公开(公告)号：US20190186271A1

公开(公告)日：2019-06-20

申请号：US15841627

申请日：2017-12-14

Applicant: United Technologies Corporation

Inventor： JinQuan Xu ,  Tracy A. Propheter-Hinckley

IPC: F01D5/14 ,  F01D5/28 ,  F01D11/08 ,  F01D25/00

CPC classification number: F01D5/145 ,  F01D5/141 ,  F01D5/142 ,  F01D5/28 ,  F01D5/282 ,  F01D5/284 ,  F01D11/08 ,  F01D11/14 ,  F01D25/005 ,  F05D2220/323 ,  F05D2230/20 ,  F05D2230/90 ,  F05D2240/11 ,  F05D2240/305 ,  F05D2260/97 ,  F05D2300/222 ,  F05D2300/603 ,  F05D2300/6033 ,  F05D2300/614

Abstract: A turbomachine airfoil element has a substrate. The substrate defines an airfoil having a pressure side and a suction side. A plurality of fiber composite ribs are along the pressure side.

公开(公告)号：US10294801B2

公开(公告)日：2019-05-21

申请号：US15659360

申请日：2017-07-25

Applicant: United Technologies Corporation

Inventor： JinQuan Xu ,  Glenn Levasseur ,  Gregory M. Dolansky

IPC: F01D5/28 ,  F04D29/32 ,  F01D5/14 ,  F01D5/20 ,  F01D5/22 ,  F01D11/08 ,  F02C3/04

Abstract: A rotor blade includes a main body that extends radially outward from a first end to a second end, and includes a platform at the second end that extends circumferentially between opposing first and second sidewalls. The platform includes a first lateral wall that is situated between leading and trailing edges of the platform. The first lateral wall extends circumferentially between the first and second sidewalls and radially outward from the platform. The first lateral wall includes an extension that extends the first lateral wall circumferentially outward from the first sidewall. Respective portions of the first and second sidewalls adjacent to the first lateral wall reside in respective first and second planes, and the extension includes an outer face situated outside of the first and second planes. A majority of the first lateral wall includes a first material, and the outer face includes a second material having a different resistance to wear than the first material.

公开(公告)号：US20190041060A1

公开(公告)日：2019-02-07

申请号：US15666958

申请日：2017-08-02

Applicant: United Technologies Corporation

Inventor： JinQuan Xu

IPC: F23R3/04 ,  F23R3/00 ,  F02C7/18

Abstract: A combustor assembly for a turbine engine includes a liner panel defining a portion of an inner surface of a combustor chamber, liner panel including an end face transverse the inner surface, and at least one diffuser through the end face. A liner panel and a method are also disclosed.

公开(公告)号：US20190032498A1

公开(公告)日：2019-01-31

申请号：US15659360

申请日：2017-07-25

Applicant: United Technologies Corporation

Inventor： JinQuan Xu ,  Glenn Levasseur ,  Gregory M. Dolansky

IPC: F01D5/28 ,  F04D29/32

Abstract: A rotor blade includes a main body that extends radially outward from a first end to a second end, and includes a platform at the second end that extends circumferentially between opposing first and second sidewalls. The platform includes a first lateral wall that is situated between leading and trailing edges of the platform. The first lateral wall extends circumferentially between the first and second sidewalls and radially outward from the platform. The first lateral wall includes an extension that extends the first lateral wall circumferentially outward from the first sidewall. Respective portions of the first and second sidewalls adjacent to the first lateral wall reside in respective first and second planes, and the extension includes an outer face situated outside of the first and second planes. A majority of the first lateral wall includes a first material, and the outer face includes a second material having a different resistance to wear than the first material.

公开(公告)号：US10040115B2

公开(公告)日：2018-08-07

申请号：US14870430

申请日：2015-09-30

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Thomas N. Slavens ,  Mark F. Zelesky ,  JinQuan Xu ,  Joel H. Wagner

IPC: B22C9/10 ,  F01D5/18 ,  F01D9/04 ,  F01D25/12 ,  B22C1/18 ,  B22C1/00 ,  B22D29/00 ,  B22F3/105 ,  B29C67/00 ,  B22F5/00 ,  B22F5/04 ,  B28B1/00 ,  B28B7/34 ,  B33Y10/00 ,  B33Y80/00

Abstract: A casting article according to an exemplary aspect of the present disclosure includes, among other things, a circuit forming portion and an interior channel formed inside of the circuit forming portion. The interior channel defines a leaching path that extends at least partially through the circuit forming portion.

公开(公告)号：US09874101B2

公开(公告)日：2018-01-23

申请号：US14652657

申请日：2013-02-12

Applicant: United Technologies Corporation

Inventor： JinQuan Xu

IPC: F01D5/14 ,  F01D9/04 ,  F01D5/02 ,  F01D9/02

CPC classification number: F01D5/147 ,  F01D5/021 ,  F01D5/143 ,  F01D5/145 ,  F01D9/02 ,  F01D9/041 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/30 ,  F05D2240/80 ,  Y02T50/673

Abstract: A gas turbine engine component includes an airfoil and a platform. The airfoil has a pressure side and an opposite suction side. The platform is connected to the airfoil and has a first curved edge to the suction side of the airfoil and a second curved edge to the pressure side of the airfoil. The first and second curved edges extend along a surface of the platform having a neutral elevation with respect to a reference axisymmetrical platform surface for the gas turbine engine.

公开(公告)号：US20170284208A1

公开(公告)日：2017-10-05

申请号：US15106875

申请日：2015-01-21

Applicant: United Technologies Corporation

Inventor： JinQuan Xu

IPC: F01D5/28 ,  B22C7/02 ,  B33Y80/00 ,  B22C9/10 ,  B22D27/04 ,  B22F5/00 ,  F01D5/18 ,  B22C9/04

CPC classification number: F01D5/28 ,  B22C7/02 ,  B22C9/04 ,  B22C9/10 ,  B22D27/045 ,  B22F3/1055 ,  B22F5/007 ,  B22F5/04 ,  B22F2999/00 ,  B33Y10/00 ,  B33Y70/00 ,  B33Y80/00 ,  C30B11/00 ,  C30B29/52 ,  F01D5/18 ,  F01D5/187 ,  F05D2220/32 ,  F05D2230/21 ,  F05D2230/50 ,  F05D2260/204 ,  F05D2300/10 ,  F05D2300/607 ,  Y02P10/292 ,  Y02P10/295

Abstract: A method is provided for manufacturing a component. This method includes additively manufacturing a crucible for casting of the component. A metal material is directionally solidified within the crucible to form a metal single crystal material. A sacrificial core is removed to reveal a metal single crystal component with internal passageways. A component is provided for a gas turbine engine that includes a metal single crystal material component with internal passageways. The metal single crystal material component was additively manufactured of a metal material concurrently with a core that forms the internal passageways. The metal material was also remelted and directionally solidified.

公开(公告)号：US20170144219A1

公开(公告)日：2017-05-25

申请号：US15219921

申请日：2016-07-26

Applicant: United Technologies Corporation

Inventor： JinQuan Xu

IPC: B22D27/04 ,  B33Y40/00 ,  B33Y80/00 ,  B22C9/10 ,  B22C9/22 ,  B22D29/00 ,  B22D25/02 ,  B22F3/105 ,  B22F3/24 ,  B22F5/04 ,  B23K15/00 ,  B23K26/342 ,  B23K26/70 ,  B23K37/00 ,  F01D5/00 ,  F01D5/12 ,  F01D9/04 ,  F02C7/22 ,  F23R3/00 ,  B33Y10/00

CPC classification number: B22D27/045 ,  B22C9/02 ,  B22C9/04 ,  B22C9/10 ,  B22C9/108 ,  B22C9/12 ,  B22C9/22 ,  B22D23/06 ,  B22D25/02 ,  B22D29/001 ,  B22F3/1055 ,  B22F3/24 ,  B22F5/007 ,  B22F5/009 ,  B22F5/04 ,  B22F2003/248 ,  B22F2998/10 ,  B23K1/0018 ,  B23K9/04 ,  B23K9/167 ,  B23K15/0046 ,  B23K15/0086 ,  B23K20/00 ,  B23K26/34 ,  B23K26/342 ,  B23K26/70 ,  B23K31/02 ,  B23K37/00 ,  B23K2101/001 ,  B23P6/005 ,  B23P6/007 ,  B23P6/045 ,  B33Y10/00 ,  B33Y40/00 ,  B33Y80/00 ,  C30B11/00 ,  C30B11/003 ,  C30B21/02 ,  C30B29/52 ,  F01D5/005 ,  F01D5/12 ,  F01D5/18 ,  F01D5/186 ,  F01D5/187 ,  F01D9/04 ,  F02C7/222 ,  F05D2220/32 ,  F05D2230/21 ,  F05D2230/233 ,  F05D2230/234 ,  F05D2230/235 ,  F05D2230/238 ,  F05D2230/30 ,  F05D2230/80 ,  F05D2240/122 ,  F05D2240/304 ,  F05D2260/202 ,  F05D2260/204 ,  F05D2300/175 ,  F05D2300/20 ,  F05D2300/606 ,  F05D2300/608 ,  F23R3/002 ,  Y02P10/292 ,  Y02P10/295

Abstract: A method of manufacturing a replacement body for a component is provided. The method includes the steps of: a) additively manufacturing a crucible for casting of the replacement body; b) solidifying a metal material within the crucible to form a directionally solidified microstructure within the replacement body; and c) removing the crucible to reveal the directionally solidified replacement body.

公开(公告)号：US09463506B2

公开(公告)日：2016-10-11

申请号：US14683401

申请日：2015-04-10

Applicant: United Technologies Corporation

Inventor： JinQuan Xu

IPC: B22D23/06 ,  B22C7/02 ,  B29C67/00 ,  B22D15/00 ,  B22F3/105 ,  B22C9/02 ,  B22C3/00 ,  B22C9/04 ,  B22F3/24 ,  B33Y10/00

CPC classification number: B22D23/06 ,  B22C3/00 ,  B22C7/02 ,  B22C9/02 ,  B22C9/04 ,  B22C9/061 ,  B22C9/068 ,  B22D15/00 ,  B22D27/045 ,  B22D29/00 ,  B22F3/1055 ,  B22F3/24 ,  B22F5/00 ,  B22F2003/242 ,  B22F2003/248 ,  B22F2998/10 ,  B23K15/0086 ,  B23K26/342 ,  B23K26/70 ,  B33Y10/00 ,  B33Y80/00 ,  B33Y99/00 ,  Y02P10/292 ,  Y02P10/295

Abstract: A method of working an additively manufactured part includes applying a layer of wax to a part manufactured with an additive manufacturing process. Then a mold is formed over the layer of wax on the part. The wax is then removed from between the mold and the part. The part is then melted in the mold, and then the part is re-solidified in the mold. Finally, the mold is removed.

Abstract translation: 加工制造部件的加工方法包括将蜡层施加到通过添加剂制造工序制造的部件上。 然后在部件上的蜡层上形成模具。 然后从模具和部件之间移除蜡。 然后将该部件在模具中熔化，然后将该部件在模具中再固化。 最后，去除模具。

公开(公告)号：US09452474B2

公开(公告)日：2016-09-27

申请号：US14706685

申请日：2015-05-07

Applicant: United Technologies Corporation

Inventor： JinQuan Xu

IPC: B22D23/06 ,  B22C7/02 ,  B22D25/02 ,  B23K31/02 ,  B22C9/02 ,  B22C9/22 ,  B22D27/04 ,  C30B11/00 ,  C30B21/02 ,  B23K1/00 ,  B23K9/04 ,  B23K15/00 ,  B23K26/34 ,  B22F3/105 ,  C30B29/52 ,  F01D5/00 ,  B22F5/00 ,  B33Y10/00 ,  B22F5/04 ,  B23P6/00 ,  F01D5/18

CPC classification number: B22D27/045 ,  B22C9/02 ,  B22C9/04 ,  B22C9/10 ,  B22C9/108 ,  B22C9/12 ,  B22C9/22 ,  B22D23/06 ,  B22D25/02 ,  B22D29/001 ,  B22F3/1055 ,  B22F3/24 ,  B22F5/007 ,  B22F5/009 ,  B22F5/04 ,  B22F2003/248 ,  B22F2998/10 ,  B23K1/0018 ,  B23K9/04 ,  B23K9/167 ,  B23K15/0046 ,  B23K15/0086 ,  B23K20/00 ,  B23K26/34 ,  B23K26/342 ,  B23K26/70 ,  B23K31/02 ,  B23K37/00 ,  B23K2101/001 ,  B23P6/005 ,  B23P6/007 ,  B23P6/045 ,  B33Y10/00 ,  B33Y40/00 ,  B33Y80/00 ,  C30B11/00 ,  C30B11/003 ,  C30B21/02 ,  C30B29/52 ,  F01D5/005 ,  F01D5/12 ,  F01D5/18 ,  F01D5/186 ,  F01D5/187 ,  F01D9/04 ,  F02C7/222 ,  F05D2220/32 ,  F05D2230/21 ,  F05D2230/233 ,  F05D2230/234 ,  F05D2230/235 ,  F05D2230/238 ,  F05D2230/30 ,  F05D2230/80 ,  F05D2240/122 ,  F05D2240/304 ,  F05D2260/202 ,  F05D2260/204 ,  F05D2300/175 ,  F05D2300/20 ,  F05D2300/606 ,  F05D2300/608 ,  F23R3/002 ,  Y02P10/292 ,  Y02P10/295

Abstract: A method of manufacturing a replacement body for a component is provided. The method includes the steps of: a) additively manufacturing a crucible for casting of the replacement body; b) solidifying a metal material within the crucible to form a directionally solidified microstructure within the replacement body; and c) removing the crucible to reveal the directionally solidified replacement body.

Abstract translation: 提供一种制造用于部件的替换体的方法。 该方法包括以下步骤：a）附加地制造用于铸造替换体的坩埚; b）在坩埚内固化金属材料，以在替换体内形成定向凝固的微结构; 和c）取出坩埚以露出定向凝固的置换体。