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    HYBRID ABLATIVE THERMAL PROTECTION SYSTEMS AND ASSOCIATED METHODS
    3.
    发明申请
    HYBRID ABLATIVE THERMAL PROTECTION SYSTEMS AND ASSOCIATED METHODS 审中-公开
    混合热保护系统及相关方法

    公开(公告)号：US20160325857A1

    公开(公告)日：2016-11-10

    申请号：US15004456

    申请日：2016-01-22

    申请人： The Boeing Company

    发明人： Bryan Clark Brewer ,  Patrick Jacob Mobers

    IPC分类号： B64G1/58 ,  B64G1/62

    CPC分类号： B64G1/58 ,  B29C65/4835 ,  B64C1/38 ,  B64G1/62

    摘要： A method of forming a thermal protection system for high speed aircraft is described. The method includes mechanically working an uncured ablator material into a first surface of a felt layer such that the ablator material penetrates a distance into a thickness of the felt layer thereby forming an region that has a mixture of felt and ablator material, adding additional uncured ablator material to the worked ablator material, and curing the combined ablator material.

    摘要翻译： 描述了形成用于高速飞行器的热保护系统的方法。 该方法包括将未固化的消融器材料机械加工到毡层的第一表面中，使得消融器材料穿过一定距离进入毡层的厚度，从而形成具有毡和烧结材料混合物的区域，添加另外未固化的烧烤器 材料到工作的消融器材料，并固化组合的消融器材料。

    High efficiency erosion resistant silicone ablator composition
    4.
    发明授权
    High efficiency erosion resistant silicone ablator composition 有权
    高效防腐硅胶消融器组成

    公开(公告)号：US09458356B2

    公开(公告)日：2016-10-04

    申请号：US14317920

    申请日：2014-06-27

    申请人： THE BOEING COMPANY

    发明人： Kelly Jonathan Courter ,  Patrick Jacob Mobers ,  Bryan Brewer

    IPC分类号： C09D183/04 ,  C08K7/28 ,  B64G1/58

    CPC分类号： C08K7/26 ,  B29B7/90 ,  B29C47/0004 ,  B29K2083/00 ,  B29K2105/16 ,  B29L2031/3076 ,  B64G1/58 ,  C08J3/203 ,  C08J2383/04 ,  C08K3/32 ,  C08K3/38 ,  C08K7/28 ,  C08K2003/322 ,  C09D183/04 ,  C08K2003/387

    摘要： A lightweight ablator formulation has been developed which offers superior thermal performance compared to current state of the art ablator formulations. The lightweight ablator formulations described herein typically include at least one endothermically decomposing (energy absorbing) material with a fluxing agent resulting in significantly reduced backface temperature response and a more stable surface. According to one implementation the ablator composition comprises about 30 to about 70 percent by weight of a base silicone resin, about 25 to about 67 percent by weight of a low-density filler, about 3 to about 7 percent by weight of a curing agent and greater than 0 and up to about 10 percent by weight of a boron-containing compound.

    摘要翻译： 已经开发出了一种轻质的消融器配方，与现有的消费者配方相比，其具有优异的热性能。 本文描述的轻质消融器配方通常包括至少一种具有助熔剂的吸热分解（能量吸收）材料，导致显着降低的背面温度响应和更稳定的表面。 根据一个实施方案，消融器组合物包含约30至约70重量％的基础有机硅树脂，约25至约67重量％的低密度填料，约3至约7重量％的固化剂，以及 大于0且至多约10重量％的含硼化合物。

    HIGH EFFICIENCY EROSION RESISTANT SILICONE ABLATOR COMPOSITION
    5.
    发明申请
    HIGH EFFICIENCY EROSION RESISTANT SILICONE ABLATOR COMPOSITION 有权
    高效耐腐蚀硅酮吸收剂组合物

    公开(公告)号：US20150376452A1

    公开(公告)日：2015-12-31

    申请号：US14317920

    申请日：2014-06-27

    申请人： THE BOEING COMPANY

    发明人： Kelly Jonathan Courter ,  Patrick Jacob Mobers

    IPC分类号： C09D183/04 ,  B64G1/58 ,  C08K7/28

    CPC分类号： C08K7/26 ,  B29B7/90 ,  B29C47/0004 ,  B29K2083/00 ,  B29K2105/16 ,  B29L2031/3076 ,  B64G1/58 ,  C08J3/203 ,  C08J2383/04 ,  C08K3/32 ,  C08K3/38 ,  C08K7/28 ,  C08K2003/322 ,  C09D183/04 ,  C08K2003/387

    摘要： A lightweight ablator formulation has been developed which offers superior thermal performance compared to current state of the art ablator formulations. The lightweight ablator formulations described herein typically include at least one endothermically decomposing (energy absorbing) material with a fluxing agent resulting in significantly reduced backface temperature response and a more stable surface. According to one implementation the ablator composition comprises about 30 to about 70 percent by weight of a base silicone resin, about 25 to about 67 percent by weight of a low-density filler, about 3 to about 7 percent by weight of a curing agent and greater than 0 and up to about 10 percent by weight of a boron-containing compound.

    摘要翻译： 已经开发出了一种轻质的消融器配方，与现有的消费者配方相比，其具有优异的热性能。 本文描述的轻量级消融器配方通常包括至少一种具有助熔剂的吸热分解（能量吸收）材料，导致显着降低的背面温度响应和更稳定的表面。 根据一个实施方案，消融器组合物包含约30至约70重量％的基础有机硅树脂，约25至约67重量％的低密度填料，约3至约7重量％的固化剂，以及 大于0且至多约10重量％的含硼化合物。