Brazed joining with electrical deposition
    1.
    发明授权
    Brazed joining with electrical deposition 有权
    钎焊接合电沉积

    公开(公告)号:US09061363B2

    公开(公告)日:2015-06-23

    申请号:US11478772

    申请日:2006-07-03

    摘要: The present method creates a relatively thin in situ brazing alloy layer upon first and second component edges which are brought together in order to create a component joint. This in situ brazing alloy layer is created by deposition of brazing elements, such as copper or nickel, from an electrical discharge cutting process electrode depletion utilized in order to cut the component edges, and then a subsequent brazing technique creates through interstitial migration between that brazing alloy layer and the underlying material substrate of the components a robust component joint wherein the in situ brazing alloy layer penetrates the respective component cut edge surface to only a limited depth such that the geometric effect is similarly limited, and the properties of the underlying component material structure are maintained.

    摘要翻译: 本方法在第一和第二部件边缘上形成相对薄的原位钎焊合金层,这些合金层被聚集在一起以形成部件接头。 这种原位钎焊合金层是通过从用于切割部件边缘的放电切割工艺电极耗尽中的钎焊元件(例如铜或镍)沉积产生的,然后通过该钎焊之间的间隙迁移产生后续的钎焊技术 合金层和组件的下层材料基底是坚固的部件接头,其中原位钎焊合金层仅穿过相应的部件切割边缘表面,仅限于有限的深度,使得几何效应被类似地限制,并且下面的部件材料的性质 维护结构。

    Joining and a repair method
    2.
    发明申请
    Joining and a repair method 有权
    加盟和修理方法

    公开(公告)号:US20100129255A1

    公开(公告)日:2010-05-27

    申请号:US12451385

    申请日:2008-05-23

    IPC分类号: B22F7/04 B23K31/02

    摘要: A method of forming a fully consolidated joint between first and second components comprising the steps of forming a slot in the first component; inserting at least part of the second component into the slot; inserting a powder material into the slot; heating the powder material to form a pressure tight skin; and applying hot isostatic pressure to the pressure tight skin to form a fully consolidated joint. Also a method of repairing a component.

    摘要翻译: 一种在第一和第二部件之间形成完全固定接头的方法,包括以下步骤:在第一部件中形成槽; 将所述第二部件的至少一部分插入所述槽中; 将粉末材料插入槽中; 加热粉末材料以形成压力紧张的皮肤; 并向耐压皮肤施加热等静压,以形成完全固结的接头。 还有一种修复组件的方法。

    Method and assembly for forming a component by isostatic pressing
    3.
    发明授权
    Method and assembly for forming a component by isostatic pressing 有权
    通过等静压法形成零件的方法和装配

    公开(公告)号:US09034246B2

    公开(公告)日:2015-05-19

    申请号:US12822394

    申请日:2010-06-24

    申请人: Wayne E. Voice

    发明人: Wayne E. Voice

    摘要: A method of forming a component (30) by isostatic pressing, the method comprising: providing a canister (4) suitable for isostatic pressing, the canister comprising first and second membranes (14, 16) which, in use, are disposed within the canister (4); the first and second membranes (14, 16) defining a component cavity (24) disposed between the first and second membranes (14, 16), a first tool cavity (26) disposed between the first membrane (14) and an adjacent wall (10) of the canister (4), and a second tool cavity (28) disposed between the second membrane (16) and another adjacent wall (12) of the canister (4); filling the component cavity (24) with the component powder for forming the component (30); filling the first and second tool cavities (26, 28) with a second tool powder; and isostatically pressing the canister (4) to form the component (30).

    摘要翻译: 一种通过等静压法形成组分(30)的方法,所述方法包括:提供适于等静压的罐(4),该罐包括第一和第二膜(14,16),其在使用中设置在罐内 (4); 第一和第二膜(14,16)限定设置在第一和第二膜(14,16)之间的部件空腔(24),设置在第一膜(14)和邻近壁(14,16)之间的第一工具空腔 以及设置在所述第二膜(16)和所述罐(4)的另一相邻壁(12)之间的第二工具腔(28); 用组分粉末填充组件空腔(24)以形成组件(30); 用第二工具粉末填充第一和第二工具空腔(26,28); 并均匀地压制罐(4)以形成部件(30)。

    Method of fluid jet machining
    4.
    发明授权
    Method of fluid jet machining 有权
    流体喷射加工方法

    公开(公告)号:US08568197B2

    公开(公告)日:2013-10-29

    申请号:US12385657

    申请日:2009-04-15

    IPC分类号: B24B49/00

    摘要: A pocket (6) is machined into the surface of a component (9) by pressurising a fluid (1) and directing a jet (11) of the pressurized fluid (1) at the surface to be machined. Continuous relative movement is provided between the component (9) and the pressurized jet (11) of fluid (1) during machining. Material is removed from the component (9) in a series of layers, whereby the path of the fluid jet (11) in one of the layers is perpendicular to the path of the fluid jet (11) in the subsequent layer. The fluid jet (11) operates continuously until the required amount of material has been removed from the component (9).

    摘要翻译: 通过加压流体(1)并将加压流体(1)的射流(11)引导到待加工的表面上,将口袋(6)加工成部件(9)的表面。 在加工过程中,组件(9)和流体(1)的加压喷嘴(11)之间提供连续相对运动。 材料以一系列层从组件(9)中移除,其中一层中的流体射流(11)的路径垂直于随后层中的流体射流(11)的路径。 流体射流(11)连续运行,直到从组件(9)中去除了所需量的材料。

    Manufacturing process and apparatus
    5.
    发明授权
    Manufacturing process and apparatus 有权
    制造工艺和设备

    公开(公告)号:US07763204B2

    公开(公告)日:2010-07-27

    申请号:US12232237

    申请日:2008-09-12

    摘要: A manufacturing process that comprises placing an article within a particulate medium (4), the article being provided with a molded body (8) of small ceramic particles. On application of heat and pressure the small ceramic particles are pushed between the particulate medium (4) to permit localized deformation of the article (2).

    摘要翻译: 一种制造方法,其包括将物品放置在颗粒介质(4)内,所述制品设置有小陶瓷颗粒的成型体(8)。 在施加热和压力的情况下,将小陶瓷颗粒推到颗粒介质(4)之间以允许制品(2)的局部变形。

    Method of heat treating titanium aluminide
    6.
    发明授权
    Method of heat treating titanium aluminide 有权
    铝化钛热处理方法

    公开(公告)号:US07704339B2

    公开(公告)日:2010-04-27

    申请号:US11654596

    申请日:2007-01-18

    IPC分类号: C22F1/18 C22C14/00

    CPC分类号: C22F1/183 C22C14/00 C22C30/00

    摘要: A gamma titanium aluminide alloy consisting of 46 at % aluminium, 8 at % tantalum and the balance titanium plus incidental impurities has an alpha transus temperature Tα between 1310° C. and 1320° C. The gamma titanium aluminide alloy was heated to a temperature T1=1330° C. and was held at T1=1330° C. for 1 hour or longer. The gamma titanium aluminide alloy was air cooled to ambient temperature to allow the massive transformation to go to completion. The gamma titanium aluminide alloy was heated to a temperature T2=1250° C. to 1290° C. and was held at T2 for 4 hours. The gamma titanium aluminide alloy was air cooled to ambient temperature. The gamma titanium aluminide alloy has a fine duplex microstructure comprising differently orientated alpha plates in a massively transformed gamma matrix. The heat treatment reduces quenching stresses and allows larger castings to be grain refined.

    摘要翻译: 由46原子%铝,8原子%钽和余量钛加附加杂质组成的γ钛铝化物合金具有在1310℃和1320℃之间的α转变温度Tα。将γ钛铝化合物加热至温度T1 = 1330℃,并在T1 = 1330℃保持1小时以上。 将γ钛化铝合金空气冷却至环境温度以使大规模转化完成。 将γ钛化铝合金加热至T2 = 1250℃至1290℃的温度,并在T2保持4小时。 将γ钛铝化合物空气冷却至环境温度。 γ钛铝化合物具有包含在大量转化的γ基质中的不同取向的α板的精细双相微结构。 热处理降低了淬火应力,并允许更大的铸件被精细化。

    Manufacturing process and apparatus
    7.
    发明申请
    Manufacturing process and apparatus 有权
    制造工艺和设备

    公开(公告)号:US20090096123A1

    公开(公告)日:2009-04-16

    申请号:US12232237

    申请日:2008-09-12

    IPC分类号: B29C67/02

    摘要: A manufacturing process that comprises placing an article within a particulate medium (4), the article being provided with a moulded body (8) of small ceramic particles. On application of heat and pressure the small ceramic particles are pushed between the particulate medium (4) to permit localised deformation of the article (2).

    摘要翻译: 一种制造方法,其包括将物品放置在颗粒介质(4)内,所述制品设置有小陶瓷颗粒的成型体(8)。 在施加热和压力的情况下,将小陶瓷颗粒推到颗粒介质(4)之间以允许制品(2)的局部变形。

    Centrifugal casting method and apparatus
    8.
    发明申请
    Centrifugal casting method and apparatus 审中-公开
    离心铸造方法和装置

    公开(公告)号:US20090071622A1

    公开(公告)日:2009-03-19

    申请号:US12222651

    申请日:2008-08-13

    申请人: Wayne E. Voice

    发明人: Wayne E. Voice

    IPC分类号: B22D13/00

    CPC分类号: B22D13/107

    摘要: Apparatus for forming a cast component has a chamber for holding an alloy and which is rotated about an axis to separate an impurity from the alloy by centrifugal force. The chamber feeds a mould that is also rotating and into which the alloy is supplied to form a component by centrifugal casting.

    摘要翻译: 用于形成铸造部件的装置具有用于保持合金的腔室,并且其围绕轴线旋转以通过离心力从合金中分离杂质。 腔室还进给也旋转的模具,通过离心铸造将合金供应到其中以形成部件。

    METHOD OF FORGING A TITANIUM ALLOY
    9.
    发明申请
    METHOD OF FORGING A TITANIUM ALLOY 失效
    锻造钛合金的方法

    公开(公告)号:US20080011035A1

    公开(公告)日:2008-01-17

    申请号:US11176382

    申请日:2005-07-08

    申请人: Wayne E. Voice

    发明人: Wayne E. Voice

    IPC分类号: B21B45/02

    摘要: A method of forging a titanium alloy component comprises applying a protective coating onto the surface of the titanium alloy component. A glass lubricant coating is applied onto the protective coating and the titanium alloy component is forged at a high temperature. The glass lubricant coating comprises a borosilicate glass lubricant coating. The protective coating comprises an aluminide coating, a silicon modified aluminide coating, a platinum aluminide coating, an aluminium coating or a platinum coating. The titanium alloy component may be a compressor blade, or a compressor vane, of a high-pressure compressor of a gas turbine engine.

    摘要翻译: 锻造钛合金部件的方法包括在钛合金部件的表面上涂覆保护涂层。 将玻璃润滑剂涂层施加到保护涂层上,并且钛合金部件在高温下锻造。 玻璃润滑剂涂层包括硼硅酸盐玻璃润滑剂涂层。 保护涂层包括铝化物涂层,硅改性铝化物涂层,铂铝化物涂层,铝涂层或铂镀层。 钛合金部件可以是燃气轮机的高压压缩机的压缩机叶片或压缩机叶片。

    Method of manufacturing a component
    10.
    发明申请
    Method of manufacturing a component 审中-公开
    制造零件的方法

    公开(公告)号:US20070272350A1

    公开(公告)日:2007-11-29

    申请号:US11802470

    申请日:2007-05-23

    IPC分类号: B32B37/00

    摘要: A first workpiece comprises a compressor disc (2) manufactured from a titanium alloy forging. A number of second workpieces, aerofoil blades (4), also forged from titanium alloy are arranged for attachment to the disc (2). The aerofoil blades (4) are evenly distributed around the radially outer surface (8) of the disc (2) and the root (6) of each blade (4) is joined to the surface (8) of the disc (2) by hot isostatic pressing. To assist in joining the blades (4) to the disc (2), one of the surfaces (6 or 8) is modified by reducing the density by 50-70% to a depth of 0.25-0.5 mm. This is achieved by depositing a layer of metal powder on the surface. Modifying one of the surfaces (6 or 8) forms a compliant layer between the workpieces (2 and 4). When pressurised this compliant layer accommodates distortion during consolidation and also acts to disrupt the other surface to reveal virgin material and enhance bonding.

    摘要翻译: 第一工件包括由钛合金锻造制成的压缩机盘(2)。 多个第二工件,也由钛合金锻造的翼面叶片(4)被布置成附接到盘(2)。 翼型叶片(4)均匀分布在盘(2)的径向外表面(8)周围,并且每个叶片(4)的根部(6)通过以下方式连接到盘(2)的表面(8): 热等静压。 为了有助于将叶片(4)连接到盘(2),通过将密度减小50-70%至0.25-0.5mm的深度来改变其中一个表面(6或8)。 这是通过在表面上沉积一层金属粉末来实现的。 修改其中一个表面(6或8)在工件(2和4)之间形成柔顺层。 当加压时,该柔性层在固结期间容纳变形,并且还用于破坏另一表面以露出原始材料并增强粘合。