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公开(公告)号：US20070007754A1
公开(公告)日：2007-01-11
申请号：US11178968
申请日：2005-07-11
申请人： Anthony Rybinski , Ilaria Accorsi , Andrew Kuzdak , William Snell
发明人： Anthony Rybinski , Ilaria Accorsi , Andrew Kuzdak , William Snell
IPC分类号： B60R21/20
CPC分类号： B60R21/2165 , B60R21/205
摘要： A chute for receipt of a deploying air bag includes a compartment having first and second sidewalls extending laterally outwardly from a rear bag receiving aperture toward a front cover panel. The expanding volume of the chute enables a deploying air bag to outwardly expand at least partially parallel to a frangible seam in the front cover panel before the bag contacts the seam and ruptures it. As a result, the force of the bag is dispersed evenly along the seam to reduce maximum bag force exerted against the portion of the front cover panel located directly in front, or in the center, of the bag.
摘要翻译： 用于接收展开气囊的滑槽包括具有从后袋接收孔朝向前盖板横向向外延伸的第一和第二侧壁的室。 滑槽的膨胀体积使得部署气囊能够在袋接触接缝并使其破裂之前至少部分地平行于前盖板中的易碎接缝向外膨胀。 结果，袋的力沿着接缝均匀地分散，以减小施加在直接位于袋的正面或中心的前盖板的部分上的最大袋力。
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公开(公告)号：US20050111392A1
公开(公告)日：2005-05-26
申请号：US10846484
申请日：2004-05-13
申请人： Mark Thompson , William Snell
发明人： Mark Thompson , William Snell
IPC分类号： H04B7/185
CPC分类号： H04B7/18523
摘要： A broadcast/narrowcast dual mode satellite is capable of selectively providing narrowcast operations or broadcast operations. The dual-mode satellite includes a broadcast/narrowcast dual-mode receiving system that receives from one or more terrestrial transmitting stations one or more communication uplink signals that selectively correspond to one or more narrowcast communication signals or one or more broadcast communication signals. Narrowcast communication signals are typically distinct from each other and are directed to one or more narrowcast geographic cells. Broadcast communication signals are directed to one or more broadcast regions, each of which encompasses plural narrowcast geographic cells. The dual-mode satellite also includes a broadcast/narrowcast dual-mode transmitting system that transmits one or more communication downlink signals that selectively correspond to broadcast communication signals and narrowcast communication signals received by the receiving system. Dual-mode satellite is capable of operating in the narrowcast mode or the broadcast mode, either separately or simultaneously together.
摘要翻译： 广播/窄幅双模卫星能够选择性地提供窄播操作或广播操作。 双模式卫星包括广播/窄幅双模接收系统，其从一个或多个地面发射站接收一个或多个选择性地对应于一个或多个窄播通信信号或一个或多个广播通信信号的通信上行链路信号。 窄播通信信号通常彼此不同，并且被定向到一个或多个窄广播地理小区。 广播通信信号被引导到一个或多个广播区域，每个广播区域包括多个狭窄的地理小区。 双模卫星还包括广播/窄幅双模传输系统，其传送选择性地对应于由接收系统接收的广播通信信号和窄播通信信号的一个或多个通信下行链路信号。 双模式卫星能够以狭窄模式或广播模式单独或同时运行。
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公开(公告)号：US08757108B2
公开(公告)日：2014-06-24
申请号：US13300550
申请日：2011-11-19
申请人： William Snell
发明人： William Snell
IPC分类号： F02B47/02
CPC分类号： F02B43/10 , F02B75/282 , Y02T10/32
摘要： A high thermal efficiency reciprocating hydrogen-fueled engine for ultra-high altitude long endurance flight and its method of operation are described. The engine is based on an opposed piston barrel design where long cylinders are employed to accommodate extraordinarily large compression and expansion strokes where the corresponding ratios are over 50:1, taking advantage of the very low ambient air pressures and temperatures at 60,000 ft and higher to reduce the overall weight and strength requirements of the inventive engine that would be a factor for operation at lower altitudes. The engine is designed to obtain more than 70% indicated thermal efficiency when operated at ultra-high altitudes of 60,000 ft and greater. A combination of large compression ratios combustion temperature optimization and management, instantaneous and complete combustion at TDC, followed by a rapid and long expansion stroke using tailored control of piston movement provide the means to achieve such high efficiencies.
摘要翻译： 描述了用于超高空长期耐久飞行的高热效率往复氢燃料发动机及其操作方法。 发动机基于相对的活塞筒设计，其中长的气缸用于适应非常大的压缩和膨胀冲程，其中对应的比率超过50:1，利用非常低的环境空气压力和60,000ft高于 减少本发明发动机的总体重量和强度要求，这将是在较低高度运行的一个因素。 发动机的设计目的是在超高达6万英尺及以上的高空作业时获得超过70％的热效率。 大型压缩比燃烧温度优化和管理，TDC瞬时和完全燃烧的组合，随后使用活塞运动的定制控制的快速和长的膨胀冲程提供了实现这种高效率的手段。
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公开(公告)号：US20130055984A1
公开(公告)日：2013-03-07
申请号：US13300550
申请日：2011-11-19
申请人： William Snell
发明人： William Snell
CPC分类号： F02B43/10 , F02B75/282 , Y02T10/32
摘要： A high thermal efficiency reciprocating hydrogen-fueled engine for ultra-high altitude long endurance flight and its method of operation are described. The engine is based on an opposed piston barrel design where long cylinders are employed to accommodate extraordinarily large compression and expansion strokes where the corresponding ratios are over 50:1, taking advantage of the very low ambient air pressures and temperatures at 60,000 ft and higher to reduce the overall weight and strength requirements of the inventive engine that would be a factor for operation at lower altitudes. The engine is designed to obtain more than 70% indicated thermal efficiency when operated at ultra-high altitudes of 60,000 ft and greater. A combination of large compression ratios combustion temperature optimization and management, instantaneous and complete combustion at TDC, followed by a rapid and long expansion stroke using tailored control of piston movement provide the means to achieve such high efficiencies.
摘要翻译： 描述了用于超高空长期耐久飞行的高热效率往复氢燃料发动机及其操作方法。 发动机基于相对的活塞筒设计，其中长的气缸用于适应非常大的压缩和膨胀冲程，其中对应的比率超过50:1，利用非常低的环境空气压力和60,000ft高于 减少本发明发动机的总体重量和强度要求，这将是在较低高度运行的一个因素。 发动机的设计目的是在超高达6万英尺及以上的高空作业时获得超过70％的热效率。 大型压缩比燃烧温度优化和管理，TDC瞬时和完全燃烧的组合，随后使用活塞运动的定制控制的快速和长的膨胀冲程提供了实现这种高效率的手段。
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公开(公告)号：US20070040359A1
公开(公告)日：2007-02-22
申请号：US11205700
申请日：2005-08-17
申请人： Chihan Chen , George Zamplas , William Snell
发明人： Chihan Chen , George Zamplas , William Snell
IPC分类号： B60R21/215 , B60R21/205
CPC分类号： B60R21/205 , B60R21/2165
摘要： A passenger side airbag installation for an automotive vehicle has a passenger airbag module mounted in a vehicle compartment in front of an instrument panel. The airbag module has an airbag adapted to deploy in a rearward direction. A door formed integrally with the panel has a crease, which, when severed, allows the door to swing open and create an opening in the panel. The crease is adapted to be severed and the door swung open by the force of the airbag when the airbag deploys to permit the airbag to project through the opening. The door may be bowed forwardly by an accidental impact caused by a passenger or object within the vehicle being thrown against the door if the vehicle is stopped too suddenly. A reinforcing bar limits forward bowing to protect the crease from rupturing.
摘要翻译： 用于机动车辆的乘客侧安全气囊安装件具有安装在仪表板前面的车厢中的乘客安全气囊模块。 气囊模块具有适于沿向后方向展开的气囊。 与面板一体形成的门具有折痕，当折断时，允许门摆动打开并在面板中形成开口。 当气囊展开以允许气囊通过开口突出时，折痕被切断并且气囊的力摆动打开。 如果车辆突然停止，车门内的乘客或物体的意外撞击可能会向前鞠躬。 钢筋限制向前弯曲，以保护起皱免受破裂。
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公开(公告)号：US09664108B1
公开(公告)日：2017-05-30
申请号：US14608186
申请日：2015-01-28
申请人： William Snell , Sean Kirkpatrick
发明人： William Snell , Sean Kirkpatrick
CPC分类号： F02B75/282 , F01B7/14 , F02B41/06 , F02B75/246 , F02B75/28 , F02B2075/025 , F16H21/18 , Y02T10/14
摘要： A dual crank mechanism is introduced for controlling and optimizing asymmetry in the motion profile of at least one piston of an opposed piston internal combustion (OPIC) engine piston pair. The dual crank mechanism produces a substantially asymmetrical non-sinusoidal, but periodic, reciprocating motion profile of the right-hand piston. A single crank mechanism is also introduced for controlling non-sinusoidal, but mostly symmetric, piston motion profile for one or both pistons of an opposed piston pair. The two novel crank mechanisms may be advantageously used exclusively or in combination in order to optimize the piston motion in a novel high efficiency OPIC engine having an externally mounted combustion chamber, an external compressing means for injecting compressed fuel mixtures directly into the external combustion chamber, and reducing cylinder porting to a single exhaust port per cylinder due to improved scavenging resulting from the asymmetric non-sinusoidal piston profiles produced by the novel crank mechanisms.
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公开(公告)号：US20080241075A1
公开(公告)日：2008-10-02
申请号：US11856036
申请日：2007-09-15
申请人： William Snell , Yanjie Liu , Robert Sinden , Oliver Billker
发明人： William Snell , Yanjie Liu , Robert Sinden , Oliver Billker
CPC分类号： A61K39/018 , A61K39/002 , A61K39/005 , A61K39/012 , A61K39/015 , A61K2039/55566 , A61K2039/55572 , C07K14/44 , Y02A50/412 , Y02A50/489
摘要： The present invention includes compositions and methods for the development and use of a vaccine that includes one or more FusM antigens in a carrier adapted to trigger a FusM-specific immune response in the human blood stream.
摘要翻译： 本发明包括用于开发和使用疫苗的组合物和方法，所述疫苗在适于触发人血液中的FusM特异性免疫应答的载体中包含一种或多种FusM抗原。
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公开(公告)号：US20050273822A1
公开(公告)日：2005-12-08
申请号：US11024500
申请日：2004-12-28
CPC分类号： H04N7/17336 , H04N7/20 , H04N21/2385 , H04N21/2393 , H04N21/25816 , H04N21/25841 , H04N21/2585 , H04N21/26216 , H04N21/4331 , H04N21/44209 , H04N21/47202 , H04N21/6143 , H04N21/6582 , H04N21/8358
摘要： A satellite video on demand system and method provide videos or other files on demand using a satellite in earth orbit. The satellite includes at least one uplink and multiple downlinks to multiple cells distributed over a geographic region. Multiple requests for video files from multiple users in multiple cells in the geographic region are received at a control station. The requests may include multiple requests from users in multiple cells for a first video file, and multiple other requests for one or more other video files from other users. The requests for the first video file are accumulated over a time period, and at least portions of the other video files are transmitted to the other users via the satellite during the time period. After the time period, the first video file is transmitted to the users who requested it with simultaneous transmissions over the satellite.
摘要翻译： 卫星视频点播系统和方法使用地球轨道上的卫星按需提供视频或其他文件。 该卫星包括分布在地理区域上的多个小区的至少一个上行链路和多个下行链路。 在控制站接收对地理区域中的多个小区中的来自多个用户的视频文件的多个请求。 请求可以包括用于第一视频文件的多个单元中的用户的多个请求，以及来自其他用户的一个或多个其他视频文件的多个其他请求。 对第一视频文件的请求在一段时间内被累积，并且在该时间段期间，其他视频文件的至少一部分经由卫星发送给其他用户。 在该时间段之后，第一个视频文件被传送到通过卫星同时发送请求的用户。
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