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    • 1. 发明授权
    • Method and apparatus for effecting fine control of aircraft velocity
    • 实现飞机速度精细控制的方法和装置
    • US4651958A
    • 1987-03-24
    • US651022
    • 1984-09-17
    • Joseph E. Zupanick
    • Joseph E. Zupanick
    • B64C9/32
    • B64C9/32B64C9/326Y02T50/32
    • In order to achieve fine control of the velocity of an aircraft flying a predetermined flight path at a predetermined nominal speed in the presence of such perturbations as wind gusts, a low inertia, fast acting device is extended or deployed into the aircraft dragstream and is rapidly position-modulated in response to sensed acceleration/deceleration to instantaneously slightly alter the total system drag to an amount which causes the aircraft to maintain the predetermined velocity. Among the exemplary alternative low inertia devices disclosed are: fuselage and wing mounted flaps which are rapidly more or less extended, a trailing cable which is rapidly reeled in or out, and a trailing inflatable member whose degree of inflation is rapidly changed, all in response to sensed acceleration/deceleration from an on-board system.
    • 为了在存在诸如阵风等扰动的情况下以预定的标称速度实现飞行预定飞行路径的飞行器的速度的精细控制,将低惯性快速作用的装置延伸或部署到飞行器的牵引流中并迅速地 响应于感测的加速/减速而进行位置调制,以瞬时轻微地将总系统拖动改变为导致飞行器保持预定速度的量。 所公开的示例性的替代性低惯量装置是:机身和机翼安装的翼片快速或多或少地延伸,快速卷入或离开的拖缆,以及充气程度迅速改变的拖尾充气构件,全部作为响应 以检测车载系统的加速/减速。
    • 2. 发明授权
    • Apparatus for determining the pulse repetition rate of a fluidic
oscillator through which a test gas is flowing
    • 用于确定测试气体通过其流动的流体振荡器的脉冲重复率的装置
    • US4175423A
    • 1979-11-27
    • US901884
    • 1978-05-01
    • Clarence BraunJoseph E. Zupanick
    • Clarence BraunJoseph E. Zupanick
    • G01N9/32G01N9/36
    • G01N9/32
    • In order to determine the pulse repetition rate of a fluidic oscillator through which a test gas, whose density is to be determined, is flowing, the pressure pulses appearing at one outlet port of the oscillator is sensed with a pressure transducer. The pulses are integrated for a sample period such that, upon transfer or display, the accumulated count directly represents the average pulse repetition frequency during the sample. Means are provided, in a surge tank, for controlling the temperature and pressure of the test gas, and temperature and pressure transducers in communication with the sample fluid in the surge tank are each coupled to voltage-to-frequency converters which drive counters in order that the temperature and pressure of the test gas may also be displayed. An interface to a thermal printer allows the preservation of written records of prf, temperature, and pressure readings. An interface to a digital tape recorder permits magnetic recording of the data for subsequent processing.
    • 为了确定流体振荡器的脉冲重复频率,通过该脉冲重复频率测定其密度要测量的测试气体正在流动,用压力传感器检测出现在振荡器的一个出口处的压力脉冲。 脉冲被集成为采样周期,使得在传送或显示时,累积计数直接表示样本期间的平均脉冲重复频率。 在缓冲罐中提供用于控制测试气体的温度和压力的装置,并且与缓冲罐中的样品流体连通的温度和压力传感器各自耦合到按顺序驱动计数器的电压 - 频率转换器 也可以显示测试气体的温度和压力。 热敏打印机的接口允许保存prf,温度和压力读数的书面记录。 数字磁带录音机的接口允许数据的磁记录用于后续处理。
    • 3. 发明授权
    • Method of and apparatus for disaggregating particulate matter
    • 分解颗粒物的方法和装置
    • US4070062A
    • 1978-01-24
    • US740895
    • 1976-11-11
    • George W. MorganJoseph E. Zupanick
    • George W. MorganJoseph E. Zupanick
    • B63B35/12B63B35/44E02B17/00
    • E02B17/0021B63B1/107B63B35/44B63B35/4413B63B2039/067B63B2211/06B63B35/12
    • A cutting-chipping system comprising an interconnected triaxial array of rotating drums each mounted for independent rotation. Each drum includes a plurality of spaced, outwardly extending teeth to sequentially cut, chip and break particulate mass such as coal or ice engaged by the system. The drums are oriented with no axis of drum rotation parallel to another and in a configuration wherein the direction of cutter travel from one drum is oblique to that of a second drum. In this manner, particulate matter engaged by the system is initially cut and chipped by a first drum to form a series of protuberances and/or weakened sections which, when struck at an oblique angle by a second drum, will chip and break away. The teeth may be comprised of picks, chisels or combinations thereof constructed and adapted for bidirectional rotation. The system may be adapted for applications upon land vehicles, water crafts, floating platforms, and the like. Variation in rotation velocity of the separate drums and/or opposing rotational directions thereof may then facilitate positional control of the system as well as depth and speed of cutting as necessitated by the particular application.
    • 一种切割碎片系统,包括每个安装用于独立旋转的旋转滚筒的互连三轴阵列。 每个鼓包括多个间隔开的向外延伸的齿,以顺序地切割,切碎和破碎由系统接合的煤或冰的颗粒物质。 滚筒被定向成没有鼓的旋转轴线平行于另一个滚筒,并且在其中切割器从一个滚筒行进的方向与第二滚筒的方向倾斜的配置中。 以这种方式,由系统接合的颗粒物质最初由第一滚筒切割并切碎,以形成一系列突起和/或弱化部分,当被第二滚筒以倾斜角撞击时,其将被切碎和脱落。 齿可以由构造和适于双向旋转的拾取器,凿子或其组合构成。 该系统可以适用于陆上车辆,水上工艺品,浮动平台等上的应用。 单独的滚筒和/或其相反的旋转方向的旋转速度的变化可以促进系统的位置控制以及特定应用所需的切割深度和速度。
    • 4. 发明授权
    • Method and apparatus for preventing fluid solidification in an aperture
    • 用于防止孔中流体凝固的方法和装置
    • US4043132A
    • 1977-08-23
    • US703865
    • 1976-07-09
    • Joseph E. Zupanick
    • Joseph E. Zupanick
    • G01C13/00E02B9/02
    • G01C13/006
    • A method of and apparatus for the installation and retrieval of instrumentation hardware supported through a hole in a section of ice is provided wherein an expansion member such as an inflatable bladder is utilized for displacing water normally subject to freezing within the hole. The inflatable bladder comprises an elongated expandable sleeve of sufficient length to substantially extend the ultimate depth of the hole in the ice for engaging and bearing against the sidewalls thereof. A portion of the hardware adapted for the surface support thereof may be disposed within the bladder as well as therebeneath and may be retrieved at a date subsequent to installation by deflating the bladder without the problem of said hardware being frozen in or beneath the ice. The configuration of the laterally expandable sleeve then permits structural interconnection from the top surface of the ice to the underneath side and communication with the environment therebeneath while providing lateral stability and preventing ice build-up which would adversely hinder its retrieval from the hole.
    • 提供了一种用于安装和回收通过冰段中的孔支撑的仪器硬件的方法和装置,其中使用诸如可膨胀囊的膨胀构件来移动通常在孔内冻结的水。 可膨胀气囊包括足够长度的细长可膨胀套管,以基本上延伸在冰中的孔的最终深度用于与其侧壁接合和支承。 适用于其表面支撑的硬件的一部分可以设置在膀胱内以及其下方,并且可以在安装之后的日期通过使气囊放气而被取回,而没有将所述硬件冻结在冰中或冰下的问题。 然后横向可膨胀套筒的构造允许从冰的顶部表面到下面的结构互连,并与其下方的环境连通,同时提供横向稳定性并防止积冰,这将不利地妨碍其从孔中取出。
    • 6. 发明授权
    • Method and apparatus for effecting fine control of aircraft velocity
    • 实现飞机速度精细控制的方法和装置
    • US4645144A
    • 1987-02-24
    • US808544
    • 1985-12-13
    • Joseph E. Zupanick
    • Joseph E. Zupanick
    • B64C9/32
    • B64C9/32B64C9/326Y02T50/32
    • In order to achieve fine control of the velocity of an aircraft flying a predetermined flight path at a predetermined nominal speed in the presence of such perturbations as wind gusts, a low inertia, fast acting device is extended or deployed into the aircraft dragstream and is rapidly position-modulated in response to sensed acceleration/deceleration to instanteneously slightly alter the total system drag to an amount which causes the aircraft to maintain the predetermined velocity. Among the exemplary alternative low inertia devices disclosed are: fuselage and wing mounted flaps which are rapidly more or less extended, a trailing cable which is rapidly reeled in or out, and a trailing inflatable member whose degree of inflation is rapidly changed, all in response to sensed acceleration/deceleration from an on-board system.
    • 为了在存在诸如阵风等扰动的情况下以预定的标称速度实现飞行预定飞行路径的飞行器的速度的精细控制,将低惯性快速作用的装置延伸或部署到飞行器的牵引流中并迅速地 响应于感测到的加速/减速而进行位置调制以便将总系统阻力瞬时稍微改变为导致飞行器保持预定速度的量。 所公开的示例性的替代性低惯量装置是:机身和机翼安装的翼片快速或多或少地延伸,快速卷入或离开的拖缆,以及充气程度迅速改变的拖尾充气构件,全部作为响应 以检测车载系统的加速/减速。
    • 8. 发明授权
    • Luminescense and reflectance detection radiometer with changeable
optical assembly
    • 具有可变光学组件的Luminescense和反射率检测辐射计
    • US4671662A
    • 1987-06-09
    • US746050
    • 1985-06-18
    • Joseph E. ZupanickCarl D. McBride
    • Joseph E. ZupanickCarl D. McBride
    • G01N21/64G02B27/10
    • G02B27/108G01N21/645G02B27/143G01N2021/6426G01N2021/6463G01N2201/0616
    • The present invention provides a radiometer for simultaneously detecting luminescence and reflectance about a particular Fraunhofer line from a material (i.e. target) which includes an interchangeable optical filter assembly of lightweight construction for each Fraunhofer line of interest which substantially alleviates the adverse polarization effects normally experienced in radiometers of this type and which further provides an improved balance between the two light beams being sensed by the radiometer. The optical filter assembly includes a single beamsplitter which reflects the majority of the light from the target with little adverse polarization effects to a narrow band filter which passes only the light existing at the particular Fraunhofer line (i.e. "c" component of luminescence). The remaining smaller fraction of the light passes through the beamsplitter with only slightly greater polarization to a broad band filter which, in turn, passes only the light in the continuums adjacent the Fraunhofer line (i.e. "d" component of luminescence). The intensity of the light from the narrow and broad band filters are measured for use in calculating the luminescence and reflectance emanating from the target.
    • 本发明提供了一种辐射计,用于从材料(即目标)同时检测关于特定弗劳恩霍夫线的发光和反射率,该材料包括用于每个Fraunhofer感兴趣线路的轻质结构的可互换光学滤光器组件,其基本上减轻了通常在 这种类型的辐射计,并且进一步提供了由辐射计感测的两个光束之间的改善的平衡。 滤光器组件包括单个分束器,其将来自目标的大部分光从具有很小的不利极化效应的窄带滤光器反射,窄带滤光器只通过在特定的弗劳恩霍夫线(即“c”分量的发光)处存在的光。 剩余的较小分数的光通过分光器,仅具有稍微更大的偏振度到宽带滤光器,该宽带滤光器又仅穿过邻近弗劳恩霍夫线(即“d”发光分量)的连续体中的光。 测量来自窄带和宽带滤光器的光的强度用于计算从目标发出的发光和反射。
    • 10. 发明授权
    • Means, employing a fluidic oscillator, for determining the density of gas
    • 意味着采用流体振荡器来确定气体的密度
    • US4170894A
    • 1979-10-16
    • US901536
    • 1978-05-01
    • Joseph E. Zupanick
    • Joseph E. Zupanick
    • G01N9/00
    • G01N9/002G01N2009/004Y10T137/2065
    • In order to determine the density of a test gas, the test gas is employed as the working fluid through an astable fluidic oscillator. Air, at the same temperature and pressure, is passed through the same or a like fluidic oscillator to obtain a second pulse repetition frequency reading. The density of the test gas is the ratio of the two pulse repetition frequencies. Preferably, for a given fluidic oscillator, graphs and/or tables are prepared giving the pulse repetition frequency of air at different temperatures and pressures in order that subsequent measurement of the pulse repetition frequency using a test gas will permit direct determination of the specific gravity of the test gas from a graph or table.
    • 为了确定试验气体的密度,通过不稳定的流体振荡器将测试气体用作工作流体。 在相同温度和压力下的空气通过相同或类似的流体振荡器以获得第二脉冲重复频率读数。 测试气体的密度是两个脉冲重复频率之比。 优选地,对于给定的流体振荡器,制备给出不同温度和压力下的空气的脉冲重复频率的曲线图和/或表格,以便使用测试气体随后测量脉冲重复频率将允许直接确定比重 来自图表或表格的测试气体。