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公开(公告)号：US07891605B2
公开(公告)日：2011-02-22
申请号：US12047833
申请日：2008-03-13
CPC分类号： B64D41/00 , B64D2041/002 , B64D2221/00
摘要： Systems and methods for operating aircraft power systems are disclosed. A power system in accordance with one embodiment of the invention includes an aircraft auxiliary power unit and a controller coupled to the aircraft auxiliary power unit, with the controller being configured to automatically stop the auxiliary power unit while the auxiliary power unit is functioning normally. The controller can also be configured to automatically start the auxiliary power unit in-flight when power supplied or expected to be supplied to a subsystem of the aircraft has a non-zero value at or below a threshold value. The controller may also be configured to start the auxiliary power unit when a load or expected load on the subsystem meets or exceeds a threshold value.
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公开(公告)号：US07564549B2
公开(公告)日：2009-07-21
申请号：US11745779
申请日：2007-05-08
申请人： Thomas A. Campbell , Kent D. Henry
发明人： Thomas A. Campbell , Kent D. Henry
IPC分类号： G01J3/44
CPC分类号： B82Y40/00 , B82Y30/00 , C01B32/152 , C01B32/17 , C01B32/172 , C01B2202/02 , G01J3/1804 , G01J3/36 , G01J3/44 , G01J5/34 , G01N21/65
摘要： The present invention provides systems and methods for quantifying, purifying and separating fullerenes, such as single wall carbon nanotubes (SWNTs). The purification/separation combination provides nearly 100% carbonaceous impurity-free SWNT content from a given impure sample and provides a desired chirality and diameter from a given non-separated sample. Nanometrological validation of the success of purification and separation uses a pyroelectric detector and Raman spectroscopy in a single system, thus providing a critical aspect for the nanomanufacturing environment. The purification/separation and nanometrological validations may be performed in a feedback loop to provide a satisfactorily refined sample and optimized purification/separation settings.
摘要翻译： 本发明提供了定量，纯化和分离富勒烯如单壁碳纳米管（SWNT）的系统和方法。 纯化/分离组合从给定的不纯样品提供近100％含碳杂质的SWNT含量，并从给定的非分离样品提供所需的手性和直径。 纯化和分离成功的纳米学验证在单一系统中使用热释电检测器和拉曼光谱，从而为纳米制造环境提供了关键方面。 纯化/分离和纳米体系验证可以在反馈回路中进行，以提供令人满意的精制样品和优化的纯化/分离设置。
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13.发明申请Automatic Control Systems for Aircraft Auxiliary Power Units, and Associated Methods 有权飞机辅助动力装置自动控制系统及相关方法公开(公告)号：US20090037036A1
公开(公告)日：2009-02-05
申请号：US12047833
申请日：2008-03-13
IPC分类号： F02C7/00
CPC分类号： B64D41/00 , B64D2041/002 , B64D2221/00
摘要： Systems and methods for operating aircraft power systems are disclosed. A power system in accordance with one embodiment of the invention includes an aircraft auxiliary power unit and a controller coupled to the aircraft auxiliary power unit, with the controller being configured to automatically stop the auxiliary power unit while the auxiliary power unit is functioning normally. The controller can also be configured to automatically start the auxiliary power unit in-flight when power supplied or expected to be supplied to a subsystem of the aircraft has a non-zero value at or below a threshold value. The controller may also be configured to start the auxiliary power unit when a load or expected load on the subsystem meets or exceeds a threshold value.
摘要翻译： 公开了用于操作飞机动力系统的系统和方法。 根据本发明的一个实施例的电力系统包括飞行器辅助动力单元和耦合到飞行器辅助动力单元的控制器，其中控制器被配置为在辅助动力单元正常运行时自动停止辅助动力单元。 控制器还可以被配置为在供电或期望提供给飞行器的子系统的电源具有等于或小于阈值的非零值时，在飞行中自动启动辅助电源单元。 控制器还可以被配置为在子系统上的负载或预期负载满足或超过阈值时启动辅助电源单元。
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公开(公告)号：US5703593A
公开(公告)日：1997-12-30
申请号：US571001
申请日：1995-12-12
IPC分类号： G01S13/44 , G01S13/524 , G01S13/72 , G01S13/534
CPC分类号： G01S13/4472 , G01S13/5242 , G01S13/449 , G01S13/5244 , G01S13/726
摘要： An ADPCA subsystem includes a weight processor for weighting the delta channel signal according to the results of an adaptive algorithm to which the output of a DPCA vector combiner is input. An AMTI vector combiner is connected to the output of the DPCA vector combiner to form the filter output. The delta channel signal is time delayed and samples of the delta channel signal are collected by the processor together with a sum channel sample and a residue sample, in order to apply the proper weights to the undelayed and delayed delta channel samples. The output of the ADPCA weight processor therefore provides an optimum correction signal to the vector combiner.
摘要翻译： ADPCA子系统包括权重处理器，用于根据输入DPCA矢量组合器的输出的自适应算法的结果对增量信道信号进行加权。 AMTI矢量组合器连接到DPCA矢量组合器的输出端以形成滤波器输出。 Δ信道信号是时间延迟的，并且Δ信道信号的样本由处理器与和信道样本和残差采样一起收集，以便将适当的权重应用于未延迟和延迟的三角形信道样本。 因此，ADPCA加权处理器的输出为矢量组合器提供最佳校正信号。
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公开(公告)号：US20110313298A1
公开(公告)日：2011-12-22
申请号：US13203800
申请日：2010-03-01
CPC分类号： A61B18/203 , A61B5/0059 , A61B5/0066 , A61B5/0084 , A61B5/411 , A61B5/442 , A61B5/444 , A61B5/685 , A61B2018/00452 , A61N5/0616 , A61N2005/0631 , A61N2005/067 , G02B6/032 , G02B6/06 , G02B6/262
摘要： The present invention relates to the field of optical imaging and therapeutics. More particularly, embodiments of the present invention provide minimally-invasive Fiberoptic Microneedle Devices (FMDs) for light-based therapeutics, which physically penetrate tissue and deliver light directly into the target area below the skin surface (FIG. 1). A preferred embodiment of the invention is a fiberoptic microneedle device comprising: (a) one or more silica-based needles capable of guiding light and comprising a length of about 0.5-6 mm, a base having an outer diameter in the range of about 100-150 micron, and a tip having an outer diameter in the range of about 5-20 micron; (b) a support member to which the needles are secured; (c) a ferrule comprising one or more holes for each of the needles, wherein the ferrule is operably configured to provide mechanical support to each needle at all or some portion of the length of the needle. Embodiments of the invention enable depth-selective and deep photothermal therapeutics and can be adapted for use with any laser-based treatment or diagnostic in which light is used to detect or treat targets under or on the skin surface.
摘要翻译： 本发明涉及光学成像和治疗领域。 更具体地说，本发明的实施例提供了用于基于光的治疗剂的微创光纤微针装置（FMD），其物理地穿透组织并将光直接传送到皮肤表面下方的目标区域（图1）。 本发明的优选实施例是一种光纤微针装置，包括：（a）一个或多个能够引导光并且包括约0.5-6mm的长度的基于二氧化硅的针，具有约100的外径的基部 -150微米，以及外径在约5-20微米范围内的尖端; （b）固定针的支撑构件; （c）套圈，其包括用于每个针的一个或多个孔，其中所述套圈可操作地构造成在所述针的所述长度的全部或某一部分处为每个针提供机械支撑。 本发明的实施方案可实现深度选择性和深度光热治疗剂，并且可适用于任何基于激光的治疗或诊断，其中光用于检测或治疗皮肤表面下或皮肤表面上的靶标。
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16.发明授权Automatic control systems for aircraft auxiliary power units, and associated methods 有权飞机辅助动力装置自动控制系统及相关方法公开(公告)号：US07364116B2
公开(公告)日：2008-04-29
申请号：US10951185
申请日：2004-09-27
IPC分类号： B64D41/00
CPC分类号： B64D41/00 , B64D2041/002 , B64D2221/00
摘要： Systems and methods for operating aircraft power systems are disclosed. A power system in accordance with one embodiment of the invention includes an aircraft auxiliary power unit and a controller coupled to the aircraft auxiliary power unit, with the controller being configured to automatically stop the auxiliary power unit while the auxiliary power unit is functioning normally. The controller can also be configured to automatically start the auxiliary power unit in-flight when power supplied or expected to be supplied to a subsystem of the aircraft has a non-zero value at or below a threshold value. The controller may also be configured to start the auxiliary power unit when a load or expected load on the subsystem meets or exceeds a threshold value.
摘要翻译： 公开了用于操作飞机动力系统的系统和方法。 根据本发明的一个实施例的电力系统包括飞行器辅助动力单元和耦合到飞行器辅助动力单元的控制器，其中控制器被配置为在辅助动力单元正常运行时自动停止辅助动力单元。 控制器还可以被配置为在供电或期望提供给飞行器的子系统的电源具有等于或小于阈值的非零值时，在飞行中自动启动辅助电源单元。 控制器还可以被配置为在子系统上的负载或预期负载满足或超过阈值时启动辅助电源单元。
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公开(公告)号：US07344107B2
公开(公告)日：2008-03-18
申请号：US10974167
申请日：2004-10-26
IPC分类号： B64D41/00
CPC分类号： F02C7/04 , B64D41/00 , B64D2033/0213 , B64D2041/002 , F02C6/06 , F02C7/042 , Y02T50/44 , Y02T50/671 , Y10T137/0536
摘要： Dual flow auxiliary power unit (APU) inlets and associated systems and methods are disclosed. An inlet in accordance with one embodiment of the invention includes an entrance aperture and a divider positioned in the inlet and located to separate a first portion of the inlet from a second portion of the inlet. The first portion can be configured to couple to an engine air intake of an APU, and the second portion can be configured to direct air away from the air intake. The divider can be positioned to direct air having a first total pressure level and a first distortion level to the first portion of the inlet, and direct air having a second total pressure level and second distortion level to the second portion of the inlet. The first total pressure level can be approximately the same as or higher than the second total pressure level, or the second distortion level can be approximately the same as or higher than the first distortion level, or both.
摘要翻译： 公开了双流辅助动力单元（APU）入口及相关系统和方法。 根据本发明的一个实施例的入口包括入口孔和分隔件，其定位在入口中并且定位成将入口的第一部分与入口的第二部分分开。 第一部分可以被配置成联接到APU的发动机进气口，并且第二部分可被配置成将空气引导离开进气口。 分隔器可以定位成将具有第一总压力水平和第一失真水平的空气引导到入口的第一部分，并且具有第二总压力水平和第二失真水平的直接空气到入口的第二部分。 第一总压力水平可以大致等于或高于第二总压力水平，或者第二失真水平可以大致等于或高于第一失真水平，或两者。
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18.发明授权Integrated axially varying engine muffler, and associated methods and systems 有权集成轴向变化的发动机消声器，以及相关的方法和系统公开(公告)号：US07267297B2
公开(公告)日：2007-09-11
申请号：US10934065
申请日：2004-09-02
IPC分类号： B64D33/04
CPC分类号： F02K1/827 , B64D33/06 , B64D41/00 , B64D2041/002 , Y02T50/671
摘要： Integrated axially varying engine mufflers, and associated methods and systems. An arrangement in accordance with one embodiment of the invention includes a tailcone having a tapering external surface, a cavity disposed within the surface, and an engine muffler disposed within the cavity. The engine muffler can have a tapering outer surface, a porous inner surface disposed inwardly from the outer surface, and a plurality of cells disposed between the outer surface and the inner surface in fluid communication with the perforations of the inner surface. The inner surface can be positioned adjacent to an exhaust gas flow path having an entrance aperture and an exit aperture. Cells positioned toward the entrance aperture can have a first dimension extending away from the gas path, and cells positioned toward the exit aperture can have a second, different, dimension extending away from the exhaust gas path. Accordingly, the tapered muffler can be integrated with the tapered tailcone, and can provide sounds attenuation over a range of frequencies.
摘要翻译： 集成轴向变化的发动机消声器，以及相关的方法和系统。 根据本发明的一个实施例的装置包括具有锥形外表面的尾管，设置在表面内的空腔和设置在腔内的发动机消声器。 发动机消声器可以具有锥形的外表面，从外表面向内设置的多孔内表面，以及设置在外表面和内表面之间的与内表面的穿孔流体连通的多个单元。 内表面可以邻近具有入口孔和出口孔的废气流动路径定位。 朝向入口孔定位的细胞可以具有远离气体路径延伸的第一尺寸，并且朝向出口孔定位的细胞可以具有远离废气路径延伸的第二不同的尺寸。 因此，锥形消音器可以与锥形尾音一体化，并且可以在一定频率范围内提供声音衰减。
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19.发明授权Method of detecting axonal damage, from associated disease states using tau monoclonal antibodies 失效使用tau单克隆抗体从相关疾病状态检测轴突损伤的方法公开(公告)号：US06797478B1
公开(公告)日：2004-09-28
申请号：US09035708
申请日：1998-03-05
IPC分类号： G08N3353
CPC分类号： C07K16/18
摘要： Patients having several neurological diseases have been shown to have elevated levels of axonally-derived proteins (i.e. tau and neurofilament proteins) in cerebrospinal fluid (CSF) and in brain tissue. Three monoclonal antibodies (MAbs) recognizing CSF tau proteins were developed. The Mabs were found to label a ladder of 30 kD to 50 kD tau proteins in CSF from patients with disease states producing axonal damage such as head trauma or CNS tumor but not in CSF from controls. High levels of tau protein in CSF were shown to be diagnostic of axonal degeneration in head trauma. An ELISA assay was developed with these MAbs to aid in the diagnosis of patients with axonal damage.
摘要翻译： 具有几种神经系统疾病的患者已被证明在脑脊液（CSF）和脑组织中具有升高的轴突衍生蛋白（即tau和神经丝蛋白）水平。 开发了识别CSF tau蛋白的三种单克隆抗体（MAb）。 发现Mab在患有CSF产生轴突损伤（例如头部创伤或CNS肿瘤）的患者的CSF中标记30kD至50kD tau蛋白的梯度，而在对照组中的CSF中未标记。 CSF中高水平的tau蛋白显示是头部创伤中轴突变性的诊断。 使用这些MAb开发ELISA测定以帮助诊断具有轴突损伤的患者。
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