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公开(公告)号：US20220174459A1
公开(公告)日：2022-06-02
申请号：US17447398
申请日：2021-09-10
发明人： Melanie TAYLOR , Kyle DUCHARME , Edmund J. SONG
摘要： A system for accident detection or detecting an unsafe driving condition in a vehicle including a device that measures and transmits at least one output signal; at least one remote device configured to receive, record, and/or display the at least one output signal from the device; a computing device configured to receive the at least one output signal from the device and display the at least one output signal in real-time; and a graphical user interface on the computing device that allows an emergency response professional to view and customize options for monitoring the at least one output signal, wherein the device, the at least one remote device, and the computing device are communicatively connected to each other via a communications network.
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公开(公告)号：US09689415B2
公开(公告)日：2017-06-27
申请号：US14793651
申请日：2015-07-07
IPC分类号： F16B35/00 , F16B23/00 , C21D9/00 , C21D6/02 , C21D1/26 , C22C38/58 , C22C38/54 , C22C38/50 , C22C38/46 , C22C38/42 , C22C38/06 , C22C38/02 , B21D53/24 , F16B33/00 , F16B35/04 , F16B37/02 , B21H3/04 , B21K1/56 , F16B37/00 , B21H3/02 , C22C38/00 , C22C38/04 , C21D8/10
CPC分类号： F16B23/00 , B21D53/24 , B21H3/02 , B21H3/04 , B21K1/56 , C21D1/26 , C21D6/02 , C21D8/105 , C21D9/0093 , C21D2261/00 , C22C38/002 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/18 , C22C38/42 , C22C38/46 , C22C38/50 , C22C38/54 , C22C38/58 , F16B23/0046 , F16B23/0053 , F16B23/0061 , F16B23/0092 , F16B33/008 , F16B35/00 , F16B35/04 , F16B35/041 , F16B37/00 , F16B37/02
摘要： A hollow screw and related process of making is provided, wherein the hollow screw is formed from a generally circular corrosion resistant stainless steel disk cut from flat roll stock. The hollow screw includes a head and an elongated and hollow shaft having a wall thickness between about 0.2 to about 0.7 millimeters extending therefrom and defining a shank portion and a threaded portion having a plurality of threads thereon with a rotational drive mechanism configured to facilitate tightening via the threads. The process involves annealing to soften the stamped hollow screw, followed by thread rolling, and then age hardening the hollow screw. As such, the resultant hollow screw is relatively lightweight, about 50% the mass of a solid core screw made from the same material, with a sufficient thread strength to meet most aerospace applications and contributes to important aircraft fuel economy.
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公开(公告)号：US20160208841A1
公开(公告)日：2016-07-21
申请号：US15079726
申请日：2016-03-24
IPC分类号： F16B23/00 , B21H3/02 , C21D1/26 , C21D6/02 , C21D8/10 , C21D9/00 , C22C38/54 , C22C38/50 , C22C38/46 , C22C38/42 , C22C38/04 , C22C38/02 , C22C38/06 , C22C38/00 , F16B35/04
CPC分类号： F16B23/00 , B21D53/24 , B21H3/02 , B21H3/04 , B21K1/56 , C21D1/26 , C21D6/02 , C21D8/105 , C21D9/0093 , C21D2261/00 , C22C38/002 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/18 , C22C38/42 , C22C38/46 , C22C38/50 , C22C38/54 , C22C38/58 , F16B23/0046 , F16B23/0053 , F16B23/0061 , F16B23/0092 , F16B33/008 , F16B35/00 , F16B35/04 , F16B35/041 , F16B37/00 , F16B37/02
摘要： A hollow screw and related process of making is provided, wherein the hollow screw is formed from a generally circular corrosion resistant stainless steel disk cut from flat roll stock. The hollow screw includes a head and an elongated and hollow shaft having a wall thickness between about 0.2 to about 0.7 millimeters extending therefrom and defining a shank portion and a threaded portion having a plurality of threads thereon with a rotational drive mechanism configured to facilitate tightening via the threads. The process involves annealing to soften the stamped hollow screw, followed by thread rolling, and then age hardening the hollow screw. As such, the resultant hollow screw is relatively lightweight, about 50% the mass of a solid core screw made from the same material, with a sufficient thread strength to meet most aerospace applications and contributes to important aircraft fuel economy.
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公开(公告)号：US20160201710A1
公开(公告)日：2016-07-14
申请号：US15080007
申请日：2016-03-24
CPC分类号： F16B23/00 , B21D53/24 , B21H3/02 , B21H3/04 , B21K1/56 , C21D1/26 , C21D6/02 , C21D8/105 , C21D9/0093 , C21D2261/00 , C22C38/002 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/18 , C22C38/42 , C22C38/46 , C22C38/50 , C22C38/54 , C22C38/58 , F16B23/0046 , F16B23/0053 , F16B23/0061 , F16B23/0092 , F16B33/008 , F16B35/00 , F16B35/04 , F16B35/041 , F16B37/00 , F16B37/02
摘要： A hollow screw and related process of making is provided, wherein the hollow screw is formed from a generally circular corrosion resistant stainless steel disk cut from flat roll stock. The hollow screw includes a head and an elongated and hollow shaft having a wall thickness between about 0.2 to about 0.7 millimeters extending therefrom and defining a shank portion and a threaded portion having a plurality of threads thereon with a rotational drive mechanism configured to facilitate tightening via the threads. The process involves annealing to soften the stamped hollow screw, followed by thread rolling, and then age hardening the hollow screw. As such, the resultant hollow screw is relatively lightweight, about 50% the mass of a solid core screw made from the same material, with a sufficient thread strength to meet most aerospace applications and contributes to important aircraft fuel economy.
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公开(公告)号：US20220136546A1
公开(公告)日：2022-05-05
申请号：US17577247
申请日：2022-01-17
摘要： The heater assembly includes a case having a heating element therein, a channel extending through the case and having a size and shape for selectively receiving therethrough a first end of an elastomeric fixture outstretched through a substrate to a first length having a first width, and a heat transfer surface positioned relative to the heating element for receiving generated heat therefrom. The heat transfer surface is generally positionable relative to the substrate to cooperate with an adhesively bondable attachment coupled to a second end of the elastomeric fixture opposite the first end and including an uncured bonding agent disposed thereon. The heater assembly and attachment simultaneously sandwich the substrate in compression engagement in between when the elastomeric fixture extends through the substrate into the central channel and relaxes to a second relatively shorter length having a second relatively larger width.
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公开(公告)号：US10161434B2
公开(公告)日：2018-12-25
申请号：US15080007
申请日：2016-03-24
IPC分类号： F16B37/00 , F16B23/00 , C21D9/00 , C21D6/02 , C21D1/26 , C22C38/58 , C22C38/54 , C22C38/50 , C22C38/46 , C22C38/42 , C22C38/06 , C22C38/02 , B21D53/24 , F16B33/00 , F16B35/04 , F16B37/02 , B21H3/04 , B21K1/56 , F16B35/00 , B21H3/02 , C22C38/00 , C22C38/04 , C22C38/18 , C21D8/10
摘要： A hollow screw and related process of making is provided, wherein the hollow screw is formed from a generally circular corrosion resistant stainless steel disk cut from flat roll stock. The hollow screw includes a head and an elongated and hollow shaft having a wall thickness between about 0.2 to about 0.7 millimeters extending therefrom and defining a shank portion and a threaded portion having a plurality of threads thereon with a rotational drive mechanism configured to facilitate tightening via the threads. The process involves annealing to soften the stamped hollow screw, followed by thread rolling, and then age hardening the hollow screw. As such, the resultant hollow screw is relatively lightweight, about 50% the mass of a solid core screw made from the same material, with a sufficient thread strength to meet most aerospace applications and contributes to important aircraft fuel economy.
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公开(公告)号：US09803676B2
公开(公告)日：2017-10-31
申请号：US15079726
申请日：2016-03-24
IPC分类号： B21K1/56 , F16B23/00 , C21D9/00 , C21D6/02 , C21D1/26 , C22C38/58 , C22C38/54 , C22C38/50 , C22C38/46 , C22C38/42 , C22C38/06 , C22C38/02 , B21D53/24 , F16B33/00 , F16B35/04 , F16B37/02 , B21H3/04 , F16B35/00 , F16B37/00 , B21H3/02 , C22C38/00 , C22C38/04 , C21D8/10
CPC分类号： F16B23/00 , B21D53/24 , B21H3/02 , B21H3/04 , B21K1/56 , C21D1/26 , C21D6/02 , C21D8/105 , C21D9/0093 , C21D2261/00 , C22C38/002 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/18 , C22C38/42 , C22C38/46 , C22C38/50 , C22C38/54 , C22C38/58 , F16B23/0046 , F16B23/0053 , F16B23/0061 , F16B23/0092 , F16B33/008 , F16B35/00 , F16B35/04 , F16B35/041 , F16B37/00 , F16B37/02
摘要： A hollow screw and related process of making is provided, wherein the hollow screw is formed from a generally circular corrosion resistant stainless steel disk cut from flat roll stock. The hollow screw includes a head and an elongated and hollow shaft having a wall thickness between about 0.2 to about 0.7 millimeters extending therefrom and defining a shank portion and a threaded portion having a plurality of threads thereon with a rotational drive mechanism configured to facilitate tightening via the threads. The process involves annealing to soften the stamped hollow screw, followed by thread rolling, and then age hardening the hollow screw. As such, the resultant hollow screw is relatively lightweight, about 50% the mass of a solid core screw made from the same material, with a sufficient thread strength to meet most aerospace applications and contributes to important aircraft fuel economy.
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公开(公告)号：US20170282236A1
公开(公告)日：2017-10-05
申请号：US15024324
申请日：2015-07-07
CPC分类号： B21D53/24 , B21H3/02 , B21H3/04 , B21K1/46 , B21K1/56 , C21D1/26 , C21D6/00 , C21D6/004 , C21D6/02 , C21D8/105 , C21D9/0093 , C21D2261/00 , C22C38/002 , C22C38/02 , C22C38/06 , C22C38/44 , C22C38/46 , C22C38/50 , C22C38/54 , C22C38/58 , F16B23/00 , F16B23/0053 , F16B23/0061 , F16B23/0092 , F16B33/008 , F16B35/00 , F16B35/041 , F16B37/02
摘要： A hollow screw and related process of making is provided, wherein the hollow screw is formed from a generally circular corrosion resistant stainless steel disk cut from flat roll stock. The hollow screw includes a head and an elongated and hollow shaft having a wall thickness between about 0.2 to about 0.7 millimeters extending therefrom and defining a shank portion and a threaded portion having a plurality of threads thereon with a rotational drive mechanism configured to facilitate tightening via the threads. The process involves annealing to soften the stamped hollow screw, followed by thread rolling, and then age hardening the hollow screw. As such, the resultant hollow screw is relatively lightweight, about 50% the mass of a solid core screw made from the same material, with a sufficient thread strength to meet most aerospace applications and contributes to important aircraft fuel economy.
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公开(公告)号：US20160003281A1
公开(公告)日：2016-01-07
申请号：US14793651
申请日：2015-07-07
IPC分类号： F16B23/00 , F16B37/00 , B21H3/02 , B21D22/28 , C21D8/10 , C21D9/00 , C21D6/02 , C21D1/26 , C22C38/58 , C22C38/54 , C22C38/50 , C22C38/46 , C22C38/42 , C22C38/06 , C22C38/02 , F16B35/04
CPC分类号： F16B23/00 , B21D53/24 , B21H3/02 , B21H3/04 , B21K1/56 , C21D1/26 , C21D6/02 , C21D8/105 , C21D9/0093 , C21D2261/00 , C22C38/002 , C22C38/02 , C22C38/04 , C22C38/06 , C22C38/18 , C22C38/42 , C22C38/46 , C22C38/50 , C22C38/54 , C22C38/58 , F16B23/0046 , F16B23/0053 , F16B23/0061 , F16B23/0092 , F16B33/008 , F16B35/00 , F16B35/04 , F16B35/041 , F16B37/00 , F16B37/02
摘要： A hollow screw and related process of making is provided, wherein the hollow screw is formed from a generally circular corrosion resistant stainless steel disk cut from flat roll stock. The hollow screw includes a head and an elongated and hollow shaft having a wall thickness between about 0.2 to about 0.7 millimeters extending therefrom and defining a shank portion and a threaded portion having a plurality of threads thereon with a rotational drive mechanism configured to facilitate tightening via the threads. The process involves annealing to soften the stamped hollow screw, followed by thread rolling, and then age hardening the hollow screw. As such, the resultant hollow screw is relatively lightweight, about 50% the mass of a solid core screw made from the same material, with a sufficient thread strength to meet most aerospace applications and contributes to important aircraft fuel economy.
摘要翻译： 提供了一种中空螺丝及相关的制造方法，其中中空螺杆由从扁平轧辊原料切割的大致圆形的耐腐蚀不锈钢盘形成。 中空螺杆包括头部和细长的空心轴，其具有从其延伸的约0.2至约0.7毫米的壁厚，并且限定了柄部分和螺纹部分，其上具有多个螺纹，旋转驱动机构构造成便于紧固通过 线程。 该过程包括退火以软化冲压的中空螺杆，随后进行螺纹滚压，然后对中空螺钉进行老化硬化。 因此，所得到的中空螺杆相对较轻，由相同材料制成的实芯螺杆的质量约为50％，具有足够的螺纹强度以满足大多数航空应用并且有助于重要的飞机燃料经济性。
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公开(公告)号：US08602764B2
公开(公告)日：2013-12-10
申请号：US13784604
申请日：2013-03-04
IPC分类号： F16J15/00
CPC分类号： F16J15/00 , B29C33/00 , B29C39/26 , B29D99/0085 , B29L2031/26 , B29L2031/773
摘要： A sealant mold for sealing a dome element particularly at a lower region about an interface with a substrate such as an aircraft fuel tank wall. The sealant mold is formed from a lightweight plastic material, and includes an outer cap portion having an opening formed therein, in combination with an integral outer skirt to define a gap or trough for receiving and supporting a metered quantity of a curable sealant material. The mold is slidably fitted onto a dome element with outer skirt displaced downwardly to extrude the sealant material about the lower region of the dome element. The sealant material is allowed to cure, after which the sealant mold can be stripped from the cured sealant material.
摘要翻译： 一种用于密封圆顶元件的密封模具，特别是在与诸如飞机燃料箱壁的基板的界面周围的下部区域处密封。 密封剂模具由轻质塑料材料形成，并且包括具有形成在其中的开口的外盖部分，与一体的外裙部组合，以限定用于接收和支撑计量的可固化密封剂材料的间隙或槽。 模具可滑动地装配到圆顶元件上，外裙向下移位以挤压围绕圆顶元件的下部区域的密封材料。 允许密封材料固化，然后可以将密封剂模具从固化的密封剂材料中剥离。
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