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1. 发明申请

US20120076987A1 ISO-GRID COMPOSITE COMPONENT 有权
标题翻译： ISO-GRID复合组件
公开(公告)号：US20120076987A1
公开(公告)日：2012-03-29
申请号：US12892014
申请日：2010-09-28
申请人： Russell B. Hanson
发明人： Russell B. Hanson
IPC分类号： B32B3/00 , B32B37/00
CPC分类号： B23P15/04 , B29C70/085 , B29C70/30 , B29D28/005 , Y10T156/10 , Y10T428/24612
摘要： An iso-grid composite component includes a spacer transverse to a uni-tape ply bundle, the spacer interrupted by the uni-tape ply bundle.
摘要翻译：等网格复合部件包括横向于单面胶带束的隔离物，隔离物被单带束层中断。

2. 发明申请

US20100139285A1 THRUST VECTORABLE FAN VARIABLE AREA NOZZLE FOR A GAS TURBINE ENGINE FAN NACELLE 有权
公开(公告)号：US20100139285A1
公开(公告)日：2010-06-10
申请号：US12616750
申请日：2009-11-11
申请人： Michael Winter , Russell B. Hanson
发明人： Michael Winter , Russell B. Hanson
IPC分类号： F02K1/06
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.

3. 发明授权

US07637095B2 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：US07637095B2
公开(公告)日：2009-12-29
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： F02K3/02
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。

4. 发明授权

US4463663A Hydraulic cylinder assembly with a liquid recovery system 失效
标题翻译：液压缸组件采用液体回收系统
公开(公告)号：US4463663A
公开(公告)日：1984-08-07
申请号：US428249
申请日：1982-09-29
申请人： Wallace A. Hanson, Jr. , Russell B. Hanson
发明人： Wallace A. Hanson, Jr. , Russell B. Hanson
IPC分类号： F15B15/14 , F15B21/04
CPC分类号： F15B15/1433 , F15B15/149
摘要： A compressible bellows surrounds a piston rod of the hydraulic cylinder of a hydraulic elevator. The lower end of the bellows surrounds a liquid receiving recess in the gland box of the cylinder and, when a sealing ring on the piston rod closes and compresses the bellows, the leaked hydraulic fluid is discharged from the recess, via a ball check valve, and a return tube to a sump.
摘要翻译：可压缩波纹管围绕液压升降机的液压缸的活塞杆。波纹管的下端围绕圆筒的压盖盒中的液体容纳凹槽，当活塞杆上的密封圈关闭并压缩波纹管时，泄漏的液压流体通过球形止回阀从凹部排出，并将回流管连接到集水槽。

5. 发明授权

US07721551B2 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风扇可变面积喷嘴
公开(公告)号：US07721551B2
公开(公告)日：2010-05-25
申请号：US11478009
申请日：2006-06-29
申请人： Russell B. Hanson
发明人： Russell B. Hanson
IPC分类号： F02K1/00
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 fan variable area nozzle (FVAN) selectively rotates a synchronizing ring relative the static ring to adjust a flap assembly through a linkage to vary an annular fan exit area through which fan air is discharged. By adjusting the FVAN, engine thrust and fuel economy are maximized during each flight regime.
摘要翻译：风扇可变区域喷嘴（FVAN）相对于静环选择性地旋转同步环，以通过连杆调节翼片组件以改变风扇空气排出的环形风扇出口区域。通过调整FVAN，发动机推力和燃油经济性在每个飞行状态下最大化。

6. 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。

7. 发明申请

US20080000235A1 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风扇可变面积喷嘴
公开(公告)号：US20080000235A1
公开(公告)日：2008-01-03
申请号：US11478009
申请日：2006-06-29
申请人： Russell B. Hanson
发明人： Russell B. Hanson
IPC分类号： F02K1/00
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 fan variable area nozzle (FVAN) selectively rotates a synchronizing ring relative the static ring to adjust a flap assembly through a linkage to vary an annular fan exit area through which fan air is discharged. By adjusting the FVAN, engine thrust and fuel economy are maximized during each flight regime.
摘要翻译：风扇可变区域喷嘴（FVAN）相对于静环选择性地旋转同步环，以通过连杆调节翼片组件以改变风扇空气排出的环形风扇出口区域。通过调整FVAN，发动机推力和燃油经济性在每个飞行状态下最大化。

8. 发明授权

US09126374B2 Iso-grid composite component 有权
标题翻译：等网复合组件
公开(公告)号：US09126374B2
公开(公告)日：2015-09-08
申请号：US12892014
申请日：2010-09-28
申请人： Russell B. Hanson
发明人： Russell B. Hanson
IPC分类号： B32B3/00 , B29C70/08 , B29C70/30 , B29D28/00
CPC分类号： B23P15/04 , B29C70/085 , B29C70/30 , B29D28/005 , Y10T156/10 , Y10T428/24612
摘要： An iso-grid composite component includes a spacer transverse to a uni-tape ply bundle, the spacer interrupted by the uni-tape ply bundle.
摘要翻译：等网格复合部件包括横向于单面胶带束的隔离物，隔离物被单带束层中断。

9. 发明授权

US08769925B2 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：US08769925B2
公开(公告)日：2014-07-08
申请号：US12616750
申请日：2009-11-11
申请人： Michael Winter , Russell B. Hanson
发明人： Michael Winter , Russell B. Hanson
IPC分类号： F02K3/02
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号，以提供例如仅修剪平衡或推力控制的操纵。

10. 发明申请

US20140216042A1 COMBUSTOR COMPONENT WITH COOLING HOLES FORMED BY ADDITIVE MANUFACTURING 审中-公开
标题翻译：具有加热制成的冷却孔的混合器组件
公开(公告)号：US20140216042A1
公开(公告)日：2014-08-07
申请号：US13630835
申请日：2012-09-28
申请人： Russell B. Hanson
发明人： Russell B. Hanson
IPC分类号： F23R3/06 , F23R3/00
CPC分类号： F23R3/06 , F23R3/002 , F23R2900/00018 , F23R2900/03043 , Y02T50/675 , Y10T29/49826
摘要： Combustor liners made using additive manufacturing techniques can employ cooling hole patterns which are not possible, or at least time consuming or expensive, to make using traditional subtractive manufacturing techniques. By additively manufacturing floatwall panels, cooling holes may be placed along axes that transect features on the floatwall panel, such as mounting studs, spacers, cooling pedestals, and rails.
摘要翻译：使用添加剂制造技术制造的燃烧器衬套可以采用冷却孔图案，这是使用传统的减法制造技术不可能或至少耗时或昂贵的冷却孔图案。通过相互制造浮动面板，可以沿着横穿浮动壁面板上的特征的轴放置冷却孔，例如安装螺柱，间隔件，冷却基座和导轨。

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