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1. 发明申请

WO2015065433A1 RIGID AIRSHIP UTILIZING A RIGID FRAME FORMED BY HIGH PRESSURE INFLATED TUBES 审中-公开
标题翻译：使用高压充气管形成的刚性框架的刚性飞行
公开(公告)号：WO2015065433A1
公开(公告)日：2015-05-07
申请号：PCT/US2013/067768
申请日：2013-10-31
申请人： TP AEROSPACE, INC.
发明人： CHAMBERS, Paul
IPC分类号： B64B1/08
CPC分类号： B64B1/08 , B64B1/14 , B64B1/20 , B64B1/32
摘要： A rigid airship comprising a hull comprising a rigid frame covered by a skin, the rigid frame comprising a plurality of high pressure inflated tubes. Lighter-than-air craft are air vehicles which have a weight which is less than the weight of the air that they displace. As a result, lighter-than-air craft can be considered to "float" in the air, in much the same way that a naval craft "floats" in water. By way of example but not limitation, a recreational "hot air" balloon is one well known lighter-than-air craft.
摘要翻译：一种刚性飞艇，包括一个包括被皮肤覆盖的刚性框架的船体，刚性框架包括多个高压膨胀管。比空中飞行的工艺是空中车辆，其重量小于它们取代的空气的重量。因此，轻型飞机可以被认为在空中“漂浮”，就像海军舰艇“漂浮在水中一样”。作为示例而非限制，娱乐“热空气”气球是一种众所周知的轻型空中飞行器。

2. 发明申请

WO2011050138A3 AEROSTAT ENVELOPE CONSTRUCTION WITH ZIPPERED SECTIONS 审中-公开
标题翻译：带拉链部分的航空包装建设
公开(公告)号：WO2011050138A3
公开(公告)日：2011-08-25
申请号：PCT/US2010053494
申请日：2010-10-21
申请人： SKYACHT AIRCRAFT INC , FABEL JOHN , NACHBAR DANIEL
发明人： FABEL JOHN , NACHBAR DANIEL
IPC分类号： B64B1/58 , B64B1/02 , B64B1/40
CPC分类号： B64B1/02 , B64B1/14 , B64B1/40 , B64B1/58
摘要： A system and method for constructing and assembling envelopes used on buoyant systems from zippered sections is presented. The system incorporates features for avoiding weak points and excessive leakage of lifting gas.
摘要翻译：提出了一种用于构建和组装拉链部分浮力系统使用的信封的系统和方法。该系统具有避免提升气体的弱点和过度泄漏的功能。

3. 发明申请

WO2011042316A1 "MOMOHELI II" LIFTING MODULE AND VEHICLES 审中-公开
标题翻译： “MOMOHELI II”提升模块和车辆
公开(公告)号：WO2011042316A1
公开(公告)日：2011-04-14
申请号：PCT/EP2010/064070
申请日：2010-09-23
申请人： MONSCH, Daniel , MONSCH, Hans
发明人： MONSCH, Daniel , MONSCH, Hans
IPC分类号： B64B1/02 , B64B1/40 , B64B1/58 , B64B1/60 , B64B1/04 , B63C7/10
CPC分类号： B64B1/62 , B64B1/02 , B64B1/08 , B64B1/14 , B64B1/22 , B64B1/30 , B64B1/40
摘要： Relates to a lifting module (1) comprising : an envelope (2) with an inside surface (3) and an outside surface (4); a flexible membrane (5), comprising an upper surface (6) and a lower surface (7), extending inside said envelope (2) and being arranged so that said envelope (2) together with said flexible membrane (5) define a first compartment (C1) and a second compartment (C2) inside the envelope (2); a valve (8) for inflating or deflating lifting fluid (Gl) into or from said first compartment (C1); and a fluid inlet (9) and conveying means (10) for inflat- ing or deflating a second fluid (G2) through said fluid inlet (9) into or from said second compartment (C2). The lifting module (1) is characterized in that said envelope (2) is of essentially spherical shape with a zenith pole (11), a base pole (12), and a diameter (13) there between; the envelope (2) and the flexible membrane (5) comprising a mutual circular connection site (14), which is arranged in a distance (15) to the base pole ( 12) of the envelope (2), said distance (15) being equal or less than 33% of the diameter (13) of the envelope (2) and said flexible membrane (5) assuming, when the second compartment (C2) is empty, the shape of a spherical calotte with a calotte height that is essentially equal to said distance (15). The lifting module (1) is further characterized in that the inside surface (3) of the envelope (2) that partially encloses the first compartment (C1) and the upper surface (6) of the flexible membrane (5) comprise a common cover layer (16) that is tight for the lifting fluid (Gl) and in that the envelope (2) that partially encloses the second compartment (C2) comprises a coating layer (17) that is tight for the second fluid (G2). Also disclosed is a respective method of controlled lifting a pay load (100).
摘要翻译：涉及提升组件（1），包括：具有内表面（3）和外表面（4）的外壳（2）; 柔性膜（5），包括在所述封套（2）内延伸的上表面（6）和下表面（7），并且布置成使得所述封套（2）与所述柔性膜（5）一起限定第一（C1）和第二隔室（C2）内; 用于将提升流体（G1）充气或放气到所述第一隔室（C1）中或从所述第一隔室（C1）中排出的阀门（8）; 和用于使第二流体（G2）通过所述流体入口（9）进入或从所述第二隔室（C2）中排出或排出的输送装置（10）。提升模块（1）的特征在于，所述外壳（2）基本上是球形，具有天顶极（11），基极（12）和其间的直径（13）所述封套（2）和所述柔性膜（5）包括与信封（2）的基极（12）一定距离（15）设置的相互圆形连接部位（14），所述距离（15）等于或小于外壳（2）和所述柔性膜（5）的直径（13）的33％，假设当第二隔室（C2）为空时，具有calotte高度的球形calotte的形状为基本上等于所述距离（15）。提升模块（1）的特征还在于，部分包围第一隔室（C1）和柔性膜（5）的上表面（6）的外壳（2）的内表面（3）包括公共盖对于提升流体（G1）紧密的层（16），并且部分包围第二隔室（C2）的外壳（2）包括对第二流体（G2）是紧的涂层（17）。还公开了控制提升负荷（100）的各自的方法。

4. 发明申请

WO2006137909A2 INFLATABLE AND DEPLOYABLE SYSTEMS WITH THREE DIMENSIONALLY REINFORCED MEMBRANES 审中-公开
标题翻译：具有三维增强膜的可充电和可分配系统
公开(公告)号：WO2006137909A2
公开(公告)日：2006-12-28
申请号：PCT/US2005036716
申请日：2005-10-13
申请人： GSSL INC , LACHENMEIER TIMOTHY T , KOH MURAI
发明人： LACHENMEIER TIMOTHY T , KOH MURAI
IPC分类号： B64D17/02
CPC分类号： B64G1/222 , B64B1/14 , B64G2001/224
摘要： An illustrative embodiment of the invention includes an apparatus and method for making air and space inflatables and deployables using three dimensionally reinforced (3DR) membranes. A 3DR process preferably takes plural substantially flat gore segments, each segment made of plural membranes and reinforcing fibers, and joins adjacent gores so the seams on opposite sides are offset. Single ply seam tape may be used. When all gores are joined, a three dimensional deployable or inflatable (e.g., balloon) structure with a minimized seam is produced. Further, localized fiber reinforcement may be used, with different characteristics depending on the desired placement in the gore, allowing the substantially flat gores, when joined and loaded, to strain to the desired three dimensional shape. In doing so, the required number of gores and seams may be reduced, while using materials with significantly lower areal densities. Thus, the 3DR process allows one to make locally reinforced materials that optimize strength to weight ratios; permits single ply and sub-gore width seam tapes; permits multi-phase optimized envelope shapes, designed to efficiently handle multiple loading conditions; and provides increased design flexibility for a wide range of shapes and characteristics impractical or unavailable under prior techniques.
摘要翻译：本发明的说明性实施例包括使用三维增强（3DR）膜制造空气和空间充气装置和展开件的装置和方法。 3DR工艺优选地采用多个基本上平坦的玻璃片段，每个片段由多个膜片和增强纤维制成，并且连接相邻的角部，使得相对侧上的接缝被偏移。可以使用单层缝带。当所有山羊被连接时，产生具有最小缝隙的三维可展开或可充气（例如气球）结构。此外，可以使用局部纤维增强物，具有不同的特性，这取决于在孔中的所需位置，允许当连接和加载时基本上平坦的孔，以应变到期望的三维形状。在这样做时，可以减少所需数量的山羊和接缝，同时使用具有明显较低的面密度的材料。因此，3DR工艺允许制造优化强度与重量比的局部增强材料; 允许单层和亚高宽度的缝带; 允许多相优化的包络形状，旨在有效地处理多种加载条件; 并为广泛的形状和特性提供了增加的设计灵活性，这在现有技术中不可行或不可用。

5. 发明申请

WO2003010375A1 FLEXIBLE WALL MATERIAL FOR USE IN AN INFLATABLE STRUCTURE 审中-公开
标题翻译：柔性壁材料用于可燃性结构
公开(公告)号：WO2003010375A1
公开(公告)日：2003-02-06
申请号：PCT/US2002/023472
申请日：2002-07-24
申请人： LOCKHEED MARTIN CORPORATION
发明人： SIDWELL, Donald, R.
IPC分类号： D03D15/00
CPC分类号： B32B5/26 , B64B1/14 , D03D1/02 , D03D11/00 , D03D15/00 , D10B2321/021 , D10B2401/063 , D10B2507/10 , Y10T428/24058 , Y10T428/24074 , Y10T428/24116 , Y10T428/24124 , Y10T428/24174 , Y10T442/2738 , Y10T442/30 , Y10T442/3472 , Y10T442/3602 , Y10T442/365 , Y10T442/3667 , Y10T442/3854 , Y10T442/3862
摘要： This invention relates to airships (10), with a volume in 15 to 60 million cubic feet of Helium. More particularly, it relates to improved structural envelope/gas bags (12) or outer covers for lighter-than-air and neutral buoyancy airships (10). In detail, the material (20) is a multi-layer cloth assembly including at least two plies of fiber cloth (62), said cloth (62) comprising 56 by 56 yarns/inch with a total weight of 150 to 450 g/m2, with the fiber of the individual cloth layers having a denier generally between 180 and 280 and with the fill of the individual plies at 90 degrees to each other. Preferably, the filaments should be between 200 and 215 denier. The fibers of each layer of cloth (62) are selected from the group consisting of extended chain polyethylene polymer or a thermotropic liquid (melt spun) crystalline polymer. The extended chain polyethylene fiber is a woven modified rip stop weave architecture, while the thermotropic liquid (melt spun) crystalline polymer fiber is a 2x2 basket weave architecture.
摘要翻译：本发明涉及飞艇（10），其体积为15至6000万立方英尺的氦气。更具体地说，本发明涉及用于轻于空气和中性浮力飞艇（10）的改进的结构外壳/气囊（12）或外盖。详细地，材料（20）是包括至少两层纤维布（62）的多层布组合件，所述布（62）包括56×56纱/英寸，总重量为150至450g / m 2 其中各个布层的纤维的旦尼尔通常在180和280之间，并且各个层的填充物彼此成90度。优选地，长丝应在200至215旦尼尔之间。每层布（62）的纤维选自延伸链聚乙烯聚合物或热致液体（熔纺）结晶聚合物。延伸链聚乙烯纤维是织造改性的撕裂织造结构，而热致液体（熔纺）结晶聚合物纤维是2x2篮子织造结构。

6. 发明申请

WO2018076779A1 胶黏剂、其制备方法及囊体材料审中-公开
公开(公告)号：WO2018076779A1
公开(公告)日：2018-05-03
申请号：PCT/CN2017/092056
申请日：2017-07-06
申请人：深圳光启空间技术有限公司
发明人：刘若鹏 , 栾琳 , 苏亚军
IPC分类号： B32B27/02 , B32B27/08 , B32B27/12 , B32B27/30 , B32B27/36 , B32B27/40 , B32B7/12 , B32B15/09 , B64B1/14 , B64B1/58 , C09J175/06 , C09J11/04
CPC分类号： B32B7/12 , B32B15/09 , B32B27/02 , B32B27/08 , B32B27/12 , B32B27/30 , B32B27/36 , B32B27/40 , B64B1/14 , B64B1/58 , C09J11/04 , C09J175/04 , C09J175/06
摘要：一种胶黏剂包括胶黏剂主体和石墨烯，且石墨烯在胶黏剂中的重量百分比为0.2～1％。在胶黏剂主体中添加石墨烯，使石墨烯分散在胶黏剂主体中，由于石墨烯对氦气具有较好的阻隔性能，因此使得具有其的胶黏剂也具有氦气阻隔性能；同时由于石墨烯用量很少，在0.2～1％之间，因而不会明显增大囊体材料面密度，这对于飞艇囊体材料的轻质化具有重要的意义；进一步地，由于石墨烯是加在胶黏剂中，因而不会提高囊体材料加工的复杂性。

7. 发明申请

WO2012135117A2 AIRSHIP INCLUDING AERODYNAMIC, FLOATATION, AND DEPLOYABLE STRUCTURES 审中-公开
标题翻译：航空包括航空，航行和可配置的结构
公开(公告)号：WO2012135117A2
公开(公告)日：2012-10-04
申请号：PCT/US2012030562
申请日：2012-03-26
申请人： LTA CORP , GOELET JOHN
发明人： GOELET JOHN
IPC分类号： B64B1/14
CPC分类号： B64B1/68 , B64B1/00 , B64B1/06 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/22 , B64B1/34 , B64B1/58 , B64B1/60 , B64B2201/00 , B64C25/32 , B64C25/56 , B64D2211/00
摘要： An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship.
摘要翻译：提供飞艇。飞艇包括构造成容纳气体的船体，耦合到船体的至少一个推进组件，并且包括推进装置，以及包括多个整流罩结构（包括一个或多个板条）的至少一个空气动力部件，其中至少一个空气动力学组件与船体相关联，并且被配置为引导飞艇周围的气流。

8. 发明申请

WO2012021581A1 AIRSHIP 审中-公开
标题翻译：飞艇
公开(公告)号：WO2012021581A1
公开(公告)日：2012-02-16
申请号：PCT/US2011/047186
申请日：2011-08-10
申请人： IREL SOLUTIONS GROUP LTD. , OCHOA, Ozden, O. , SCHNEIDER, William, C.
发明人： OCHOA, Ozden, O. , SCHNEIDER, William, C.
IPC分类号： B64B1/02 , B64B1/58
CPC分类号： B64B1/08 , B64B1/14 , B64B1/58 , B64C37/02
摘要： An airship system having a flexible envelope and at least one bladder positioned therein is described. The bladder(s) provide an impervious barrier between the gas within the bladder(s) and the air exterior to the bladder(s). The envelope includes longitudinal and hoops straps weaved together in a criss-cross manner. The envelope also includes rings positioned thereon that include truss members for receiving struts for removably coupling the airship to another airship. A tri-hull delta dirigible system is also described, comprising three airships coupled together using struts and arranged in an equilateral triangle formation. The tri-hull delta dirigible system has a similar lift capacity (volume) as a conventional large mono-hull dirigible, while minimizing the detrimental bending in the center of the conventional mono-hull dirigible.
摘要翻译：描述了具有柔性外壳和位于其中的至少一个气囊的飞艇系统。膀胱在膀胱内的气体和膀胱外部的空气之间提供不透过的屏障。信封包括以十字交叉的方式编织在一起的纵向和环形带。信封还包括定位在其上的环，其包括用于接收支柱的桁架构件，用于将飞艇可移除地联接到另一个飞艇。还描述了三壳三角系统，其包括使用支杆联接在一起并以等边三角形形成的三个飞艇。三体三角洲系统具有与传统的大型单壳体相似的升力能力（体积），同时最小化传统单体船体中心的有害弯曲。

9. 发明申请

WO2011056791A3 OPTICALLY ENHANCED FILMS FOR AEROSTATS 审中-公开
标题翻译：用于航天器的光学增强电影
公开(公告)号：WO2011056791A3
公开(公告)日：2011-08-11
申请号：PCT/US2010055119
申请日：2010-11-02
申请人： INTERFACIAL SOLUTIONS IP LLC , CERNOHOUS JEFFREY JACOB , PAWLOSKI ADAM R , GRANLUND NEIL R , KASKE KENT
发明人： CERNOHOUS JEFFREY JACOB , PAWLOSKI ADAM R , GRANLUND NEIL R , KASKE KENT
IPC分类号： B64B1/58 , B32B7/00 , B64B1/02 , B64B1/40
CPC分类号： G09F21/10 , B32B7/12 , B32B27/08 , B32B27/18 , B32B27/20 , B32B27/32 , B32B27/34 , B32B27/36 , B32B2264/02 , B32B2264/06 , B32B2264/08 , B32B2264/10 , B32B2264/101 , B32B2264/105 , B32B2264/12 , B32B2270/00 , B32B2307/40 , B32B2307/41 , B32B2307/416 , B32B2307/518 , B32B2307/5825 , B32B2307/702 , B32B2307/704 , B32B2307/732 , B32B2307/75 , B32B2605/00 , B32B2605/18 , B64B1/14 , Y10T156/10
摘要： The present invention enhances the optical features of acrostats. The invention utilizes a barrier film having at least one layer containing optically enhancing elements. Aerostats formed from the barrier film possess unique aesthetic features.
摘要翻译：本发明增强了acrostats的光学特征。本发明使用具有至少一个含光学增强元件的层的阻挡膜。由屏障膜形成的浮法器具有独特的美学特征。

10. 发明申请

WO2010121384A1 SPLITTER PLATE FOR HYBRID AIRSHIP CONTROL 审中-公开
标题翻译：混合飞行控制分机板
公开(公告)号：WO2010121384A1
公开(公告)日：2010-10-28
申请号：PCT/CA2010/000631
申请日：2010-04-23
申请人： SOLARSHIP , DELAURIER, James D.
发明人： DELAURIER, James D.
IPC分类号： B64B1/02 , B64C13/50 , B64C31/00
CPC分类号： B64B1/06 , B64B1/14 , B64B1/20 , B64B1/30 , B64B2201/00 , B64C2201/00 , G09F21/08 , G09F21/10
摘要： A hybrid airship comprises a non-rigid body having a delta-wing shape and an airfoil cross-section. The body is shaped for generating aerodynamic lift during forward flight, and contains a gas for generating buoyancy lift. At least one splitter plate is pivotally connected along a trailing edge of the body. The splitter plate is configured to be controllably pivoted for controlling the airship.
摘要翻译：混合式飞艇包括具有三角翼形状和翼型横截面的非刚性体。身体形状适合在前进飞行期间产生空气动力升力，并且包含产生浮力升力的气体。至少一个分离板沿主体的后缘枢转地连接。分离板构造成可控地枢转以控制飞艇。

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