1 Flexible, deployment rate damped hinge 有权
标题翻译：灵活的部署速度阻尼铰链
公开(公告)号：US20050022465A1
公开(公告)日：2005-02-03
申请号：US10891907
申请日：2004-07-15
申请人： Peter Warren , John Williams , Victor Leemon , Michael Winter
发明人： Peter Warren , John Williams , Victor Leemon , Michael Winter
IPC分类号： B64G1/22 , B64G99/00 , E04B1/344 , E04C3/00 , E04C3/04 , E04C3/07 , E04C3/08 , E04C3/28 , E04C3/29 , E04H12/00
CPC分类号： B64G9/00 , B64G1/222 , E04B1/3441 , E04C3/005 , E04C3/07 , E04C3/08 , E04C3/28 , E04C3/291 , E04C2003/0413 , E04C2003/0417 , E04C2003/0421 , E04C2003/043 , E04C2003/0434 , E04C2003/0447 , E04C2003/0495 , E05D1/02 , E05F15/60 , E05Y2201/43 , E05Y2800/67 , E05Y2900/502 , Y10T16/525 , Y10T16/548 , Y10T16/555
摘要： A flexible hinge including a first set of plies and a second set of plies, and a hinge area where the first set of plies and the second set of plies bend. A damping material is disposed between plies of the first set and the second set at least at the hinge area thereof to control the deployment of the hinge.
摘要翻译：包括第一组帘布层和第二组帘布层的柔性铰链以及第一组帘布层和第二组帘布层弯曲的铰链区域。阻尼材料至少在其铰链区域处设置在第一组和第二组的层之间，以控制铰链的展开。

2. 发明授权

US08074324B2 Flexible, deployment rate damped hinge 有权
标题翻译：灵活的部署速度阻尼铰链
公开(公告)号：US08074324B2
公开(公告)日：2011-12-13
申请号：US10891907
申请日：2004-07-15
申请人： Peter A. Warren , John Williams , Victor Leemon , Michael Winter
发明人： Peter A. Warren , John Williams , Victor Leemon , Michael Winter
IPC分类号： E05D5/00 , E05D1/00
CPC分类号： B64G9/00 , B64G1/222 , E04B1/3441 , E04C3/005 , E04C3/07 , E04C3/08 , E04C3/28 , E04C3/291 , E04C2003/0413 , E04C2003/0417 , E04C2003/0421 , E04C2003/043 , E04C2003/0434 , E04C2003/0447 , E04C2003/0495 , E05D1/02 , E05F15/60 , E05Y2201/43 , E05Y2800/67 , E05Y2900/502 , Y10T16/525 , Y10T16/548 , Y10T16/555
摘要： A flexible hinge including a first set of plies and a second set of plies, and a hinge area where the first set of plies and the second set of plies bend. A damping material is disposed between plies of the first set and the second set at least at the hinge area thereof to control the deployment of the hinge.
摘要翻译：包括第一组帘布层和第二组帘布层的柔性铰链以及第一组帘布层和第二组帘布层弯曲的铰链区域。阻尼材料至少在其铰链区域处设置在第一组和第二组的层之间，以控制铰链的展开。

3. 发明授权

US09719428B2 Gas turbine engine with pylon mounted accessory drive 有权
公开(公告)号：US09719428B2
公开(公告)日：2017-08-01
申请号：US11947842
申请日：2007-11-30
申请人： Michael Winter
发明人： Michael Winter
IPC分类号： F02C6/00 , F02C7/32 , F02C7/36 , F02K3/06
CPC分类号： F02C7/32 , F02C7/36 , F02K3/06 , F05D2260/4031 , Y02T50/671
摘要： A gas turbine engine includes an accessory gearbox within an engine pylon. The accessory components may be mounted within the engine pylon to save weight and space within the core nacelle as well as provide a relatively lower temperature operating environment.

4. 发明授权

US08727267B2 Variable contraction ratio nacelle assembly for a gas turbine engine 有权
标题翻译：用于燃气涡轮发动机的可变收缩比机舱组件
公开(公告)号：US08727267B2
公开(公告)日：2014-05-20
申请号：US11750398
申请日：2007-05-18
申请人： Ashok K. Jain , Michael Winter
发明人： Ashok K. Jain , Michael Winter
IPC分类号： B64D33/02
CPC分类号： F02K3/06 , F02C7/042 , F02C7/057 , F05D2300/505 , Y02T50/671
摘要： A nacelle assembly includes an inlet lip section having a highlight diameter and a throat diameter. One of the highlight diameter and the throat diameter is fixed and the other of the highlight diameter and the throat diameter is selectively adjustable in each of a first direction and a second direction relative to the inlet lip section to influence a contraction ratio associated with the inlet lip section.
摘要翻译：机舱组件包括具有突出直径和喉部直径的入口唇部。突出直径和喉部直径之一是固定的，并且突出直径和喉部直径中的另一个相对于入口唇部分在第一方向和第二方向中的每一个中是可选择性的，以影响与入口相关联的收缩比唇部。

5. 发明授权

US08650854B2 Bifurcation and aft vent used to vary fan nozzle exit area 有权
标题翻译：分岔和尾部通风口用于改变风扇喷嘴出口区域
公开(公告)号：US08650854B2
公开(公告)日：2014-02-18
申请号：US12374336
申请日：2006-10-12
申请人： Edward F. Migliaro, Jr. , Michael Winter , Ashok K. Jain
发明人： Edward F. Migliaro, Jr. , Michael Winter , Ashok K. Jain
IPC分类号： F02K1/00
CPC分类号： F02K1/15 , F02K1/30 , F02K3/06 , F05D2220/326 , F05D2220/327
摘要： A turbofan engine includes a core nacelle housing a spool having a turbine. A turbofan is arranged upstream from the core nacelle and is coupled to the spool. A fan nacelle surrounds the turbofan and core nacelle. A bifurcation supports the core nacelle relative to the fan nacelle and extends radially between the nacelles. The core and fan nacelles provide a bypass flow path receiving bypass flow from the turbofan. In the example, the nacelles provide a fixed nozzle exit area. The bifurcation includes an inlet that is in communication with a passage. The passage is selectively opened and closed by a valve to provide air from the inlet to a vent opening near the nozzle exit area. By opening the valve, the nozzle exit area is effectively increased to provide increased bypass flow through the turbine engine.
摘要翻译：涡轮风扇发动机包括容纳具有涡轮的阀芯的核心机舱。涡轮风扇布置在核心机舱的上游并联接到线轴。风扇机舱围绕涡轮风扇和核心机舱。分叉支撑相对于风扇机舱的核心机舱，并且在发动机舱之间径向延伸。核心和风扇舱提供旁路流路，从涡轮风扇接收旁路流。在该示例中，发动机舱提供固定的喷嘴出口区域。分叉包括与通道连通的入口。该通道由阀选择性地打开和关闭，以将空气从入口提供到喷嘴出口区域附近的通风口。通过打开阀门，喷嘴出口区域被有效地增加，以提供通过涡轮发动机的增加的旁路流量。

6. 发明授权

US08137060B2 Actuation of a turbofan engine bifurcation to change an effective nozzle exit area 有权
标题翻译：启动涡轮风扇发动机分岔，以改变有效的喷嘴出口区域
公开(公告)号：US08137060B2
公开(公告)日：2012-03-20
申请号：US12441576
申请日：2006-10-12
申请人： Michael Winter , Ashok K. Jain
发明人： Michael Winter , Ashok K. Jain
IPC分类号： F01D17/00
CPC分类号： F02K3/075 , F01D17/141 , F02K1/12
摘要： The invention relates to a turbine engine that includes a spool supporting at least one of a compressor and a turbine. A turbofan is coupled to the spool The spool is arranged in a core nacelle, and the turbofan is arranged upstream from the core nacelle. A fan nacelle surrounds the turbofan and the core nacelle and provides a bypass flow path. A structure extends radially between the core and fan nacelles to support the core nacelle relative to the fan nacelle. Surfaces are supported relative to the fixed structure and are moveable between closed and open positions to selectively obstruct bypass flow through the bypass flow path, thereby changing the effective area of the exit nozzle. A change in the effective area of the nozzle exit can be used to improve the efficiency and operation of the turbine engine.
摘要翻译：本发明涉及一种涡轮发动机，其包括支撑压缩机和涡轮机中的至少一个的阀芯。涡轮风扇联接到阀芯上。阀芯布置在核心机舱中，涡轮风扇布置在核心机舱的上游。风扇机舱围绕涡轮风扇和核心机舱，并提供旁路流动路径。结构在核心和风扇机舱之间径向延伸，以相对于风扇机舱支撑核心机舱。表面相对于固定结构被支撑，并且可在闭合位置和打开位置之间移动，以选择性地阻碍旁路流动通过旁路流动路径，从而改变出口喷嘴的有效面积。可以使用喷嘴出口的有效面积的变化来提高涡轮发动机的效率和操作。

7. 发明申请

US20110004388A1 TURBOFAN TEMPERATURE CONTROL WITH VARIABLE AREA NOZZLE 审中-公开
标题翻译： TURBOFAN温度控制与可变区域喷嘴
公开(公告)号：US20110004388A1
公开(公告)日：2011-01-06
申请号：US12495960
申请日：2009-07-01
申请人： Michael Winter
发明人： Michael Winter
IPC分类号： F02C9/00 , F02K3/02
CPC分类号： F01D17/162 , F01D17/085 , F01D25/34 , F02C9/20 , F02C9/22 , F02C9/28 , F02K1/06 , F02K1/08 , F02K1/09 , F02K3/06 , F05D2270/303
摘要： A control system for a turbofan comprises a variable area nozzle for regulating core flow through the turbofan, an actuator, a temperature sensor, a flight controller and a nozzle control. The actuator is coupled to the variable area nozzle to regulate the core flow by positioning the variable area nozzle. The temperature sensor is positioned in the turbofan to sense a gas path temperature of the core flow. The flight controller is connected to the turbofan to make a thrust demand based on a flight condition of the turbofan. The nozzle control is connected to the flight controller and the actuator for directing the actuator based on the gas path temperature and the flight condition, such that the gas path temperature is controlled by adjusting the variable area nozzle to regulate the core flow while the turbofan meets the thrust demand.
摘要翻译：用于涡轮风扇的控制系统包括用于调节通过涡轮风扇的磁芯流量的可变区域喷嘴，致动器，温度传感器，飞行控制器和喷嘴控制。致动器联接到可变区域喷嘴以通过定位可变区域喷嘴来调节芯流。温度传感器位于涡轮风扇中以感测核心流的气体路径温度。飞行控制器连接到涡轮风扇，以根据涡扇风机的飞行状态产生推力需求。喷嘴控制器连接到飞行控制器和执行器，用于基于气体路径温度和飞行条件来引导致动器，使得通过调节可变面积喷嘴来控制气体路径温度以调节涡轮风扇遇到的核心流量推力需求。

8. 发明申请

US20100236216A1 TURBOFAN ENGINE WITH VARIABLE AREA FAN NOZZLE AND LOW SPOOL GENERATOR FOR EMERGENCY POWER GENERATION AND METHOD FOR PROVIDING EMERGENCY POWER 有权
标题翻译：具有可变区域的涡轮发动机用于紧急发电的发动机和低压发电机，以及用于提供紧急功率的方法
公开(公告)号：US20100236216A1
公开(公告)日：2010-09-23
申请号：US12373165
申请日：2006-10-12
申请人： Michael Winter , Charles E. Lents
发明人： Michael Winter , Charles E. Lents
IPC分类号： F02C9/18 , F02C7/32 , F02K3/06
CPC分类号： F02C7/262 , F01D21/00 , F02C3/113 , F02C7/32 , F05D2270/061 , F05D2270/092 , Y02T50/671
摘要： A turbofan engine (10) employs a flow control device (41) that changes an effective exit nozzle area (40) associated with a bypass flow path (B) of the turbofan engine. A spool (14) couples a fan (20) to a generator (52). The turbofan emergency power system includes a controller (50) that communicates with the flow control device (41). Upon sensing an emergency condition, the controller manipulates the flow control device to reduce the effective nozzle exit area (40) of the bypass flow path, which chokes the flow through the bypass flow path thereby increasing the rotational speed of the fan. In this manner, the generator is driven at a higher rotational speed than if the flow through the bypass flow path was not choked, which enables a smaller generator to be utilized.
摘要翻译：涡轮风扇发动机（10）采用流量控制装置（41），其改变与涡扇发动机的旁路流路（B）相关联的有效出口喷嘴区域（40）。线轴（14）将风扇（20）连接到发电机（52）。涡轮风扇应急电力系统包括与流量控制装置（41）通信的控制器（50）。在感测到紧急情况时，控制器操纵流量控制装置以减少旁路流动路径的有效喷嘴出口区域（40），其阻塞通过旁路流动路径的流动，从而增加风扇的转速。以这种方式，与通过旁路流路的流动没有被阻塞的转速相比，发电机被驱动，这使得能够使用较小的发电机。

9. 外观设计

USD487712S1 Natural gemstone, artificial gemstone ornamental object made of glass 失效
标题翻译：天然宝石，玻璃制造的人造宝石装饰物
公开(公告)号：USD487712S1
公开(公告)日：2004-03-23
申请号：US29181474
申请日：2003-05-13
申请人： Wolfgang Bamminger , Herbert Öfner , Michael Winter
设计人： Wolfgang Bamminger , Herbert Öfner , Michael Winter

10. 外观设计

USD487411S1 Natural gemstone, artificial gemstone; ornamental object made of glass 失效
标题翻译：天然宝石，人造宝石; 由玻璃制成的装饰物
公开(公告)号：USD487411S1
公开(公告)日：2004-03-09
申请号：US29181475
申请日：2003-05-13
申请人： Wolfgang Bamminger , Herbert Öfner , Michael Winter
设计人： Wolfgang Bamminger , Herbert Öfner , Michael Winter

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