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    UBER-COOLED MULTI-ALLOY INTEGRALLY BLADED ROTOR
    1.
    发明申请
    UBER-COOLED MULTI-ALLOY INTEGRALLY BLADED ROTOR 审中-公开
    UBER-COOLED多合金综合叶片转子

    公开(公告)号：US20140140859A1

    公开(公告)日：2014-05-22

    申请号：US13630120

    申请日：2012-09-28

    申请人： Daniel A. Bales ,  Steven D. Jenkel ,  Benjamin T. Fisk

    发明人： Daniel A. Bales ,  Steven D. Jenkel ,  Benjamin T. Fisk

    IPC分类号： F01D5/18

    CPC分类号： F01D5/18 ,  F01D5/28 ,  F01D5/30 ,  F01D5/34 ,  F02C7/00 ,  F05D2230/40 ,  Y10T29/49339

    摘要： Uber-cooled multi-alloy integrally bladed rotors (IBR) are made having blades with internal cooling passages with a cavity in the root portion attached to a disk having a protrusion on the periphery of the disk. The blades are put on the protrusion and the blade and disk are forced together, followed by locally heating the blade cavity/disk protrusion to a temperature between the blade and disk material softening temperatures, causing the protrusion to deform against the blade cavity, and holding them in place until bonding occurs. Subsequent to bonding the portion of the blade that defines the cavity is removed.

    摘要翻译： Uber冷却的多合金整体叶片式转子（IBR）制成具有内部冷却通道的叶片，其中根部部分中的腔体附接到具有在盘周边上的突起的盘。 将刀片放在突起上，将刀片和盘片压在一起，随后将刀片腔/盘突起局部加热到刀片和盘材料软化温度之间的温度，导致突起相对于刀片腔变形，并保持 它们到位，直到粘合发生。 在粘合之后，去除限定空腔的叶片的部分。

    Non-destructive inspection method for metallic alloys
    2.
    发明授权
    Non-destructive inspection method for metallic alloys 有权
    金属合金无损检测方法

    公开(公告)号：US08616077B2

    公开(公告)日：2013-12-31

    申请号：US12535896

    申请日：2009-08-05

    申请人： Joseph Parkos ,  Daniel A. Bales ,  Mimi Nguyen-Vu ,  Gary M. Lomasney ,  Philip H. Ratliff

    发明人： Joseph Parkos ,  Daniel A. Bales ,  Mimi Nguyen-Vu ,  Gary M. Lomasney ,  Philip H. Ratliff

    IPC分类号： G01N21/66

    CPC分类号： G01N33/20 ,  C23F1/00 ,  G01N1/4055 ,  G01N2001/4061

    摘要： A non-destructive inspection method for detecting the presence of a contaminant that has alloyed with a metallic alloy of a part includes exposing the metallic alloy of the part to an extraction solution. The extraction solution extracts at least a portion of any of the contaminant that has alloyed with the metallic alloy. The extraction solution can then be analyzed to determine whether the solution includes any of the contaminant element, which indicates whether the part includes any of the contaminant element.

    摘要翻译： 用于检测与部件的金属合金合金化的污染物的存在的非破坏性检查方法包括将该部件的金属合金暴露于提取溶液中。 提取溶液提取与金属合金合金化的任何污染物的至少一部分。 然后可以分析提取溶液以确定溶液是否包含任何污染元素，其指示该部分是否包括任何污染物元素。

    Die inserts for die casting
    6.
    发明授权
    Die inserts for die casting 有权
    压铸模插件

    公开(公告)号：US08814557B2

    公开(公告)日：2014-08-26

    申请号：US12730498

    申请日：2010-03-24

    申请人： Daniel A. Bales ,  Steven J. Bullied ,  Carl R. Verner

    发明人： Daniel A. Bales ,  Steven J. Bullied ,  Carl R. Verner

    IPC分类号： B22D17/24 ,  B29C39/26 ,  B28B7/34 ,  B22C9/08 ,  B22C9/10

    CPC分类号： B22D19/00 ,  B22D17/24

    摘要： An apparatus for casting material has a die for receiving a compressive force, the die having a shaped-opening for receiving a die insert. The die insert has an exterior shape that is adapted to cooperate with and be received in the opening such that compressive forces impinging upon the die are focused upon the die insert such that tensile forces within the die and impinging upon the die insert are minimized.

    摘要翻译： 用于铸造材料的设备具有用于接收压缩力的模具，该模具具有用于接收模具插入件的成形开口。 模具插入件具有适于与开口配合并被接收在开口中的外部形状，使得冲击模具的压缩力聚焦在模具插入件上，使得模具内的冲击力和冲击在模具插入件上的冲击力被最小化。

    Method of making a diffusion bonded rocket chamber
    9.
    发明授权
    Method of making a diffusion bonded rocket chamber 失效
    制造扩散粘结火箭筒的方法

    公开(公告)号：US5386628A

    公开(公告)日：1995-02-07

    申请号：US812319

    申请日：1991-12-23

    申请人： Mark L. Hartman ,  Daniel A. Bales

    发明人： Mark L. Hartman ,  Daniel A. Bales

    IPC分类号： B23P15/00 ,  F02K9/64

    CPC分类号： B23P15/008 ,  F02K9/64 ,  Y10T29/49346 ,  Y10T29/49364

    摘要： A method of producing a rocket thrust chamber includes positioning cooling tubes within a structural jacket to form a tube bundle, and positioning a mandrel within the tube bundle thereby sandwiching the tubes between the jacket and the mandrel. The tubes are then inflated at high temperature into intimate contact with adjacent tubes and the jacket, and the temperature is maintained until bonding has occurred between the tubes and jacket.

    摘要翻译： 制造火箭推进室的方法包括将冷却管定位在结构夹套内以形成管束，并将心轴定位在管束内，从而将管夹在套管和心轴之间。 然后将管在高温下充气以与相邻的管和护套紧密接触，并保持温度，直到管和护套之间发生粘合。

    Method of making a rocket chamber construction
    10.
    发明授权
    Method of making a rocket chamber construction 失效
    制造火箭筒室的方法

    公开(公告)号：US5375325A

    公开(公告)日：1994-12-27

    申请号：US889002

    申请日：1992-05-26

    申请人： Daniel A. Bales ,  Mark L. Hartman

    发明人： Daniel A. Bales ,  Mark L. Hartman

    IPC分类号： B23P15/00 ,  F02K9/64

    CPC分类号： B23P15/008 ,  F02K9/64 ,  Y10T29/49346 ,  Y10T29/49364

    摘要： A method of producing a rocket thrust chamber includes positioning sleeved cooling tubes within a structural jacket to form a tube bundle, and positioning a liner within the tube bundle thereby sandwiching the tubes between the jacket and the liner. The tubes are then subjected to high internal pressure and inflated at high temperature while the liner is simultaneously subjected to the same high pressure, thereby forcing the sleeved tubes into intimate contact with adjacent sleeved tubes, the liner and the jacket, and the temperature is maintained until bonding has occurred between the liner, sleeved tubes and jacket.

    摘要翻译： 制造火箭推进室的方法包括将套管冷却管定位在结构夹套内以形成管束，并将衬管定位在管束内，从而将管夹在套管和衬套之间。 然后使管受到高内压并在高温下充气，同时衬套同时经受相同的高压，从而迫使套管与相邻的套管，衬套和护套紧密接触，并保持温度 直到衬套，套管和护套之间发生粘合。