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1. 发明授权

US5842665A Launch vehicle with engine mounted on a rotor 失效
标题翻译：发动机搭载在转子上的发动机
公开(公告)号：US5842665A
公开(公告)日：1998-12-01
申请号：US711964
申请日：1996-09-09
申请人： Bevin C. McKinney , Gary C. Hudson
发明人： Bevin C. McKinney , Gary C. Hudson
IPC分类号： B64C27/18 , B64C29/02 , B64G1/00 , B64G1/14 , B64G1/40 , B64G1/62 , B64C39/00
CPC分类号： B64G1/401 , B64C27/18 , B64C29/02 , B64G1/002 , B64G1/14 , B64G1/62
摘要： A launch vehicle which employs a rotor similar to a helicopter. The vehicle has a four bladed rotor which is mounted on the vehicle body. The body of the vehicle includes propellant tanks and a payload compartment contained within an integral aeroshell. Rocket engines used to propel the vehicle into earth orbit are mounted at the ends of the rotor blades. The engines are connected by propellant feed lines to a propellant transfer hub surrounding the axis of rotation of the rotor. Propellants are fed from an oxidizer tank and a fuel tank through a propellant transfer coupling to oxidizer and fuel lines which extend to the engines at the rotor blades ends. The rotor blades incorporate air foils. To operate the vehicle the vehicle is positioned on a concrete or asphalt pad and fueled with liquid oxygen and kerosene. The engine are positioned tangent to the blade paths and ignited. The thrust of the engines which is tangent to the rotor causes the rotor to turn which accelerates the rotor thus increasing the pressure developed by the propellants as they flow towards the engines. When the rotor has reached operational speed the airfoil creates sufficient lift that the vehicle begins to ascend vertically. As the vehicle exits the atmosphere the rocket engines are aligned with the flight path of the vehicle. After reentry from earth orbit the vehicle utilizes the spun up rotor to fly the vehicle to a soft landing.
摘要翻译：使用类似于直升机的转子的运载火箭。车辆具有安装在车体上的四叶片转子。车辆的车身包括推进剂罐和包含在整体式气囊内的有效载荷舱。用于将车辆推进地球轨道的火箭发动机安装在转子叶片的端部。发动机通过推进剂进料管线连接到围绕转子旋转轴线的推进剂传递轮毂。推进剂从氧化剂罐和燃料箱通过推进剂传递耦合馈送到氧化剂和燃料管线，其在转子叶片端部延伸到发动机。转子叶片包含气翼。为了操作车辆，车辆定位在混凝土或沥青垫上，并用液氧和煤油燃料。发动机定位成与叶片路径相切并点燃。与转子相切的发动机的推力导致转子转动，从而加速转子，从而增加推进剂在向发动机流动时产生的压力。当转子达到操作速度时，机翼产生足够的升力，使车辆开始垂直上升。当车辆离开大气时，火箭发动机与车辆的飞行路线对准。在从地球轨道重新进入后，车辆利用旋转转子将车辆飞行到软着陆。

2. 发明授权

US5488746A Polyester fiber and foam core mattress pad 失效
标题翻译：聚酯纤维和泡沫芯床垫
公开(公告)号：US5488746A
公开(公告)日：1996-02-06
申请号：US323684
申请日：1994-10-18
申请人： Gary C. Hudson
发明人： Gary C. Hudson
IPC分类号： A47C27/00 , A47C27/22 , A47G9/00
CPC分类号： A47C27/22 , A47C27/007 , A47C27/144 , A47C27/146 , A47C31/105
摘要： A mattress cover in which a convoluted sheet of foam is removably enclosed in a pocket or pouch composed of two layers, at least one of which is quilted to enclose quantities of fiber batting. A zippered closure joins the two layers and may be opened to remove the layer of foam and permit effective laundering of the outer layers.
摘要翻译：一种床垫罩，其中卷曲的泡沫片可拆卸地封闭在由两层组成的口袋或小袋中，其中至少一层被绗缝以包围数量的纤维棉絮。拉链封闭件连接两层，并且可以打开以除去泡沫层并允许有效地洗涤外层。

3. 发明申请

US20120175465A1 Capsule Spacecraft Emergency Landing System 有权
标题翻译：胶囊航天器紧急着陆系统
公开(公告)号：US20120175465A1
公开(公告)日：2012-07-12
申请号：US13323699
申请日：2011-12-12
申请人： Gary C. Hudson
发明人： Gary C. Hudson
IPC分类号： B64D25/12
CPC分类号： B64G1/62 , B64G1/12 , B64G1/52
摘要： A method of landing a capsule-spacecraft having a crew compartment containing crew, light cargo, and whatever other elements are associated with crew safety and comfort during emergency recovery, such as survival equipment and a service component including any propulsion components, heat shield, heavier structure, or other equipment not directly connected with the crew component. In the event of a propulsion system failure, the crew compartment component is immediately separated from the service component, either by automatic or crew action. One or more parachutes are then deployed by rapid methods, such as rocket extraction, from the crew compartment. Because the space craft is separated into two parts the weight of the parachutes is reduced in proportion as the weight of the crew compartment is to the total capsule-spacecraft.
摘要翻译：具有包含船员，轻型货物和任何其他元件的船员舱的胶囊 - 航天器的方法与紧急恢复期间船员的安全性和舒适性相关联，诸如生存设备和包括任何推进部件，隔热罩，重物结构或与机组组件没有直接连接的其他设备。在推进系统故障的情况下，船员舱部件通过自动或机组动作立即与服务部件分离。然后通过快速方法（如火箭提取）从船员舱部署一个或多个降落伞。因为航天飞船被分成两部分，所以降落伞的重量按照船员舱的重量是相对于整个胶囊 - 航天器的比例减小。

4. 外观设计

USD314685S Sculpted contour pillow 失效
公开(公告)号：USD314685S
公开(公告)日：1991-02-19
申请号：US354936
申请日：1989-05-22
申请人： Gary C. Hudson
设计人： Gary C. Hudson

5. 外观设计

USD400385S Varicolored convoluted mattress pad 失效
公开(公告)号：USD400385S
公开(公告)日：1998-11-03
申请号：US83271
申请日：1998-02-09
申请人： Gary C. Hudson
设计人： Gary C. Hudson

6. 发明授权

US5545199A Hot and cold therapeutic pillow 失效
标题翻译：冷热治疗枕头
公开(公告)号：US5545199A
公开(公告)日：1996-08-13
申请号：US497876
申请日：1995-07-03
申请人： Gary C. Hudson
发明人： Gary C. Hudson
IPC分类号： A47C21/04 , A47G9/00 , A47G9/10 , A61F7/02 , A61F7/00
CPC分类号： A61F7/02 , A47G9/1036 , A47G9/1081 , A47G2009/008
摘要： A hot and cold therapeutic pillow which includes a cervical roll having relatively firm ends and a relatively soft middle portion. The core of the pillow is hollow and accommodates a cylindrical gel pack which may be heated by microwave radiation or cooled by freezing. The cervical roll may be integrally combined with a head cradle which has a soft middle or central portion and firm ends.
摘要翻译：一种冷热治疗枕头，其包括具有相对坚固的端部的颈椎辊和相对较软的中间部分。枕头的核心是中空的，并且容纳可以通过微波辐射加热或通过冷冻冷却的圆柱形凝胶组合物。颈椎辊可以与具有软的中间部分或中央部分和坚固的末端的头架一体地组合。

7. 发明授权

US5121515A Pillow 失效
标题翻译：枕头
公开(公告)号：US5121515A
公开(公告)日：1992-06-16
申请号：US777592
申请日：1991-10-16
申请人： Gary C. Hudson
发明人： Gary C. Hudson
IPC分类号： B68G1/00
CPC分类号： B68G1/00 , Y10S5/926
摘要： A pillow comprising a container made of edge-joined slabs of polyurethane foam filled with a mixture of polyurethane foam chips averaging about one-quarter inch square and polyester fibers averaging about two inches in length, said fibers being coated with silicone, said mixture being homogeneous and consisting of 70 to 50 percent of said polyurethane foam chips and 30 to 50 percent of said coated polyester fiber.
摘要翻译：一种枕头，包括由聚氨酯泡沫的边缘连接板填充的容器，该容器填充有平均约四分之一英寸的聚氨酯泡沫芯片的混合物，平均约2英寸长的聚酯纤维，所述纤维涂覆有硅氧烷，所述混合物是均匀的并且由70％至50％的所述聚氨酯泡沫芯片和30％至50％的所述涂覆的聚酯纤维组成。

8. 发明授权

US5061737A Filling material 失效
标题翻译：灌装材料
公开(公告)号：US5061737A
公开(公告)日：1991-10-29
申请号：US719976
申请日：1991-06-24
申请人： Gary C. Hudson
发明人： Gary C. Hudson
IPC分类号： B68G1/00
CPC分类号： B68G1/00
摘要： A filling material for pillows or the like composed of a homogeneous mixture of polyurethane foam chips and lengths of polyester fiber. The foam chips may constitute 70 to 50 percent and the fiber lengths may constitute 30 to 50 percent of the mixture. The foam may have an indent load deflection of 8 to 20 lbs. and may be in the form of chips one-quarter inch square. The fibers may be of 5 to 15 denier and average two inches in length. The fiber lengths are coated with silicone to slicken their surfaces.
摘要翻译：用于由聚氨酯泡沫片和长度聚酯纤维的均匀混合物组成的枕头等的填充材料。泡沫芯片可以构成70-50％，纤维长度可以占混合物的30-50％。泡沫可能具有8至20磅的压痕载荷偏移。并可能采用四分之一英寸的芯片形式。纤维的长度可以为5至15旦，平均两英寸。纤维长度涂有硅胶以使其表面变薄。

9. 发明授权

US08690104B2 Capsule spacecraft emergency landing system 有权
标题翻译：胶囊航天器紧急着陆系统
公开(公告)号：US08690104B2
公开(公告)日：2014-04-08
申请号：US13323699
申请日：2011-12-12
申请人： Gary C. Hudson
发明人： Gary C. Hudson
IPC分类号： B64D25/12
CPC分类号： B64G1/62 , B64G1/12 , B64G1/52
摘要： A method of landing a capsule-spacecraft having a crew compartment containing crew, light cargo, and whatever other elements are associated with crew safety and comfort during emergency recovery, such as survival equipment and a service component including any propulsion components, heat shield, heavier structure, or other equipment not directly connected with the crew component. In the event of a propulsion system failure, the crew compartment component is immediately separated from the service component, either by automatic or crew action. One or more parachutes are then deployed by rapid methods, such as rocket extraction, from the crew compartment. Because the space craft is separated into two parts the weight of the parachutes is reduced in proportion as the weight of the crew compartment is to the total capsule-spacecraft.
摘要翻译：具有包含船员，轻型货物和任何其他元件的船员舱的胶囊 - 航天器的方法与紧急恢复期间船员的安全性和舒适性相关联，诸如生存设备和包括任何推进部件，隔热罩，重物结构或与机组组件没有直接连接的其他设备。在推进系统故障的情况下，船员舱部件通过自动或机组动作立即与服务部件分离。然后通过快速方法（如火箭提取）从船员舱部署一个或多个降落伞。因为航天飞船被分成两部分，所以降落伞的重量按照船员舱的重量是相对于整个胶囊 - 航天器的比例减小。

10. 发明授权

US07484692B1 Integrated abort rocket and orbital propulsion system 有权
标题翻译：综合中止火箭和轨道推进系统
公开(公告)号：US07484692B1
公开(公告)日：2009-02-03
申请号：US10987442
申请日：2004-11-12
申请人： Bevin C. McKinney , Gary C. Hudson
发明人： Bevin C. McKinney , Gary C. Hudson
IPC分类号： B64G1/40 , B64G1/00
CPC分类号： B64G1/002 , B64G1/005 , B64G1/12 , B64G1/401 , B64G1/402 , F02K9/50
摘要： An orbital stage system has an orbital stage and one or more launch stages. The orbital stage incorporates an orbital maneuvering system (OMS) and an abort propulsion system which both utilize the same propellants, propellant tankage, and propellant pressurization system, but which employ radically different engines. The OMS engines are comprised of at least two engines which have a combined thrust in the neighborhood of 1/10 the weight of the orbital stage, an area ratio of 50 or more and an operating life of many hundred seconds, preferably many thousands of seconds or more. The abort engine may be a single engine and typically has a thrust of three, four, or more times the weight of the vehicle and an area ratio in the neighborhood of two and an operating life of at most a few tens of seconds.
摘要翻译：轨道平台系统具有轨道平台和一个或多个发射阶段。轨道舞台包括轨道机动系统（OMS）和中止推进系统，它们都使用相同的推进剂，推进剂罐和推进剂加压系统，但采用完全不同的发动机。 OMS发动机由至少两个发动机组成，其具有在轨道平台重量的1/10附近的组合推力，面积比为50或更大，并且操作寿命为几百秒，优选数千秒或者更多。中止发动机可以是单个发动机，并且通常具有车辆重量的三倍，四倍或更多倍的推力，并且在两个附近的面积比和最多几十秒的使用寿命。

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