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    UBER-COOLED MULTI-ALLOY INTEGRALLY BLADED ROTOR
    11.
    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。

    METHOD FOR SOLUTION HEAT TREATED ALLOY COMPONENTS
    12.
    发明申请
    METHOD FOR SOLUTION HEAT TREATED ALLOY COMPONENTS 审中-公开
    溶解热处理合金组分的方法

    公开(公告)号：US20140090753A1

    公开(公告)日：2014-04-03

    申请号：US13630566

    申请日：2012-09-28

    申请人： Chris Vargas ,  Eric A. Hansen ,  Raymond C. Benn ,  Daniel A. Bales ,  Ivan M. Schmidt ,  David W. Anderson ,  David Ulrich Furrer ,  William F. Matzke

    发明人： Chris Vargas ,  Eric A. Hansen ,  Raymond C. Benn ,  Daniel A. Bales ,  Ivan M. Schmidt ,  David W. Anderson ,  David Ulrich Furrer ,  William F. Matzke

    IPC分类号： C21D11/00

    CPC分类号： C21D11/005 ,  C21D11/00 ,  C22F1/10

    摘要： A method for adjusting properties of components made of an alloy includes providing historical data for one or more properties of components made of an alloy and produced at different times. The components are solution heat treated at a pre-established solution heat treatment condition. A trending change in the one or more properties is then identified and test specimens made of the alloy are provided. The test specimens are divided into a plurality of groups and solution heat treated at different conditions. The test specimens are then mechanically tested to provide empirical data. The empirical data is compared to performance criteria and a solution heat treatment condition is identified over which the empirical data meets the performance criteria. The pre-established solution heat treatment condition is then adjusted for future ones of the plurality of components according to the identified solution heat treatment condition.

    摘要翻译： 用于调整由合金制成的部件的性能的方法包括提供用于由不同时间生产的由合金制成的部件的一个或多个特性的历史数据。 组分在预先确定的固溶热处理条件下进行固溶热处理。 然后鉴定一种或多种性质的趋势变化，并提供由合金制成的试样。 将试样分成多组，在不同条件下进行热处理。 然后对试样进行机械测试以提供经验数据。 将经验数据与性能标准进行比较，并确定经验数据符合性能标准的解热处理条件。 然后根据所识别的固溶热处理条件，对多个部件中的未来部件调整预先设定的固溶热处理条件。

    IBR fixture and method of machining
    16.
    发明授权
    IBR fixture and method of machining 失效
    IBR夹具和加工方法

    公开(公告)号：US5867885A

    公开(公告)日：1999-02-09

    申请号：US115709

    申请日：1998-07-15

    申请人： Daniel A. Bales ,  Leroy F. Turner, Sr.

    发明人： Daniel A. Bales ,  Leroy F. Turner, Sr.

    IPC分类号： B23P15/02 ,  B23P15/00 ,  B23Q3/08 ,  B23Q7/00

    CPC分类号： B23Q3/086 ,  B23P15/006 ,  Y10T29/49316 ,  Y10T29/49998 ,  Y10T29/53961 ,  Y10T29/53978

    摘要： A fixture for use in the final machining operation of the integral bladed rotor (IBR) of a gas turbine engine comprises a rigid ring for surrounding the outer periphery of the IBR and supporting tapered pins that fit into the space between the blades and then molded therein with a plaster or plastic medium for securing the unit to the IBR for enhancing its structural integrity. The method of finishing the airfoils of the IBR includes inserting the pins in alternate spaces and working half of the blade surfaces in the pinless spaces and then removing the pins and inserting pins in the previously worked spaces and then molding the pins in place. The other half of the bladed surface is then worked in the pinless spaces until the airfoils are finally contoured. The unit is removed and heated to melt the residual cast medium to produce the finished product.

    摘要翻译： 用于燃气涡轮发动机的整体叶片式转子（IBR）的最终加工操作的固定装置包括用于围绕IBR的外周的刚性环和支撑锥形销，该锥形销装配到叶片之间的空间中，然后在其中模制 使用石膏或塑料介质将设备固定在IBR上，以提高其结构完整性。 完成IBR的翼型的方法包括将销钉插入交替的空间中，并将刀片表面的一半的刀片表面插入无钉空间中，然后将销钉插入先前加工的空间中，然后将销钉成型到位。 然后将刀片表面的另一半加工到无钉空间中，直到翼型件最终成型。 将单元取出并加热以熔化残留的流延介质以产生成品。

    DIE INSERTS FOR DIE CASTING
    18.
    发明申请
    DIE INSERTS FOR DIE CASTING 有权
    DIE铸件插件

    公开(公告)号：US20110233378A1

    公开(公告)日：2011-09-29

    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： B22C9/00 ,  B28B7/00

    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。

    IBR fixture
    19.
    发明授权
    IBR fixture 失效
    IBR夹具

    公开(公告)号：US5822841A

    公开(公告)日：1998-10-20

    申请号：US768370

    申请日：1996-12-17

    申请人： Daniel A. Bales ,  Leroy F. Turner, Sr.

    发明人： Daniel A. Bales ,  Leroy F. Turner, Sr.

    IPC分类号： B23P15/02 ,  B23P15/00 ,  B23Q3/08 ,  B25B27/14

    CPC分类号： B23Q3/086 ,  B23P15/006 ,  Y10T29/49316 ,  Y10T29/49998 ,  Y10T29/53961 ,  Y10T29/53978

    摘要： A fixture for use in the final machining operation of the integral bladed rotor (IBR) of a gas turbine engine comprises a rigid ring for surrounding the outer periphery of the IBR and supporting tapered pins that fit into the space between the blades and then molded therein with a plaster or plastic medium for securing the unit to the IBR for enhancing its structural integrity. The method of finishing the airfoils of the IBR includes inserting the pins in alternate spaces and working half of the blade surfaces in the pinless spaces and then removing the pins and inserting pins in the previously worked spaces and then molding the pins in place. The other half of the bladed surface is then worked in the pinless spaces until the airfoils are finally contoured. The unit is removed and heated to melt the residual cast medium to produce the finished product.

    摘要翻译： 用于燃气涡轮发动机的整体叶片转子（IBR）的最终加工操作的固定装置包括用于围绕IBR的外周的刚性环和支撑锥形销，该锥形销装配到叶片之间的空间中，然后在其中模制 使用石膏或塑料介质将设备固定在IBR上，以提高其结构完整性。 完成IBR的翼型的方法包括将销钉插入交替的空间中，并将刀片表面的一半的刀片表面插入无钉空间中，然后将销钉插入先前加工的空间中，然后将销钉成型到位。 然后将刀片表面的另一半加工到无钉空间中，直到翼型件最终成型。 将单元取出并加热以熔化残留的流延介质以产生成品。

    Method of simultaneously forming rocket thrust chamber cooling tubes
    20.
    发明授权
    Method of simultaneously forming rocket thrust chamber cooling tubes 失效
    同时形成火箭推进室冷却管的方法

    公开(公告)号：US5477613A

    公开(公告)日：1995-12-26

    申请号：US213306

    申请日：1994-03-14

    申请人： Daniel A. Bales ,  James R. Joyce

    发明人： Daniel A. Bales ,  James R. Joyce

    IPC分类号： B23P15/00 ,  F02K9/64

    CPC分类号： B23P15/26 ,  B23P15/008 ,  F02K9/64 ,  Y10T29/49346 ,  Y10T29/49897

    摘要： A plurality of tubes are placed side-by-side on the forming surface of a die, another die is brought into contact with the tubes, thus sandwiching the tubes therebetween. The two dies are then placed into a press that forces the dies together, simultaneously deforming the tubes into intimate contact with each other, thereby producing an exacting fit between adjacent tubes.

    摘要翻译： 将多个管并排放置在模具的成形表面上，使另一个管芯与管接触，从而将管夹在其间。 然后将两个模具放置在压力机中，该压力机将模具压在一起，同时使管彼此变形成紧密接触，从而在相邻的管之间产生严格的配合。