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公开(公告)号：US07048228B2
公开(公告)日：2006-05-23
申请号：US10678474
申请日：2003-10-03
申请人： John C. Vassberg , Lie-Mine Gea , James D. McLean , David P. Witkowski , Steven E. Krist , Richard L. Campbell
发明人： John C. Vassberg , Lie-Mine Gea , James D. McLean , David P. Witkowski , Steven E. Krist , Richard L. Campbell
IPC分类号： B64C3/48
CPC分类号： B64C3/28 , B64C21/02 , B64C2003/149 , B64C2230/20 , Y02T50/12 , Y02T50/166
摘要： An aircraft wing includes a leading airfoil element and a trailing airfoil element. At least one slot is defined by the wing during at least one transonic condition of the wing. The slot may either extend spanwise along only a portion of the wingspan, or it may extend spanwise along the entire wingspan. In either case, the slot allows a portion of the air flowing along the lower surface of the leading airfoil element to split and flow over the upper surface of the trailing airfoil element so as to achieve a performance improvement in the transonic condition.
摘要翻译： 飞机机翼包括一个先导的翼型元件和一个后翼型元件。 在机翼的至少一个跨音速条件期间，机翼限定了至少一个槽。 狭槽可以沿翼展的翼展方向延伸，或者可以沿着整个翼展展开翼展。 在任一种情况下，狭槽允许空气沿着先导翼型元件的下表面流动的一部分分流并流过后翼型元件的上表面，从而在跨音速条件下实现性能改进。
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公开(公告)号：US5099685A
公开(公告)日：1992-03-31
申请号：US565802
申请日：1990-08-09
申请人： James D. McLean , Peter P. Sullivan
发明人： James D. McLean , Peter P. Sullivan
IPC分类号： G01M9/04
CPC分类号： G01M9/04
摘要： A wind tunnel having a test section and a fan section, interconnected by two passageways to form a recirculating air flow through said sections. There is a diffuser immediately downstream of the test section, and a second diffuser immediately downstream of the fan section. Each diffuser has an intermediate flow section where the side wall extends radially outwardly in a downstream direction at a relatively sharp angle. At the upstream end of the intermediate section there is a peripheral suction slot to draw in boundary layer air, and a by-pass passageway to discharge the air tangentially in a downstream location of the diffuser. This enables a substantial reduction in air velocity in a relatively short axial length.
摘要翻译： 具有测试部分和风扇部分的风洞，其通过两个通道互连以形成通过所述部分的再循环空气流。 在测试部分的下游有一个扩散器，紧邻风扇部分的下游的第二扩散器。 每个扩散器具有中间流动部分，其中侧壁以相对尖锐的角度沿下游方向径向向外延伸。 在中间部分的上游端有一个周边的抽吸槽，以便在边界层空气中进行抽吸，以及一个旁通通道，用于在扩散器的下游位置切向排出空气。 这使得能够在较短的轴向长度上显着降低空气速度。
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公开(公告)号：US20110073710A1
公开(公告)日：2011-03-31
申请号：US12566907
申请日：2009-09-25
CPC分类号： B64C21/10 , B29C65/4855 , B64C2230/26 , F15D1/12 , Y02T50/166 , Y10T156/1039
摘要： An array of aerodynamic riblets is formed with a surface layer for adhering to an aerodynamic surface and a plurality of riblet tips having a parabolic cross section extending from the surface layer.
摘要翻译： 空气动力肋阵列形成有用于粘附到空气动力学表面的表面层和具有从表面层延伸的抛物线横截面的多个肋尖。
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公开(公告)号：US07048235B2
公开(公告)日：2006-05-23
申请号：US10678397
申请日：2003-10-03
IPC分类号： B64C3/50
CPC分类号： B64C9/18 , B64C3/28 , B64C21/02 , B64C2003/149 , B64C2230/20 , Y02T50/12 , Y02T50/166 , Y02T50/32
摘要： A swept aircraft wing includes a leading airfoil element and a trailing airfoil element. At least one full-span slot is defined by the wing during at least one transonic condition of the wing. The full-span slot allows a portion of the air flowing along the lower surface of the leading airfoil element to split and flow over the upper surface of the trailing airfoil element so as to achieve a performance improvement in the transonic condition.
摘要翻译： 一架扫掠的飞机机翼包括一个先导的翼型元件和一个后翼型元件。 在机翼的至少一个跨音速条件期间，机翼定义至少一个全跨缝隙。 全跨缝隙允许沿着先导翼型元件的下表面流动的一部分空气分裂并流过后翼型元件的上表面，以便在跨音速条件下实现性能改进。
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5.发明授权Chromatography apparatus with electrochemical detector having carbon-black containing working electrode 失效具有电化学检测器的具有含碳黑色工作电极的色谱仪
公开(公告)号：US4343767A
公开(公告)日：1982-08-10
申请号：US252665
申请日：1981-04-09
CPC分类号： G01N27/4045 , G01N30/64
摘要： A flow-through electrochemical cell distinguished by the feature of a working electrode comprising selected carbon black powder(s) dispersed within an inert binder. An outstanding characteristic of the invention is the markedly improved signal/noise ratio of the electrode which enables a significant gain in the sensitivity level at which trace compounds can be detected. As an example of utility, as little as 5 to 30 parts per billion (ppb) of most phenolic compounds in water can be determined by liquid chromatographic separation of species and amperometric electrochemical detection, using the described flow-through cell to monitor the column effluent. No sample preparation is required.
摘要翻译： 一种流通电化学电池，其特征在于包含分散在惰性粘合剂中的选定的炭黑粉末的工作电极的特征。 本发明的突出特点是显着提高了电极的信号/噪声比，使得能够检测到痕量化合物的灵敏度水平显着增加。 作为效用的一个例子，通过物质的液相色谱分离和电流电化学检测可以确定水中大多数酚类化合物的百分之五至十十分之一（ppb），使用所描述的流通池来监测柱流出物 。 不需要样品制备。
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公开(公告)号：US4315609A
公开(公告)日：1982-02-16
申请号：US154235
申请日：1971-06-16
摘要： A target locating and missile guidance system comprising reconnaissance araft equipped with laser or radar range-measuring apparatus in conjunction with a plurality of selectively predetermined ground stations. Range and altitude of the aircraft relative to a detected surface target are obtained at two or more points on its flight path. The positions of the aircraft with respect to the ground stations are simultaneously determined by pulse-time-of-arrival technique. Using triangulation techniques the location of the target is determined with respect to a pulse grid coordinate system associated with the ground stations. At any time after the determination of the location of the target, properly timed signals from the ground stations or command signals based upon time-of-arrival data with respect to pulses from the missile are used to provide accurate guidance of the missile to the target.
摘要翻译： 一种目标定位和导弹引导系统，包括配备有多个选择性预定地面站的激光或雷达测距装置的侦察机。 在其飞行路径上的两个或更多个点处获得飞行器相对于检测到的表面目标的范围和高度。 飞机相对于地面站的位置同时由脉冲时间到达技术确定。 使用三角测量技术，相对于与地面站相关联的脉冲网格坐标系确定目标的位置。 在确定目标位置后的任何时间，使用来自地面站的适当定时信号或基于来自导弹的脉冲的到达时间数据的命令信号来提供对目标的导弹的精确指导 。
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公开(公告)号：USD260889S
公开(公告)日：1981-09-22
申请号：US297
申请日：1979-01-02
申请人： James D. McLean , David E. Snider
设计人： James D. McLean , David E. Snider
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公开(公告)号：US08413928B2
公开(公告)日：2013-04-09
申请号：US12566907
申请日：2009-09-25
CPC分类号： B64C21/10 , B29C65/4855 , B64C2230/26 , F15D1/12 , Y02T50/166 , Y10T156/1039
摘要： An array of aerodynamic riblets is formed with a surface layer for adhering to an aerodynamic surface and a plurality of riblet tips having a parabolic cross section extending from the surface layer.
摘要翻译： 空气动力肋阵列形成有用于粘附到空气动力学表面的表面层和具有从表面层延伸的抛物线横截面的多个肋尖。
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9.发明授权Efficient wing tip devices and methods for incorporating such devices into existing wing designs 有权有效的翼尖装置和将这些装置并入现有翼设计中的方法公开(公告)号：US06886778B2
公开(公告)日：2005-05-03
申请号：US10611212
申请日：2003-06-30
申请人： James D. McLean
发明人： James D. McLean
CPC分类号： B64C3/10 , B64C5/04 , B64C23/069 , Y02T50/12 , Y02T50/164
摘要： Efficient wing tip devices for use with aircraft wings. In one embodiment, an aircraft wing/winglet combination includes a wing having a wing root portion and a wing tip portion spaced apart from the wing root portion. The wing tip portion can have a wash-out twist relative to the wing root portion. The aircraft wing/winglet combination can further include a winglet extending from the wing tip portion of the wing. The winglet can be swept at least generally forward relative to the wing to favorably change the lift distribution on the wing and in turn reduce the induced drag on the wing.
摘要翻译： 用于飞机机翼的高效翼尖装置。 在一个实施例中，飞行器机翼/小翼组合包括具有翼根部分和与翼根部分间隔开的翼尖部分的翼。 翼尖部分可以相对于翼根部分具有洗出扭曲。 飞机机翼/小翼组合还可以包括从机翼的翼尖部分延伸的小翼。 小翼可以相对于机翼至少大致向前扫掠，以有利地改变机翼上的升力分布，从而减小机翼上的诱导阻力。
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公开(公告)号：US4440603A
公开(公告)日：1984-04-03
申请号：US389360
申请日：1982-06-17
CPC分类号： G01N27/4168
摘要： Liquids are monitored for dissolved halogens using amperometric detection based on the use of halogen specific electrodes of a conductive substrate on which is formed an adherent surface film of [Ti.sub.x (Ru, Ir).sub.1-x ]O.sub.2, wherein x=mole fraction .gtoreq.0 to
摘要翻译： 使用电导率检测基于使用导电基底的卤素特定电极（其上形成[Tix（Ru，Ir）1-x] O 2）的粘附表面膜，使用安培计检测来监测溶液，其中x =摩尔分数> / = 0至<1，（Ru，Ir）表示钌或铱或其混合物。 所描述的电极在极其恶劣的环境（例如热浓缩盐水溶液）中抵抗腐蚀和破坏。
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