公开(公告)号：US06294491B1

公开(公告)日：2001-09-25

申请号：US09311511

申请日：1999-05-13

申请人： Ralph Michael Fay ,  Jeffrey Canon Townsend ,  Foster Laverne Harding ,  Jon Frederick Bauer ,  Harry Hand Russell, III ,  Xiaojie Xu

发明人： Ralph Michael Fay ,  Jeffrey Canon Townsend ,  Foster Laverne Harding ,  Jon Frederick Bauer ,  Harry Hand Russell, III ,  Xiaojie Xu

IPC分类号： C03C1300

CPC分类号： C03C13/00 ,  C03C2213/02 ,  Y10T428/249933 ,  Y10T428/249935 ,  Y10T428/2913 ,  Y10T428/2933 ,  Y10T428/2938

摘要： An insulation product especially suited for use as an aircraft insulation includes a blanket of randomly oriented entangled glass fibers bonded together by a thermosetting binder and having a mean diameter of about 1+/−0.25 microns. The blanket has a density between about 0.25 and about 1.5 pounds per cubic foot and a thickness between about 0.35 inches and about 2.0 inches. The blanket, exclusive of anything else, has an average machine direction tensile strength of at least 0.6 pounds/inch of blanket width and an average cross machine direction tensile strength of at least 0.3 pounds/inch of blanket length; a transverse airflow resistance between about 300 Rayls and about 1800 Rayls; and a thermal conductivity equal to or less than about 0.32 BTU-in/hr-ft2-° F. The glass fibers of the blanket have a biodissolution rate in excess of 150 ng/cm2/hr.

摘要翻译： 特别适用于飞机绝缘的绝缘产品包括由热固性粘合剂粘合在一起并且具有约1 +/- 0.25微米的平均直径的随机取向缠结玻璃纤维的毯子。 毯子具有约0.25至约1.5磅/立方英尺之间的密度和约0.35英寸至约2.0英寸之间的厚度。 除了其他任何东西之外，毯子的平均机器方向拉伸强度为橡皮布宽度的至少0.6磅/英寸，平均横向拉伸强度为橡皮布长度的至少0.3磅/英寸。 约300雷和约1800雷之间的横向气流阻力; 和热导率等于或小于约0.32BTU / in-hr-ft 2 -F。该毯的玻璃纤维的生物溶解速率超过150ng / cm 2 / hr。

公开(公告)号：US06565040B2

公开(公告)日：2003-05-20

申请号：US09974207

申请日：2001-10-09

申请人： Ralph Michael Fay ,  Rebecca Sue Wulliman ,  James Walter Stacy ,  Jeffrey Canon Townsend ,  Steven N. Volenec

发明人： Ralph Michael Fay ,  Rebecca Sue Wulliman ,  James Walter Stacy ,  Jeffrey Canon Townsend ,  Steven N. Volenec

IPC分类号： B64C140

CPC分类号： B32B5/26 ,  B32B5/22 ,  B32B5/32 ,  B32B15/08 ,  B32B15/20 ,  B32B27/065 ,  B32B27/12 ,  B32B27/20 ,  B32B27/281 ,  B32B29/007 ,  B32B29/02 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2262/101 ,  B32B2266/0214 ,  B32B2307/3065 ,  B32B2379/08 ,  B32B2605/18 ,  B64C1/12 ,  B64C1/40

摘要： An encapsulated insulation composite system for increasing the burn through resistance of an aircraft fuselage includes: an insulation layer of glass fiber or foam insulation and a coating or interleaf barrier layer of a high temperature resistant material and/or a coating or barrier layer of a high temperature resistant material on an outer major surface of the insulation layer of the composite and a film encapsulating the composite. Preferably, the barrier layer or layers include a reflective mineral, such as a reflective mineral containing coating carried on a sheet material. Preferably, the encapsulating film is a polymeric film such as a polyimide film.

公开(公告)号：US06322022B1

公开(公告)日：2001-11-27

申请号：US09440010

申请日：1999-11-12

申请人： Ralph Michael Fay ,  Rebecca Sue Wulliman ,  James Walter Stacy ,  Jeffrey Canon Townsend ,  Steven N. Volenec

发明人： Ralph Michael Fay ,  Rebecca Sue Wulliman ,  James Walter Stacy ,  Jeffrey Canon Townsend ,  Steven N. Volenec

IPC分类号： B64C140

CPC分类号： B32B5/26 ,  B32B5/22 ,  B32B5/32 ,  B32B15/08 ,  B32B15/20 ,  B32B27/065 ,  B32B27/12 ,  B32B27/20 ,  B32B27/281 ,  B32B29/007 ,  B32B29/02 ,  B32B2260/021 ,  B32B2260/046 ,  B32B2262/101 ,  B32B2266/0214 ,  B32B2307/3065 ,  B32B2379/08 ,  B32B2605/18 ,  B64C1/12 ,  B64C1/40

摘要： An encapsulated insulation composite system for increasing the burn through resistance of an aircraft fuselage includes: an insulation layer of glass fiber or foam insulation and a coating or interleaf barrier layer of a high temperature resistant material and/or a coating or barrier layer of a high temperature resistant material on an outer major surface of the insulation layer of the composite and a film encapsulating the composite. Preferably, the barrier layer or layers include a reflective mineral, such as a reflective mineral containing coating carried on a sheet material. Preferably, the encapsulating film is a polymeric film such as a polyimide film.

摘要翻译： 一种用于通过飞机机身的阻力增加燃烧的封装绝缘复合系统包括：玻璃纤维或泡沫绝缘体的绝缘层和耐高温材料的涂层或插层阻挡层和/或高的涂层或阻挡层 复合材料绝缘层外表面上的耐高温材料和封装复合材料的薄膜。 优选地，阻挡层或层包括反射性矿物，例如在片材上承载的含反射矿物的涂层。 优选地，包封膜是聚酰亚胺膜等聚合物膜。

公开(公告)号：US5962107A

公开(公告)日：1999-10-05

申请号：US960465

申请日：1997-10-29

申请人： Barry Lynn Lowery ,  Jeffrey Canon Townsend ,  Ralph Michael Fay ,  Kevin Patrick McHugh

发明人： Barry Lynn Lowery ,  Jeffrey Canon Townsend ,  Ralph Michael Fay ,  Kevin Patrick McHugh

IPC分类号： G10K11/16 ,  B24B3/24 ,  E04B1/82

CPC分类号： G10K11/16 ,  Y10T428/24273 ,  Y10T428/24479 ,  Y10T428/249953 ,  Y10T83/0481

摘要： A cellular material, preferably a low density foam material, having an initial average normal incidence sound absorption coefficient for a selected frequency range is perforated to form a perforated cellular sound absorption material. The perforated cellular sound absorption material formed has an average normal incidence sound absorption coefficient for the selected frequency range greater than the initial average normal incidence sound absorption coefficient of the cellular sound absorption material. The depth(s), diameter(s), shape(s) and pattern of the perforations provide the cellular sound absorption material with the improved sound absorption properties that are reflected in the increased average normal incidence sound absorption coefficient of the material.

摘要翻译： 对具有选定频率范围的初始平均法线入射吸声系数的多孔材料，优选低密度泡沫材料进行穿孔以形成穿孔的细胞吸声材料。 所形成的穿孔的细胞吸声材料具有大于蜂窝吸声材料的初始平均法线入射吸声系数的所选频率范围的平均法线入射吸声系数。 穿孔的深度，直径，形状和图案提供了具有改善的吸声性能的蜂窝吸声材料，其反映在材料的平均法线入射吸声系数的增加中。