In situ tumor temperature profile measuring probe and method
    11.
    发明授权
    In situ tumor temperature profile measuring probe and method 失效
    原位肿瘤温度曲线测量探针和方法

    公开(公告)号:US06916290B2

    公开(公告)日:2005-07-12

    申请号:US10090576

    申请日:2002-03-05

    CPC classification number: A61B5/01

    Abstract: An in situ breast tumor temperature profile measuring probe includes a rod, thermal sensors and electrical output leads. The thermal sensors are formed in spaced apart holes in an outer insulating layer of the rod and a common electrical input lead to provide an electrical input signal to the thermal sensors is disposed below and has portions exposed at the holes and electrically connected to the thermal sensors. The thermal sensors receive the electrical input signal from the common electrical input lead, sense the temperature of biological matter adjacent to the thermal sensors and produce an electrical output signal correlated thereto. Each electrical output lead mounted to the outer insulating layer is in electrical contact with a different one of the thermal sensors to receive the electrical output signal from the one thermal sensor and output the same.

    Abstract translation: 原位乳腺肿瘤温度剖面测量探头包括杆,热传感器和电输出引线。 热传感器形成在杆的外部绝缘层中的间隔开的孔中,并且公共电输入引线提供到热传感器的电输入信号设置在下方并且具有暴露在孔处的部分并电连接到热传感器 。 热传感器接收来自公共电输入引线的电输入信号,感测与热传感器相邻的生物物质的温度,并产生与之相关的电输出信号。 安装到外绝缘层的每个电输出引线与不同的一个热传感器电接触,以接收来自一个热传感器的电输出信号并输出​​。

    Single sided laser shock peening
    12.
    发明授权
    Single sided laser shock peening 失效
    单面激光冲击硬化

    公开(公告)号:US06559415B1

    公开(公告)日:2003-05-06

    申请号:US10195095

    申请日:2002-07-12

    CPC classification number: F01D5/286 C21D10/005

    Abstract: A method for single sided laser shock peening an article includes laser shock peening a laser shock peening surface on a first side of the article while maintaining an opposite second surface on a back side of the article in acoustic communication with a shock attenuating material. The second surface is opposite the laser shock peening surface. The shock attenuating material is a material that does not allow tensile waves to be reflected back off the back side through the article. The shock attenuating material may be a liquid metal and the article made from a titanium alloy. One such article is a gas turbine engine airfoil of an integrally bladed disk and the surfaces may be on an edge of the airfoil. The shock attenuating material may be one that dissipates compressive waves or reflects back compressive shock waves caused by the laser shock peening.

    Abstract translation: 用于单面激光冲击硬化物品的方法包括在制品的第一侧上激光冲击硬化激光冲击硬化表面,同时保持与冲击衰减材料声学连通的制品背面上的相对的第二表面。 第二个表面与激光冲击喷丸表面相对。 冲击衰减材料是不允许拉伸波从背面反射穿过物品的材料。 冲击衰减材料可以是液态金属,并且由钛合金制成的制品。 一个这样的物品是整体叶片盘的燃气涡轮发动机翼型,并且表面可以在翼型的边缘上。 冲击衰减材料可以是消除压缩波或反射由激光冲击喷丸引起的压缩冲击波的材料。

    Combined burner and grate
    14.
    发明授权
    Combined burner and grate 失效
    组合燃烧器和炉排

    公开(公告)号:US06435173B1

    公开(公告)日:2002-08-20

    申请号:US09691743

    申请日:2000-10-18

    CPC classification number: F24C15/10 F23D2900/14042

    Abstract: A combined burner and grate structure for use in connection with a gas range includes one or more burner elements. Each burner element has one or more fuel inlets, one or more fuel outlets disposed on one or more side surfaces, and a top surface. A horizontal planar support for a cooking vessel is made up of the top surface of each burner element. A gas rangetop can include one or more of these combined burner and grate structures.

    Abstract translation: 用于与气体范围相结合的组合式燃烧器和炉排结构包括一个或多个燃烧器元件。 每个燃烧器元件具有一个或多个燃料入口,设置在一个或多个侧表面上的一个或多个燃料出口和顶表面。 用于烹饪容器的水平平面支撑件由每个燃烧器元件的顶表面构成。 气体顶部可以包括这些组合的燃烧器和炉排结构中的一个或多个。

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