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61. 发明申请

US20090178416A1 BIFURCATION AND AFT VENT USED TO VARY FAN NOZZLE EXIT AREA 有权
标题翻译：用于风扇喷嘴出口区域的分岔和通风口
公开(公告)号：US20090178416A1
公开(公告)日：2009-07-16
申请号：US12374336
申请日：2006-10-12
申请人： Edward F. Migliaro , Michael Winter , Ashok K. Jain
发明人： Edward F. Migliaro , Michael Winter , Ashok K. Jain
IPC分类号： F02K1/30 , F02K3/06
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。

62. 发明申请

US20090092482A1 Systems and Methods for Altering Inlet Airflow of Gas Turbine Engines 有权
标题翻译：改变燃气轮机入口气流的系统和方法
公开(公告)号：US20090092482A1
公开(公告)日：2009-04-09
申请号：US11869040
申请日：2007-10-09
申请人： Michael Winter
发明人： Michael Winter
IPC分类号： F01D17/00
CPC分类号： F02C7/042 , F02C7/047 , F02K3/06
摘要： Systems and methods for altering airflow to gas turbine engines are provided. In this regard, a representative system includes a gas turbine engine inlet having a slat, the slat being movable between a retracted position and an extended position. In the extended position, the slat increases an effective diameter of the inlet compared to the diameter of the inlet when in the retracted position.
摘要翻译：提供了改变燃气轮机发动机气流的系统和方法。在这方面，代表性系统包括具有板条的燃气涡轮发动机入口，所述板条可在缩回位置和伸出位置之间移动。在延伸位置，当处于缩回位置时，板条增加入口的有效直径与入口的直径相比。

63. 发明申请

US20080001039A1 Thrust vectorable fan variable area nozzle for a gas turbine engine fan nacelle 有权
标题翻译：用于燃气涡轮发动机风扇机舱的推力矢量风机可变面积喷嘴
公开(公告)号：US20080001039A1
公开(公告)日：2008-01-03
申请号：US11582219
申请日：2006-10-17
申请人： Michael Winter , Russell B. Hanson
发明人： Michael Winter , Russell B. Hanson
IPC分类号： B64D33/00
CPC分类号： F01D17/141 , F02K1/06 , F02K1/1207 , F02K1/15 , F02K3/06 , F02K3/075 , F05D2260/50 , F05D2270/60 , F05D2270/62
摘要： A thrust vectorable fan variable area nozzle (FVAN) includes a synchronizing ring, a static ring, and a flap assembly mounted within a fan nacelle. An actuator assembly selectively rotates synchronizing ring segments relative the static ring to adjust segments of the flap assembly to vary the annular fan exit area and vector the thrust through asymmetrical movement of the thrust vectorable FVAN segments. In operation, adjustment of the entire periphery of the thrust vectorable FVAN in which all segments are moved simultaneously to maximize engine thrust and fuel economy during each flight regime. By separately adjusting the segments of the thrust vectorable FVAN, engine trust is selectively vectored to provide, for example only, trim balance or thrust controlled maneuvering.
摘要翻译：推力可动风扇可变区域喷嘴（FVAN）包括安装在风扇机舱内的同步环，静止环和挡板组件。致动器组件选择性地相对于静态环旋转同步环段，以调整翼片组件的段以改变环形风扇出口区域，并且通过推力可动的FVAN段的不对称运动来矢量推力。在操作中，调整可推力矢量FVAN的整个周边，其中所有段同时移动，以在每个飞行状态期间最大化发动机推力和燃料经济性。通过单独调节推力可矢量的FVAN的段，选择性地引导发动机信任，以提供例如仅修剪平衡或推力控制的操纵。

64. 发明授权

US06422039B1 Gem 有权
公开(公告)号：US06422039B1
公开(公告)日：2002-07-23
申请号：US09732730
申请日：2000-12-11
申请人： Wolfgang Bamminger , Herbert Öfner , Emil Reisigl , Harald Weingärtner , Michael Winter
发明人： Wolfgang Bamminger , Herbert Öfner , Emil Reisigl , Harald Weingärtner , Michael Winter
IPC分类号： A44C1700
摘要： A gemstone has a faceted crown which is inclined with respect to the main axis and which is defined on the one end by a preferably flat table and on the other hand by a peripheral edge of the gemstone. A faceted pavilion is inclined with respect to the main axis, adjoins the peripheral edge, and converges to a tip. The facets (3) of the crown (2) are all inclined at the same crown angle (&bgr;) with respect to the main axis (1), while the facets (7, 7′) of the pavilion (6) are inclined at two different pavilion angles (&agr;1, &agr;2) with respect to the main axis (1). The first set of facets (7) of the pavilion (6) which are inclined at a first pavilion angle (&agr;1) extend to the peripheral edge (5), and the second set of facets (7′) of the pavilion (6) which are inclined at a second pavilion angle (&agr;2) start from the tip (8) without reaching the peripheral edge (5).

65. 外观设计

USD460376S1 Ornamental object 失效
标题翻译：观赏对象
公开(公告)号：USD460376S1
公开(公告)日：2002-07-16
申请号：US29133638
申请日：2000-12-05
申请人： Wolfgang Bamminger , Herbert Öfner , Emil Reisigl , Harald Weingärtner , Michael Winter
设计人： Wolfgang Bamminger , Herbert Öfner , Emil Reisigl , Harald Weingärtner , Michael Winter

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