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    • 13. 发明申请
    • ANTI-DECUBITUS ULCER MATTRESS OVERLAY SYSTEM WITH SELECTIVE ELEVATION STRUCTURE
    • 具有选择性高度结构的防腐剂ULCER MATTRESS覆盖系统
    • US20150026894A1
    • 2015-01-29
    • US14515085
    • 2014-10-15
    • Michael Dennis
    • Michael Dennis
    • A61G7/057A47C27/15
    • A61G7/05715A47C27/15
    • An elevation structure system possesses anti-decubitus ulcer characteristics, and may cooperate with a mattress overlay also having anti-decubitus ulcer capabilities as part of a mattress overlay system, in which multiple elongate, positionally adjustable, relatively moveable risers are configured for selective placement in conditions of transverse, subposed, under-engagement with the sides of an overlay to create substantially non-inclined, elevated, depth-supplemented regions at locations along the length of the overlay. The elevation structure and overlay may each include a dynamic-response core expanse formed of an open-cell, compressible viscoelastic foam coated with an elastomeric, moisture- and gas-flow-managing, differential-thickness coating structure load-transmissively bonded to the entirety of the outside of said core expanse to function as a dynamically-responsive unit therewith.
    • 高度结构系统具有抗褥疮溃疡特征,并且可以与具有抗褥疮溃疡能力的床垫覆盖物配合,作为床垫覆盖系统的一部分,其中多个细长的位置可调节相对可移动的上升管被配置成选择性地放置在 与覆盖层的侧面横向,叠置,欠接合的条件,以在覆盖层的长度上的位置处形成基本上非倾斜,升高的深度补充区域。 高程结构和覆盖层可以各自包括动态响应核心,其由涂覆有弹性体,湿气和气流管理的差分厚度涂层结构的开孔,可压缩粘弹性泡沫形成,负载 - 透射结合到整体 所述核心的外部扩展以用作其动态响应单元。
    • 14. 发明申请
    • ANTI-DECUBITUS ULCER MATTRESS OVERLAY SYSTEM WITH SELECTIVE ELEVATION STRUCTURE
    • 具有选择性高度结构的防腐剂ULCER MATTRESS覆盖系统
    • US20130086752A1
    • 2013-04-11
    • US13647328
    • 2012-10-08
    • Michael Dennis
    • Michael Dennis
    • A47C27/14
    • A61G7/05715A47C27/15
    • An elevation structure system possesses anti-decubitus ulcer characteristics, and may cooperate with a mattress overlay also having anti-decubitus ulcer capabilities as part of a mattress overlay system, in which multiple elongate, positionally adjustable, relatively moveable risers are configured for selective placement in conditions of transverse, subposed, under engagement with the sides of an overlay to create substantially non-inclined, elevated, depth-supplemented regions at locations along the length of the overlay. The evelation structure and overlay may each include a dynamic-response core expanse formed of an open-cell, compressible viscoelastic foam coated with elastomeric, moisture- and gas-flow-managing, differential-thickness coating structure load-transmissively bonded to the entirety of the outside of said core expanse to function as a dynamically-responsive unit therewith.
    • 高度结构系统具有抗褥疮溃疡特征,并且可以与具有抗褥疮溃疡能力的床垫覆盖物配合,作为床垫覆盖系统的一部分,其中多个细长的位置可调节相对可移动的上升管被配置成选择性地放置在 与覆盖层的侧面横向,叠置,下接合的条件,以在覆盖层的长度上的位置处形成基本上非倾斜,升高的深度补充区域。 开发结构和覆盖层可以各自包括由开放细胞,可压缩的粘弹性泡沫形成的动态响应核心层,其涂覆有弹性体,湿气和气体流量管理的差分厚度涂层结构,负载 - 透射结合到整个 所述核心的外部扩展成用作其动态响应单元。
    • 16. 发明申请
    • Solid-fuel-combustion fire-insulation interface with adjacent container-wall
    • 固体燃料燃烧防火接口与相邻容器壁
    • US20070084198A1
    • 2007-04-19
    • US11545001
    • 2006-10-08
    • Thomas OhnstadMichael DennisRussell Monk
    • Thomas OhnstadMichael DennisRussell Monk
    • F01N3/00
    • B64G1/403F02K9/346F42B39/18
    • A solid-fuel rocket assembly including an elongate fuel container having a long axis, and an inner surface spaced outwardly from, and generally circumsurrounding, that axis, and a continuous, elastomeric, heat-insulative, intumescence-behavior jacket adhered to the container's inner surface and defining a central chamber for receiving an elongate body of solid fuel. This structure implements a method for minimizing, in a solid-fuel rocket, heat damage to the wall of a solid-fuel container during burning of contained solid fuel including the steps of (a) producing dual-interface, continuous-presence, heat-insulative barriering in the zone existing between the container and burning fuel, with such barriering being characterized by (1) interfacially following any heat-produced deformations in the container wall, and (2) interfacially confronting the burning fuel with a tendency for intumescence-driven barrier-thickening.
    • 固体燃料火箭组件,其包括具有长轴线的细长燃料容器和从该轴线向外间隔开并且大致环绕该轴线的内表面,以及连续的弹性体热绝缘性膨胀性能护套,其粘附到容器的内部 并且限定用于接收固体燃料的细长体的中心室。 该结构实施了一种在固体燃料火箭中使包含的固体燃料燃烧期间对固体燃料容器的壁的热损伤最小化的方法,包括以下步骤:(a)产生双界面,连续存在, 在容器和燃烧燃料之间存在的区域中的绝缘阻塞,这种阻塞的特征在于(1)在容器壁中的任何热产生的变形之间进行界面上的跟随,以及(2)将燃烧燃料与燃烧驱动的趋势面对面 屏障增厚。