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1.发明申请COLLAPSIBLE SHAPE MEMORY ALLOY (SMA) NOSE CONES FOR AIR VEHICLES, METHOD OF MANUFACTURE AND USE 有权可拆卸形状记忆合金（SMA）空气车辆的编号，制造和使用方法公开(公告)号：US20090314890A1
公开(公告)日：2009-12-24
申请号：US12141426
申请日：2008-06-18
CPC分类号： B64C1/36 , F42B10/46 , F42B12/76 , Y10T29/49865
摘要： A nose cone formed from a shape memory alloy (SMA) having a recoverable strain of at least 2% collapses about the dome for storage, deploys at launch to protect the sensor dome and reduce drag during atmospheric flight and is shed to allow sensing for terminal maneuvers. The SMA is shape-set at elevated temperatures in its Austenite phase with a memorized shape having a radius of curvature greater than that of the sensor dome to reduce aerodynamic drag. The temperature is reduced and the SMA collapsed to conform to the curvature of the sensor dome within the recoverable strain for storage. A first mechanism is configured to return the collapsed SMA to its memorized shape at launch or prior to going supersonic. In one embodiment, the SMA is stored below its Martensite finish temperature in a temperature-induced Martensite phase in which case the mechanism heats the SMA above the Austenite finish temperature to return the material to its memorized shape. In another embodiment, the SMA is stored above its Austenite finish temperature in which case collapsing the SMA places the material in a strain-induced Martensite phase. The mechanism holds the collapsed SMA in place and the releases the stored energy allowing the SMA to return to the memorized shape.
摘要翻译： 由具有至少2％的可恢复应变的形状记忆合金（SMA）形成的鼻锥在穹顶周围塌陷以进行存储，在发射时展开以保护传感器圆顶并在大气飞行期间减小阻力并被释放以允许感测终端 机动 SMA在其奥氏体相中的高温下成形，具有比传感器圆顶的曲率半径大的记忆形状，以减少气动阻力。 温度降低，并且SMA收缩以符合传感器圆顶在可恢复应变中的曲率以进行存储。 第一机构被配置为在发射或超音速之前将折叠的SMA返回到其记忆形状。 在一个实施例中，SMA在温度诱导的马氏体相中存储在其马氏体终止温度之下，在这种情况下，机构将SMA加热到高于奥氏体终点温度以将材料返回到其记忆形状。 在另一个实施方案中，SMA被存储在其奥氏体终点温度之上，在这种情况下，SMA将材料放置在应变诱发的马氏体相中。 该机构将折叠的SMA保持在适当的位置，释放存储的能量，使SMA能够返回到记忆形状。
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2.发明授权Collapsible shape memory alloy (SMA) nose cones for air vehicles, method of manufacture and use 有权用于空中客车的可折叠形状记忆合金（SMA）鼻锥，制造和使用方法公开(公告)号：US08058595B2
公开(公告)日：2011-11-15
申请号：US12141426
申请日：2008-06-18
IPC分类号： B64C7/00
CPC分类号： B64C1/36 , F42B10/46 , F42B12/76 , Y10T29/49865
摘要： A nose cone formed from a shape memory alloy (SMA) having a recoverable strain of at least 2% collapses about the dome for storage, deploys at launch to protect the sensor dome and reduce drag during atmospheric flight and is shed to allow sensing for terminal maneuvers. The SMA is shape-set at elevated temperatures in its Austenite phase with a memorized shape having a radius of curvature greater than that of the sensor dome to reduce aerodynamic drag. The temperature is reduced and the SMA collapsed to conform to the curvature of the sensor dome within the recoverable strain for storage. A first mechanism is configured to return the collapsed SMA to its memorized shape at launch or prior to going supersonic. In one embodiment, the SMA is stored below its Martensite finish temperature in a temperature-induced Martensite phase in which case the mechanism heats the SMA above the Austenite finish temperature to return the material to its memorized shape. In another embodiment, the SMA is stored above its Austenite finish temperature in which case collapsing the SMA places the material in a strain-induced Martensite phase. The mechanism holds the collapsed SMA in place and the releases the stored energy allowing the SMA to return to the memorized shape.
摘要翻译： 由具有至少2％的可恢复应变的形状记忆合金（SMA）形成的鼻锥在穹顶周围塌陷以进行存储，在发射时展开以保护传感器圆顶并在大气飞行期间减小阻力并被释放以允许感测终端 机动 SMA在其奥氏体相中的高温下成形，具有比传感器圆顶的曲率半径大的记忆形状，以减少气动阻力。 温度降低，并且SMA收缩以符合传感器圆顶在可恢复应变中的曲率以进行存储。 第一机构被配置为在发射或超音速之前将折叠的SMA返回到其记忆形状。 在一个实施例中，SMA在温度诱导的马氏体相中存储在其马氏体终止温度之下，在这种情况下，机构将SMA加热到高于奥氏体终点温度以将材料返回到其记忆形状。 在另一个实施方案中，SMA被存储在其奥氏体终点温度之上，在这种情况下，SMA将材料放置在应变诱发的马氏体相中。 该机构将折叠的SMA保持在适当的位置，释放存储的能量，使SMA能够返回到记忆形状。
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公开(公告)号：US08418455B2
公开(公告)日：2013-04-16
申请号：US12332004
申请日：2008-12-10
CPC分类号： F03G7/065
摘要： Embodiments of separating apparatuses are generally described herein. Other embodiments may be described and claimed. In an embodiment, a separating apparatus is provided that comprises a pre-strained member formed from a shape memory alloy that is configured to separate upon application of heat.
摘要翻译： 本文一般地描述分离装置的实施例。 可以描述和要求保护其他实施例。 在一个实施例中，提供了一种分离装置，其包括由形状记忆合金形成的预应变构件，其被配置为在施加热量时分离。
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4.发明授权公开(公告)号：US09334675B2
公开(公告)日：2016-05-10
申请号：US13586188
申请日：2012-08-15
CPC分类号： E05B15/00 , E05B47/0009 , E05B51/005 , E05B65/104 , F03G7/065 , Y10T292/57
摘要： A system includes a structure having a first structural element and a second structural element. The system also includes a latch configured to releasably secure the first structural element to the second structural element. The latch includes first and second portions. The latch also includes a ball lock configured to hold the first and second portions of the latch together when the ball lock is engaged. The ball lock is also configured to allow the first and second portions of the latch to separate when the ball lock is disengaged. The latch further includes a shape memory material member configured to fracture when exposed to an elevated temperature and thereby disengage the ball lock. The shape memory material member could include an elongated structure that is configured to decrease in length when exposed to the elevated temperature. The elongated structure could have at least one notch.
摘要翻译： 一种系统包括具有第一结构元件和第二结构元件的结构。 该系统还包括构造成将第一结构元件可释放地固定到第二结构元件的闩锁。 闩锁包括第一和第二部分。 闩锁还包括球锁，其构造成当球锁接合时将闩锁的第一和第二部分保持在一起。 球锁还被构造成当球锁脱离时允许闩锁的第一和第二部分分离。 闩锁还包括形状记忆材料构件，其构造成当暴露于升高的温度时断裂，从而使球锁脱离。 形状记忆材料构件可以包括细长结构，其被构造成当暴露于升高的温度时其长度减小。 细长结构可以具有至少一个凹口。
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公开(公告)号：US20110232278A1
公开(公告)日：2011-09-29
申请号：US13155575
申请日：2011-06-08
CPC分类号： F03G7/065
摘要： A shape memory stored energy assembly includes a projectile housing having a projectile lumen. A projectile is within the projectile lumen and the projectile is movable relative to the projectile housing. A shape memory actuator is coupled between the projectile anchored end and the projectile housing. The shape memory actuator is configured to transition from a strained energy stored configuration to a fractured kinetic delivery configuration at a specified temperature range to propel the projectile through the projectile lumen. A method includes storing energy in a shape memory actuator coupled with a projectile. The stored energy in the shape memory actuator is released and propels the projectile. Releasing the stored energy includes heating the shape memory actuator, tensioning the shape memory actuator, and fracturing the tensioned shape memory actuator at a fracture locus to propel the projectile away from the fracture locus.
摘要翻译： 形状记忆存储能量组件包括具有射弹腔的射弹壳体。 射弹在射弹腔内，射弹相对于射弹壳体是可移动的。 形状记忆致动器耦合在弹丸锚定端和射弹壳体之间。 形状记忆致动器被配置为在规定的温度范围内从应变能量储存结构转变为断裂的动力输送构型，以推动射弹穿过射弹腔。 一种方法包括将能量存储在与射弹耦合的形状记忆致动器中。 形状记忆致动器中存储的能量被释放并推动了抛射体。 释放存储的能量包括加热形状记忆致动器，张紧形状记忆致动器，以及在断裂位置压裂张紧的形状记忆致动器，以推动射弹远离裂缝轨迹。
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6.发明申请公开(公告)号：US20150084353A1
公开(公告)日：2015-03-26
申请号：US13586188
申请日：2012-08-15
IPC分类号： E05B15/00
CPC分类号： E05B15/00 , E05B47/0009 , E05B51/005 , E05B65/104 , F03G7/065 , Y10T292/57
摘要： A system includes a structure having a first structural element and a second structural element. The system also includes a latch configured to releasably secure the first structural element to the second structural element. The latch includes first and second portions. The latch also includes a ball lock configured to hold the first and second portions of the latch together when the ball lock is engaged. The ball lock is also configured to allow the first and second portions of the latch to separate when the ball lock is disengaged. The latch further includes a shape memory material member configured to fracture when exposed to an elevated temperature and thereby disengage the ball lock. The shape memory material member could include an elongated structure that is configured to decrease in length when exposed to the elevated temperature. The elongated structure could have at least one notch.
摘要翻译： 一种系统包括具有第一结构元件和第二结构元件的结构。 该系统还包括构造成将第一结构元件可释放地固定到第二结构元件的闩锁。 闩锁包括第一和第二部分。 闩锁还包括球锁，其构造成当球锁接合时将闩锁的第一和第二部分保持在一起。 球锁还被构造成当球锁脱离时允许闩锁的第一和第二部分分离。 闩锁还包括形状记忆材料构件，其构造成当暴露于升高的温度时断裂，从而使球锁脱离。 形状记忆材料构件可以包括细长结构，其被构造成当暴露于升高的温度时其长度减小。 细长结构可以具有至少一个凹口。
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公开(公告)号：US08789366B2
公开(公告)日：2014-07-29
申请号：US13155575
申请日：2011-06-08
IPC分类号： F01B29/08
CPC分类号： F03G7/065
摘要： A shape memory stored energy assembly includes a projectile housing having a projectile lumen. A projectile is within the projectile lumen and the projectile is movable relative to the projectile housing. A shape memory actuator is coupled between the projectile anchored end and the projectile housing. The shape memory actuator is configured to transition from a strained energy stored configuration to a fractured kinetic delivery configuration at a specified temperature range to propel the projectile through the projectile lumen. A method includes storing energy in a shape memory actuator coupled with a projectile. The stored energy in the shape memory actuator is released and propels the projectile. Releasing the stored energy includes heating the shape memory actuator, tensioning the shape memory actuator, and fracturing the tensioned shape memory actuator at a fracture locus to propel the projectile away from the fracture locus.
摘要翻译： 形状记忆存储能量组件包括具有射弹腔的射弹壳体。 射弹在射弹腔内，射弹相对于射弹壳体是可移动的。 形状记忆致动器耦合在弹丸锚定端和射弹壳体之间。 形状记忆致动器被配置为在规定的温度范围内从应变能量储存结构转变为断裂的动力输送构型，以推动射弹穿过射弹管腔。 一种方法包括将能量存储在与射弹耦合的形状记忆致动器中。 形状记忆致动器中存储的能量被释放并推动了抛射体。 释放存储的能量包括加热形状记忆致动器，张紧形状记忆致动器，以及在断裂位置压裂张紧的形状记忆致动器，以推动射弹远离裂缝轨迹。
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公开(公告)号：US08764286B2
公开(公告)日：2014-07-01
申请号：US13155592
申请日：2011-06-08
CPC分类号： F03G7/065
摘要： Embodiments of separating apparatuses are generally described herein. Other embodiments may be described and claimed. In one embodiment, a thermal sensor assembly includes a shape memory substrate anchored within an isolation housing and braced between first and second anchors. The shape memory substrate is configured to transition from the strained configuration to the fractured configuration at a specified temperature range, and the first substrate end fractures from the second substrate end at the specified temperature. In another embodiment, a fracture indicator is coupled with the shape memory substrate, and the fracture indicator is configured to indicate the fractured configuration corresponding to meeting or exceeding of the specified temperature. In one example, the specified temperature range includes a range of temperatures or a single temperature.
摘要翻译： 本文一般地描述分离装置的实施例。 可以描述和要求保护其他实施例。 在一个实施例中，热传感器组件包括固定在隔离壳体内并且支撑在第一和第二锚定件之间的形状记忆基板。 形状记忆基板被构造成在规定的温度范围内从应变构型转变为断裂构造，并且第一基底端在指定温度下从第二基底端部断裂。 在另一个实施例中，断裂指示器与形状记忆基板相连，断裂指示器被配置为指示对应于达到或超过指定温度的断裂构造。 在一个示例中，指定的温度范围包括温度范围或单个温度。
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公开(公告)号：US20110234362A1
公开(公告)日：2011-09-29
申请号：US13155581
申请日：2011-06-08
CPC分类号： H01H37/323 , F03G7/065 , H01H37/46 , Y10T29/49105
摘要： A shape memory circuit breaker includes a shape memory substrate having first and second opposed substrate ends. The shape memory substrate is configured to transition from a strained conductive configuration to a fractured non-conductive configuration. An isolation housing is coupled with the shape memory substrate. The isolation housing includes first and second anchors coupled near the first and second substrate ends. A brace extends between the first and second anchors, and the brace statically positions the first and second anchors and the respective first and second substrate ends. The shape memory substrate is configured to transition from the strained conductive configuration to the fractured non-conductive configuration at or above a specified temperature range corresponding to a specified overload current range or voltage range, and the first substrate end fractures from the second substrate end at or above the specified temperature range resulting in an open circuit.
摘要翻译： 形状记忆断路器包括具有第一和第二相对基底端的形状记忆基片。 形状记忆基板被配置为从应变导电构型转变到断裂非导电构型。 隔离壳体与形状记忆基板耦合。 隔离壳体包括耦合在第一和第二基板端附近的第一和第二锚定件。 支架在第一和第二锚固件之间延伸，并且支架静态地定位第一和第二锚固件以及相应的第一和第二基板端部。 形状记忆基板被配置为在对应于规定的过载电流范围或电压范围的规定温度范围内或高于指定的过载电流范围或电压范围的过渡期间，从应变导电配置转变到断裂非导电配置，并且第一衬底端部从第二衬底端部 或高于指定的温度范围，导致开路。
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公开(公告)号：US20110232562A1
公开(公告)日：2011-09-29
申请号：US13155592
申请日：2011-06-08
CPC分类号： F03G7/065
摘要： Embodiments of separating apparatuses are generally described herein. Other embodiments may be described and claimed. In one embodiment, a thermal sensor assembly includes a shape memory substrate anchored within an isolation housing and braced between first and second anchors. The shape memory substrate is configured to transition from the strained configuration to the fractured configuration at a specified temperature range, and the first substrate end fractures from the second substrate end at the specified temperature. In another embodiment, a fracture indicator is coupled with the shape memory substrate, and the fracture indicator is configured to indicate the fractured configuration corresponding to meeting or exceeding of the specified temperature. In one example, the specified temperature range includes a range of temperatures or a single temperature.
摘要翻译： 本文一般地描述分离装置的实施例。 可以描述和要求保护其他实施例。 在一个实施例中，热传感器组件包括固定在隔离壳体内并且支撑在第一和第二锚定件之间的形状记忆基板。 形状记忆基板被构造成在规定的温度范围内从应变构型转变为断裂构造，并且第一基底端在指定温度下从第二基底端部断裂。 在另一个实施例中，断裂指示器与形状记忆基板相连，断裂指示器被配置为指示对应于达到或超过指定温度的断裂构造。 在一个示例中，指定的温度范围包括温度范围或单个温度。
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