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    • 27. 发明授权
    • Ultrasonic inspection method and system for detecting critical flaws
    • 检测关键缺陷的超声波检测方法及系统
    • US06408695B1
    • 2002-06-25
    • US09454189
    • 1999-12-03
    • Bernard Patrick BewlayJohn Broddus Deaton, Jr.Michael Francis Xavier Gigliotti, Jr.Robert Snee Gilmore
    • Bernard Patrick BewlayJohn Broddus Deaton, Jr.Michael Francis Xavier Gigliotti, Jr.Robert Snee Gilmore
    • G01N332
    • G01N29/348G01N29/11G01N2291/015G01N2291/02458G01N2291/2693
    • An ultrasonic inspection method for inspecting titanium material is provided. The ultrasonic inspection method is capable of detecting critical flaws in the titanium material that may limit titanium material applications. The ultrasonic inspection method comprises fixing at least one of frequency or acoustic entity size of the titanium material as a constant for the ultrasonic inspecting; wherein the frequency that is fixed is selected based on the size of the flaws deemed critical for mechanical performance—including fatigue performance—in the titanium material, and the grain size that is fixed selected based on the size of the flaws deemed critical for mechanical performance—including fatigue performance—in the titanium material; ultrasonic inspecting the titanium material in which the step of ultrasonic inspecting the titanium material generates scattering from microstructural characteristics and features of the titanium material; detecting generated scattering; characterizing the type of detected scattering; and determining if the titanium material comprises critical flaws based on the type of scattering. If the scattering comprises predominantly Rayleigh scattering, the step of determining determines that the titanium material comprises uniform-fine grain titanium, however, if the scattering comprises Rayleigh scattering and other types of scattering, the step of determining determines that the titanium material may comprise critical flaws that may limit applications of the titanium material. The invention also provides a system for implementing the method, as embodied by the invention.
    • 提供了用于检查钛材料的超声检查方法。 超声波检测方法能够检测可能限制钛材料应用的钛材料的临界缺陷。 超声波检查方法包括将钛材料的频率或声学实体尺寸中的至少一个固定为超声波检查的常数; 其中固定的频率基于对钛材料的机械性能(包括疲劳性能)至关重要的缺陷的尺寸和基于对于机械性能至关重要的缺陷尺寸而选择的晶粒尺寸进行选择 - 包括疲劳性能 - 钛材料; 超声波检查钛材料的超声波检测步骤从钛材料的显微组织特征和特征产生散射的钛材料; 检测产生的散射; 表征检测到的散射的类型; 以及确定钛材料是否包括基于散射类型的关键缺陷。 如果散射主要包括瑞利散射,则确定步骤确定钛材料包含均匀细晶粒钛,然而,如果散射包括瑞利散射和其它类型的散射,则确定步骤确定钛材料可能包括关键的 可能限制钛材料应用的缺陷。 本发明还提供了一种用于实现本发明所体现的方法的系统。
    • 29. 发明授权
    • Graded bond coat for a thermal barrier coating system
    • 分层粘合涂层用于热障涂层系统
    • US06001492A
    • 1999-12-14
    • US35800
    • 1998-03-06
    • Melvin Robert JacksonAnn Melinda RitterMichael Francis Xavier Gigliotti, Jr.
    • Melvin Robert JacksonAnn Melinda RitterMichael Francis Xavier Gigliotti, Jr.
    • B32B15/04F01D5/28
    • F01D5/288B32B15/04F05D2300/121F05D2300/132F05D2300/143F05D2300/226F05D2300/6031Y10T428/12458Y10T428/12493Y10T428/12549Y10T428/12611Y10T428/12618Y10T428/12854Y10T428/12931Y10T428/12944
    • A bond coat (20) of a thermal barrier coating system for components designed for use in a hostile thermal environment, such as turbine, combustor and augmentor components of a gas turbine engine. The composition of the bond coat (20) has graded thermal expansion properties that moderate the transition between a metal substrate (10) and a thermal-insulating ceramic layer (12) of a TBC protecting the substrate (10), while also reducing the service temperature of the bond coat (20) so as to reduce its rate of oxidation. Preferably, the bond coat (20) has multiple layers (20a, 20b, 20c), with the coefficients of thermal conductivity of the individual bond coat layers (20a, 20b, 20c) being very close to that of the substrate (10) in order to promote heat transfer from the outward layer (20c) of the bond coat (20) to the substrate (10). By minimizing the service temperature of the bond coat (20) while grading the thermal expansion properties through the coating system, a more spall-resistant coating system is achieved. The inward layer (20a) of the bond coat (20) preferably contains a metallic constituent, such as an aluminum and/or chromium-containing intermetallic, MCrAl and/or MCrAlY, a middle layer (20b) of the bond coat (20) also contains the metallic constituent in addition to a chromium phase, and an outward layer (20c) of the bond coat (20) contains the chromium phase and at least one platinum-containing phase. The middle and outermost layers (20b, 20c) may also contain chromium carbides such as Cr.sub.3 C.sub.2.
    • 用于在恶劣热环境中使用的部件的热障涂层系统的粘结涂层(20),其用于燃气涡轮发动机的涡轮机,燃烧器和增压器部件。 粘合涂层(20)的组成具有渐变的热膨胀性能,其可以缓和金属基板(10)和保护基板(10)的TBC的绝热陶瓷层(12)之间的转变,同时还减少了服务 粘合涂层(20)的温度以降低其氧化速率。 优选地,粘合涂层(20)具有多个层(20a,20b,20c),各个粘结涂层(20a,20b,20c)的导热系数非常接近基底(10)的导热系数 以促进从粘合涂层(20)的外层(20c)到基底(10)的热传递。 通过使粘合涂层(20)的使用温度最小化,同时通过涂布系统对热膨胀性能进行分级,可实现更多的防剥落涂层体系。 接合涂层(20)的内层(20a)优选含有金属成分,例如铝和/或含铬金属间化合物,MCrAl和/或MCrAlY,粘结涂层(20)的中间层(20b) 还含有除铬相以外的金属成分,并且粘合涂层(20)的外层(20c)含有铬相和至少一种含铂相。 中间层和最外层(20b,20c)也可以含有Cr 3 C 2等碳化铬。