| 发明名称 |
SYSTEM FOR NON-DESTRUCTIVE INSPECTION OF STRUCTURAL COMPONENTS |
| 摘要 |
A system for non-destructive inspection of structural components comprising an ultrasonic probe having a contact face for contacting a surface of a structural component to be inspected and being adapted to emit ultrasonic energy into the structural component when the contact face abuts on a surface of the structural component, a thermal imaging camera adapted to inspect a portion of a surface of the structural component to detect region of the surface of the structural component where an increase of the temperature occurs, and a control unit connected to the ultrasonic probe and the thermal imaging camera. The contact face extends in a plane and is provided with at least two bars which are arranged in parallel and have a common separation distance from each other. |
| 申请公布号 |
US2016299108(A1) |
申请公布日期 |
2016.10.13 |
| 申请号 |
US201615089661 |
申请日期 |
2016.04.04 |
| 申请人 |
Airbus Operations GmbH |
发明人 |
Bisle Wolfgang;Scherling Dieter;Bock Frederic;Rahammer Markus;Solodov Igor |
| 分类号 |
G01N29/24;G01J5/02 |
主分类号 |
G01N29/24 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for non-destructive inspection of structural components comprising:
an ultrasonic probe having a contact face configured to contact a surface of a structural component to be inspected and being adapted to emit ultrasonic energy into the structural component when the contact face abuts on a surface of the structural component, a thermal imaging camera configured to inspect a portion of a surface of the structural component to detect a region of the surface of the structural component where an increase of the temperature occurs, and a control unit connected to the ultrasonic probe and the thermal imaging camera, wherein the contact face extends in a plane and is provided with at least two bars, which bars are arranged in parallel and have a common distance therebetween. |
| 地址 |
Hamburg DE |
