公开(公告)号：US10370984B2

公开(公告)日：2019-08-06

申请号：US15100663

申请日：2014-11-19

Applicant: United Technologies Corporation

Inventor： Iuliana Cernatescu ,  Thomas J. Watson ,  James O. Hansen ,  David Ulrich Furrer ,  Randy P. Salva

IPC: F01D5/28 ,  C30B29/52 ,  F01D5/14

Abstract: An airfoil includes an airfoil body that extends at least between leading and trailing edges, first and second sides, and radially inner and outer ends. The airfoil body includes an aluminum alloy that has a controlled crystallographic texture with respect to a predefined three-dimensional coordinate system. The airfoil can be used in the fan of a gas turbine engine.

公开(公告)号：US10252511B2

公开(公告)日：2019-04-09

申请号：US15441639

申请日：2017-02-24

Applicant: United Technologies Corporation

Inventor： Sergei F. Burlatsky ,  Dmitri Novikov ,  William J. Brindley ,  David Ulrich Furrer

IPC: B33Y10/00 ,  B33Y30/00 ,  B33Y50/02 ,  B33Y50/00 ,  B22F3/105 ,  G06F17/50 ,  B29C64/153 ,  B29C64/20 ,  B29C64/386 ,  B29C64/124

Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, each of the bounds being defined on a distinct parameter of an additive manufacturing process and each of the bounds being directly related to the occurrence of a balling flaw, each of the parameters being a dimension in a multi-dimensional coordinate system, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as free of balling flaws when the coordinate position is within the multi-dimensional space.

公开(公告)号：US10252509B2

公开(公告)日：2019-04-09

申请号：US15441630

申请日：2017-02-24

Applicant: United Technologies Corporation

Inventor： Sergei F. Burlatsky ,  Dmitri Novikov ,  William J. Brindley ,  David Ulrich Furrer

IPC: B33Y10/00 ,  B33Y30/00 ,  B33Y50/02 ,  G05B19/042 ,  B29C67/00 ,  G06F17/50 ,  B33Y50/00 ,  B29C64/386 ,  B29C64/153

Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, each of the bounds being defined on a distinct parameter of an additive manufacturing process and each of the parameters affecting the occurrence of a keyhole porosity flaw, each of the parameters being a dimension in a multi-dimensional coordinate system, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as free of keyhole porosity flaws when the coordinate position is within the multi-dimensional space.

公开(公告)号：US10252508B2

公开(公告)日：2019-04-09

申请号：US15441607

申请日：2017-02-24

Applicant: United Technologies Corporation

Inventor： Sergei F. Burlatsky ,  Dmitri Novikov ,  William J. Brindley ,  David Ulrich Furrer

IPC: B33Y10/00 ,  B33Y30/00 ,  B33Y50/02 ,  B22F3/105 ,  G06F17/50 ,  B29C64/153 ,  B29C64/393 ,  B29K105/00

Abstract: A method of evaluating and validating additive manufacturing operations includes generating a multidimensional space defined by a plurality of bounds, determining a coordinate position of at least one additive manufacturing operation within the multi-dimensional coordinate system, and categorizing the operation as flaw free when the coordinate position is within the multi-dimensional space. Each of the bounds is defined on a distinct parameter of an additive manufacturing process, each of said parameters being a dimension in a multi-dimensional coordinate system.

公开(公告)号：US20190063256A1

公开(公告)日：2019-02-28

申请号：US15692757

申请日：2017-08-31

Applicant: United Technologies Corporation

Inventor： Max A. Kaplan ,  Xuan Liu ,  David Ulrich Furrer

IPC: F01D25/00 ,  F01D5/02 ,  F04D29/32 ,  F04D29/02 ,  C22C19/05

Abstract: An embodiment of a superalloy composition includes 0 to 3.5 wt % Al; 0.005 to 0.05 wt % B; 0.005 to 0.25 wt % C; 10 to 27 wt % Co; 12 to 20 wt % Cr; 6 to 10 wt % Ti; 0.01 to 0.1 wt % Zr; and balance Ni and incidental impurities.

公开(公告)号：US20190030787A1

公开(公告)日：2019-01-31

申请号：US15661448

申请日：2017-07-27

Applicant: United Technologies Corporation

Inventor： Wendell V. Twelves,, JR. ,  David Ulrich Furrer

IPC: B29C64/112 ,  B29C63/00 ,  B29C63/02

Abstract: An additively manufactured component includes a planar sheet and a coating applied to the planar sheet to form the component. The component is configured for attachment to a non-planar surface of a workpiece.

公开(公告)号：US20180128284A1

公开(公告)日：2018-05-10

申请号：US15344638

申请日：2016-11-07

Applicant: United Technologies Corporation

Inventor： Agnieszka M. Wusatowska-Sarnek ,  Sergei F. Burlatsky ,  David Ulrich Furrer ,  J. Michael McQuade

IPC: F04D29/38 ,  F04D29/16 ,  F04D29/52 ,  F04D29/02 ,  F01D11/12 ,  F01D5/28

CPC classification number: F04D29/388 ,  F01D5/20 ,  F01D5/288 ,  F01D11/122 ,  F04D29/023 ,  F04D29/164 ,  F04D29/327 ,  F04D29/526 ,  F05D2220/32 ,  F05D2230/53 ,  F05D2230/90 ,  F05D2240/307 ,  F05D2300/609 ,  F05D2300/611

Abstract: A rotor for a turbomachine is provided which includes a hub; and a plurality of blades extending radially from the hub, the plurality of blades comprising a first subset of blades having first tips and an abrasive coating on the first tips, and a second subset of blades having second tips with no abrasive coating on the second tips, wherein a radius (R2) of the first subset of blades, including thickness of the abrasive coating, is greater than a radius (R1) of the second subset of blades, and wherein a base radius (R) of the first subset of blades, not including thickness of the abrasive coating, is less than the radius (R1) of the second subset of blades.

公开(公告)号：US09957826B2

公开(公告)日：2018-05-01

申请号：US14731743

申请日：2015-06-05

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Dmitri Novikov ,  David Ulrich Furrer ,  Sergei F Burlatsky

IPC: F16J15/34 ,  F01D11/00 ,  C10M109/00 ,  F01D11/12 ,  C04B35/56 ,  C04B35/58

CPC classification number: F01D11/001 ,  C04B35/5607 ,  C04B35/5611 ,  C04B35/5618 ,  C04B35/5622 ,  C04B35/58 ,  C04B35/58007 ,  C04B35/58014 ,  C04B35/58021 ,  C04B35/58028 ,  C04B2235/5212 ,  C10M109/00 ,  F01D11/122 ,  F05D2240/55 ,  F05D2300/226 ,  F05D2300/228 ,  F05D2300/509 ,  Y02T50/672

Abstract: A stiffness controlled abradeable seal system for a gas turbine engine includes a cantilevered arm that supports one of a rotating seal surface and a static seal surface, a stiffness of the cantilevered arm controlled to achieve a desired operational temperature at a seal interface.

公开(公告)号：US20170021413A1

公开(公告)日：2017-01-26

申请号：US15113082

申请日：2015-01-09

Applicant: United Technologies Corporation

Inventor： Steven J. Bullied ,  David Ulrich Furrer ,  John Joseph Marcin ,  Venkatarama K. Seetharaman

IPC: B22D27/04 ,  C30B29/06 ,  C30B11/02 ,  C30B11/00 ,  B22D27/08 ,  B22C9/04

CPC classification number: B22D27/045 ,  B22C9/04 ,  B22D27/08 ,  C30B11/002 ,  C30B11/007 ,  C30B11/02 ,  C30B29/06

Abstract: An investment casting apparatus includes a furnace having an opening, a mold support, and a multi-axis actuator connected with the mold support and configured to retract the mold support from the opening with multiple-axis motion. An investment casting method includes withdrawing, with multiple-axis motion, a mold through the opening of the furnace to solidify a molten metal- or metalloid-based material in the mold. The apparatus and method can be used to form a cast article that has a body formed of the metal- or metalloid-based material. The body has a multi-textured, single crystal microstructure.

Abstract translation: 熔模铸造装置包括具有开口的炉，模具支撑件和与模具支撑件连接的多轴致动器，并被配置为使模具支撑件从多个轴线运动的开口缩回。 熔模铸造方法包括通过炉的开口取出多轴运动的模具，以使模具中的熔融金属或准金属基材料固化。 该装置和方法可用于形成具有由金属或准金属基材料形成的主体的铸造制品。 身体具有多纹理，单晶微结构。

公开(公告)号：US20160001407A1

公开(公告)日：2016-01-07

申请号：US14768633

申请日：2013-12-16

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： James O. Hansen ,  David Ulrich Furrer

IPC: B23P15/04 ,  F01D5/28

CPC classification number: B23P15/04 ,  B21D53/78 ,  B21H7/00 ,  B21K3/04 ,  F01D5/288 ,  F04D29/324 ,  F05D2220/32 ,  F05D2230/20 ,  F05D2240/303

Abstract: A method for manufacturing a protective sheath for a fan blade leading edge is described. The method may comprise generating a preform plate from a stock plate wherein the preform plate has a flattened surface and an inclined surface having a spike flanked by a first side and a second side. The method may further comprise bending the first side and the second side away from the spike to generate a sheath intermediate followed by generating the protective sheath from the sheath intermediate by shaping an outer surface and an inner surface of the sheath intermediate to match the contour of the fan blade leading edge.

Abstract translation: 描述了用于制造用于风扇叶片前缘的保护套的方法。 该方法可以包括从坯料板产生预成型板，其中预成型板具有扁平表面和具有侧面为第一侧和第二侧的尖端的倾斜表面。 该方法还可以包括将第一侧和第二侧弯曲远离尖峰以产生鞘中间体，随后通过使护套中间体的外表面和内表面成形来匹配护套中间体的保护鞘，以匹配护套中间体的轮廓 风扇叶片前缘。