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1.发明申请SMART SUSCEPTOR FOR A SHAPE MEMORY ALLOY (SMA) ACTUATOR INDUCTIVE HEATING SYSTEM 有权形状记忆合金（SMA）执行器感应加热系统的智能断路器公开(公告)号：US20150096293A1
公开(公告)日：2015-04-09
申请号：US14045121
申请日：2013-10-03
Applicant: The Boeing Company
Inventor： Moushumi Shome , Frederick T. Calkins , Stephen R. Amorosi , Flint M. Jamison , Sahrudine Apdalhaliem , Robert James Miller
CPC classification number: F03G7/065 , H01F41/02 , Y10T29/4902
Abstract: A system for heating a shape memory alloy (SMA) actuator may include an SMA actuator, a smart susceptor, a plurality of induction coils, and a control module. The SMA actuator may have at least one layup. The SMA actuator may be selectively heated to a transition temperature. The smart susceptor may be in thermal contact with the at least one layup of the SMA actuator. The induction heating coils may be configured to receive an alternating current and generate a magnetic field based on the alternating current. The magnetic field may create an eddy current in at least one of the SMA actuator and the smart susceptor to heat the SMA actuator to the transition temperature. The control module may be configured to drive the alternating current supplied to the induction heating coils.
Abstract translation: 用于加热形状记忆合金（SMA）致动器的系统可以包括SMA致动器，智能基座，多个感应线圈和控制模块。 SMA致动器可以具有至少一个叠层。 可以将SMA致动器选择性地加热到转变温度。 智能基座可以与SMA致动器的至少一个叠层热接触。 感应加热线圈可以被配置为接收交流电流并且基于交流电产生磁场。 磁场可以在SMA致动器和智能基座中的至少一个中产生涡流，以将SMA致动器加热到转变温度。 控制模块可以被配置为驱动提供给感应加热线圈的交流电。
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2.发明授权Smart susceptor for a shape memory alloy (SMA) actuator inductive heating system 有权用于形状记忆合金（SMA）致动器感应加热系统的智能感受体公开(公告)号：US09581146B2
公开(公告)日：2017-02-28
申请号：US14045121
申请日：2013-10-03
Applicant: The Boeing Company
Inventor： Moushumi Shome , Frederick T. Calkins , Stephen R. Amorosi , Flint M. Jamison , Sahrudine Apdalhaliem , Robert James Miller
CPC classification number: F03G7/065 , H01F41/02 , Y10T29/4902
Abstract: A system for heating a shape memory alloy (SMA) actuator may include an SMA actuator, a smart susceptor, a plurality of induction coils, and a control module. The SMA actuator may have at least one layup. The SMA actuator may be selectively heated to a transition temperature. The smart susceptor may be in thermal contact with the at least one layup of the SMA actuator. The induction heating coils may be configured to receive an alternating current and generate a magnetic field based on the alternating current. The magnetic field may create an eddy current in at least one of the SMA actuator and the smart susceptor to heat the SMA actuator to the transition temperature. The control module may be configured to drive the alternating current supplied to the induction heating coils.
Abstract translation: 用于加热形状记忆合金（SMA）致动器的系统可以包括SMA致动器，智能基座，多个感应线圈和控制模块。 SMA致动器可以具有至少一个叠层。 可以将SMA致动器选择性地加热到转变温度。 智能基座可以与SMA致动器的至少一个叠层热接触。 感应加热线圈可以被配置为接收交流电流并且基于交流电产生磁场。 磁场可以在SMA致动器和智能基座中的至少一个中产生涡流，以将SMA致动器加热到转变温度。 控制模块可以被配置为驱动提供给感应加热线圈的交流电。
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公开(公告)号：US09463869B2
公开(公告)日：2016-10-11
申请号：US14298105
申请日：2014-06-06
Applicant: The Boeing Company
Inventor： Flint M. Jamison , Stephen R. Amorosi , Michael K. Klein
CPC classification number: B64C13/24 , B64C3/28 , B64C3/38 , B64C3/50 , B64C9/02 , B64C9/16 , B64C2003/147 , Y02T50/12 , Y02T50/14 , Y02T50/32 , Y02T50/44
Abstract: A wing includes a trailing edge, and a divergent trailing edge device slideable along an aft surface of the trailing edge between a stowed position and a fully deployed position. The trailing edge device is located entirely within the trailing edge when stowed, and it increases lift over drag of the wing when deployed.
Abstract translation: 机翼包括后缘，以及沿收起位置和完全展开位置之间的后缘的后表面可滑动的发散后缘装置。 后缘装置在收起时完全位于后缘内，并且当展开时它增加了机翼的牵引力。
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公开(公告)号：US20150353188A1
公开(公告)日：2015-12-10
申请号：US14298105
申请日：2014-06-06
Applicant: THE BOEING COMPANY
Inventor： Flint M. Jamison , Stephen R. Amorosi , Michael K. Klein
CPC classification number: B64C13/24 , B64C3/28 , B64C3/38 , B64C3/50 , B64C9/02 , B64C9/16 , B64C2003/147 , Y02T50/12 , Y02T50/14 , Y02T50/32 , Y02T50/44
Abstract: A wing includes a trailing edge, and a divergent trailing edge device slideable along an aft surface of the trailing edge between a stowed position and a fully deployed position. The trailing edge device is located entirely within the trailing edge when stowed, and it increases lift over drag of the wing when deployed.
Abstract translation: 机翼包括后缘，以及沿收起位置和完全展开位置之间的后缘的后表面可滑动的发散后缘装置。 后缘装置在收起时完全位于后缘内，并且当展开时它增加了机翼的牵引力。
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