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公开(公告)号:US20170042271A1
公开(公告)日:2017-02-16
申请号:US15227593
申请日:2016-08-03
Applicant: Wayne H. Tuttle , Lisa C. Whitaker
Inventor: Wayne H. Tuttle , Lisa C. Whitaker
Abstract: A helmet configured to protect a human head against mild traumatic brain injury upon impact includes an outer shell and a liner consisting of pairs of fluid fillable flexible fluid chambers fluidly connected to each other by fluid connections between each of the pairs of fluid fillable flexible fluid chambers being spaced on opposite sides of the helmet and configured to fill a space between the head and the outer shell when the helmet is positioned on the head. Impact resistant flexible pads are also inside the liner and are spaced around an inner circumference of the outer shell adjacent to each of the fluid fillable flexible fluid chambers. A flexible inner shell inside the liner is configured to fit closely on the head. The flexible fluid chambers are configured to compress in response to impacting of the helmet on an impact side and to force liquid through the fluid connections to inflate fluid chambers on an opposite side of the helmet thereby cushioning the head against a rebound impact on the opposite side.
Abstract translation: 被配置为保护人体头部免受冲击时的轻度创伤性脑损伤的头盔包括外壳和由两对可流体填充的柔性流体室组成的衬套,所述衬套通过每对可流体填充的柔性流体室之间的流体连接彼此流体连接 在头盔的相对侧上间隔开并配置成当头盔位于头部上时填充头部和外壳之间的空间。 抗冲击柔性垫也在衬里内,并且围绕与每个可流体填充的柔性流体室相邻的外壳的内圆周间隔开。 衬里内部的柔性内壳构造成紧密地配合在头部上。 柔性流体室被构造成响应于头盔在冲击侧的冲击而压缩,并且迫使液体通过流体连接件来使头盔的相对侧上的流体室膨胀,从而缓冲头部抵抗在相对侧的反弹冲击 。
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公开(公告)号:US20120241459A1
公开(公告)日:2012-09-27
申请号:US13052862
申请日:2011-03-21
Applicant: Wayne H. Tuttle
Inventor: Wayne H. Tuttle
CPC classification number: B64G1/402 , F02K9/605 , F05D2230/90 , F05D2300/133 , F05D2300/51 , F17C13/008 , F17C2201/0128 , F17C2201/054 , F17C2201/056 , F17C2203/0607 , F17C2203/0646 , F17C2203/0648 , F17C2203/0663 , F17C2209/221 , F17C2209/228 , F17C2221/08 , F17C2270/0194 , Y10T29/49888 , Y10T137/2931 , Y10T137/3127 , Y10T137/86212 , Y10T137/86348
Abstract: A demisable fuel supply system for a satellite includes a pressurized aluminum alloy tank with an aluminum alloy propellant management device therein. The propellant management device (PMD) can have any capillary action surface tension fluid transport features known in the art. Selected inner surfaces of the tank and the PMD are covered with a titanium based coating to guarantee propellant wettability and corrosion resistance of the fuel supply system.
Abstract translation: 卫星的可燃燃料供应系统包括其中具有铝合金推进剂管理装置的加压铝合金罐。 推进剂管理装置(PMD)可以具有本领域已知的任何毛细作用表面张力流体输送特性。 油箱和PMD的选定内表面均覆盖有钛基涂层,以确保燃油供应系统的推进剂润湿性和耐腐蚀性。
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公开(公告)号:US4963715A
公开(公告)日:1990-10-16
申请号:US328949
申请日:1989-03-27
Applicant: Wayne H. Tuttle
Inventor: Wayne H. Tuttle
CPC classification number: B23K9/0738 , B23K9/0672 , G05F1/08
Abstract: Disclosed is a variable polarity power supply for arc welding that quickly switches between polarities in order to more easily re-establish the arc. The variable polarity power supply includes a current-limited boost circuit for providing increased open circuit voltage to re-establish the arc, while limiting the re-establishment current. The variable polarity power supply is particularly suitable for computer-controlled welding applications because it periodically restarts the arc in either direction without using high frequency radiation, and provides quick switching times along with a low reverse current to reduce the heat in the torch, thereby increasing the longevity of the torch.
Abstract translation: 公开了一种用于电弧焊的可变极性电源,其在极性之间快速切换以便更容易地重建电弧。 可变极性电源包括限流升压电路,用于提供增加的开路电压以重新建立电弧,同时限制重建电流。 可变极性电源特别适用于计算机控制的焊接应用,因为它不使用高频辐射来周期性地重新启动电弧,并且提供快速切换时间以及低反向电流以减少焊炬中的热量,从而增加 火炬的长寿
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公开(公告)号:US20170280814A1
公开(公告)日:2017-10-05
申请号:US15623110
申请日:2017-06-14
Applicant: Wayne H. Tuttle , Lisa C. Whitaker
Inventor: Wayne H. Tuttle , Lisa C. Whitaker
CPC classification number: A42B3/121 , A42B3/063 , A42B3/069 , A42B3/08 , A42B3/125 , A42C2/00 , A63B71/081 , A63B2102/14 , A63B2102/18 , A63B2102/22 , A63B2102/24 , A63B2243/007 , A63B2244/19 , A63B2244/20 , A63B2244/24 , F41H1/04
Abstract: A helmet configured to protect a human head against mild traumatic brain injury upon impact includes an outer shell and a liner consisting of fluid fillable flexible fluid chambers fluidly connected to each other by fluid connections. The fluid chambers being spaced around the circumference of the helmet and configured to fill a space between the head and the outer shell when the helmet is positioned on the head. Impact resistant flexible pads are also in the liner and are spaced around an inner circumference of the outer shell adjacent to each of the fluid fillable flexible fluid chambers. A flexible inner shell inside the liner is configured to fit closely on the head. The flexible fluid chambers are configured to compress in response to impacting of the helmet on an impact side and to force liquids through the fluid connections to inflate other fluid chambers inside the helmet thereby cushioning the head against a rebound impact on the inside of the helmet.
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公开(公告)号:US08534489B2
公开(公告)日:2013-09-17
申请号:US13432618
申请日:2012-03-28
Applicant: Wayne H. Tuttle , David Adams , Marcial Alexander Anaya , Jeffry K. Pearson
Inventor: Wayne H. Tuttle , David Adams , Marcial Alexander Anaya , Jeffry K. Pearson
CPC classification number: F02K9/605 , B64G1/402 , F05D2230/312 , F05D2230/90 , F05D2260/95 , F05D2300/121 , F05D2300/133 , Y10T29/49982 , Y10T137/2931 , Y10T137/3127 , Y10T137/86212 , Y10T137/86348
Abstract: A demisable fuel supply system for a satellite includes a pressurized aluminum alloy tank with an aluminum alloy propellant management device therein. The propellant management device (PMD) can have any capillary action surface tension fluid transport features known in the art. Selected inner surfaces of the tank and the PMD are covered with a plasma powder sprayed titanium based coating to guarantee propellant wettability and corrosion resistance of the fuel supply system.
Abstract translation: 卫星的可燃燃料供应系统包括其中具有铝合金推进剂管理装置的加压铝合金罐。 推进剂管理装置(PMD)可以具有本领域已知的任何毛细作用表面张力流体输送特性。 罐体和PMD的内表面被等离子体喷涂的钛基涂层覆盖,以保证燃料供应系统的推进剂润湿性和耐腐蚀性。
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公开(公告)号:US10779602B2
公开(公告)日:2020-09-22
申请号:US15227593
申请日:2016-08-03
Applicant: Wayne H. Tuttle , Lisa C. Whitaker
Inventor: Wayne H. Tuttle , Lisa C. Whitaker
Abstract: A helmet configured to protect a human head against mild traumatic brain injury upon impact includes an outer shell and a liner consisting of pairs of fluid fillable flexible fluid chambers fluidly connected to each other by fluid connections between each of the pairs of fluid fillable flexible fluid chambers being spaced on opposite sides of the helmet and configured to fill a space between the head and the outer shell when the helmet is positioned on the head. Impact resistant flexible pads are also inside the liner and are spaced around an inner circumference of the outer shell adjacent to each of the fluid fillable flexible fluid chambers. A flexible inner shell inside the liner is configured to fit closely on the head. The flexible fluid chambers are configured to compress in response to impacting of the helmet on an impact side and to force liquid through the fluid connections to inflate fluid chambers on an opposite side of the helmet thereby cushioning the head against a rebound impact on the opposite side.
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公开(公告)号:US08511504B2
公开(公告)日:2013-08-20
申请号:US13052862
申请日:2011-03-21
Applicant: Wayne H. Tuttle
Inventor: Wayne H. Tuttle
IPC: F17C2270/0197 , C23C16/06 , B64G1/40
CPC classification number: B64G1/402 , F02K9/605 , F05D2230/90 , F05D2300/133 , F05D2300/51 , F17C13/008 , F17C2201/0128 , F17C2201/054 , F17C2201/056 , F17C2203/0607 , F17C2203/0646 , F17C2203/0648 , F17C2203/0663 , F17C2209/221 , F17C2209/228 , F17C2221/08 , F17C2270/0194 , Y10T29/49888 , Y10T137/2931 , Y10T137/3127 , Y10T137/86212 , Y10T137/86348
Abstract: A demisable fuel supply system for a satellite includes a pressurized aluminum alloy tank with an aluminum alloy propellant management device therein. The propellant management device (PMD) can have any capillary action surface tension fluid transport features known in the art. Selected inner surfaces of the tank and the PMD are covered with a titanium based coating to guarantee propellant wettability and corrosion resistance of the fuel supply system.
Abstract translation: 卫星的可燃燃料供应系统包括其中具有铝合金推进剂管理装置的加压铝合金罐。 推进剂管理装置(PMD)可以具有本领域已知的任何毛细作用表面张力流体输送特性。 油箱和PMD的选定内表面均覆盖有钛基涂层,以确保燃油供应系统的推进剂润湿性和耐腐蚀性。
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公开(公告)号:US20120241355A1
公开(公告)日:2012-09-27
申请号:US13432618
申请日:2012-03-28
Applicant: Wayne H. Tuttle , David Adams , Marcial Alexander Anaya , Jeffry K. Pearson
Inventor: Wayne H. Tuttle , David Adams , Marcial Alexander Anaya , Jeffry K. Pearson
CPC classification number: F02K9/605 , B64G1/402 , F05D2230/312 , F05D2230/90 , F05D2260/95 , F05D2300/121 , F05D2300/133 , Y10T29/49982 , Y10T137/2931 , Y10T137/3127 , Y10T137/86212 , Y10T137/86348
Abstract: A demisable fuel supply system for a satellite includes a pressurized aluminum alloy tank with an aluminum alloy propellant management device therein. The propellant management device (PMD) can have any capillary action surface tension fluid transport features known in the art. Selected inner surfaces of the tank and the PMD are covered with a plasma powder sprayed titanium based coating to guarantee propellant wettability and corrosion resistance of the fuel supply system.
Abstract translation: 卫星的可燃燃料供应系统包括其中具有铝合金推进剂管理装置的加压铝合金罐。 推进剂管理装置(PMD)可以具有本领域已知的任何毛细作用表面张力流体输送特性。 罐体和PMD的内表面被等离子体喷涂的钛基涂层覆盖,以保证燃料供应系统的推进剂润湿性和耐腐蚀性。
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