公开(公告)号：US20020187042A1

公开(公告)日：2002-12-12

申请号：US09867213

申请日：2001-05-29

发明人： Ching-Pang Lee ,  Jonathan James Stow ,  John Peter Heyward ,  John Howard Starkweather ,  Lawrence Joseph Roedl ,  Joseph Howell Bowden JR.

IPC分类号： F01D005/08

CPC分类号： B23P6/005 ,  B23P6/007 ,  B23P15/04 ,  F01D5/005 ,  F01D5/18 ,  F01D5/20 ,  F05D2230/23 ,  F05D2230/80 ,  F05D2260/201 ,  F05D2260/202 ,  Y10T29/49318 ,  Y10T29/49341

摘要： An airfoil for a gas turbine engine, the airfoil having a core body with an airfoil body, an integral partial height squealer tip, and an integral tip cap between the airfoil body and the integral partial height squealer tip; and a squealer tip extension bonded to the partial height squealer tip. A method for manufacture and repair of an airfoil.

摘要翻译： 一种用于燃气涡轮发动机的翼型件，所述翼型件具有带有翼型本体的芯体，整体部分高度尖叫尖端以及在所述翼型件本身和所述整体式部分高度拨号器尖端之间的整体式顶盖; 以及一个与部分高度的尖叫声结合的尖叫尖端。 一种用于制造和修理翼型的方法。

公开(公告)号：US20020184762A1

公开(公告)日：2002-12-12

申请号：US09878848

申请日：2001-06-11

发明人： Gilbert Farmer ,  David Bruce Patterson ,  Steven Allen Stiverson ,  James Michael Caldwell ,  Edward John Emilianowicz ,  Jeffrey Michael Martini

IPC分类号： B23P006/00 ,  B23P019/04

CPC分类号： B23P6/005 ,  B23P2700/13 ,  F23R3/002 ,  F23R3/08 ,  F23R2900/00005 ,  F23R2900/00016 ,  Y02T50/67 ,  Y02T50/675 ,  Y10T29/49318 ,  Y10T29/49346 ,  Y10T29/49721 ,  Y10T29/4973 ,  Y10T29/49737

摘要： A replacement method facilitates replacing of a portion of a combustor liner within a gas turbine engine combustor in a cost-effective and reliable manner. The combustor includes a combustion zone that is defined by an inner and an outer liner. The inner and outer liners each include a series of panels and a plurality of nuggets formed by adjacent panels. The method includes the steps of cutting between an outer surface and an inner surface of at least one liner panel, removing at least one panel that is adjacent the area of the liner that was cut, and installing a replacement panel into the combustor for each panel that was removed from the combustor.

摘要翻译： 替代方法有利于以成本有效和可靠的方式更换燃气涡轮发动机燃烧器内的燃烧器衬套的一部分。 燃烧器包括由内衬和外衬层限定的燃烧区。 内衬和内衬各自包括一系列面板和由相邻面板形成的多个块。 该方法包括以下步骤：在至少一个衬板的外表面和内表面之间切割，除去邻近被切割的衬垫区域的至少一个面板，以及将替换面板安装到每个面板的燃烧器中 从燃烧器中取出。

公开(公告)号：US06416709B1

公开(公告)日：2002-07-09

申请号：US09504126

申请日：2000-02-15

申请人： Kevin Rafferty ,  Bruce Rowe

发明人： Kevin Rafferty ,  Bruce Rowe

IPC分类号： B22F702

CPC分类号： B23P6/005 ,  B23K35/0233 ,  B23K35/0238 ,  B23K35/0244 ,  B23P6/007 ,  B32B15/08 ,  G01N33/5302 ,  G01N33/542 ,  G01N33/54366 ,  G01N35/08

摘要： A base metal repair tape includes a first layer formed braze alloy bonded together with fibrillated polytetrafluoroethylene, a second layer formed from powdered base metal bonded together by fibrillated polytetrafluoroethylene and a third layer comprising a brazing alloy bonded together by fibrillated polytetrafluoroethylene. This is used to repair base metal by placing the first layer on the base metal and brazing the base metal powder so that the brazing alloy melts and diffuses into the base metal powder bonding it to the surface of the article. This permits the braze powder to be bonded to the base metal surface with minimal distance between the base powder particles. The number of alternating layers of base metal and braze alloy can be increased to increase the thickness of the repair. This can also be used to form small intricate parts.

摘要翻译： 贱金属修补带包括与原纤化聚四氟乙烯结合在一起的第一层形成的钎焊合金，由原纤化聚四氟乙烯粘合在一起的粉状母材形成的第二层和由原纤化聚四氟乙烯粘结在一起的钎焊合金的第三层。 这用于通过将第一层放置在基底金属上并钎焊基底金属粉末以使钎焊合金熔化并扩散到将其粘合到制品表面的基底金属粉末中来修复基底金属。 这使得钎焊粉末能够以基础粉末颗粒之间的最小距离与基底金属表面结合。 可以增加贱金属和钎焊合金的交替层数，以增加修补的厚度。 这也可用于形成复杂的小零件。

公开(公告)号：US06370752B1

公开(公告)日：2002-04-16

申请号：US09556182

申请日：2000-04-21

申请人： William C. Anderson ,  Dewey D. Dunkman ,  Gerald R. Geverdt ,  Ronald D. Stapperfenne

发明人： William C. Anderson ,  Dewey D. Dunkman ,  Gerald R. Geverdt ,  Ronald D. Stapperfenne

IPC分类号： B23P1904

CPC分类号： B23P6/005 ,  B23P2700/06 ,  F01D5/005 ,  F01D5/186 ,  Y02T50/672 ,  Y02T50/676 ,  Y10T29/49318 ,  Y10T29/49732 ,  Y10T29/49734 ,  Y10T29/49938

摘要： A method for repositioning or repairing holes in metal substrates such as metal components used in jet engines and the like. The hole to be repositioned or repaired is enlarged and a recess is formed at each end of the enlarged hole. A deformable metal insert is then inserted within the enlarged hole and then subjected to physical forces so as to cause it to deform and frictionally engage the walls of the recesses and the enlarged hole so that the insert becomes axially fixed therein. A new, repositioned hole can then be formed in the fixed insert that extends completely therethrough.

摘要翻译： 用于重新定位或修理金属基底中的孔的方法，例如用于喷气发动机等中的金属部件。 要重新定位或修复的孔被扩大，并且在扩大的孔的每个端部处形成凹部。 然后将可变形金属插入件插入到扩大的孔内，然后经受物理力，使其变形并摩擦地接合凹部和扩大的孔，使得插入件轴向固定在其中。 然后可以在完全延伸穿过其中的固定插入件中形成新的重新定位的孔。

公开(公告)号：US06332490B1

公开(公告)日：2001-12-25

申请号：US09296628

申请日：1999-04-23

申请人： Philip R. Griggs

发明人： Philip R. Griggs

IPC分类号： B32B3500

CPC分类号： F01D5/005 ,  B23P6/005 ,  B29C73/02 ,  B29C73/30 ,  B29L2031/08 ,  F01D5/3092 ,  Y10T29/37 ,  Y10T29/49746

摘要： A method for repairing a discrete damaged part of a strip bonded to an article surface includes applying a first removable masking member along and adjacent the damaged part of the strip and separated from the strip by a gap of at least 0.005″, and applying a second removable masking member to the outer surface of the strip. A repair adhesive, which can be cured at a curing temperature less than a higher temperature which can result in damage to properties of the article or a surface coating, is applied at and beneath an edge of the damaged part of the strip. Then the repair adhesive is cured at the curing temperature. Apparatus for bonding a strip to an end portion of the article includes a body having a channel there through defined, in part, by spaced apart support surfaces for article surfaces and positioned relative one to the other at a relative spatial position substantially coinciding with the relative spatial position of the article surfaces. The support surfaces include surface profiles substantially reproducing surface profiles of the article surfaces.

摘要翻译： 用于修复接合到制品表面的条带的离散的受损部分的方法包括沿着并且邻近带的损坏部分施加第一可移除掩模构件，并与条带间隔至少0.005“的间隙，并施加 第二可移除掩蔽构件到条的外表面。 修复粘合剂可以在低于较高温度的固化温度下固化，这可以导致制品或表面涂层的性能的损坏，并且被施加在带的损坏部分的边缘处和下方。 然后修复粘合剂在固化温度下固化。 用于将条带粘合到制品的端部的装置包括具有通道的主体，该主体具有通过限定的用于制品表面的间隔开的支撑表面，并且相对于另一个在相对空间位置处相对定位，该相对空间位置基本上与相对的 物品表面的空间位置。 支撑表面包括基本上再现物品表面的表面轮廓的表面轮廓。

公开(公告)号：US06274215B1

公开(公告)日：2001-08-14

申请号：US09217661

申请日：1998-12-21

申请人： Gulcharan S. Brainch ,  Michael J. Danowski ,  Jonathan P. Clarke

发明人： Gulcharan S. Brainch ,  Michael J. Danowski ,  Jonathan P. Clarke

IPC分类号： B32B314

CPC分类号： B23P6/005 ,  B23P15/02 ,  F01D5/187 ,  F01D5/288 ,  Y10T156/1089

摘要： An article having a design external aerodynamic shape includes a body with a body external surface and an outer portion external surface of an outer portion bonded with a part of but less than substantially all of the body surface. The external surfaces of the body and outer portion each define less than the design external aerodynamic shape. However, together they define such shape. The article is made by selecting the design external aerodynamic shape from an existing article having a first body and a first outer portion. A replacement outer portion is selected in an amount less than the first outer portion and bonded with a region less than substantially all of a replacement body external surface. The replacement body has a replacement body external surface and replacement body external shape different from the first body substantially by that amount. The replacement body is made with the replacement body external shape. Then the replacement outer portion is bonded with the region of the replacement body external surface. The result is that the external surfaces of the replacement body and replacement outer portion together define the design external aerodynamic shape.

摘要翻译： 具有设计外部空气动力学形状的物品包括具有主体外表面的主体和外部部分的外部部分外表面，该外部部分的外部部分与身体表面的一部分但基本上全部接合。 主体和外部部分的外表面各自限定为小于设计的外部空气动力学形状。 然而，它们一起定义了这样的形状。 通过从具有第一主体和第一外部部分的现有制品中选择设计的外部空气动力学形状来制造制品。 替换外部部分的选择量小于第一外部部分，并且以小于基本上全部替换体外表面的区域粘合。 替换体具有与第一体不同的替换体外表面和替换体外形，基本上为该量。 更换机身采用更换机身外形。 然后，替换外部部分与替换体外表面的区域结合。 结果是，替换体的外表面和置换外部部分一起限定了外部设计的空气动力学形状。

公开(公告)号：US06238187B1

公开(公告)日：2001-05-29

申请号：US09418115

申请日：1999-10-14

申请人： Jeff L. Dulaney ,  Allan H. Clauer ,  Joseph F. Clarady ,  Robert Baumgarten ,  Jerry G. Weinstein ,  Benjamin R. Hack

发明人： Jeff L. Dulaney ,  Allan H. Clauer ,  Joseph F. Clarady ,  Robert Baumgarten ,  Jerry G. Weinstein ,  Benjamin R. Hack

IPC分类号： B63H126

CPC分类号： B23P6/005 ,  C21D10/005 ,  F01D5/005

摘要： A method is disclosed for repairing damage to an airfoil. The method provides for the removal of a section of the airfoil that substantially encompasses the damaged area, which consequently leaves a void and a cut-away surface in the airfoil. A replacement piece larger than the residual void is provided for use in replacing the section removed from the airfoil. A joining operation welds or otherwise joins the replacement piece to the airfoil at the cut-away surface to form a joined airfoil. The joined airfoil has a seam between the airfoil and the replacement piece. At least a portion of the seam is processed by laser shock peening to induce compressive residual stresses therein.

摘要翻译： 公开了一种修复对翼型的损伤的方法。 该方法提供了去除基本上包围损坏区域的翼型部分，从而在翼型件中留下空隙和切除表面。 提供大于残余空隙的替换件，用于替换从翼型移除的部分。 接合操作在切割表面处焊接或以其他方式将更换件连接到翼型件以形成接合的翼型件。 连接的翼型件在翼型件和替换件之间具有接缝。 通过激光冲击喷丸处理至少一部分接缝以在其中引起压缩残余应力。

公开(公告)号：US6115917A

公开(公告)日：2000-09-12

申请号：US200724

申请日：1998-11-27

申请人： John Francis Nolan ,  Thomas Eugene Gustafson ,  David John Grubish

发明人： John Francis Nolan ,  Thomas Eugene Gustafson ,  David John Grubish

IPC分类号： B23K9/00 ,  B23K9/02 ,  B23K9/028 ,  B23K9/16 ,  B23K9/167 ,  B23P6/00 ,  C21D1/30 ,  C21D9/38 ,  F01D5/00 ,  F01D5/06

CPC分类号： B23P6/005 ,  B23K9/0026 ,  B23K9/0213 ,  B23K9/028 ,  B23K9/16 ,  B23K9/167 ,  C21D9/38 ,  F01D5/005 ,  F01D5/063 ,  B23K2201/001 ,  C21D1/30 ,  F05D2230/80 ,  F05D2250/293 ,  G01N2291/044 ,  G01N2291/2675 ,  G01N2291/2693 ,  Y10T29/49318 ,  Y10T29/4973

摘要： A method of repairing a turbine rotor wheel having an annular damaged dovetail includes removing the annular damaged dovetail from the turbine wheel, leaving a wheel body having a rim. A forged ring is welded to the rim and dovetails are formed in the forged ring to accommodate turbine bucket dovetails. The welding process including preheating, welding, and stress-relieving are performed while the rotor under repair is disposed in a lathe for rotation about a horizontal axis. The turbine rotor repair is accomplished from start to finish without displacing the rotor from the lathe.

摘要翻译： 修复具有环形损坏的燕尾榫的涡轮转子轮的方法包括从涡轮机叶轮移除环形损坏的燕尾榫，留下具有轮辋的轮体。 锻造环焊接到轮辋上，燕尾形成在锻造环中，以适应涡轮斗式燕尾榫。 在将修理的转子设置在车床中以围绕水平轴线旋转的同时进行包括预热，焊接和应力消除的焊接过程。 涡轮转子修复从头到尾完成，而不会使转子从车床移位。

公开(公告)号：US6065344A

公开(公告)日：2000-05-23

申请号：US200722

申请日：1998-11-27

申请人： John Francis Nolan ,  Robert Matthew Benson ,  Dennis Eugene Lessard

发明人： John Francis Nolan ,  Robert Matthew Benson ,  Dennis Eugene Lessard

IPC分类号： B23K9/00 ,  B23K9/02 ,  B23K9/167 ,  G01N29/24 ,  G01N29/00

CPC分类号： B23P6/005 ,  B23K9/0026 ,  B23K9/0213 ,  B23K9/167 ,  G01N29/24 ,  B23K2201/001 ,  G01N2291/044 ,  G01N2291/2675 ,  G01N2291/2693

摘要： A damaged turbine rotor wheel dovetail is repaired by cutting off the annular dovetail and welding a new forged ring onto the remaining wheel body. Fine-line welding is accomplished by inserting welding apparatus into grooves opening through axial faces of the wheel body and ring and rotating the rotor to provide multiple welding passes. Periodic ultrasonic inspection of the welds is provided by applying an ultrasonic transducer to the periphery of the ring to detect defects in the weld. To enable the transducer to operate at high welding temperatures, a manifold is disposed about the transducer defining a coolant cavity. Cooling medium is supplied the coolant cavity to maintain the transducer operable within predetermined temperature operating limits.

摘要翻译： 通过切割环形燕尾榫并将新的锻造环焊接到剩余的车轮主体上来修复损坏的涡轮转子轮燕尾榫。 通过将焊接设备插入通过轮体和环的轴向面的槽中并且使转子旋转以提供多个焊接过程来实现细线焊接。 通过在环的周围施加超声波换能器来检测焊缝中的缺陷，来提供对焊缝的定期超声波检查。 为了使传感器能够在高焊接温度下工作，歧管围绕换能器设置，限定冷却剂腔。 向冷却介质供应冷却剂腔，以使换能器在预定的温度操作限度内可操作。

公开(公告)号：US6049979A

公开(公告)日：2000-04-18

申请号：US200723

申请日：1998-11-27

申请人： John Francis Nolan ,  Lawrence Michael Grycko ,  David Roy Parker ,  Gerald Richard Crawmer

发明人： John Francis Nolan ,  Lawrence Michael Grycko ,  David Roy Parker ,  Gerald Richard Crawmer

IPC分类号： B23K9/00 ,  B23K9/02 ,  B23K9/095 ,  B23K9/167 ,  C21D1/30 ,  C21D9/38 ,  F01D5/00 ,  B23P15/00

CPC分类号： B23P6/005 ,  B23K9/0026 ,  B23K9/0213 ,  B23K9/0956 ,  B23K9/167 ,  C21D9/38 ,  F01D5/005 ,  B23K2201/001 ,  C21D1/30 ,  F05D2250/293 ,  G01N2291/044 ,  G01N2291/2675 ,  G01N2291/2693 ,  Y10T29/49318 ,  Y10T29/49336

摘要： The welding method for repairing a turbine rotor dovetail includes removal of buckets from damaged dovetails, removing a damaged dovetail from a turbine wheel, leaving a rotor wheel body having a rim. A plurality of ring sections are disposed about the wheel body rim, leaving axially opening annular grooves along opposite sides of the wheel. Welding apparatus including an electrode, welding wire and gas-carrying tube are inserted into the groove through an axial face of the wheel. One or more cover plates are disposed to overlie the groove at the location of its opening through the axial face of the wheel to at least partially seal the groove at its opening and maintain welding gas in the groove, enveloping the electrode and weld wire.

摘要翻译： 用于修理涡轮转子燕尾榫的焊接方法包括从损坏的燕尾槽中移除铲斗，从涡轮机轮移除损坏的燕尾榫，留下具有轮辋的转子轮体。 多个环形部分围绕车轮轮缘设置，沿车轮的相对侧留下轴向打开的环形槽。 包括电极，焊丝和气体输送管的焊接装置通过车轮的轴向面插入槽中。 一个或多个盖板被设置成在其开口的位置处通过轮的轴向面覆盖在凹槽上，以在其开口处至少部分地密封凹槽，并将焊接气体保持在凹槽中，包围电极和焊丝。