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1. 发明授权

US11651798B2 Base member and method of manufacturing the same, spindle motor, and hard disk drive device 有权
公开(公告)号：US11651798B2
公开(公告)日：2023-05-16
申请号：US17490634
申请日：2021-09-30
申请人： MINEBEA MITSUMI Inc.
发明人： Akihiko Suzuki , Tadashi Akahori
IPC分类号： G11B33/02 , B22D19/10
CPC分类号： G11B33/02 , B22D19/10
摘要： A base member serving as a part of a housing of a hard disk drive device. The base member includes a base body being a cast product, a machined surface obtained by machining a part of the base body at a side of an interior of the housing, an impregnating agent filled into a casting cavity exposed at the machined surface, and a coating film covering a surface including the machined surface of the base body.

2. 发明授权

US10422228B2 Manufacturing a monolithic component with discrete portions formed of different metals 有权
公开(公告)号：US10422228B2
公开(公告)日：2019-09-24
申请号：US15096544
申请日：2016-04-12
申请人： United Technologies Corporation
发明人： Lea Kennard Castle , Mario P. Bochiechio
IPC分类号： B22D19/00 , B22D19/04 , B22D19/16 , B22D21/00 , B22D25/02 , B22D27/04 , F01D5/14 , F04D29/32 , F04D29/38 , F01D5/28 , B22D19/10
摘要： Methods are provided for manufacturing a component. In one method, first metal material is cast into a first body. At least a portion of the first body is machined. Second metal material is cast onto at least the machined portion of the first body to form a monolithic second body. A first portion of the second body is formed by the first metal material, A second portion of the second body is formed by the second metal material. The second metal material is different from the first metal material.

3. 发明授权

US10265810B2 System and method for performing an in situ repair of an internal component of a gas turbine engine 有权
公开(公告)号：US10265810B2
公开(公告)日：2019-04-23
申请号：US14957660
申请日：2015-12-03
申请人： General Electric Company
发明人： David Scott Diwinsky , Herbert Chidsey Roberts
IPC分类号： B23P6/00 , B22D19/10 , B22D25/02 , F01D25/24 , B22F7/06 , F01D5/00 , B22F5/04 , B23P6/04 , G02B23/24 , B22F5/00
摘要： In one aspect, a method for performing in situ repairs of internal components of a gas turbine engine may generally include inserting a repair tool through an access port of the gas turbine engine such that the repair tool includes a tip end positioned within the gas turbine engine and a material supply end positioned outside the gas turbine engine. The method may also include positioning the tip end of the repair tool adjacent to a defect of an internal component of the gas turbine engine, wherein the defect defines a fillable volume along a portion of the internal component. In addition, the method may include supplying a filler material to the tip end of the repair tool and expelling the filler material from the tip end of the repair tool such that the fillable volume is at least partially filled with the filler material.

4. 发明授权

US09718127B2 Method for forming components using additive manufacturing and re-melt 有权
公开(公告)号：US09718127B2
公开(公告)日：2017-08-01
申请号：US15228585
申请日：2016-08-04
申请人： United Technologies Corporation
发明人： JinQuan Xu
IPC分类号： B22D23/06 , B22C7/02 , B22D27/04 , B33Y10/00 , B33Y40/00 , B28B1/00 , B33Y70/00 , B33Y80/00 , F01D25/00 , B22F3/105 , B22F5/04 , B22F7/06 , B23K15/00 , B23K26/00 , B23K26/342 , B22D19/10 , B22F5/00 , B23P6/00 , C30B11/00 , C30B21/02 , C22C19/03 , C22C19/07 , C30B29/52 , C22C38/00 , F01D5/00 , F01D5/14 , F01D5/18 , F01D5/28 , F01D5/30 , F01D5/34 , B22C9/24 , B23K101/00 , B23K103/18 , B23K103/00 , B23P15/02 , B22F3/24
CPC分类号： B22D27/045 , B22C9/24 , B22D19/10 , B22F3/1055 , B22F5/007 , B22F5/04 , B22F7/06 , B22F2003/248 , B22F2998/10 , B23K15/0086 , B23K15/0093 , B23K26/0006 , B23K26/342 , B23K2101/001 , B23K2103/18 , B23K2103/52 , B23P6/007 , B23P15/02 , B28B1/001 , B33Y10/00 , B33Y40/00 , B33Y70/00 , B33Y80/00 , C22C19/03 , C22C19/07 , C22C38/00 , C30B11/00 , C30B11/002 , C30B11/003 , C30B21/02 , C30B29/52 , F01D5/005 , F01D5/14 , F01D5/18 , F01D5/186 , F01D5/187 , F01D5/284 , F01D5/3084 , F01D5/34 , F01D25/005 , F05D2220/32 , F05D2230/21 , F05D2230/31 , F05D2230/50 , F05D2240/10 , F05D2240/24 , F05D2300/10 , F05D2300/175 , F05D2300/20 , F05D2300/21 , F05D2300/22 , F05D2300/222 , F05D2300/6033 , F05D2300/607 , F05D2300/609 , Y02P10/292 , Y02P10/295
摘要： A method of manufacturing a component includes additively manufacturing a crucible; directionally solidifying a metal material within the crucible; and removing the crucible to reveal the component. A component for a gas turbine engine includes a directionally solidified metal material component, the directionally solidified metal material component having been additively manufactured of a metal material concurrently with a core, the metal material having been remelted and directionally solidified.

5. 发明授权

US09144822B2 Methods and systems for joining materials 有权
标题翻译：连接材料的方法和系统
公开(公告)号：US09144822B2
公开(公告)日：2015-09-29
申请号：US13631162
申请日：2012-09-28
申请人： General Electric Company
发明人： Qi Zhao , Robert John Zabala , Laurent Cretegny , Jeffrey Jon Schoonover , Mark Kevin Meyer , Keith Anthony Lauria , William R Catlin
IPC分类号： B05B7/16 , B05C11/10 , B05D1/26 , B22D19/10 , B23K3/06 , B05C5/00
CPC分类号： B05D1/26 , B05C5/001 , B22D19/10 , B23K3/0638
摘要： A method is provided for joining a filler material to a substrate material. The method includes melting the filler material within a melting chamber of a crucible such that the filler material is molten. The crucible has an outlet fluidly connected to the melting chamber. The method also includes holding the filler material within the melting chamber of the crucible by applying a first pressure differential across the outlet of the crucible, and releasing the filler material from the melting chamber of the crucible by applying a second pressure differential across the outlet of the crucible to deliver the filler material to a target site of the substrate material. The second pressure differential has a different value than the first pressure differential.
摘要翻译：提供了一种用于将填充材料接合到基底材料的方法。该方法包括在坩埚的熔化室内熔化填料，使填料材料熔化。坩埚具有流体连接到熔化室的出口。该方法还包括通过在坩埚的出口处施加第一压力差来将填料材料保持在坩埚的熔化室内，并且通过在坩埚的出口处施加第二压差来从坩埚的熔化室释放填充材料坩埚将填充材料输送到基材材料的靶位置。第二压力差具有与第一压差不同的值。

6. 发明申请

US20090217499A1 VEHICLE COLLISION REPAIR PROCESS AND SYSTEM 审中-公开
标题翻译：车辆碰撞维修过程和系统
公开(公告)号：US20090217499A1
公开(公告)日：2009-09-03
申请号：US12399674
申请日：2009-03-06
申请人： MICHAEL GIARRIZZO, JR.
发明人： MICHAEL GIARRIZZO, JR.
IPC分类号： B23P6/00 , B22D19/10 , B65G35/00
CPC分类号： B60S5/00 , B23P6/00 , B60S13/00 , Y10T29/49718 , Y10T29/49721 , Y10T29/4973 , Y10T29/49746
摘要： A vehicle collision repair system and process is provided. The system and process utilizes interdependent collision repair stages and specifically tooled stations or work spaces. The system and process utilizes a rail system for advancing vehicles having collision damage through the stages of the collision repair process.
摘要翻译：提供车辆碰撞修复系统和过程。系统和过程利用相互依赖的碰撞修复阶段，特别是工具站或工作空间。该系统和过程利用轨道系统，用于通过碰撞修复过程的阶段推进具有碰撞损坏的车辆。

7. 发明申请

US20070068648A1 Method for repairing die cast dies 审中-公开
标题翻译：修模模具的方法
公开(公告)号：US20070068648A1
公开(公告)日：2007-03-29
申请号：US11238383
申请日：2005-09-28
申请人： Yiping Hu , William Hehmann , Clyde Taylor
发明人： Yiping Hu , William Hehmann , Clyde Taylor
IPC分类号： B22D19/10
CPC分类号： B22D7/068 , B22D17/2209
摘要： Methods are provided for repairing a worn surface of a steel die-cast die. The method includes heating an amorphous material to a predetermined temperature with a laser beam and allowing the melted amorphous material to solidify to thereby form an amorphous layer over the worn surface. These processes are useful for eliminating or minimizing cracking and/or part distortion and minimize heat-affected zone during welding. In addition, the formation of an amorphous layer over the worn surface allows the repaired die-cast die to better withstand typical operating environments than previous repair materials. These methods combine low heat input welding with amorphous alloys to effectively repair die-cast dies.
摘要翻译：提供了用于修复钢模压模的磨损表面的方法。该方法包括用激光束将非晶材料加热至预定温度，并使熔融的无定形材料固化，从而在磨损表面上形成非晶层。这些方法对于消除或最小化开裂和/或部件变形以及使焊接期间的热影响区域最小化是有用的。此外，在磨损表面上形成非晶层允许修复的压铸模具比以前的修补材料更好地承受典型的操作环境。这些方法结合了低热输入焊接和非晶态合金，有效地修复了压铸模具。

8. 发明授权

US6024418A Axle repair method and related assembly 失效
标题翻译：车轴修理方法及相关装配
公开(公告)号：US6024418A
公开(公告)日：2000-02-15
申请号：US846139
申请日：1997-04-25
申请人： James L. Ebert
发明人： James L. Ebert
IPC分类号： B23K31/02 , B22D19/10
CPC分类号： B23K31/02 , B23K2201/04 , Y10T29/49737
摘要： A technique and related assembly for repairing axles such as large heavy duty axles for semitrailers and vehicles are disclosed. A single replacement spindle is utilized in conjunction with one of several sleeve components for the repair. The technique enables a wide array of axles to be easily repaired with a relatively small selection of components.
摘要翻译：公开了用于修理车轴的技术和相关组件，例如用于半挂车和车辆的大型重型车轴。单个更换主轴与几个套筒组件中的一个一起用于修理。该技术可以通过相对较小的组件选择轻松修复各种轴组。

9. 发明授权

US5822852A Method for replacing blade tips of directionally solidified and single crystal turbine blades 失效
标题翻译：用于更换定向凝固和单晶涡轮叶片的叶片尖端的方法
公开(公告)号：US5822852A
公开(公告)日：1998-10-20
申请号：US892034
申请日：1997-07-14
申请人： Bernard Patrick Bewlay , Melvin Robert Jackson
发明人： Bernard Patrick Bewlay , Melvin Robert Jackson
IPC分类号： B22D19/10 , B23K1/00 , B23P6/00 , C30B11/00 , F01D5/00 , F01D5/20 , B23P15/00
CPC分类号： F01D5/20 , B22D19/10 , B23K1/0018 , B23P6/005 , C30B11/00 , C30B29/52 , F01D5/005 , B23K2201/001 , Y10T29/49318 , Y10T29/49339 , Y10T29/49737 , Y10T29/49742
摘要： A method for repairing a blade tip of a turbine blade of a gas turbine engine. The method is particularly directed to replacing the squealer tip (14) of a directionally solidified (DS) or single crystal (SX) turbine blade (10), and can be carried out using a brazing or welding technique. The method generally entails the step of machining the tip (14) to remove any damaged, worn, oxidized or eroded portions thereof sustained by the blade (10) during engine operation. A DS or SX superalloy replacement tip (18) is then placed on the surface generated by the machining operation. If a brazing operation is used, a brazing alloy composition (16) is first applied to the blade tip or replacement tip (18) prior to placement of the replacement tip (18). The brazing alloy composition (16) is composed of at least two alloys, one of which having a melting point lower than the recrystallization temperature and solvus temperature of the superalloy of the turbine blade (10), such that heating causes the brazing alloy composition (16) to flow and thereby join the replacement tip (18) to the blade tip of the turbine blade (10). Alternatively, if a welding operation is employed, the joining operation entails transmitting current through the turbine blade (10) and replacement tip (18) to resistance weld the replacement tip (18) to the blade tip of the blade (10).
摘要翻译：一种用于修复燃气涡轮发动机的涡轮叶片的叶片尖端的方法。该方法特别涉及更换定向凝固（DS）或单晶（SX）涡轮叶片（10）的尖叫尖端（14），并且可以使用钎焊或焊接技术进行。该方法通常需要加工尖端（14）以消除在发动机操作期间由叶片（10）持续的任何损坏，磨损，氧化或侵蚀的部分的步骤。然后将DS或SX超合金替代头（18）放置在由加工操作产生的表面上。如果使用钎焊操作，则在放置替换刀片（18）之前，首先将钎焊合金组合物（16）施加到刀片尖端或替换刀片（18）。钎焊合金组合物（16）由至少两种合金组成，其中一种熔点低于涡轮叶片（10）的超合金的再结晶温度和溶解温度，使得加热导致钎焊合金组成（ 16）流动，从而将更换的尖端（18）连接到涡轮叶片（10）的叶片尖端。或者，如果采用焊接操作，则接合操作需要传递电流通过涡轮叶片（10）和更换尖端（18），以将替换尖端（18）电阻焊接到叶片（10）的叶片尖端。

10. 发明授权

US5676191A Solidification of an article extension from a melt using an integral mandrel and ceramic mold 失效
标题翻译：使用一体式心轴和陶瓷模具从熔体固化制品延伸
公开(公告)号：US5676191A
公开(公告)日：1997-10-14
申请号：US669793
申请日：1996-06-27
申请人： Bernard Patrick Bewlay , Melvin Robert Jackson , Ann Melinda Ritter , Wayne Alan Demo , Stephen Joseph Ferrigno
发明人： Bernard Patrick Bewlay , Melvin Robert Jackson , Ann Melinda Ritter , Wayne Alan Demo , Stephen Joseph Ferrigno
IPC分类号： F01D5/18 , B22D19/00 , B22D19/10 , B22D27/04 , F01D5/28 , B22D23/06
CPC分类号： B22D19/10 , C30B11/00 , C30B29/52 , Y10T29/49318
摘要： An extension is formed directly on an article by dipping a portion or end of the article having an attached integral mandrel into a molten bath of a compatible alloy, followed by withdrawal of the end under controlled conditions sufficient to cause an integral extension to solidify on the article. A ceramic mold is utilized over the dipped end of the article and the integral mandrel with a mold cavity that generally defines the shape of the extension to be formed. The mold may be formed in situ on the mandrel, or preformed and attached to the subject article over the mandrel. The integral mandrel is melted within the mold by dipping the mandrel into the molten alloy. The mandrel acts as a buffer between the molten material and the article while permitting melting of the article end and solidification of the integral extension. Extensions formed by the method of this invention have a microstructure that is continuous and compatible with that of the article. Such microstructures may include epitaxial growth of the extension from the microstructure of the article. The method establishes a temperature gradient within the article during solidification that may be further controlled by auxiliary heating and/or cooling of the article and/or extension during the practice of the method.
摘要翻译：通过将具有附接的整体心轴的制品的一部分或端部浸入相容合金的熔池中，直接在制品上形成延伸部，然后在足以引起整体延伸固化的受控条件下将端部取出文章。陶瓷模具被利用在制品的浸入端上，并且整体心轴具有通常限定待形成的延伸部的形状的模腔。模具可以在心轴上原位形成，或者通过心轴预成型并附着到主体制品上。通过将心轴浸入熔融合金中，整体心轴在模具内熔化。心轴作为熔融材料和制品之间的缓冲液，同时允许制品端部熔化并且整体延伸部分的固化。通过本发明的方法形成的延伸部具有与制品的连续且兼容的微结构。这种微结构可以包括从制品的微观结构延伸的外延生长。该方法在固化期间在制品内建立温度梯度，其可以在该方法的实践期间通过辅助加热和/或冷却制品和/或延伸来进一步控制。

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