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    • 5. 发明申请
    • NON-THERMAL PLASMA JET DEVICE AS SOURCE OF SPATIAL IONIZATION FOR AMBIENT MASS SPECTROMETRY AND METHOD OF APPLICATION
    • 非热等离子体喷射装置作为环境质谱法的空间离子源和应用方法
    • US20150262804A1
    • 2015-09-17
    • US14433008
    • 2013-10-07
    • Sandra MARTÍNEZ JARQUÍNRobert WINKLER
    • Sandra Martínez JarquínRobert Winkler
    • H01J49/10H05H1/24
    • H01J49/105H01J49/142H05H1/2406H05H2001/2437H05H2001/2443
    • The present invention relates to a non-thermal plasma jet device as spatial ionization source for ambient mass spectrometry of the type which allows a free adjustment of the geometry of the plasma beam, wherein the device comprises a double dielectric barrier probe of non-thermal plasma or NTP probe, which generates a non-thermal plasma jet; a high voltage and high frequency transformer circuit that connects an outer electrode through which it is possible to perform a discharge for the ionization of a gas which produces plasma, and wherein said plasma generator circuit is in turn connected to a source of AC power; an inner electrode which is grounded and allows to perform the discharge for the production of plasma; a storage tank of a gas serving as discharge gas; a test sample on which the non-thermal plasma jet is applied; and a ion transfer adapter to direct the ions produced by the device from the vacuum-free sample into a mass analyzer. The device described allows to directly analyzing live samples (plants, for example) without causing any damage to them.
    • 本发明涉及一种非热等离子体喷射装置,其是用于环境质谱的空间电离源,其允许自由调节等离子体束的几何形状,其中该装置包括非热等离子体的双电介质阻挡探针 或NTP探针,其产生非热等离子体射流; 高电压和高频变压器电路,其连接外部电极,通过该外部电极可以执行用于产生等离子体的气体的电离的放电,并且其中所述等离子体发生器电路又连接到AC电源; 内部电极接地并允许进行用于制造等离子体的放电; 用作放电气体的气体的储罐; 其上施加非热等离子体射流的测试样品; 以及离子转移适配器,用于将由装置产生的离子从无真空样品引导到质量分析器中。 所描述的装置允许直接分析活样品(例如植物)而不对它们造成任何损害。
    • 7. 发明授权
    • Treating remains containing sodium chloride and sodium sulphate
    • 处理含有氯化钠和硫酸钠的残留物
    • US3998709A
    • 1976-12-21
    • US615187
    • 1975-09-19
    • Robert Winkler
    • Robert Winkler
    • C01D3/08C01D5/16C25B15/08C25B1/16B01D1/00C25B1/26
    • C25B15/08C01D5/16
    • Method of dissolving out a sodium sulphate component of a residual product obtained upon evaporation and cooling of a sodium hydroxide solution originating from a diaphragm electrolysis, the product occuring in form of a crystallized salt mixture containing sodium chloride and sodium sulphate. First of all residues of the sodium hydroxide are removed from the product. Thereafter the mixture of sodium chloride and sodium sulphate is so slurried in water and treated that a maximum of the sodium chloride and a first part of the sodium sulphate are dissolved up to a solution being saturated of said two components while a second part of the sodium sulphate and a possible rest of the sodium chloride remain suspended. Whereafter the suspended solid substance is then separated from the sodium chloride-sodium sulphate mother brine.
    • 在蒸发和冷却源自隔膜电解的氢氧化钠溶液中得到的残留产物的硫酸钠组分溶解的方法,该产物以含有氯化钠和硫酸钠的结晶盐混合物的形式存在。 首先从产物中除去氢氧化钠的残留物。 此后,氯化钠和硫酸钠的混合物在水中如此浆化并经过处理,最大量的氯化钠和第一部分的硫酸钠被溶解到饱和所述两种组分的溶液中,而第二部分的钠 硫酸盐和可能的其余氯化钠保持悬浮。 然后将悬浮的固体物质与氯化钠 - 硫酸钠母体盐水分离。
    • 8. 发明申请
    • WING SLOT SEAL
    • US20140312575A1
    • 2014-10-23
    • US13376846
    • 2011-04-07
    • William D. BarryRobert WinklerJohn R. FranziniKenneth D. ClevelandAdam Butland
    • William D. BarryRobert WinklerJohn R. FranziniKenneth D. ClevelandAdam Butland
    • F16J15/00
    • F42B10/14F42B39/00
    • A low cost, lightweight frangible wing slot seal can be applied to a guidance wing slot of a folding fin aerial rocket or missile, providing a barrier against exposure of internal missile components to external contaminants, while allowing unhindered deployment of missile guidance wings simply by bursting through the seals. The simple design is nearly foolproof, and has no impact the likelihood of weapon. failure. The seal is a flexible sheet which is sufficiently thin so as not to exceed the required volume envelope of the missile. The sheet includes a burst seam, which is breached when impacted by the leading edge of a deploying wing. No additional wing deployment force is required, and after deployment the seal has minimal impact on the aerodynamic performance of the wing.
    • 低成本,轻量级的易碎翼槽密封件可应用于折叠式飞机空中火箭或导弹的引导翼槽,提供防止内部导弹部件暴露于外部污染物的屏障,同时允许简单地通过爆裂而不受阻挡地部署导弹引导翼 通过印章。 简单的设计几乎是万无一失的,对武器的可能性没有影响。 失败。 密封件是足够薄的柔性片材,以便不超过导弹的所需体积包络线。 该片材包括爆裂缝,当爆炸缝由部署翼的前缘撞击时,该缝隙被破坏。 不需要额外的机翼部署力,在部署之后,密封件对机翼的空气动力性能影响最小。
    • 10. 发明授权
    • Wing slot seal
    • 翼槽密封
    • US08895908B2
    • 2014-11-25
    • US13376846
    • 2011-04-07
    • William D. BarryRobert WinklerJohn R. FranziniKenneth D. ClevelandAdam Butland
    • William D. BarryRobert WinklerJohn R. FranziniKenneth D. ClevelandAdam Butland
    • F42B10/14B64D45/00F42B10/00
    • F42B10/14F42B39/00
    • A low cost, lightweight frangible wing slot seal can be applied to a guidance wing slot of a folding fin aerial rocket or missile, providing a barrier against exposure of internal missile components to external contaminants, while allowing unhindered deployment of missile guidance wings simply by bursting through the seals. The simple design is nearly foolproof, and has no impact the likelihood of weapon failure. The seal is a flexible sheet which is sufficiently thin so as not to exceed the required volume envelope of the missile. The sheet includes a burst seam, which is breached when impacted by the leading edge of a deploying wing. No additional wing deployment force is required, and after deployment the seal has minimal impact on the aerodynamic performance of the wing.
    • 低成本,轻量级的易碎翼槽密封件可应用于折叠式飞机空中火箭或导弹的导向翼槽,提供防止内部导弹部件暴露于外部污染物的屏障,同时允许简单地通过爆裂而不受阻挡地部署导弹引导翼 通过印章。 简单的设计几乎是万无一失的,对武器失效的可能性没有影响。 密封件是足够薄的柔性片材,以便不超过导弹的所需体积包络线。 该片材包括爆裂缝,当爆炸缝由部署翼的前缘撞击时,该缝隙被破坏。 不需要额外的机翼部署力,在部署之后,密封件对机翼的空气动力性能影响最小。