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公开(公告)号：US08536502B2
公开(公告)日：2013-09-17
申请号：US13430678
申请日：2012-03-26
摘要： A vehicle for launching from a gas gun having a housing; preferably incorporating a precessional attitude control system; and utilizing a flared base, fins, or active use of the attitude control system during passage through the atmosphere. Subtly canting the fins can produce desired spinning of the vehicle. The propulsion system can employ liquid, hybrid, or solid fuel. A removable aero-shell assists atmospheric flight with thermal protection being provided by anticipated ablation, an ablative aero-spike, or transpirational cooling. And a releasable sabot enhances the effectiveness of the launch.
摘要翻译： 用于从具有外壳的气枪发射的车辆; 优选地包括进动姿态控制系统; 并且在通过大气的过程中利用喇叭形底座，翅片或主动使用姿态控制系统。 细小的鳍片可以产生所需的车辆旋转。 推进系统可以采用液体，混合或固体燃料。 可移动的航空壳可以帮助大气飞行，通过预期的消融，消融空气尖峰或蒸气冷却提供热保护。 并且可释放的sabot增强了发射的有效性。
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公开(公告)号：US08979033B2
公开(公告)日：2015-03-17
申请号：US13430671
申请日：2012-03-26
摘要： A gas gun launcher having a pump tube and a launch tube with a first end of the launch tube slidably inserted into a second end of the pump tube. A sliding seal is employed to retain the gas within the launch tube and the pump tube A launch tube alignment system is preferably automatic, again to enhance the accuracy of launches. And an embodiment of the gas gun launcher suitable for use in water such as an ocean or large lake preferably utilizes a neutrally buoyant launch tube and a neutrally buoyant pump tube. And a fast-closing muffler at the second end of the launch tube conserves the light gas utilized for launching a vehicle.
摘要翻译： 一种具有泵管和发射管的气枪发射器，其中发射管的第一端可滑动地插入泵管的第二端。 使用滑动密封件将气体保持在发射管内，并且泵管A发射管对准系统优选地是自动的，以再次提高发射的准确性。 适用于诸如海洋或大型湖泊的水中的气枪发射器的实施例优选利用中性浮力发射管和中性浮力泵管。 而发射管第二端的快关消声器节省了用于发射车辆的轻型气体。
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公开(公告)号：US20120175457A1
公开(公告)日：2012-07-12
申请号：US13430678
申请日：2012-03-26
摘要： A vehicle for launching from a gas gun having a housing; preferably incorporating a precessional attitude control system; and utilizing a flared base, fins, or active use of the attitude control system during passage through the atmosphere. Subtly canting the fins can produce desired spinning of the vehicle. The propulsion system can employ liquid, hybrid, or solid fuel. A removable aero-shell assists atmospheric flight with thermal protection being provided by anticipated ablation, an ablative aero-spike, or transpirational cooling. And a releasable sabot enhances the effectiveness of the launch.
摘要翻译： 用于从具有外壳的气枪发射的车辆; 优选地包括进动姿态控制系统; 并且在通过大气的过程中利用喇叭形底座，翅片或主动使用姿态控制系统。 细小的鳍片可以产生所需的车辆旋转。 推进系统可以采用液体，混合或固体燃料。 可移动的航空壳可以帮助大气飞行，通过预期的消融，消融空气尖峰或蒸气冷却提供热保护。 并且可释放的sabot增强了发射的有效性。
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公开(公告)号：US20120187249A1
公开(公告)日：2012-07-26
申请号：US13430671
申请日：2012-03-26
摘要： A gas gun launcher having a pump tube and a launch tube with a first end of the launch tube slidably inserted into a second end of the pump tube. A sliding seal is employed to retain the gas within the launch tube and the pump tube A launch tube alignment system is preferably automatic, again to enhance the accuracy of launches. And an embodiment of the gas gun launcher suitable for use in water such as an ocean or large lake preferably utilizes a neutrally buoyant launch tube and a neutrally buoyant pump tube. And a fast-closing muffler at the second end of the launch tube conserves the light gas utilized for launching a vehicle.
摘要翻译： 一种具有泵管和发射管的气枪发射器，其中发射管的第一端可滑动地插入泵管的第二端。 使用滑动密封件将气体保持在发射管内，并且泵管A发射管对准系统优选地是自动的，以再次提高发射的准确性。 适用于诸如海洋或大型湖泊的水中的气枪发射器的实施例优选利用中性浮力发射管和中性浮力泵管。 而发射管第二端的快关消声器节省了用于发射车辆的轻型气体。
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公开(公告)号：US06536350B2
公开(公告)日：2003-03-25
申请号：US09799572
申请日：2001-03-07
申请人： Harry E. Cartland , John W. Hunter
发明人： Harry E. Cartland , John W. Hunter
IPC分类号： F42B1500
摘要： A propulsion-assisted projectile has a body, a cowl forming a combustion section and a nozzle section. The body has a fuel reservoir within a central portion of the body, and a fuel activation system located along the central axis of the body and having a portion of the fuel activation system within the fuel reservoir. The fuel activation system has a fuel release piston with a forward sealing member where the fuel release piston is adapted to be moved when the forward sealing member is impacted with an air flow, and an air-flow channel adapted to conduct ambient air during flight to the fuel release piston.
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6.发明授权
公开(公告)号：US6015969A
公开(公告)日：2000-01-18
申请号：US8234
申请日：1998-01-16
申请人： Howard Nathel , Harry E. Cartland , Billy W. Colston, Jr. , Matthew J. Everett , Jeffery N. Roe
发明人： Howard Nathel , Harry E. Cartland , Billy W. Colston, Jr. , Matthew J. Everett , Jeffery N. Roe
CPC分类号： G01N21/314
摘要： An oxygen concentration measurement system for blood hemoglobin comprises a multiple-wavelength low-coherence optical light source that is coupled by single mode fibers through a splitter and combiner and focused on both a target tissue sample and a reference mirror. Reflections from both the reference mirror and from the depths of the target tissue sample are carried back and mixed to produce interference fringes in the splitter and combiner. The reference mirror is set such that the distance traversed in the reference path is the same as the distance traversed into and back from the target tissue sample at some depth in the sample that will provide light attenuation information that is dependent on the oxygen in blood hemoglobin in the target tissue sample. Two wavelengths of light are used to obtain concentrations. The method can be used to measure total hemoglobin concentration [Hb.sub.deoxy +Hb.sub.oxy ] or total blood volume in tissue and in conjunction with oxygen saturation measurements from pulse oximetry can be used to absolutely quantify oxyhemoglobin [HbO.sub.2 ] in tissue. The apparatus and method provide a general means for absolute quantitation of an absorber dispersed in a highly scattering medium.
摘要翻译： 用于血液血红蛋白的氧浓度测量系统包括多波长低相干光学光源，其由单模光纤通过分离器和组合器耦合并聚焦在目标组织样本和参考反射镜两者上。 来自参考镜和来自目标组织样本的深度的反射被携带并混合以在分离器和组合器中产生干涉条纹。 参考镜被设置为使得在参考路径中穿过的距离与在样本中的某个深度处从目标组织样本穿过的距离相同，其将提供取决于血液血红蛋白中的氧的光衰减信息 在目标组织样本中。 使用两个波长的光来获得浓度。 该方法可用于测量组织中总血红蛋白浓度[Hbdeoxy + Hboxy]或总体积，并结合脉搏血氧饱和度测量结果，可用于绝对量化组织中的氧合血红蛋白[HbO2]。 该装置和方法提供了用于绝对定量分散在高度散射介质中的吸收体的一般手段。
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