公开(公告)号：US11306595B2

公开(公告)日：2022-04-19

申请号：US16131451

申请日：2018-09-14

Applicant: United Technologies Corporation

Inventor： Dilip M. Shah ,  Alan D. Cetel ,  Venkatarama K. Seetharaman

IPC: B23P15/02 ,  F01D5/14 ,  B21J5/00 ,  B21J5/02 ,  C21D9/00 ,  C22F1/10 ,  F01D5/30

Abstract: A method for manufacturing a blade, the method includes casting a nickel alloy blade precursor having an airfoil and a root. The airfoil and the root are solution heat treating differently from each other. After the solution heat treating, the root is wrought processed. After the wrought processing, an exterior of the root is machined.

公开(公告)号：US10661380B2

公开(公告)日：2020-05-26

申请号：US15451228

申请日：2017-03-06

Applicant: United Technologies Corporation

Inventor： Grant O. Cook, III ,  Kevin W. Schlichting ,  Venkatarama K. Seetharaman

IPC: B23K20/00 ,  C04B37/00 ,  B23K20/16 ,  B23K35/32 ,  B23K35/30 ,  B23K35/36 ,  B32B15/01 ,  C04B37/02 ,  F01D5/28 ,  F01D5/12

Abstract: A method for joining engine components includes positioning a first plurality of thermal protection structures across a thermal protection space between a first thermal protection surface and a second thermal protection surface. The first and second engine components are locally joined by forming a first plurality of transient liquid phase (TLP) or partial transient liquid phase (PTLP) bonds along corresponding ones of the first plurality of thermal protection structures between the first thermal protection surface and the second thermal protection surface. The second thermal protection surface is formed from a second surface material different from a first surface material of the first thermal protection surface.

公开(公告)号：US20180231478A1

公开(公告)日：2018-08-16

申请号：US15948662

申请日：2018-04-09

Applicant: United Technologies Corporation

Inventor： Iuliana Cernatescu ,  David U. Furrer ,  Venkatarama K. Seetharaman

IPC: G01N23/20 ,  G01N23/20025 ,  G01N23/18 ,  G01N23/12 ,  G01N23/087 ,  G01N23/083 ,  G01N23/20016 ,  G01N23/06 ,  G01N23/205

CPC classification number: G01N23/20 ,  G01N23/06 ,  G01N23/083 ,  G01N23/087 ,  G01N23/12 ,  G01N23/18 ,  G01N23/20016 ,  G01N23/20025 ,  G01N23/205 ,  G01N2223/316 ,  G01N2223/61 ,  G01N2223/6116 ,  G01N2223/63 ,  G01N2223/6466

Abstract: Aspects of the disclosure are directed to an analysis of a material of a component. A radiation source is activated to transmit radiation to the component. A beam pattern is obtained based on the component interfering with the radiation. The beam pattern is compared to a reference beam pattern. An anomaly is detected to exist in the material when the comparison indicates a deviation between the beam pattern and the reference beam pattern.

公开(公告)号：US20170173729A1

公开(公告)日：2017-06-22

申请号：US15451228

申请日：2017-03-06

Applicant: United Technologies Corporation

Inventor： Grant O. Cook, III ,  Kevin W. Schlichting ,  Venkatarama K. Seetharaman

IPC: B23K20/16 ,  C04B37/02 ,  C04B37/00

Abstract: A method for joining engine components includes positioning a first plurality of thermal protection structures across a thermal protection space between a first thermal protection surface and a second thermal protection surface. The first and second engine components are locally joined by forming a first plurality of transient liquid phase (TLP) or partial transient liquid phase (PTLP) bonds along corresponding ones of the first plurality of thermal protection structures between the first thermal protection surface and the second thermal protection surface. The second thermal protection surface is formed from a second surface material different from a first surface material of the first thermal protection surface.

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。