公开(公告)号：US20160237848A1

公开(公告)日：2016-08-18

申请号：US14620256

申请日：2015-02-12

Applicant: United Technologies Corporation

Inventor： Thomas N. Slavens ,  Brooks E. Snyder

IPC: F01D25/12

CPC classification number: F01D25/12 ,  B22F3/1055 ,  B22F5/009 ,  F01D5/147 ,  F05D2220/32 ,  F05D2230/13 ,  F05D2230/30 ,  F05D2230/31 ,  F05D2260/20 ,  F05D2260/201 ,  F05D2260/2214 ,  F05D2300/177 ,  Y02P10/295

Abstract: A conduction riser additively manufactured onto thin metal parts, the conduction riser extending in a build direction of the thin metal part and traversing the thin metal part as the conduction riser extends in the build direction. The conduction riser transferring heat from the upper layers of additively manufactured part during manufacturing, preventing thermal deflection of the part.

Abstract translation: 导电提升器相加地制造在薄金属部件上，导电提升管沿着薄金属部件的构造方向延伸，并且随着导电提升管在构建方向上延伸而穿过薄金属部分。 导电提升管在制造期间从附加制造的部件的上层传递热量，防止部件的热偏转。

公开(公告)号：US20160222793A1

公开(公告)日：2016-08-04

申请号：US14917855

申请日：2014-09-09

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Brooks E. Snyder ,  Thomas N. Slavens

IPC: F01D5/18

CPC classification number: F01D5/187 ,  F01D5/189 ,  F01D9/065 ,  F05D2220/32 ,  F05D2250/25 ,  F05D2260/201 ,  Y02T50/676

Abstract: This disclosure relates to a gas turbine engine. The engine includes a component having a first wall and a second wall spaced-apart from the first wall. The component further includes a cooling passageway provided in part by a helical wall between the first wall and the second wall.

Abstract translation: 本公开涉及燃气涡轮发动机。 发动机包括具有第一壁和与第一壁间隔开的第二壁的部件。 该部件还包括由第一壁和第二壁之间的螺旋壁部分地设置的冷却通道。

公开(公告)号：US20160208705A1

公开(公告)日：2016-07-21

申请号：US15022990

申请日：2014-10-16

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Thomas N. Slavens ,  Brooks E. Snyder

IPC: F02C7/18 ,  F01D25/30 ,  F01D5/18 ,  F01D11/08 ,  F23R3/04

CPC classification number: F02C7/18 ,  F01D5/186 ,  F01D5/187 ,  F01D11/08 ,  F01D25/30 ,  F05D2240/305 ,  F05D2260/202 ,  F05D2260/204 ,  F23R3/002 ,  F23R3/005 ,  F23R3/04 ,  F23R3/06 ,  F23R2900/03042 ,  F23R2900/03044 ,  Y02T50/676

Abstract: A cooling circuit for a gas turbine engine comprises a first wall having a first surface facing a first cavity and a second surface facing away from the first cavity. A second wall is spaced outwardly of the second surface of the first wall to provide at least one second cavity. Cooling fluid is configured to flow from the first cavity and exit to an external surface of the second wall via at least one hole to provide cooling to the external surface. A gas turbine engine and a method of forming a cooling circuit for a gas turbine engine are also disclosed.

Abstract translation: 用于燃气涡轮发动机的冷却回路包括具有面向第一腔的第一表面和背离第一腔的第二表面的第一壁。 第二壁与第一壁的第二表面向外间隔开以提供至少一个第二腔。 冷却流体构造成从第一腔流出并经由至少一个孔离开第二壁的外表面，以向外表面提供冷却。 还公开了一种燃气涡轮发动机和形成燃气涡轮发动机的冷却回路的方法。

公开(公告)号：US20160024938A1

公开(公告)日：2016-01-28

申请号：US14804865

申请日：2015-07-21

Applicant: United Technologies Corporation

Inventor： Thomas N. Slavens ,  Brooks E. Snyder ,  Andrew D. Burdick

IPC: F01D5/18

CPC classification number: F01D5/187 ,  F05D2220/32 ,  F05D2240/303 ,  F05D2250/322 ,  F05D2260/2212 ,  Y02T50/676

Abstract: An airfoil for a gas turbine engine, the airfoil includes a wall that has a leading edge and a trailing edge and at least partially defining a boundary of a leading edge cavity radially along the leading edge. A cooling jet structure is operatively associated with a portion of the wall proximate the leading edge and is configured to direct a cooling fluid tangent to the portion of the wall.

Abstract translation: 用于燃气涡轮发动机的翼型件，翼型件包括具有前缘和后缘的壁，并且沿着前缘至少部分地限定前缘腔的边界径向地限定。 冷却射流结构与靠近前缘的壁的一部分可操作地相关联，并且构造成引导与壁的该部分相切的冷却流体。

公开(公告)号：US10563583B2

公开(公告)日：2020-02-18

申请号：US15022990

申请日：2014-10-16

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Thomas N. Slavens ,  Brooks E. Snyder

IPC: F02C7/18 ,  F01D5/18 ,  F23R3/06 ,  F23R3/00 ,  F01D11/08 ,  F01D25/30 ,  F23R3/04

Abstract: A cooling circuit for a gas turbine engine comprises a first wall having a first surface facing a first cavity and a second surface facing away from the first cavity. A second wall is spaced outwardly of the second surface of the first wall to provide at least one second cavity. Cooling fluid is configured to flow from the first cavity and exit to an external surface of the second wall via at least one hole to provide cooling to the external surface. A gas turbine engine and a method of forming a cooling circuit for a gas turbine engine are also disclosed.

公开(公告)号：US20200011187A1

公开(公告)日：2020-01-09

申请号：US16571724

申请日：2019-09-16

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Nicholas M. LoRicco ,  James Tilsley Auxier ,  Brooks E. Snyder ,  Thomas N. Slavens

IPC: F01D5/18 ,  F23R3/00 ,  F01D25/12 ,  F01D11/08 ,  F01D9/02 ,  F01D5/28

Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a body, a wall extending inside of the body and a plurality of vortex promoting features arranged in a helical pattern along the wall.

公开(公告)号：US10370981B2

公开(公告)日：2019-08-06

申请号：US15112497

申请日：2015-01-26

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Thomas N. Slavens ,  Brooks E. Snyder

IPC: F01D5/18 ,  F01D25/12 ,  F01D9/02 ,  F23R3/00 ,  F01D11/08 ,  F01D25/30

Abstract: A component according to an exemplary aspect of the present disclosure includes, among other things, a pedestal that traverses a flow channel disposed between a first wall and a second wall. The pedestal includes at least one interior bore configured to communicate a cooling fluid inside of the pedestal.

公开(公告)号：US10364683B2

公开(公告)日：2019-07-30

申请号：US15036833

申请日：2014-11-05

Applicant: United Technologies Corporation

Inventor： Brooks E. Snyder ,  Thomas N. Slavens ,  Nicholas M. LoRicco ,  James T. Auxier

IPC: F01D5/18

Abstract: A gas turbine engine component includes opposing walls that provide an interior cooling passage. One of the walls has a turbulator with a hook that is enclosed within the walls.

公开(公告)号：US20190085719A1

公开(公告)日：2019-03-21

申请号：US16125080

申请日：2018-09-07

Applicant: United Technologies Corporation

Inventor： Thomas N. Slavens ,  Brooks E. Snyder

IPC: F01D25/12 ,  F01D5/14 ,  B22F5/00 ,  B22F3/105

Abstract: A conduction riser is additively manufactured onto thin metal parts, the conduction riser extends in a build direction of the thin metal part and traverses a surface of the thin metal part as the conduction riser extends in the build direction. The conduction riser transfers heat from the upper layers of the additively manufactured part during manufacturing to prevent thermal deflection of the part during the manufacturing process.

公开(公告)号：US09845524B2

公开(公告)日：2017-12-19

申请号：US14587841

申请日：2014-12-31

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Brooks E. Snyder

IPC: C23C4/01 ,  F01D5/28 ,  C23C14/22 ,  F01D9/04 ,  C23C14/04 ,  C23C4/134

CPC classification number: C23C4/01 ,  C23C4/134 ,  C23C14/042 ,  C23C14/22 ,  F01D5/288 ,  F01D9/04 ,  Y02T50/672

Abstract: The present disclosure relates generally to a fixture for use in applying a coating to a multiple vane nozzle for use in a turbomachine. The fixture includes first and second masks that are applied to opposite sides of the nozzle to mimic the geometry and spacing of the vanes of the nozzle.