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公开(公告)号：US20100187237A1
公开(公告)日：2010-07-29
申请号：US12586544
申请日：2009-09-23
CPC分类号： F17C1/12 , F17C2201/0128 , F17C2203/0325 , F17C2203/0329 , F17C2203/0358 , F17C2203/0391 , F17C2203/0395 , F17C2203/0604 , F17C2203/0629 , F17C2203/0643 , F17C2203/0646 , F17C2203/0673 , F17C2205/0314 , F17C2205/0332 , F17C2205/0352 , F17C2209/22 , F17C2209/221 , F17C2209/227 , F17C2209/238 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2223/047 , F17C2227/0304 , F17C2227/0306 , F17C2227/0381 , F17C2250/0408 , F17C2250/043 , F17C2250/0636 , F17C2260/012 , F17C2260/033 , F17C2265/034 , F17C2270/0189 , Y02E60/321 , Y10T29/49 , Y10T29/49826 , Y10T137/0318
摘要： A hydrogen storage tank for a hydrogen fueled aircraft. The tank has a wall made of layers of aerogel sections around a hard shell layer, sealed within a flexible outer layer, and having the air removed to form a vacuum. The periphery of each layer section abuts other sections of that layer, but only overlies the periphery of the sections of other layers at individual points. The wall is characterized by a thermal conductivity that is lower near its gravitational top than its gravitational bottom. The tank has two exit passageways, one being direct, and the other passing through a vapor shield that extends through the wall between two layers of aerogel. A control system controls the relative flow through the two passages to regulate the boil-off rate of the tank.
摘要翻译： 用于氢燃料飞机的储氢罐。 罐具有由围绕硬壳层的气凝胶部分的层制成的壁，密封在柔性外层内，并且除去空气以形成真空。 每个层部分的周边邻接该层的其他部分，但仅在各个点处覆盖其它层的部分的周边。 该壁的特征在于导热系数在其重力顶部附近比其引力底部更低。 该罐具有两个出口通道，一个是直接通道，另一个通过蒸气屏蔽，其在两层气凝胶之间延伸穿过壁。 控制系统控制通过两个通道的相对流量来调节罐的沸腾速率。
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公开(公告)号：US09829155B2
公开(公告)日：2017-11-28
申请号：US13533442
申请日：2012-06-26
IPC分类号： F17C1/12
CPC分类号： F17C1/12 , F17C2201/0128 , F17C2203/0325 , F17C2203/0329 , F17C2203/0358 , F17C2203/0391 , F17C2203/0395 , F17C2203/0604 , F17C2203/0629 , F17C2203/0643 , F17C2203/0646 , F17C2203/0673 , F17C2205/0314 , F17C2205/0332 , F17C2205/0352 , F17C2209/22 , F17C2209/221 , F17C2209/227 , F17C2209/238 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2223/047 , F17C2227/0304 , F17C2227/0306 , F17C2227/0381 , F17C2250/0408 , F17C2250/043 , F17C2250/0636 , F17C2260/012 , F17C2260/033 , F17C2265/034 , F17C2270/0189 , Y02E60/321 , Y10T29/49 , Y10T29/49826 , Y10T137/0318
摘要： A hydrogen storage tank for a hydrogen fueled aircraft. The tank has a wall made of layers of aerogel sections around a hard shell layer, sealed within a flexible outer layer, and having the air removed to form a vacuum. The periphery of each layer section abuts other sections of that layer, but only overlies the periphery of the sections of other layers at individual points. The wall is characterized by a thermal conductivity that is lower near its gravitational top than its gravitational bottom. The tank has two exit passageways, one being direct, and the other passing through a vapor shield that extends through the wall between two layers of aerogel. A control system controls the relative flow through the two passages to regulate the boil-off rate of the tank.
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公开(公告)号：US08960482B2
公开(公告)日：2015-02-24
申请号：US12586544
申请日：2009-09-23
IPC分类号： F17C1/12
CPC分类号： F17C1/12 , F17C2201/0128 , F17C2203/0325 , F17C2203/0329 , F17C2203/0358 , F17C2203/0391 , F17C2203/0395 , F17C2203/0604 , F17C2203/0629 , F17C2203/0643 , F17C2203/0646 , F17C2203/0673 , F17C2205/0314 , F17C2205/0332 , F17C2205/0352 , F17C2209/22 , F17C2209/221 , F17C2209/227 , F17C2209/238 , F17C2221/012 , F17C2223/0161 , F17C2223/033 , F17C2223/047 , F17C2227/0304 , F17C2227/0306 , F17C2227/0381 , F17C2250/0408 , F17C2250/043 , F17C2250/0636 , F17C2260/012 , F17C2260/033 , F17C2265/034 , F17C2270/0189 , Y02E60/321 , Y10T29/49 , Y10T29/49826 , Y10T137/0318
摘要： A hydrogen storage tank for a hydrogen fueled aircraft. The tank has a wall made of layers of aerogel sections around a hard shell layer, sealed within a flexible outer layer, and having the air removed to form a vacuum. The periphery of each layer section abuts other sections of that layer, but only overlies the periphery of the sections of other layers at individual points. The wall is characterized by a thermal conductivity that is lower near its gravitational top than its gravitational bottom. The tank has two exit passageways, one being direct, and the other passing through a vapor shield that extends through the wall between two layers of aerogel. A control system controls the relative flow through the two passages to regulate the boil-off rate of the tank.
摘要翻译： 用于氢燃料飞机的储氢罐。 罐具有由围绕硬壳层的气凝胶部分的层制成的壁，密封在柔性外层内，并且除去空气以形成真空。 每个层部分的周边邻接该层的其他部分，但仅在各个点处覆盖其它层的部分的周边。 该壁的特征在于导热系数在其重力顶部附近比其引力底部更低。 该罐具有两个出口通道，一个是直接通道，另一个通过蒸气屏蔽，其在两层气凝胶之间延伸穿过壁。 控制系统控制通过两个通道的相对流量来调节罐的沸腾速率。
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