专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明申请

US20160123937A1 METHOD FOR EVALUATING PRETREATMENT OF COAT MATERIAL ON MICRO-PORE OF AUTOMOBILE BODY PANELS 审中-公开
标题翻译：汽车车身微孔涂层预处理方法
公开(公告)号：US20160123937A1
公开(公告)日：2016-05-05
申请号：US14876691
申请日：2015-10-06
申请人： Hyundai Motor Company
发明人： Seung Yul YOON
IPC分类号： G01N33/00
CPC分类号： G01N33/00 , G01N2033/0083
摘要： A method for evaluating pretreatment of a coat material applied to a micro-pore of body panels of an automobile includes preparing a jig including a pair of steel plates, a spacer constituting the micro-pore between the steel plates, and a fixing means fixing the steel plates and the spacer outside the steel plates in order to fix the steel plates and the spacer while the spacer is inserted between the steel plates, inserting the spacer between the steel plates by setting the micro-pore of the jig and manufacturing an evaluating jig by using fixing means, forming a coat by applying the coat material to the micro-pore of the jig, and removing the jig and measuring and evaluating the weight of the formed coat.
摘要翻译：一种用于评价施加于汽车车身板的微孔的涂层材料的预处理的方法包括：准备夹具，该夹具包括一对钢板，构成钢板之间的微孔的间隔件和固定装置钢板和钢板之间的间隔件，以便在钢板之间插入间隔件时固定钢板和间隔件，将间隔件插入钢板之间，通过设置夹具的微孔并制造评估夹具通过使用固定装置，通过将涂层材料施加到夹具的微孔而形成涂层，并且去除夹具并测量和评估成形涂层的重量。

2. 发明授权

US09152744B2 Methods, systems, and computer readable media for generating a non-destructive inspection model for a composite part from a design model of the composite part 有权
标题翻译：用于从复合部件的设计模型生成用于复合部件的非破坏性检查模型的方法，系统和计算机可读介质
公开(公告)号：US09152744B2
公开(公告)日：2015-10-06
申请号：US13434394
申请日：2012-03-29
申请人： Olivier Grellou , Sjoerd Van Der Veen
发明人： Olivier Grellou , Sjoerd Van Der Veen
IPC分类号： G06F17/50 , G06T15/08 , G01N33/00
CPC分类号： G06F17/5009 , G01N2033/0083 , G01N2033/0096 , G06F17/5095 , G06F2217/46 , G06T15/08
摘要： Methods, systems, and computer readable media for generating a nondestructive inspection model are provided, where such methods, systems and computer readable media are particularly suitable for use with aerospace parts or components. The method can include occurring at a computing platform with a memory and a processor, and analyzing, by the processor, a design model file stored in the memory to determine one or more properties of a composite part, the design model file describing one or more physical characteristics of the composite part. The method also can include generating, by the processor, a non-destructive inspection model for the composite part based on the one or more properties of the composite part determined by analyzing the design model file.
摘要翻译：提供了用于产生非破坏性检查模型的方法，系统和计算机可读介质，其中这些方法，系统和计算机可读介质特别适合于与航空航天部件一起使用。该方法可以包括在具有存储器和处理器的计算平台上发生，并且由处理器分析存储在存储器中的设计模型文件以确定复合部件的一个或多个属性，描述一个或多个复合材料的物理特性。该方法还可以包括由处理器基于通过分析设计模型文件确定的复合部件的一个或多个属性来生成复合零件的非破坏性检查模型。

3. 发明授权

US08601878B2 Base excitation testing system using spring elements to pivotally mount wind turbine blades 有权
标题翻译：使用弹簧元件枢转安装风力涡轮机叶片的基础激励测试系统
公开(公告)号：US08601878B2
公开(公告)日：2013-12-10
申请号：US12990069
申请日：2009-05-01
申请人： Jason Cotrell , Scott Hughes , Sandy Butterfield , Scott Lambert
发明人： Jason Cotrell , Scott Hughes , Sandy Butterfield , Scott Lambert
IPC分类号： G01M7/06 , F03D11/00 , F03D11/04 , G01M13/00 , G01N3/32 , G01M7/02 , G01N3/02
CPC分类号： F03D11/0091 , F03D13/22 , F03D17/00 , F05B2250/42 , F05B2260/83 , G01M7/025 , G01M7/027 , G01M7/06 , G01N3/02 , G01N3/32 , G01N2033/0083 , G01N2203/0035 , G01N2203/0073
摘要： A system (1100) for fatigue testing wind turbine blades (1102) through forced or resonant excitation of the base (1104) of a blade (1102). The system (1100) includes a test stand (1112) and a restoring spring assembly (1120) mounted on the test stand (1112). The restoring spring assembly (1120) includes a primary spring element (1124) that extends outward from the test stand (1112) to a blade mounting plate (1130) configured to receive a base (1104) of blade (1102). During fatigue testing, a supported base (1104) of a blade (1102) may be pivotally mounted to the test stand (1112) via the restoring spring assembly (1120). The system (1100) may include an excitation input assembly (1140) that is interconnected with the blade mounting plate (1130) to selectively apply flapwise, edgewise, and/or pitch excitation forces. The restoring spring assembly (1120) may include at least one tuning spring member (1127) positioned adjacent to the primary spring element (1124) used to tune the spring constant or stiffness of the primary spring element (1124) in one of the excitation directions.
摘要翻译：一种用于通过叶片（1102）的基座（1104）的强制或共振激励来疲劳测试风力涡轮机叶片（1102）的系统（1100）。系统（1100）包括安装在测试台（1112）上的测试台（1112）和恢复弹簧组件（1120）。复原弹簧组件（1120）包括从测试台（1112）向外延伸到构造成接收叶片（1102）的基部（1104）的叶片安装板（1130）的主弹簧元件（1124）。在疲劳测试期间，刀片（1102）的支撑基座（1104）可以经由复位弹簧组件（1120）枢转地安装到测试台（1112）。系统（1100）可以包括与叶片安装板（1130）互连的激励输入组件（1140），以选择性地施加翼形，沿边和/或俯仰激励力。恢复弹簧组件（1120）可以包括至少一个调节弹簧构件（1127），其邻近主弹簧元件（1124）定位，用于调节主弹簧元件（1124）的一个激励方向上的弹簧常数或刚度。

4. 发明授权

US4864863A Mechanism for testing helicopter rotor blade fatigue properties 失效
标题翻译：直升机转子叶片疲劳性能测试机理
公开(公告)号：US4864863A
公开(公告)日：1989-09-12
申请号：US184919
申请日：1988-04-22
申请人： Jay M. Yarm
发明人： Jay M. Yarm
IPC分类号： G01N3/00 , G01N3/02 , G01N3/04 , G01N3/32 , G01N33/00
CPC分类号： G01N3/32 , G01N2033/0083 , G01N2203/0005 , G01N2203/0021 , G01N2203/0023 , G01N2203/0037 , G01N2203/0073 , G01N2203/0258 , G01N2203/0435
摘要： Mechanism for determining the fatigue properties of helicopter rotor blade flexbeam sections using one motor driven eccentric for imparting combined bending, twisting and deflection loads to a flexbeam.
摘要翻译：用于使用一个电动机驱动的偏心轮来确定直升机转子叶片柔性梁部分的疲劳性能的机制，用于将弯曲，扭转和挠曲载荷组合到柔性梁上。

5. 发明授权

US3482430A Portable rebound or skid resistance tester 失效
标题翻译：便携式或耐油测试仪
公开(公告)号：US3482430A
公开(公告)日：1969-12-09
申请号：US3482430D
申请日：1966-12-05
申请人： UNIROYAL INC
发明人： PERCARPIO EDWARD P , BEVILACQUA EDWARD M
IPC分类号： G01N3/30 , G01N33/00 , G01N33/44 , G01N3/62 , G01N3/00 , G01N3/52
CPC分类号： G01N3/30 , G01N33/445 , G01N2033/0083

6. 发明授权

US09311699B2 Clear mottle analyzer for multilayer laminates 有权
标题翻译：用于多层层压板的透明斑驳分析仪
公开(公告)号：US09311699B2
公开(公告)日：2016-04-12
申请号：US13306233
申请日：2011-11-29
申请人： Jeffrey B. Hurlbut
发明人： Jeffrey B. Hurlbut
IPC分类号： H04N7/18 , G06T7/00 , G01N33/38 , G01N33/00
CPC分类号： G06T7/001 , G01N33/386 , G01N2033/0083
摘要： This disclosure relates to systems, devices and methods utilized to quantitatively measure the level of mottle in multilayer laminates. The systems and method are generally free of the inconsistencies, variability and inherent biases of the traditional subjective process by which a person of ordinary skill in the art can assess and categorize the mottle of a multilayer laminate. In the method, variations in the images of mottle produced by a shadowgraph are quantified, measured and classified.
摘要翻译：本公开涉及用于定量测量多层层压板中斑点水平的系统，装置和方法。系统和方法通常没有本领域普通技术人员可以评估和分类多层层压体的斑点的传统主观过程的不一致性，变异性和固有偏差。在该方法中，对由阴影片产生的斑点的图像的变化进行量化，测量和分类。

7. 发明授权

US08955387B2 Fatigue test arrangement 有权
标题翻译：疲劳试验装置
公开(公告)号：US08955387B2
公开(公告)日：2015-02-17
申请号：US12919811
申请日：2009-02-18
申请人： Stephen J Smith , Philip D Blavins , Andrew T Backler
发明人： Stephen J Smith , Philip D Blavins , Andrew T Backler
IPC分类号： G01N3/32 , G01M7/02 , G01N3/36 , G01N33/00
CPC分类号： G01N3/32 , G01M7/025 , G01M7/027 , G01N3/36 , G01N2033/0083 , G01N2203/0042 , G01N2203/0044 , G01N2203/0048 , G01N2203/0073 , G01N2203/0246
摘要： High cycle fatigue testing is required with regard to a large number of components in order to evaluate their performance and capabilities. Typically such components are mounted such that an excitation mechanism such as through use of air jets can be utilized in order to stimulate vibration. In order to isolate a desired vibration mode generally, an isolation device is utilized. The isolation device presents an edge to a node within the component in order to inhibit vibration modes other than that of interest. Unfortunately, prior isolation elements tend to wear resulting in spurious results. By providing an isolation element within an isolation device, a fatigue test arrangement can be achieved in which both axial movement in the direction of a spring upon which the element is presented as well as lateral movement can be achieved.
摘要翻译：为了评估其性能和能力，需要对大量组件进行高循环疲劳测试。通常安装这样的部件，使得可以利用诸如通过使用空气射流的激励机构来刺激振动。为了通常隔离期望的振动模式，使用隔离装置。隔离装置向组件内的节点呈现边缘，以便抑制除感兴趣的振动模式之外的振动模式。不幸的是，先前的隔离元件往往会磨损，导致虚假的结果。通过在隔离装置内设置隔离元件，可以实现疲劳试验装置，其中可以实现在元件呈现的弹簧的方向上的轴向运动以及横向移动。

8. 发明申请

US20110041617A1 BASE EXCITATION TESTING SYSTEM USING SPRING ELEMENTS TO PIVOTALLY MOUNT WIND TURBINE BLADES 有权
标题翻译：基础激振试验系统使用弹簧元件调节风力涡轮叶片
公开(公告)号：US20110041617A1
公开(公告)日：2011-02-24
申请号：US12990069
申请日：2009-05-01
申请人： JASON COTRELL , SCOTT HUGHES , SANDY BUTTERFIELD , SCOTT LAMBERT
发明人： JASON COTRELL , SCOTT HUGHES , SANDY BUTTERFIELD , SCOTT LAMBERT
IPC分类号： G01M13/00
CPC分类号： F03D11/0091 , F03D13/22 , F03D17/00 , F05B2250/42 , F05B2260/83 , G01M7/025 , G01M7/027 , G01M7/06 , G01N3/02 , G01N3/32 , G01N2033/0083 , G01N2203/0035 , G01N2203/0073
摘要： A system (1100) for fatigue testing wind turbine blades (1102) through forced or resonant excitation of the base (1104) of a blade (1102). The system (1100) includes a test stand (1112) and a restoring spring assembly (1120) mounted on the test stand (1112). The restoring spring assembly (1120) includes a primary spring element (1124) that extends outward from the test stand (1112) to a blade mounting plate (1130) configured to receive a base (1104) of blade (1102). During fatigue testing, a supported base (1104) of a blade (1102) may be pivotally mounted to the test stand (1112) via the restoring spring assembly (1120). The system (1100) may include an excitation input assembly (1140) that is interconnected with the blade mounting plate (1130) to selectively apply flapwise, edgewise, and/or pitch excitation forces. The restoring spring assembly (1120) may include at least one tuning spring member (1127) positioned adjacent to the primary spring element (1124) used to tune the spring constant or stiffness of the primary spring element (1124) in one of the excitation directions.
摘要翻译：一种用于通过叶片（1102）的基座（1104）的强制或共振激励来疲劳测试风力涡轮机叶片（1102）的系统（1100）。系统（1100）包括安装在测试台（1112）上的测试台（1112）和恢复弹簧组件（1120）。复原弹簧组件（1120）包括从测试台（1112）向外延伸到构造成接收叶片（1102）的基部（1104）的叶片安装板（1130）的主弹簧元件（1124）。在疲劳测试期间，刀片（1102）的支撑基座（1104）可以经由复位弹簧组件（1120）枢转地安装到测试台（1112）。系统（1100）可以包括与叶片安装板（1130）互连的激励输入组件（1140），以选择性地施加翼形，沿边和/或俯仰激励力。恢复弹簧组件（1120）可以包括至少一个调节弹簧构件（1127），其邻近主弹簧元件（1124）定位，用于调节主弹簧元件（1124）的一个激励方向上的弹簧常数或刚度。

9. 发明申请

US20080229844A1 GLASS TESTING APPARATUS 失效
标题翻译：玻璃测试仪
公开(公告)号：US20080229844A1
公开(公告)日：2008-09-25
申请号：US12051540
申请日：2008-03-19
申请人： Randy L. Mackey , Christopher M. Boyle , Michael P. Boyle
发明人： Randy L. Mackey , Christopher M. Boyle , Michael P. Boyle
IPC分类号： G01N3/20
CPC分类号： G01N3/04 , G01M5/0033 , G01M5/005 , G01M5/0066 , G01N2033/0083 , G01N2203/0222 , G01N2203/0246
摘要： Embodiments of the present invention provide methods and apparatuses for testing the structural integrity of glass. Embodiments of the present invention provide a method and apparatus for testing glass by applying one or more stresses to the glass in a controlled manner. Embodiments of the invention may hold a sheet of glass and may subject the glass to a variety of stresses by flexing, twisting, vibrating, etc.
摘要翻译：本发明的实施例提供了用于测试玻璃的结构完整性的方法和装置。本发明的实施例提供了一种通过以受控的方式对玻璃施加一个或多个应力来测试玻璃的方法和装置。本发明的实施例可以保持玻璃板并且可以通过弯曲，扭转，振动等使玻璃受到各种应力。

10. 发明授权

US5394754A Apparatus for testing a hem flange and method for same 失效
标题翻译：用于测试下摆法兰的装置及其方法
公开(公告)号：US5394754A
公开(公告)日：1995-03-07
申请号：US18775
申请日：1993-02-17
申请人： James M. Herring, Jr.
发明人： James M. Herring, Jr.
IPC分类号： G01N3/00 , G01N19/04 , G01N33/00 , G01N3/08
CPC分类号： G01N19/04 , G01N2033/0083 , G01N2203/0025
摘要： A test apparatus for testing hem flanges that join automotive body panels is provided. This testing apparatus operates by engaging a hook member with a first body panel such that the first body panel is maintained in a held relationship with respect to the hook member. A ram member then extends from the testing apparatus and engages with and loads a second automotive body panel member. As a result, a tensile load is applied to the hem flange, permitting the hem flange to be analyzed for defective construction.
摘要翻译：提供一种用于测试连接汽车车身面板的下摆法兰的测试装置。该测试装置通过将钩构件与第一主体面板接合来操作，使得第一主体面板相对于钩构件保持保持关系。然后，冲头构件从测试装置延伸并与第二汽车车身面板构件接合并加载。结果，拉伸载荷被施加到下摆法兰上，允许下摆法兰被分析为有缺陷的构造。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式