公开(公告)号：US10041444B2

公开(公告)日：2018-08-07

申请号：US14842246

申请日：2015-09-01

Applicant: United Technologies Corporation

Inventor： Donald W. Peters

IPC: F23R3/20 ,  F02K3/10 ,  F02C7/22 ,  F23D11/38

Abstract: A fuel delivery system is provided for a turbine engine. This fuel delivery system includes a variable orifice jet configured to spray fuel received from a spray bar fuel conduit. The variable orifice jet includes a flexible body and a pintle that extends through a sidewall of the flexible body. An area of an orifice between the sidewall and the pintle is variable.

公开(公告)号：US20170058692A1

公开(公告)日：2017-03-02

申请号：US14630228

申请日：2015-02-24

Applicant: United Technologies Corporation

Inventor： Nicholas W. Kantany ,  Edward Boucher ,  Kristine Marie Carnavos ,  Adam Covino ,  Melaine Ho ,  Jorge I. Farah ,  Donald W. Peters

IPC: F01D17/14 ,  F01D25/00

CPC classification number: F01D17/145 ,  F01D17/141 ,  F01D17/143 ,  F01D17/167 ,  F01D25/005 ,  F04D27/0215 ,  F05D2220/32 ,  F05D2270/3061 ,  F16K39/045

Abstract: An air modulating system for a gas turbine engine includes a fixed plate with a fluid passage inlet, a floating plate with a first side adjacent to the fluid passage inlet, an actuated mount configured to move the floating plate relative to the fixed plate, and a linkage element for connecting the floating plate to the actuated mount. The linkage element includes a mounting flange configured to slidably engage the floating plate.

Abstract translation: 用于燃气涡轮发动机的空气调节系统包括具有流体通道入口的固定板，具有与流体通道入口相邻的第一侧的浮动板，构造成使浮动板相对于固定板移动的致动安装板，以及 连接元件，用于将浮动板连接到致动的安装座。 联动元件包括安装凸缘，该安装凸缘被构造成可滑动地接合浮动板。

公开(公告)号：US20160348590A1

公开(公告)日：2016-12-01

申请号：US14727475

申请日：2015-06-01

Applicant: United Technologies Corporation

Inventor： Steven D. Porter ,  Donald W. Peters ,  James P. Bangerter

IPC: F02C7/28 ,  F16J15/34 ,  F02C3/04

CPC classification number: F02C7/28 ,  F02C3/04 ,  F02K1/805 ,  F05D2220/32 ,  F05D2240/55 ,  F05D2240/58 ,  F05D2250/14 ,  F05D2250/314 ,  F05D2250/34 ,  F05D2250/41 ,  F05D2260/38 ,  F05D2260/57 ,  F05D2300/603 ,  F05D2300/6034 ,  F16J15/3488 ,  Y02T50/672

Abstract: A seal system is provided. The seal system may comprise a first duct having an annular geometry, a second duct overlapping the first duct in a radial direction, and a seal disposed between the first duct and the second duct. The seal may comprise a groove defined by the first duct and a piston configured to slideably engage the groove.

Abstract translation: 提供密封系统。 密封系统可以包括具有环形几何形状的第一管道，在径向方向上与第一管道重叠的第二管道以及设置在第一管道和第二管道之间的密封件。 密封件可以包括由第一管道限定的凹槽和构造成可滑动地接合凹槽的活塞。

公开(公告)号：US09464655B2

公开(公告)日：2016-10-11

申请号：US13661650

申请日：2012-10-26

Applicant: United Technologies Corporation

Inventor： Donald W. Peters

IPC: F23R3/60 ,  F16B21/16 ,  F23M5/04 ,  F23R3/00 ,  F16B5/06

CPC classification number: F16B21/165 ,  F16B5/065 ,  F16B5/0664 ,  F23M5/04 ,  F23M2900/05004 ,  F23R3/007 ,  F23R3/60 ,  Y10T403/592

Abstract: A push-lock pin for connecting a plate to surface includes a cylindrical pin housing and a shaft within the housing. The shaft has a ball-lock mechanism and a push-down pop-up mechanism.

Abstract translation: 用于将板连接到表面的推锁销包括圆柱形销壳体和壳体内的轴。 轴具有球锁机构和下推弹出机构。

公开(公告)号：US20160069298A1

公开(公告)日：2016-03-10

申请号：US14842246

申请日：2015-09-01

Applicant: United Technologies Corporation

Inventor： Donald W. Peters

IPC: F02K3/10 ,  F23R3/20

CPC classification number: F02K3/10 ,  F02C7/222 ,  F23D11/38 ,  F23R3/20

Abstract: A fuel delivery system is provided for a turbine engine. This fuel delivery system includes a variable orifice jet configured to spray fuel received from a spray bar fuel conduit. The variable orifice jet includes a flexible body and a pintle that extends through a sidewall of the flexible body. An area of an orifice between the sidewall and the pintle is variable.

Abstract translation: 为涡轮发动机提供燃料输送系统。 该燃料输送系统包括构造成喷射从喷杆燃料导管接收的燃料的可变喷嘴喷射器。 可变孔口射流包括柔性体和枢轴，其延伸穿过柔性体的侧壁。 侧壁和枢轴之间的孔口的面积是可变的。

公开(公告)号：US11156359B2

公开(公告)日：2021-10-26

申请号：US16727178

申请日：2019-12-26

Applicant: United Technologies Corporation

Inventor： Donald W. Peters ,  San Quach ,  Jeffrey T. Morton ,  Matthew D. Parekh

IPC: F23R3/00 ,  F02C7/18 ,  F23R3/60 ,  F23R3/06

Abstract: A liner panel for use in a combustor of a gas turbine engine, the liner panel including a cold side; and a rail that extends from the cold side, the rail includes a first diffusion interface passage surface and a second diffusion interface passage surface, the first diffusion interface passage surface angled with respect to the second diffusion interface passage surface.

公开(公告)号：US10823412B2

公开(公告)日：2020-11-03

申请号：US15477518

申请日：2017-04-03

Applicant: United Technologies Corporation

Inventor： San Quach ,  Andreas Sadil ,  Donald W. Peters

IPC: F23R3/00 ,  F01D25/14 ,  F02K1/82 ,  F02K9/97 ,  C23C2/00 ,  C23C4/02 ,  B32B3/30

Abstract: A coated panel for a gas turbine engine includes a panel having a panel inner surface and a pocket formed in the panel inner surface, the pocket having a pocket depth. A coating is applied to the pocket such that a coating edge is disposed within the pocket to enhance coating retention to the panel. A gas turbine engine includes a turbine, a combustor to supply hot combustion gases to the turbine along a gas path, and one or more coated panels located along the gas path. The one or more panels includes a panel having a panel inner surface, and a pocket formed in the panel inner surface, the pocket having a pocket depth. A coating is applied to the pocket such that a coating edge is located within the pocket to enhance coating retention to the panel.

公开(公告)号：US10760529B2

公开(公告)日：2020-09-01

申请号：US15910827

申请日：2018-03-02

Applicant: United Technologies Corporation

Inventor： Donald W. Peters ,  Emma J. Place

IPC: F02K1/80 ,  F02K1/12 ,  F01D25/16 ,  F16C29/00 ,  F16C29/02 ,  F16C33/20

Abstract: A composite wear pad for being coupled to a slider block of a convergent nozzle of a gas turbine engine includes a high heat capacity composite having a resin and a plurality of carbon fibers bonded together by the resin. The composite wear pad also includes a first rod coupled to the high heat capacity composite at a first axial end of the composite wear pad such that a first end thickness. The composite wear pad also includes a second rod coupled to the high heat capacity composite at a second axial end of the composite wear pad such that the first axial end and the second axial end of the composite wear pad each have an end thickness that is greater than a middle thickness of the composite wear pad.

公开(公告)号：US10352248B2

公开(公告)日：2019-07-16

申请号：US14812926

申请日：2015-07-29

Applicant: United Technologies Corporation

Inventor： Nicholas W. Kantany ,  Edward Boucher ,  Kristine Marie Carnavos ,  Robert Russell Mayer ,  Donald W. Peters

IPC: F02K3/075 ,  F02C7/28 ,  F02C9/20 ,  F02K3/115

Abstract: A system for modulating air flow in a gas turbine engine is provided. The system may include a seal wall comprising an opening, a seal door configured to slideably engage the seal wall, and an actuator configured to move the seal door over the opening. In various embodiments, the system may include a surface forward of the seal door. The seal door may be configured to seal a passage through the surface and the opening of the seal wall. A track may be disposed under the seal door. The track may comprise cobalt. Rollers may be coupled to the seal door with the rollers on the track. The seal door may comprise a nickel-chromium alloy. A sync ring may be coupled to the seal door. The actuator may be coupled through the sync ring to the seal door.

公开(公告)号：US10180105B2

公开(公告)日：2019-01-15

申请号：US14850382

申请日：2015-09-10

Applicant: United Technologies Corporation

Inventor： Donald W. Peters

IPC: F02C7/20 ,  F02K1/82 ,  F23R3/00 ,  F01D9/02 ,  F16L3/00 ,  F16M11/14 ,  F16B5/06 ,  F23R3/60 ,  F16L3/16 ,  F16L3/14 ,  F16L3/20 ,  F16L3/18 ,  F01D25/28 ,  F16L3/123 ,  B64D27/26 ,  F16L3/133 ,  F16M11/12 ,  F02K1/04

Abstract: A hanger includes a connector assembly for coupling the hanger to a first annular duct, a bracket for coupling the hanger to a second annular duct concentrically disposed within the first annular duct, and a cable formed by a plurality of wires bound together that extend from the connector assembly to the bracket. A plurality of circumferentially-spaced hangers placed in tension support an exhaust duct liner relative to an exhaust duct. The hangers permit circumferential and axial displacement at each hanger of the exhaust duct liner relative to the exhaust duct. The displacement of the exhaust duct liner relative to the exhaust duct at each hanger is permitted in a first radial direction that decreases tension in the cable and is restrained in a second radial direction that increases tension in the cable.