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    • 2. 发明授权
    • Blackline indicator for use in tomographic and/or radioscopic inspection
of weld joints
    • 用于断层和/或焊接接头放射检查的黑线指示器
    • US5283822A
    • 1994-02-01
    • US953151
    • 1992-09-29
    • Francis H. LittleGerald B. Nightingale
    • Francis H. LittleGerald B. Nightingale
    • G01N23/18H05G1/26H05G1/28
    • G01N23/18H05G1/26G01N2223/1016G01N2223/629
    • A blackline indictor for use in tomographic and/or radioscopic inspection of a weld joint is disclosed. The indicator includes a first elongated member having a first end and a second end and a second elongated member juxtaposed to said first member and also having a first end and a second end. The first ends of the elongated members are in contact with one another, and a spacer is disposed between the first and second members to position the second ends of the members at a selected distance from one another. The selected distance is at least equal to a thickness of the weld joint under inspection, and the first and second members and the spacer define a calibrated wedge shaped gap which is radiographically imageable to permit determination and control of the x-ray inspection parameters. The blackline indicator constituents may be magnetized to hold the constituents together and to permit attachment of the indicator to a workpiece under inspection in a position where the calibrated wedge shaped gap will be substantially superimposed over the weld joint in a radiographic image thereof with one of the elongated members being substantially parallel to the weld joint.
    • 公开了用于焊接接头的断层和/或放射检查的黑线指示器。 指示器包括具有第一端和第二端的第一细长构件和与所述第一构件并置并且还具有第一端和第二端的第二细长构件。 细长构件的第一端彼此接触,并且间隔件设置在第一构件和第二构件之间,以将构件的第二端彼此间隔开选定的距离。 所选择的距离至少等于被检查的焊接接头的厚度,并且第一和第二构件和间隔件限定校准的楔形间隙,其可放射学地成像以允许X射线检查参数的确定和控制。 黑线指示器成分可以被磁化以将组件保持在一起,并且允许将指示器附接到被检查的工件,其中校准的楔形间隙将在其放射线图像中基本上叠加在焊接接头上的位置,其中 细长构件基本上平行于焊接接头。
    • 4. 发明授权
    • Eddy current calibration standard
    • 涡流校准标准
    • US06356069B1
    • 2002-03-12
    • US09453089
    • 1999-12-02
    • Richard L. TrantowFrancis H. LittleGigi O. GambrellJohn W. Ertel
    • Richard L. TrantowFrancis H. LittleGigi O. GambrellJohn W. Ertel
    • G01R3500
    • G01N27/9086
    • A calibration standard for calibrating an eddy current inspection probe sized and shaped to inspect a preselected non-planar feature of a manufactured part. The feature extends in a longitudinal direction and in a lateral direction. Further, the feature has an end profile as viewed in the longitudinal direction having a substantially invariant shape and orientation. The calibration standard includes a body having a non-planar surface extending in a longitudinal direction and in a lateral direction. The standard also has an end profile as viewed in the longitudinal direction of the surface substantially identical to the profile of the feature. The surface of the body has an elongate narrow opening extending into the body substantially normal to the surface and traversing the surface of the body at a substantially constant angle with respect to the longitudinal direction of the surface as viewed normal to the surface.
    • 用于校准涡流检查探头的校准标准,其尺寸和形状用于检查制造部件的预选非平面特征。 该特征沿纵向方向和横向方向延伸。 此外,该特征具有在纵向方向上具有基本上不变的形状和取向的端部轮廓。 校准标准包括具有在纵向方向和横向方向上延伸的非平面表面的主体。 该标准还具有在表面的纵向方向上观察的端部轮廓,其基本上与特征的轮廓相同。 主体的表面具有一个细长的狭窄的开口,其基本上垂直于表面延伸到主体中,并且以垂直于表面的方式相对于表面的纵向方向以基本恒定的角度横过主体的表面。
    • 5. 发明授权
    • Eddy current array inspection device
    • 涡流电流阵列检测装置
    • US5442286A
    • 1995-08-15
    • US125469
    • 1993-09-22
    • George H. Sutton, Jr.Francis H. LittleCarl Granger, Jr.Philip F. Stapf
    • George H. Sutton, Jr.Francis H. LittleCarl Granger, Jr.Philip F. Stapf
    • G01N27/90G01N27/82
    • G01N27/902
    • A device for inspecting a component, such as a dovetail slot of a gas turbine engine or the like, includes an eddy current array circuit having an active face for positioning on the surface of the component during the inspection operation and a backing disposed on a face of the eddy current array circuit opposite to the active face. The eddy current array circuit and the backing are disposed over the operating face and expandable sides of an expandable bar. The expandable bar has a slot formed therein with interior side edges which narrow toward the operating face of the bar at a predetermined slope. An expanding wedge with angled sides is positioned to cause the angled sides to respectively matingly engage the interior sides of the slot to cause the exterior sides of the expandable bar to expand outwardly a greater distance as the wedge is pushed deeper into the slot to cause the eddy current array circuit into conformance with the shape of the surface being inspected.
    • 用于检查诸如燃气涡轮发动机等的燕尾槽的部件的装置包括涡流阵列电路,其具有用于在检查操作期间在部件的表面上定位的主动面和设置在面部上的背衬 与激活面相反的涡流阵列电路。 涡流阵列电路和背衬设置在可扩张杆的操作面和可膨胀侧上。 可膨胀杆具有形成在其中的槽,其内侧边缘以预定斜率朝向杆的操作面变窄。 定位的具有成角度侧面的膨胀楔形物使得成角度的侧面分别配合地接合槽的内侧,以使得可膨胀杆的外侧向外扩张更大的距离,因为楔被更深地推入槽中, 涡流阵列电路符合正在检查的表面的形状。
    • 6. 发明授权
    • Rotate/rotate method and apparatus for computed tomography x-ray
inspection of large objects
    • 旋转/旋转大型物体计算机断层X线检查的方法和装置
    • US5119408A
    • 1992-06-02
    • US607337
    • 1990-10-31
    • Francis H. LittleAndrew J. GalishRalph G. Isaacs
    • Francis H. LittleAndrew J. GalishRalph G. Isaacs
    • G01N23/04
    • G01N23/046G01N2223/419
    • A method for inspecting a component having dimensions larger than a fan beam angle of an x-ray inspection system includes the steps of: providing an x-ray beam having a selected fan angle in a source focal point; positioning a portion of the component substantially completely within the x-ray beam; rotating the component 360 degrees around a component inspection rotational axis; collecting the attenuated x-ray beam that passes through the component during rotation; generating a multiplicity of electrical signals responsive to the collected x-ray beam; incrementally moving the component inspection rotational axis about the x-ray source focal point to position another portion of the component within the x-ray beam; and repeating the steps of rotating the part 360 degrees about a component inspection rotational axis and incrementally moving the part inspection rotational axis about the x-ray source focal point until the entire component has passed through the fan beam.
    • 一种用于检查尺寸大于X射线检查系统的扇形束角度的部件的方法包括以下步骤:在源焦点中提供具有选定的扇角的X射线束; 将部件的一部分基本上完全定位在X射线束内; 围绕部件检查旋转轴线旋转部件360度; 收集在旋转期间通过部件的衰减的X射线束; 响应于所收集的x射线束产生多个电信号; 围绕X射线源焦点递增地移动部件检查旋转轴线以将部件的另一部分定位在X射线束内; 并且重复以围绕零件检查旋转轴线旋转部件360度并逐渐移动围绕x射线源焦点的零件检查旋转轴直到整个部件已经通过风扇光束的步骤。
    • 7. 发明授权
    • Eddy current array inspection device for shaped holes
    • 涡流电流阵列检查装置用于成形孔
    • US5903147A
    • 1999-05-11
    • US819833
    • 1997-03-18
    • Carl Granger, Jr.Francis H. LittleThomas B. HewtonKristina H. V. Hedengren
    • Carl Granger, Jr.Francis H. LittleThomas B. HewtonKristina H. V. Hedengren
    • G01N27/90G01N27/72G01N27/82G01R33/12
    • G01N27/9013
    • An eddy current device for inspecting a component, such as a closed surface area of a gas turbine engine or the like, includes an eddy current array circuit having an active face for positioning on a surface portion of the component during an inspection operation and backing on a surface of the eddy current array circuit opposite to the active face. The eddy current array circuit and backing are disposed over the operating face and expandable sides of an extendible pin. The extendible pin has a slot formed therein with interior side edges which narrow toward the operating face of the pin at a predetermined slope. The expanding pin is positioned to cause the angled sides to mate while engaging the interior angled sides of the round or shaped hole to cause the exterior sides of the expandable pin to expand outwardly a greater distance as the pin is pushed deeper into the hole. This causes the eddy current circuit to conform with the shape of the surface to be inspected. The array sensor is so shaped that it can cover the closed surface in as little as one scan.
    • 用于检查诸如燃气涡轮发动机等的封闭表面积的部件的涡流装置包括涡流阵列电路,其具有用于在检查操作期间定位在部件的表面部分上的主动面,并且支撑 涡流阵列电路的表面与主动面相对。 涡流阵列电路和背衬设置在可伸缩销的操作面和可膨胀侧上。 可延伸销具有形成在其中的槽,其内侧边缘以预定斜率朝向销的操作面变窄。 定位膨胀销使得成角度的侧面在与圆形或成形孔的内部成角度的侧面配合,以使得当销被更深地推入孔中时,可膨胀销的外侧向外扩展更大的距离。 这使得涡流电路符合要检查的表面的形状。 阵列传感器的形状使其能够在少至一次的扫描中覆盖封闭的表面。
    • 8. 发明授权
    • Computed tomography metrology
    • 计算机断层扫描计量学
    • US5848115A
    • 1998-12-08
    • US850673
    • 1997-05-02
    • Francis H. LittleJohn C. Janning
    • Francis H. LittleJohn C. Janning
    • G01N23/04G06T1/00G06T17/00A61B6/03
    • G06T17/00G01N23/046G01N2223/419Y10S378/901
    • The invention is a three-dimensional computed tomography method for inspecting and comparing actual geometry to predetermined geometry of an object. The method includes the following steps: A) three-dimensionally scanning the object using computed tomography to produce multiple slices of actual geometrical data of the object; B) processing the multiple slices of actual geometrical data into actual boundary data which defines internal and external boundaries of the object; and C) producing actual point cloud data from the actual boundary data. The method further includes comparing the actual point cloud data to object geometry predetermined data. The comparing may include outputting an image comparing the point cloud data to the predetermined data and the image may represent the geometry of non-conformance between the point cloud data and the predetermined data. The image may be rotated to present the non-conformance from different viewpoints around the feature.
    • 本发明是用于检查和比较实际几何与对象的预定几何的三维计算机断层摄影方法。 该方法包括以下步骤:A)使用计算机断层摄影三维扫描物体以产生物体的实际几何数据的多个切片; B)将实际几何数据的多个切片处理成实际边界数据,界定对象的内部和外部边界; 和C)从实际边界数据生成实际点云数据。 该方法还包括将实际点云数据与对象几何预定数据进行比较。 比较可以包括输出将点云数据与预定数据进行比较的图像,并且图像可以表示点云数据和预定数据之间的不一致的几何形状。 可以旋转图像以从特征周围的不同视点呈现不一致。