公开(公告)号：US08156649B2

公开(公告)日：2012-04-17

申请号：US12420578

申请日：2009-04-08

申请人： Simone Hövel ,  Alexander Stankowski ,  Günter Ambrosy ,  Matthias Hoebel ,  Alexander Schnell ,  Hans Bissig ,  Rainer Kurtz

发明人： Simone Hövel ,  Alexander Stankowski ,  Günter Ambrosy ,  Matthias Hoebel ,  Alexander Schnell ,  Hans Bissig ,  Rainer Kurtz

IPC分类号： B23P6/00

CPC分类号： B23P6/005 ,  B23K1/0018 ,  B23K1/0056 ,  B23K9/0026 ,  B23K10/00 ,  B23K26/0093 ,  B23K28/02 ,  B23K2101/001 ,  F01D5/005 ,  F05D2230/235 ,  F05D2230/80 ,  Y10T29/49318 ,  Y10T29/49728 ,  Y10T29/49732

摘要： A gas turbine engine hot gas component repair method for defects that do not extend through the thickness of the component is provided. First defects are removed by machining a cavity in the surface of a component. Coupons, fittable within the cavities are manufactured, are for example coated with brazing medium on an inner surface and then joined to the component by joining means such as laser metal forming. The joint holds the coupon during later heat treatment, thereby eliminating a need for holding aids. Before heat treatment, a further brazing medium can be applied to the surface of the coupon overlapping onto the component. A single heat treatment, brazing the coupon to the component and, brazing the brazing medium to the outer surface of the coupon can, then be used to complete the repair.

摘要翻译： 提供了一种用于不延伸通过部件的厚度的缺陷的燃气涡轮发动机热气体部件修复方法。 通过在部件的表面中加工空腔来去除第一缺陷。 制造在空腔内配合的优惠券，例如在内表面上涂覆有钎焊介质，然后通过诸如激光金属成形之类的接合方法与部件接合。 在后续的热处理过程中，关节保持优惠券，从而不需要固定助剂。 在热处理之前，可以将另外的钎焊介质施加到与组件重叠的试样表面上。 单独的热处理，将试样钎焊到部件上，并将钎焊介质钎焊到试样的外表面上，然后用于完成修复。

公开(公告)号：US20090255117A1

公开(公告)日：2009-10-15

申请号：US12420578

申请日：2009-04-08

申请人： Simone Hovel ,  Alexander Stankowski ,  Gunter Ambrosy ,  Matthias Hoebel ,  Alexander Schnell ,  Hans Bissig ,  Rainer Kurtz

发明人： Simone Hovel ,  Alexander Stankowski ,  Gunter Ambrosy ,  Matthias Hoebel ,  Alexander Schnell ,  Hans Bissig ,  Rainer Kurtz

IPC分类号： B23P6/00

CPC分类号： B23P6/005 ,  B23K1/0018 ,  B23K1/0056 ,  B23K9/0026 ,  B23K10/00 ,  B23K26/0093 ,  B23K28/02 ,  B23K2101/001 ,  F01D5/005 ,  F05D2230/235 ,  F05D2230/80 ,  Y10T29/49318 ,  Y10T29/49728 ,  Y10T29/49732

摘要： A gas turbine engine hot gas component repair method for defects that do not extend through the thickness of the component is provided. First defects are removed by machining a cavity in the surface of a component. Coupons, fittable within the cavities are manufactured, are for example coated with brazing medium on an inner surface and then joined to the component by joining means such as laser metal forming. The joint holds the coupon during later heat treatment, thereby eliminating a need for holding aids. Before heat treatment, a further brazing medium can be applied to the surface of the coupon overlapping onto the component. A single heat treatment, brazing the coupon to the component and, brazing the brazing medium to the outer surface of the coupon can, then be used to complete the repair.

摘要翻译： 提供了一种用于不延伸通过部件的厚度的缺陷的燃气涡轮发动机热气体部件修复方法。 通过在部件的表面中加工空腔来去除第一缺陷。 制造在空腔内配合的优惠券，例如在内表面上涂覆有钎焊介质，然后通过诸如激光金属成形之类的接合方法与部件接合。 在后续的热处理过程中，关节保持优惠券，从而不需要固定助剂。 在热处理之前，可以将另外的钎焊介质施加到与组件重叠的试样表面上。 单独的热处理，将试样钎焊到部件上，并将钎焊介质钎焊到试样的外表面上，然后用于完成修复。

公开(公告)号：US06524100B2

公开(公告)日：2003-02-25

申请号：US09893722

申请日：2001-06-28

申请人： Rainer Kurtz ,  Bernd Schenker ,  Richard Kressmann

发明人： Rainer Kurtz ,  Bernd Schenker ,  Richard Kressmann

IPC分类号： F27B914

CPC分类号： B23K37/0408 ,  B23K1/008 ,  B23K1/012 ,  F26B15/10 ,  F26B25/06 ,  F27B9/024 ,  F27B9/025 ,  F27D3/00 ,  F27D2003/0063 ,  Y10T156/10 ,  Y10T156/1702

摘要： A facility for the thermal treatment of workpieces has a processing or heating chamber and at least one transport device, extending essentially completely through the processing or heating chamber, with which the workpieces to be treated can be transported through the processing or heating chamber. At least two processing or heating levels are hereby located on top of one another in the processing or heating chamber, with each processing or heating level having at least one separate transport device. This type of facility can preferably be used as a soldering facility, particularly a reflow soldering facility, or as a facility for the hardening or drying of plastics or adhesives.

公开(公告)号：US20080283308A1

公开(公告)日：2008-11-20

申请号：US12066439

申请日：2006-08-11

申请人： Rainer Kurtz ,  Mark Cannon ,  Wolfram Hubsch ,  Harald Grumm

发明人： Rainer Kurtz ,  Mark Cannon ,  Wolfram Hubsch ,  Harald Grumm

IPC分类号： G06F3/041

CPC分类号： H05K3/0008 ,  G03F9/7038 ,  G03F9/7069 ,  G03F9/7088 ,  H05K1/0269 ,  H05K3/1216 ,  H05K2201/09918

摘要： The invention pertains to a device for determining the relative position in the X-Y plane between two essentially flat elements that are spaced apart in the Z-direction and are essentially arranged on top of one another, wherein said device features at least one optical sensor that is arranged between the elements and is able to sense at least two points of the mutually facing surfaces of the elements, as well as an evaluation unit, in which the images of the points can be evaluated with respect to their relative position in the X-Y plane. In this case, the optical sensor features at least one line sensor that can be displaced relative to the two elements in such a way that the mutually facing surfaces of the elements can be optically scanned at least in sections in the manner of a scanner.

摘要翻译： 本发明涉及一种用于确定XY平面中在Z方向间隔开并且基本上布置在彼此之上的两个基本平坦的元件之间的相对位置的装置，其中所述装置具有至少一个光学传感器， 布置在元件之间并且能够感测元件的相互面对的表面中的至少两个点以及评估单元，其中点的图像可以相对于它们在XY平面中的相对位置被评估。 在这种情况下，光学传感器具有至少一个线传感器，其可以相对于两个元件移位，使得元件的相互面对的表面可以以扫描仪的方式至少以部分进行光学扫描。