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1. 发明公开

EP2070688A2 Aircraft structures bonded with adhesive including magnetostrictive material 有权
标题翻译：用粘合剂材料飞机结构magnetstriktivem粘结
公开(公告)号：EP2070688A2
公开(公告)日：2009-06-17
申请号：EP08171118.6
申请日：2008-12-09
申请人： The Boeing Company
发明人： Rawlings, Diane C. , Miller, Robert J , Krienke, Kenneth A. , Mabe, James H. , Ruggeri, Robert T. , Clingman, Dan J.
IPC分类号： B29C65/48 , B64C1/00
CPC分类号： B29C66/721 , B29C65/4815 , B29C65/4835 , B29C65/485 , B29C65/4855 , B29C65/4875 , B29C65/8253 , B29C65/8284 , B29C66/7212 , B29C70/88 , B29K2101/10 , B29K2101/12 , B29K2105/16 , B29K2503/06 , B29K2705/00 , B29K2705/12 , B29K2995/0003 , B29L2031/3082 , B29L2031/3085 , B64C1/06 , B64F5/60 , C09J5/00 , C09J9/00 , C09J11/00 , G01L1/125 , G01M5/0016 , G01M5/0041 , G01M5/0091 , G01N29/2412 , Y02T50/43 , Y10T403/477 , B29K2307/04
摘要： First and second aircraft structures (110,120) are bonded together with an adhesive (130) including strain-sensitive magnetostrictive material.

2. 发明授权

EP3127804B1 SHAPE MEMORY ALLOY-ACTUATED PROPELLER BLADES AND SHAPE MEMORY ALLOY-ACTUATED PROPELLER ASSEMBLIES 有权
公开(公告)号：EP3127804B1
公开(公告)日：2019-05-15
申请号：EP16171216.1
申请日：2016-05-25
申请人： The Boeing Company
发明人： Bigbee-Bansen, William J. , Clingman, Dan J. , Mabe, James H.
IPC分类号： B64C11/30 , B64C11/44

3. 发明公开

EP2801521A1 Vortex generator using shape memory alloys 有权
标题翻译： Wirbelgenerator unter Verwendung von Formspeicherlegierungen
公开(公告)号：EP2801521A1
公开(公告)日：2014-11-12
申请号：EP14167782.3
申请日：2014-05-09
申请人： The Boeing Company
发明人： Shivashankara, Belur N. , Mabe, James H. , Clingman, Dan J.
IPC分类号： B64C23/06
CPC分类号： F03G7/065 , B64C9/32 , B64C23/06 , Y02T50/162 , Y10T29/49002
摘要： In one embodiment, the disclosed vortex generator may include a flap (12); a bearing (16) configured to be mounted on a surface (20); an axle (14) retained in the bearing, the flap attached to the axle such that the flap rotates relative to the bearing about the axle; and an actuator (32) made of a shape memory alloy attached to the flap and to a support, the actuator shaped to receive the axle therethrough, such that a change in temperature of the actuator causes the actuator to rotate the flap relative to the bearing.
摘要翻译：在一个实施例中，所公开的涡流发生器可以包括挡板（12）; 构造成安装在表面（20）上的轴承（16）; 保持在所述轴承中的轴（14），所述翼片附接到所述轴，使得所述翼片相对于所述轴承绕所述轴线旋转; 以及致动器（32），其由形状记忆合金制成，附接到所述翼片和支撑件，所述致动器成形为接收所述轴穿过其中，使得所述致动器的温度变化使致动器相对于所述轴承旋转所述翼片。

4. 发明公开

EP2428679A2 Remotely actuated wind tunnel model rudder using shape memory alloy 有权
标题翻译： Ferngesteuertes Windtunnelmodellruder mit Formspeicherlegierung
公开(公告)号：EP2428679A2
公开(公告)日：2012-03-14
申请号：EP11180043.9
申请日：2011-09-05
申请人： The Boeing Company
发明人： Gunter, Ian , Ruggeri, Robert T. , Mabe, James H. , Arbogast, Darin , Butterfield, Ordie D. , Morgenroth, Daniel
IPC分类号： F03G7/06
CPC分类号： F03G7/065
摘要： A rotational actuator assembly (10) employs a first torsion actuator (24) having a shape memory alloy (SMA) tube with a first trained twist direction and a second torsion actuator (26) having a SMA tube with an opposite trained twist direction collinear with the first torsion actuator (24) with abutting proximal ends (28,30). A central fitting (32) oins the proximal ends (28,30). A control system for temperature control of the first torsion actuator (24) and second torsion actuator (26) about an average temperature provides combined antagonistic rotation of the central fitting (32).
摘要翻译：旋转致动器组件（10）采用具有第一经训练的扭转方向的形状记忆合金（SMA）管的第一扭转致动器（24）和具有SMA管的第二扭转致动器（26），所述SMA管具有与所述第一扭转致动器（24）具有邻接的近端（28,30）。中心配件（32）靠近近端（28,30）。围绕平均温度的用于第一扭转致动器（24）和第二扭转致动器（26）的温度控制的控制系统提供中心配件（32）的组合的对抗旋转。

5. 发明授权

EP2801521B1 Vortex generator using shape memory alloys 有权
标题翻译：涡流发生器使用形状记忆合金
公开(公告)号：EP2801521B1
公开(公告)日：2018-04-25
申请号：EP14167782.3
申请日：2014-05-09
申请人： The Boeing Company
发明人： Shivashankara, Belur N. , Mabe, James H. , Clingman, Dan J.
IPC分类号： B64C23/06
CPC分类号： F03G7/065 , B64C9/32 , B64C23/06 , Y02T50/162 , Y10T29/49002
摘要： In one embodiment, the disclosed vortex generator may include a flap (12); a bearing (16) configured to be mounted on a surface (20); an axle (14) retained in the bearing, the flap attached to the axle such that the flap rotates relative to the bearing about the axle; and an actuator (32) made of a shape memory alloy attached to the flap and to a support, the actuator shaped to receive the axle therethrough, such that a change in temperature of the actuator causes the actuator to rotate the flap relative to the bearing.

6. 发明公开

EP3127804A1 SHAPE MEMORY ALLOY-ACTUATED PROPELLER BLADES AND SHAPE MEMORY ALLOY-ACTUATED PROPELLER ASSEMBLIES 有权
标题翻译： FORMGEDÄCHTNISLEGIERUNGSBETÄTIGTEPROPELLERBLÄTTERFORFORMGEDÄCHTNISLEGIERUNGSBETÄTIGTEPROPELLERANORDNUNGEN
公开(公告)号：EP3127804A1
公开(公告)日：2017-02-08
申请号：EP16171216.1
申请日：2016-05-25
申请人： The Boeing Company
发明人： Bigbee-Bansen, William J. , Clingman, Dan J. , Mabe, James H.
IPC分类号： B64C11/30 , B64C11/44
CPC分类号： B64C11/06 , B64C11/20 , B64C11/30 , B64C11/44 , B64C2027/7288 , F05D2300/505 , Y02T50/34
摘要： Shape memory alloy-actuated propeller blades and shape memory alloy-actuated propeller assemblies are disclosed. An example propeller blade includes a propeller body (212), a plate (222) coupled to the propeller body (212), a torque transfer member (220), and a shape memory alloy (SMA) actuator (218). The torque transfer member (220) has a distal end attached to the plate (222) such that the torque transfer member (220) applies to the plate (222) at least a portion of a torque applied to the torque transfer member (220) at a proximal end ofthe torque transfer member (220). The SMA actuator (218) has a distal end and a proximal end. The distal end of the SMA actuator (218) is attached to the torque transfer member. (220) The proximal end ofthe SMA actuator (218) is coupled to the propeller body (212) such that the distal end is mated to the propeller body. (212) The SMA actuator (218)is configured to apply the torque to the proximal end of the torque transfer member (220) in response to an application of heat to the SMA actuator (218).
摘要翻译：公开了形状记忆合金致动的螺旋桨叶片和形状记忆合金致动的螺旋桨组件。示例性螺旋桨叶片包括螺旋桨体（212），联接到螺旋桨体（212）的板（222），扭矩传递构件（220）和形状记忆合金（SMA）致动器（218）。转矩传递构件（220）具有附接到板（222）的远端，使得扭矩传递构件（220）向施加到扭矩传递构件（220）的扭矩的至少一部分施加到板（222）在扭矩传递构件（220）的近端处。 SMA致动器（218）具有远端和近端。 SMA致动器（218）的远端附接到扭矩传递构件。（220）SMA致动器（218）的近端联接到螺旋桨体（212），使得远端与螺旋桨体配合。（212）SMA致动器（218）被配置为响应于向SMA致动器（218）施加热量而将扭矩施加到转矩传递构件（220）的近端。

7. 发明公开

EP2428679A3 Remotely actuated wind tunnel model rudder using shape memory alloy 有权
标题翻译：遥控风洞模型划船形状记忆合金
公开(公告)号：EP2428679A3
公开(公告)日：2015-04-22
申请号：EP11180043.9
申请日：2011-09-05
申请人： The Boeing Company
发明人： Gunter, Ian , Ruggeri, Robert T. , Mabe, James H. , Arbogast, Darin , Butterfield, Ordie D. , Morgenroth, Daniel
IPC分类号： F03G7/06
CPC分类号： F03G7/065
摘要： A rotational actuator assembly (10) employs a first torsion actuator (24) having a shape memory alloy (SMA) tube with a first trained twist direction and a second torsion actuator (26) having a SMA tube with an opposite trained twist direction collinear with the first torsion actuator (24) with abutting proximal ends (28,30). A central fitting (32) oins the proximal ends (28,30). A control system for temperature control of the first torsion actuator (24) and second torsion actuator (26) about an average temperature provides combined antagonistic rotation of the central fitting (32).

8. 发明授权

EP2070688B1 Aircraft structures bonded with adhesive including magnetostrictive material 有权
公开(公告)号：EP2070688B1
公开(公告)日：2018-08-29
申请号：EP08171118.6
申请日：2008-12-09
申请人： The Boeing Company
发明人： Rawlings, Diane C. , Miller, Robert J , Krienke, Kenneth A. , Mabe, James H. , Ruggeri, Robert T. , Clingman, Dan J.
IPC分类号： B29C65/48 , B64C1/00
CPC分类号： B29C66/721 , B29C65/4815 , B29C65/4835 , B29C65/485 , B29C65/4855 , B29C65/4875 , B29C65/8253 , B29C65/8284 , B29C66/7212 , B29C70/88 , B29K2101/10 , B29K2101/12 , B29K2105/16 , B29K2503/06 , B29K2705/00 , B29K2705/12 , B29K2995/0003 , B29L2031/3082 , B29L2031/3085 , B64C1/06 , B64F5/60 , C09J5/00 , C09J9/00 , C09J11/00 , G01L1/125 , G01M5/0016 , G01M5/0041 , G01M5/0091 , G01N29/2412 , Y02T50/43 , Y10T403/477 , B29K2307/04
摘要： First and second aircraft structures (110,120) are bonded together with an adhesive (130) including strain-sensitive magnetostrictive material.

9. 发明授权

EP2428679B1 Remotely actuated wind tunnel model rudder using shape memory alloy 有权
标题翻译：遥控风洞模型划船形状记忆合金
公开(公告)号：EP2428679B1
公开(公告)日：2016-11-09
申请号：EP11180043.9
申请日：2011-09-05
申请人： The Boeing Company
发明人： Gunter, Ian , Ruggeri, Robert T. , Mabe, James H. , Arbogast, Darin , Butterfield, Ordie D. , Morgenroth, Daniel
IPC分类号： F03G7/06
CPC分类号： F03G7/065

10. 发明公开

EP2070688A3 Aircraft structures bonded with adhesive including magnetostrictive material 有权
标题翻译：材料gebundene Flugzeugstrukturen
公开(公告)号：EP2070688A3
公开(公告)日：2011-06-29
申请号：EP08171118.6
申请日：2008-12-09
申请人： The Boeing Company
发明人： Rawlings, Diane C. , Miller, Robert J , Krienke, Kenneth A. , Mabe, James H. , Ruggeri, Robert T. , Clingman, Dan J.
IPC分类号： B29C65/48 , B64C1/00
CPC分类号： B29C66/721 , B29C65/4815 , B29C65/4835 , B29C65/485 , B29C65/4855 , B29C65/4875 , B29C65/8253 , B29C65/8284 , B29C66/7212 , B29C70/88 , B29K2101/10 , B29K2101/12 , B29K2105/16 , B29K2503/06 , B29K2705/00 , B29K2705/12 , B29K2995/0003 , B29L2031/3082 , B29L2031/3085 , B64C1/06 , B64F5/60 , C09J5/00 , C09J9/00 , C09J11/00 , G01L1/125 , G01M5/0016 , G01M5/0041 , G01M5/0091 , G01N29/2412 , Y02T50/43 , Y10T403/477 , B29K2307/04
摘要： First and second aircraft structures (110,120) are bonded together with an adhesive (130) including strain-sensitive magnetostrictive material.
摘要翻译：第一和第二飞行器结构（110,120）用包括应变敏感的磁致伸缩材料的粘合剂（130）结合在一起。

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