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1. 发明授权

US5056156A Helmet of a laminate construction of polycarbonate and polysulfone polymeric material 失效
标题翻译：聚碳酸酯和聚砜聚合材料的层压结构头盔
公开(公告)号：US5056156A
公开(公告)日：1991-10-15
申请号：US443414
申请日：1989-11-30
申请人： Joseph J. Kosmo , Frederic S. Dawn
发明人： Joseph J. Kosmo , Frederic S. Dawn
IPC分类号： A42B3/06 , A42B3/22 , B32B27/06
CPC分类号： A42B3/063 , A42B3/22 , B32B27/06 , Y10T428/24967 , Y10T428/31507 , Y10T428/31533 , Y10T428/31681
摘要： An article of laminate construction comprising an underlayer of polycarbonate polymer material 16 to which is applied a chemically resistant outer layer of polysulfone material 17. The layers 16, 17 which are joined by compression-heat molding, are moldable to form the shape of a body protective shell such as a space helmet 10 comprising a shell 18 of polycarbonate, polysulfone laminate construction attached at its open end to a sealing ring 19 adapted for connection to a space suit. The front portion of the shell 18 provides a transparent visor for the helmet. An outer visor 25 of polycarbonate polysulfone polymer laminate construction is pivotally mounted to the sealing ring 19 for covering the transparent visor portion of the shell 18 during extravehicular activities. The polycarbonate under layer of the outer visor 25 is coated on its inner surface with a vacuum deposit of gold to provide additional thermal radiation resistance.
摘要翻译：一种层叠结构的制品，包括聚碳酸酯聚合物材料16的底层，其上施加有抗化学腐蚀的聚砜材料外层17.通过压缩热成型连接的层16,17可模制成形成主体的形状保护壳，例如包括聚碳酸酯壳体18的太空头盔10，在其开口端连接到适于连接到太空服的密封环19的聚砜叠层结构。外壳18的前部提供用于头盔的透明遮阳板。聚碳酸酯聚砜聚合物层压结构的外遮阳板25枢转地安装到密封环19上，用于在舱外活动期间覆盖壳体18的透明遮阳板部分。外罩25的聚碳酸酯层在其内表面上涂覆有金的真空沉积物以提供额外的耐热辐射性。

2. 发明授权

US4923741A Hazards protection for space suits and spacecraft 失效
标题翻译：太空服和航天器的危害保护
公开(公告)号：US4923741A
公开(公告)日：1990-05-08
申请号：US213880
申请日：1988-06-30
申请人： Joseph J. Kosmo , Frederic S. Dawn
发明人： Joseph J. Kosmo , Frederic S. Dawn
IPC分类号： A41D31/00 , A62B17/00 , A62D5/00 , B32B5/26 , G21F1/10 , G21F3/025
CPC分类号： B32B5/26 , A41D31/0027 , A41D31/0072 , A62B17/00 , A62D5/00 , G21F1/106 , G21F3/025 , Y10S428/911 , Y10T428/256 , Y10T428/31544 , Y10T428/31663 , Y10T428/31681 , Y10T428/31725 , Y10T442/3049 , Y10T442/3179 , Y10T442/3407 , Y10T442/3528
摘要： A flexible multi-layered covering article 10 for protection against the hazards of exposure to the environment of outer space. The covering 10 includes an outer layer section 12 comprising an outermost lamina 14 of woven expanded tetrafluoroethylene yarns (Gore-Tex) for protecting against abrasion and tearing, an underlying weave 16 of meta-aramid yarns (Nomex) and para-aramid yarns (Kevlar) for particle impart protection, an electrostatic charge dissipation and control system 18 incorporated therein, and a chemical contaminants control barrier applied as a coating 19. A middle section includes a succession of thermal insulating layers 21 of polymeric thermoplastic or thermoforming material, each of which is coated with a metal deposit of high infra-red emissivity and low solar radiation absorption characteristics and separated from adjacent insulating layers 21 by a low thermal conductance material 26. The covering 10 further includes a radiation attenuating layer 28 of a tungsten-loaded polymeric elastomer binder for protecting against "bremsstrahlung" radiation and an inner layer 32 of "rip-stop" polyester material for abrasion protection. A chloroprene coating may be supplied the polyester-material for added micrometeroid protection. Securing means 36 of low heat conductance material secures the multi-layers together as a laminar composite.
摘要翻译：一种灵活的多层覆盖物10，用于防止暴露于外太空环境的危害。覆盖物10包括外层部分12，其包括用于防止磨损和撕裂的编织的膨胀四氟乙烯纱线（Gore-Tex）的最外层14，间位芳族聚酰胺纱线（Nomex）和对位芳族聚酰胺纱线（Kevlar ），用于赋予粒子的保护，其中并入的静电电荷耗散和控制系统18以及作为涂层19应用的化学污染物控制屏障。中间部分包括一系列聚合物热塑性或热成型材料的隔热层21，涂覆有高红外辐射率和低太阳辐射吸收特性的金属沉积物，并通过低导热材料26与相邻的绝缘层21分离。覆盖物10还包括负载钨的聚合弹性体的辐射衰减层28 用于防止“bre致辐射”辐射的粘合剂和“撕裂”聚酯的内层32 磨损保护材料氯丁橡胶涂层可以提供聚酯材料，以增加微米级保护。低导热材料的固定装置36将多层固定在一起作为层状复合材料。

3. 发明授权

US5384083A Method for forming a glove attachment 失效
标题翻译：形成手套附件的方法
公开(公告)号：US5384083A
公开(公告)日：1995-01-24
申请号：US929556
申请日：1992-08-14
申请人： Frederic S. Dawn , Walter W. Guy , Joseph J. Kosmo , Arthur P. Drennan , Richard P. Tschirch
发明人： Frederic S. Dawn , Walter W. Guy , Joseph J. Kosmo , Arthur P. Drennan , Richard P. Tschirch
IPC分类号： A41D19/015 , B29C70/08 , B29C70/34 , B29C39/12 , B29C67/14
CPC分类号： B29C70/34 , A41D19/01558 , B29C70/08 , B29K2083/00 , B29K2277/10 , B29L2031/4864
摘要： A method for forming a glove attachment principally for the palm of an astronaut glove to enhance the gripping area of the palm without detracting from the flexibility and utility of the glove. The attachment is a composite construction formed from a layer of silicone rubber having an outer surface with a friction configuration and an another layer of silicone rubber in which a meta-aramid mesh fabric is embedded prior to curing. The method of construction involves the use of a mold with a friction configuration surface. A first layer of silicone rubber or sealant is disposed in the mold and allowed to set for an hour. A second layer of silicone rubber or sealant is layered over the first layer and leveled. A meta-aramid mesh fabric is embedded into the second layer and the composite is permitted to cure. When cured, a configured area of the composite construction is glued or stitched to the palm area of the glove.
摘要翻译：形成用于宇航员手掌的手套附着物的方法，以增强手掌的抓握面积，而不会降低手套的柔韧性和效用。附件是由具有摩擦构造的外表面和另一层硅橡胶的硅橡胶层形成的复合结构，其中在固化之前嵌入间位芳族聚酰胺网状织物。施工方法涉及使用具有摩擦配置表面的模具。将第一层硅橡胶或密封剂置于模具中并允许放置一小时。第二层硅橡胶或密封剂层叠在第一层上并平整。将间位芳族聚酰胺网状织物嵌入第二层中，并使复合物固化。当固化时，复合结构的配置区域胶合或缝合到手套的手掌区域。

4. 发明授权

US4887749A Don/Doff support stand for use with rear entry space suits 失效
标题翻译： Don / Doff支持支持后置入口太空服
公开(公告)号：US4887749A
公开(公告)日：1989-12-19
申请号：US221472
申请日：1988-07-19
申请人： Joseph J. Kosmo , Terry O. Tri , William E. Spenny , Philip R. West
发明人： Joseph J. Kosmo , Terry O. Tri , William E. Spenny , Philip R. West
IPC分类号： A47G25/90 , B64G6/00
CPC分类号： A47G25/90 , B64G6/00
摘要： A don/doff support stand for use with rear entry space suits is disclosed. The support stand is designed for use in one-g environments; however, certain features of the stand can be used on future space-craft, lunar or planetary bases. The present invention has a retainer which receives a protruding lug fixed on the torso section of the space suit. When the lug is locked in the retainer, the space suit is held in a generally upright position. In a one-g environment a portable ladder is positioned adjacent to the rear entry of the space suit supported by the stand. The astronaut climbs up the ladder and grasps a hand bar assembly positioned above the rear entry. The astronaut then slips his legs through the open rear entry and down into the abdominal portion of the suit. The astronaut then lowers himself fully into the suit. The portable ladder is then removed and the astronaut can close the rear entry door. The lug is then disengaged from the retainer and the astronaut is free to engage in training exercises in the suit. When suit use is over, the astronaut returns to the stand and inserts the lug into the retainer. A technician repositions the ladder. The astronaut opens the rear entry door, grasps the hand bar assembly and does a chin-up to extricate himself from the suit. The astronaut climbs down the movable ladder while the suit is supported by the stand.
摘要翻译：公开了一种用于后进入空间服的don / doff支撑架。支撑架设计用于一g环境中; 然而，立场的某些特征可以用于未来的太空飞船，月球或行星基地。本发明具有保持器，该保持器容纳固定在太空服的躯干部分上的突出的突出部。当凸耳锁定在保持器中时，太空西装保持在大致直立的位置。在一个环境中，一个便携式梯子位于与支架支撑的太空服的后部入口附近。宇航员爬上梯子，抓住位于后部入口上方的手杆组件。然后，宇航员通过打开的后部入口滑下他的腿，然后下降到西装的腹部。然后宇航员将自己完全放下衣服。然后便携式梯子被拆下，宇航员可以关上后门。然后将耳片从保持架上脱开，宇航员可以自由参与西装的训练。当西装使用结束时，宇航员返回到支架并将凸耳插入保持架。技术员重新安置梯子。宇航员打开后门，抓住手杆组件，并做一个下巴，从衣服上脱身。当西装由支架支撑时，宇航员爬上可移动的梯子。

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