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1. 发明授权

US07342081B2 Fluoropolymer compositions, coated articles, and method of making the same 失效
标题翻译：含氟聚合物组合物，涂覆制品及其制备方法
公开(公告)号：US07342081B2
公开(公告)日：2008-03-11
申请号：US11024131
申请日：2004-12-28
申请人： Blake E. Chandler , Thomas J. Blong , Dale E. Hutchens
发明人： Blake E. Chandler , Thomas J. Blong , Dale E. Hutchens
IPC分类号： C08F16/24
CPC分类号： C08J3/12 , C08J2327/12 , C09D5/031 , C09D5/037
摘要： A fluoropolymer composition comprising a fluoropolymer with a particle size distribution having a ratio of the mode to D95 of 0.75 or greater and wherein when the fluoropolymer is a copolymer consisting of interpolymerized units derived from tetrafluoroethylene and perfluoro(propyl vinyl) ether, the fluoropolymer has less than 60 unstable endgroups per million carbon atoms; coated articles comprising the fluoropolymer; and methods for making the same.
摘要翻译：一种氟聚合物组合物，其含有具有模式与D95的比率为0.75以上的粒度分布的含氟聚合物，并且其中当所述含氟聚合物是由衍生自四氟乙烯和全氟（丙基乙烯基）醚的共聚单元组成的共聚物时，所述含氟聚合物具有较少的每百万个碳原子超过60个不稳定的端基; 包含含氟聚合物的涂层制品; 和制作相同的方法。

2. 发明授权

US5762746A Method of internally insulating a propellant combustion chamber 失效
标题翻译：内燃绝热推进剂燃烧室的方法
公开(公告)号：US5762746A
公开(公告)日：1998-06-09
申请号：US394706
申请日：1989-08-16
申请人： James A. Hartwell , Dale E. Hutchens , Kenneth E. Junior , James D. Byrd
发明人： James A. Hartwell , Dale E. Hutchens , Kenneth E. Junior , James D. Byrd
IPC分类号： C06B45/12 , C08L77/10 , C08L79/00 , C08L85/02 , F02K9/34 , B32B31/00
CPC分类号： F02K9/346 , C06B45/12 , C08L85/02 , C08L77/10 , C08L79/00 , Y10S60/909
摘要： A composition consisting essentially of a polyphosphazene binder having the following repeating units: ##STR1## wherein n is from about 20 to about 50,000, A is selected from --O-- and --NH--, and R.sup.1 and R.sup.2 are independently selected from alkyl having from one to about 20 carbon atoms, aryl having from 6 to about 14 carbon atoms, alkaryl having from 7 to about 30 carbon atoms, any of the preceding moieties substituted with halogen, hydroxyl, alkoxy, aryloxy, or nitro groups, or any of the preceding moieties linked by ether or amine linkages. Combined with an organic fiber filler, this material provides an erosion resistant insulation composition for temporarily protecting the interior of a rocket motor combustion chamber from thermal damage while the rocket is firing. Provided as a barrier coating or layer between the propellant grain and other structures within a rocket motor, this material prevents migration of plasticizers, nitrate esters, and other fluid or mobile ingredients from the propellant grain.
摘要翻译：基本上由具有以下重复单元的聚磷腈粘合剂组成的组合物：其中n为约20至约50,000，A选自-O-和-NH-，并且R 1和R 2独立地选自具有 1至约20个碳原子，具有6至约14个碳原子的芳基，具有7至约30个碳原子的烷芳基，任何前述部分被卤素，羟基，烷氧基，芳氧基或硝基取代，或任何前述部分通过醚或胺键连接。结合有机纤维填料，该材料提供耐腐蚀绝缘组合物，用于在火箭发射时临时保护火箭发动机燃烧室内部免受热损伤。作为火箭发动机内的推进剂颗粒和其他结构之间的阻隔涂层或层，该材料防止增塑剂，硝酸酯和其它流体或可移动成分从推进剂颗粒中迁移。

3. 发明授权

US6051087A Low smoke rocket motor liner compositions 失效
标题翻译：低烟火箭发动机衬套组成
公开(公告)号：US6051087A
公开(公告)日：2000-04-18
申请号：US991467
申请日：1992-12-16
申请人： Dale E. Hutchens , Norman Cohen
发明人： Dale E. Hutchens , Norman Cohen
IPC分类号： C06B45/12 , C06B45/10
CPC分类号： C06B45/12
摘要： A formulation is provided which is capable of performing as a liner layer between a rocket motor casing and the propellant grain disposed within the interior of the rocket motor casing. The composition produces relatively little smoke during the operation of the rocket motor and is capable of securely bonding a wide range of conventional propellants to a wide range of conventional casings. In one preferred formulation, the liner consists of from from about 50% to about 75% oxygen containing polymer; from about 3% to about 15% curing agent; from about 5% to about 50% filler and from about 0.01% to about 0.5% cure catalyst.
摘要翻译：提供了能够在火箭发动机壳体和设置在火箭发动机壳体内部的推进剂颗粒之间作为衬垫层的配方。该组合物在火箭发动机操作期间产生相对较少的烟雾，并且能够将广泛范围的常规推进剂牢固地粘合到各种常规壳体上。在一个优选的制剂中，衬垫由约50％至约75％的含氧聚合物组成; 约3％至约15％的固化剂; 约5％至约50％的填料和约0.01％至约0.5％的固化催化剂。

4. 发明授权

US5377593A Interpenetrating network combination of ultraviolet and thermally cured rocket motor liner composition and method 失效
标题翻译：紫外线和热固化火箭发动机衬套的互穿网络组合和方法
公开(公告)号：US5377593A
公开(公告)日：1995-01-03
申请号：US838091
申请日：1992-02-20
申请人： Richard E. Boothe , Dale E. Hutchens
发明人： Richard E. Boothe , Dale E. Hutchens
IPC分类号： C06B45/12 , C06B45/00 , C06D5/06
CPC分类号： C06B45/12
摘要： An interpenetrating network combination of ultraviolet and thermally curable rocket motor liner formulation comprising an optional solid filler, at least one ultraviolet curable polymer, an optional ultraviolet reactive diluent, at least one thermally curable polymer and at least one curing agent.
摘要翻译：包括紫外线和热固化火箭发动机衬里配方的互穿网络组合，其包括任选的固体填料，至少一种紫外线固化聚合物，任选的紫外线反应性稀释剂，至少一种可热固化的聚合物和至少一种固化剂。

5. 发明授权

US5031539A Radiation curable rocket motor liner for case bonded solid propellant 失效
标题翻译：用于壳体粘结固体推进剂的辐射固化火箭发动机衬套
公开(公告)号：US5031539A
公开(公告)日：1991-07-16
申请号：US467728
申请日：1990-01-19
申请人： Dale E. Hutchens
发明人： Dale E. Hutchens
IPC分类号： C06B45/12 , C08G18/69 , C08G18/81 , F02K9/34
CPC分类号： C06B45/12 , C08G18/69 , C08G18/8175 , F02K9/346
摘要： Improved bonding of hydroxyl-terminated polybutadiene based propellant grains to rocket motor liners and liners which are ultraviolet light radiation curable are provided by employing an acrylated polymer and an [[[(isocyanatoorgano)amino]carbonyl]oxy] alkyl propenoate in the liner composition.
摘要翻译：通过在衬垫组合物中使用丙烯酸酯化聚合物和[[（异氰酸根合有机基）氨基]羰基]氧基]丙烯酸酯，提供了将基于羟基封端的聚丁二烯基推进剂颗粒与火箭发动机衬垫和衬垫的紫外光可辐射固化的改进粘合。

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