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1. 发明授权

US08061214B2 Biaxial stress, sheer, permeability, and peel test method and machine to conduct the same 有权
标题翻译：双轴应力，透明度，剥离试验方法和机器进行相同
公开(公告)号：US08061214B2
公开(公告)日：2011-11-22
申请号：US12117016
申请日：2008-05-08
申请人： Paul E. Liggett , Dennis L. Carter , Nicholas L. Barnes , James I. Mascolino , Anthony L. Dunne , Aaron C. Graham
发明人： Paul E. Liggett , Dennis L. Carter , Nicholas L. Barnes , James I. Mascolino , Anthony L. Dunne , Aaron C. Graham
IPC分类号： G01N3/00
CPC分类号： G01N33/367 , G01N3/08 , G01N15/082 , G01N2203/0254 , G01N2203/0272 , G01N2203/0282
摘要： The subject invention relates to an apparatus and process for testing various parameters and properties of high strength flexible, fabric laminates. In particular, the apparatus comprises a machine using individually controlled loads to test various material parameters.
摘要翻译：本发明涉及用于测试高强度柔性织物层压材料的各种参数和性能的装置和方法。特别地，该设备包括使用单独控制的负载来测试各种材料参数的机器。

2. 发明授权

US4554300A Reducing the speed of aliphatic diamine curing agents in polyurethane cements 失效
标题翻译：降低聚氨酯水泥中脂肪族二胺固化剂的速度
公开(公告)号：US4554300A
公开(公告)日：1985-11-19
申请号：US722630
申请日：1985-04-12
申请人： Paul E. Liggett , Daniel A. Chung
发明人： Paul E. Liggett , Daniel A. Chung
IPC分类号： C08G18/00 , C08G18/10 , C08G18/42 , C08K3/34 , C09D175/06 , C08L75/06
CPC分类号： C08K3/34 , C08G18/10 , C09D175/06 , C08G2390/40 , Y10T428/31529
摘要： A method for preparing a polyurethane suitable for lining fuel tanks, said polyurethane having good, fuel resistance and improved hydrolysis resistance by using a ketimine of an aliphatic diamine as a curing agent in a three-component system composed of a prepolymer solution, a cement solution and a curing agent solution.
摘要翻译：一种制备聚氨酯的方法，所述聚氨酯适用于衬里燃料箱，所述聚氨酯具有良好的耐燃料性和耐水解性，通过在由预聚物溶液组成的三组分体系中使用脂族二胺的酮亚胺作为固化剂，水泥溶液和固化剂溶液。

3. 发明授权

US08524621B2 Metallized flexible laminate material for lighter-than-air vehicles 有权
标题翻译：用于轻型车辆的金属化柔性层压材料
公开(公告)号：US08524621B2
公开(公告)日：2013-09-03
申请号：US11991499
申请日：2006-09-20
申请人： Paul E. Liggett , Dennis L. Carter , Anthony L. Dunne , Dhiraj H. Darjee , Gerald W. Placko , James I. Mascolino , Lowell J. McEowen
发明人： Paul E. Liggett , Dennis L. Carter , Anthony L. Dunne , Dhiraj H. Darjee , Gerald W. Placko , James I. Mascolino , Lowell J. McEowen
IPC分类号： B32B27/12 , B32B15/14 , B32B27/32 , B29D22/02 , B64B1/00
CPC分类号： B32B5/024 , B32B5/022 , B32B5/026 , B32B5/12 , B32B5/26 , B32B27/08 , B32B27/12 , B32B27/20 , B32B27/304 , B32B37/12 , B32B2038/0092 , B32B2255/10 , B32B2255/205 , B32B2305/08 , B32B2307/416 , B32B2307/5825 , B32B2307/71 , B32B2307/712 , B32B2307/718 , B32B2307/7242 , B32B2375/00 , B32B2605/00 , B64B1/14 , Y10T428/1355 , Y10T428/1359 , Y10T428/1362 , Y10T428/31504 , Y10T428/3154 , Y10T428/31551 , Y10T428/31562 , Y10T428/31678 , Y10T442/2582 , Y10T442/259 , Y10T442/2598 , Y10T442/3447 , Y10T442/656 , Y10T442/674 , Y10T442/677
摘要： A laminate material for lighter-than-air vehicles includes at least one monofilament yarn layer, a polymeric film layer adjacent to the at least one monofilament layer, and a metallized coating adjacent to said polymeric film layer. A clear film cover layer may be adhered to the metallized coating, and one or more fluorescent dyes may be incorporated into the clear film layer.
摘要翻译：用于轻型车辆的层压材料包括至少一根单丝纱线层，与该至少一根单丝层相邻的聚合物薄膜层和与该聚合物薄膜层相邻的金属化涂层。可以将透明膜覆盖层粘附到金属化涂层，并且可以将一种或多种荧光染料引入到透明膜层中。

4. 发明授权

US08256086B2 Method of producing missile nose cones 有权
标题翻译：制造导弹鼻锥的方法
公开(公告)号：US08256086B2
公开(公告)日：2012-09-04
申请号：US12491953
申请日：2009-06-25
申请人： Robert A. Shutler , Margaret Rose Manning , Paul A. Leitch , Paul E. Liggett
发明人： Robert A. Shutler , Margaret Rose Manning , Paul A. Leitch , Paul E. Liggett
IPC分类号： B23Q17/00
CPC分类号： F42B19/005 , F42B10/46 , F42B15/22 , F42B19/46 , G01N3/12 , G01N2203/0274 , Y10T29/49346 , Y10T29/49771 , Y10T29/49778 , Y10T29/4978
摘要： A method for producing a missile nose cone is disclosed. The method consists of manufacturing a first missile nose cone from a first lot of polymeric material and determining a first rupture value. The method further consists of manufacturing a second missile nose cone from a second lot of polymeric material and determining a second rupture value of the second missile nose cone. Both first and second lots of material are mixed into a test batch with one another based on their associated rupture values. An evaluation missile nose cone is then manufactured from the test batch and a determination is made as to whether the evaluation missile nose cone has a desired rupture value. If a desired rupture value is not obtained, then the mixing and evaluation steps are repeated.
摘要翻译：公开了一种用于制造导弹鼻锥体的方法。该方法包括从第一批聚合物材料制造第一导弹鼻锥并确定第一破裂值。该方法还包括从第二批聚合材料制造第二导弹鼻锥并确定第二导弹鼻锥的第二破裂值。基于它们相关联的破裂值，将第一批和第二批材料混合成彼此的测试批次。然后从测试批次制造评估导弹鼻锥，并且确定评估导弹鼻锥是否具有期望的破裂值。如果未获得所需的破裂值，则重复混合和评价步骤。

5. 发明授权

US07875795B2 Thermocouple array for generating electrical power for lighter than air vehicles 失效
标题翻译：用于产生比空中车辆轻的电力的热电偶阵列
公开(公告)号：US07875795B2
公开(公告)日：2011-01-25
申请号：US12039959
申请日：2008-02-29
申请人： Paul E. Liggett
发明人： Paul E. Liggett
IPC分类号： H01L31/058 , H01L35/02
CPC分类号： H01L35/32 , B64B1/14 , H02S10/40
摘要： An energy generating device for lighter-than-air vehicles having a gas impervious outer flexible fabric including a flexible photovoltaic array located on the outer layer of the gas impervious fabric; a thermocouple array located between the photovoltaic cells and the gas impervious fabric; a thermally conductive layer or heat spreader between the thermocouple array and the photovoltaic array and between the thermocouple array and the gas impervious flexible fabric; an electrically conductive means connected to said thermocouple array for drawing electrical power away from said thermocouple array; and an electrical load, such as an electrical storage device or a device that consumes electricity, for drawing electricity from the thermocouple array.
摘要翻译：一种用于轻型车辆的能量产生装置，其具有不透气的外柔性织物，其包括位于不透气织物的外层上的柔性光伏阵列; 位于光伏电池和不透气织物之间的热电偶阵列; 热电偶阵列和光电阵列之间以及热电偶阵列和不透气的柔性织物之间的导热层或散热器; 连接到所述热电偶阵列的导电装置，用于从所述热电偶阵列拉出电力; 以及用于从热电偶阵列牵引电力的诸如蓄电装置或消耗电力的装置的电负载。

6. 发明申请

US20100326182A1 METHOD OF PRODUCING MISSILE NOSE CONES 有权
标题翻译：生产漏洞状态的方法
公开(公告)号：US20100326182A1
公开(公告)日：2010-12-30
申请号：US12491953
申请日：2009-06-25
申请人： Robert A. Shulter , Margaret Rose Manning , Paul A. Leitch , Paul E. Liggett
发明人： Robert A. Shulter , Margaret Rose Manning , Paul A. Leitch , Paul E. Liggett
IPC分类号： G01L5/14
CPC分类号： F42B19/005 , F42B10/46 , F42B15/22 , F42B19/46 , G01N3/12 , G01N2203/0274 , Y10T29/49346 , Y10T29/49771 , Y10T29/49778 , Y10T29/4978
摘要： A method for producing a missile nose cone is disclosed. The method consists of manufacturing a first missile nose cone from a first lot of polymeric material and determining a first rupture value. The method further consists of manufacturing a second missile nose cone from a second lot of polymeric material and determining a second rupture value of the second missile nose cone. Both first and second lots of material are mixed into a test batch with one another based on their associated rupture values. An evaluation missile nose cone is then manufactured from the test batch and a determination is made as to whether the evaluation missile nose cone has a desired rupture value. If a desired rupture value is not obtained, then the mixing and evaluation steps are repeated.
摘要翻译：公开了一种用于制造导弹鼻锥体的方法。该方法包括从第一批聚合物材料制造第一导弹鼻锥并确定第一破裂值。该方法还包括从第二批聚合材料制造第二导弹鼻锥并确定第二导弹鼻锥的第二破裂值。基于它们相关联的破裂值，将第一批和第二批材料混合成彼此的测试批次。然后从测试批次制造评估导弹鼻锥，并且确定评估导弹鼻锥是否具有期望的破裂值。如果未获得所需的破裂值，则重复混合和评价步骤。

7. 发明授权

US07687129B2 Splice seam 有权
公开(公告)号：US07687129B2
公开(公告)日：2010-03-30
申请号：US11651243
申请日：2007-01-08
申请人： Paul E. Liggett
发明人： Paul E. Liggett
IPC分类号： B32B3/10
CPC分类号： B64B1/14 , A41D27/245 , B29C65/4815 , B29C65/483 , B29C65/5042 , B29C66/1122 , B29C66/1142 , B29C66/43 , B29C66/72321 , B29C66/7234 , B29C66/729 , B29K2313/00 , B29K2995/0069 , B29L2009/00 , D06M17/00 , D06M17/10 , D06M23/18 , Y10T428/19 , Y10T428/192 , Y10T428/197
摘要： A splice seam for joining various sections of fabric together is disclosed, wherein the fabric sections are initially delaminated into their constituent plies. The plies associated with each fabric section are then interleaved with each other, and bonded together. The amount of surface area between each interleaved plies can be adjusted as so as to achieve a desired level of load carrying strength between the fabric sections. Additionally, the splice seam may utilize an external and/or internal seam tape to increase the strength of the resultant seam.

8. 发明申请

US20100055372A1 SPLICE SEAM 失效
公开(公告)号：US20100055372A1
公开(公告)日：2010-03-04
申请号：US12617856
申请日：2009-11-13
申请人： Paul E. LIGGETT
发明人： Paul E. LIGGETT
IPC分类号： B32B3/06
CPC分类号： B64B1/14 , A41D27/245 , B29C65/4815 , B29C65/483 , B29C65/5021 , B29C65/5042 , B29C65/5057 , B29C66/1122 , B29C66/1142 , B29C66/43 , B29C66/7234 , B29C66/729 , B29K2079/08 , B29K2313/00 , B29K2995/0067 , B29K2995/0069 , B29L2009/00 , B29L2022/022 , B29L2031/3076 , B32B3/28 , B32B5/022 , B32B5/024 , B32B5/22 , B32B5/26 , B32B7/045 , B32B7/06 , B32B7/12 , B32B27/12 , B32B27/281 , B32B27/34 , B32B27/40 , B32B2250/44 , B32B2262/0276 , B32B2307/50 , B32B2307/7242 , B32B2605/18 , D06H5/001 , D06M17/00 , D06M17/10 , D06M23/18 , Y10T428/19 , Y10T428/192
摘要： A splice seam for joining various sections of fabric together is disclosed, wherein the fabric sections are initially delaminated into their constituent plies. The plies associated with each fabric section are then fully interleaved with each other, and bonded together. The amount of surface area between each interleaved plies can be adjusted as so as to achieve a desired level of load carrying strength between the fabric sections.
摘要翻译：公开了用于将织物的各个部分连接在一起的接合缝，其中织物部分最初被分层成它们的构成层。然后，与每个织物部分相关联的层彼此完全交错并结合在一起。可以调节每个交错层之间的表面积的量，以便在织物部分之间达到期望的承载强度水平。

9. 发明申请

US20090220740A1 HIGHLY REFLECTIVE MATERIALS FOR USE AS LOGOS AND/OR IDENTIFICATION 有权
标题翻译：用作LOGOS和/或识别的高反射材料
公开(公告)号：US20090220740A1
公开(公告)日：2009-09-03
申请号：US12039985
申请日：2008-02-29
申请人： Paul E. LIGGETT
发明人： Paul E. LIGGETT
IPC分类号： B32B7/12 , B32B15/04 , B32B7/02
CPC分类号： G09F13/16 , G09F21/10 , Y10T428/24 , Y10T428/24355 , Y10T428/24942 , Y10T428/28 , Y10T428/2848 , Y10T428/2857
摘要： The present invention is generally directed to tapes or laminates designed for use in conjunction with lighter-than-air vehicles, platforms or other inflated structures. In one embodiment, the present invention is directed to tapes or laminates designed for use in logos and/or identification numbers that can be, for example, used on a lighter-than-air vehicle, platform or other inflated structure. In another embodiment, the present invention is directed to tapes or laminates that include, among other layers, at least one dichroic layer designed to produce a logo, letter and/or number that can be, for example, used on a lighter-than-air vehicle, platform or other inflated.
摘要翻译：本发明一般涉及被设计用于与轻于空气的车辆，平台或其它膨胀结构一起使用的带或层压板。在一个实施例中，本发明涉及设计用于标识和/或识别号码的带或层压板，其可以例如在比轻型车辆，平台或其他充气结构使用。在另一个实施方案中，本发明涉及带或层压材料，其包括除其它层之外的至少一个二色性层，其被设计成产生可以例如在比较轻质材料上使用的标识，字母和/或数字，飞机，平台或其他充气。

10. 发明申请

US20090220726A1 CONDUCTIVE SEAM COVER TAPE 有权
标题翻译：导电封口胶带
公开(公告)号：US20090220726A1
公开(公告)日：2009-09-03
申请号：US12039992
申请日：2008-02-29
申请人： Paul E. Liggett , Steven L. Sinsabaugh , James I. Mascolino
发明人： Paul E. Liggett , Steven L. Sinsabaugh , James I. Mascolino
IPC分类号： B32B3/00 , B32B27/00 , B32B27/06
CPC分类号： B64B1/14 , B32B7/045 , B32B7/12 , B32B27/08 , B32B27/281 , B32B27/304 , B32B2255/10 , B32B2255/205 , B32B2255/26 , B32B2262/101 , B32B2262/103 , B32B2262/106 , B32B2264/105 , B32B2264/108 , B32B2307/202 , B32B2307/206 , B32B2307/31 , B32B2307/416 , B32B2307/546 , B32B2307/71 , B32B2307/714 , B32B2307/718 , B32B2307/7242 , B32B2307/7265 , B32B2307/73 , B32B2405/00 , C09J7/29 , C09J183/00 , C09J2400/163 , C09J2427/006 , C09J2479/081 , C09J2483/00 , Y10T428/24 , Y10T428/24355 , Y10T428/28 , Y10T428/31504 , Y10T428/3154 , Y10T428/31721
摘要： The present invention is generally directed to tapes designed for use in conjunction with lighter-than-air vehicles, platforms or other inflated structures. In one embodiment, the present invention is directed to conductive seam cover tape that can be, for example, used to protect and/or cover one or more seams in a lighter-than-air vehicle, platform or other inflated structure. In another embodiment, the present invention is directed to a conductive seam cover tape that can be, for example, used to protect and/or cover fabric panels or sections that are used to form lighter-than-air vehicles, platforms or other inflated structures that are in, one instance, designed for deployment at high altitudes.
摘要翻译：本发明一般涉及被设计用于与轻于空气的车辆，平台或其他膨胀结构一起使用的带。在一个实施例中，本发明涉及导电缝覆盖带，其可以例如用于保护和/或覆盖轻于空气的车辆，平台或其他膨胀结构中的一个或多个接缝。在另一个实施例中，本发明涉及一种导电缝覆盖带，其可以例如用于保护和/或覆盖用于形成轻型空中车辆，平台或其他充气结构的织物面板或部分一个例子是设计用于高空部署。

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