公开(公告)号：US10668874B1

公开(公告)日：2020-06-02

申请号：US16359184

申请日：2019-03-20

Applicant: United Technologies Corporation

Inventor： Andre Herman Troughton ,  Ryan K. Snyder ,  Jose A. Carrion ,  Alexander Trabal ,  Jimmy C. Pujols

IPC: B60R16/02 ,  F16B2/02 ,  H02G3/32

Abstract: A clamp assembly includes a grommet with a non-circular aperture with a multiple of crush apertures defined at least partially around the non-circular aperture. A method of supporting a wiring harness within a clamp assembly for a gas turbine engine includes installing a wiring harness through a non-circular aperture with a multiple of crush apertures defined in an arc at least partially around a major axis of the non-circular aperture; and compressing the grommet to compress the multiple of crush apertures to retain the wiring harness within the non-circular aperture.

公开(公告)号：US10411756B2

公开(公告)日：2019-09-10

申请号：US15480794

申请日：2017-04-06

Applicant: United Technologies Corporation

Inventor： Ryan K. Snyder ,  Eric J. Heims

IPC: H04B3/52 ,  F16L9/19 ,  H01P5/04 ,  F01D21/00 ,  F16L41/02

Abstract: A wave guide assembly for a control and diagnostic system for a machine, the wave guide assembly includes a housing defining an exterior surface and an internal cavity extending between distal ends. A wave guide is defined within the internal cavity. At least one open conduit is defined within the internal cavity providing a space for routing conductors through the housing. A fluid passage is defined within the internal cavity separate from the wave guide. A control and diagnostic system for a machine and a gas turbine engine are also disclosed.

公开(公告)号：US10307138B2

公开(公告)日：2019-06-04

申请号：US15480757

申请日：2017-04-06

Applicant: United Technologies Corporation

Inventor： Eric J. Heims ,  Ryan K. Snyder ,  Kurt J. Sobanski

IPC: A61B8/00 ,  A61B8/08 ,  A61B8/13 ,  A61B8/14 ,  H01P1/04 ,  F01D21/00

Abstract: A wave guide assembly for a control and diagnostic system for a machine includes a housing defining an exterior surface and an internal cavity extending between distal ends. At least one wave guide within the internal cavity defines a wave propagation passage for at least one wave form signal. At least one conductor within the internal cavity is separate from the wave guide. A control and diagnostic system for a machine and a gas turbine engine are also disclosed.

公开(公告)号：US10247102B2

公开(公告)日：2019-04-02

申请号：US14891236

申请日：2014-02-27

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Michael Dreher ,  Ryan K. Snyder ,  James M. McPherson ,  Ping Su ,  Fernando Quinones ,  Gabriel Rivera

IPC: F02C1/00 ,  F02C7/22 ,  F02C7/06 ,  F02C7/224 ,  F23K5/04 ,  F23K5/06 ,  F02C7/14

Abstract: A single, unitary fuel/oil manifold for a gas turbine engine is provided which comprises one or more interfaces for mounting various fuel system and lubricating system components directly to the fuel/oil manifold. The fuel/oil manifold also defines fluid passages for transferring fuel or lubricant from one component to another component. Packing numerous fuel system and lubricating system components within the fuel/oil manifold reduces cost and weight and simplifies maintenance.

公开(公告)号：US20180294838A1

公开(公告)日：2018-10-11

申请号：US15480794

申请日：2017-04-06

Applicant: United Technologies Corporation

Inventor： Ryan K. Snyder ,  Eric J. Heims

IPC: H01P3/12 ,  H04B3/52 ,  F01D21/00 ,  F16L41/02 ,  F16L9/19

CPC classification number: H04B3/52 ,  F01D21/003 ,  F05D2220/32 ,  F05D2260/80 ,  F05D2270/01 ,  F16L9/19 ,  F16L41/021 ,  H01P5/04

Abstract: A wave guide assembly for a control and diagnostic system for a machine, the wave guide assembly includes a housing defining an exterior surface and an internal cavity extending between distal ends. A wave guide is defined within the internal cavity. At least one open conduit is defined within the internal cavity providing a space for routing conductors through the housing. A fluid passage is defined within the internal cavity separate from the wave guide. A control and diagnostic system for a machine and a gas turbine engine are also disclosed.

公开(公告)号：US09873522B2

公开(公告)日：2018-01-23

申请号：US14866119

申请日：2015-09-25

Applicant: United Technologies Corporation

Inventor： Ryan K. Snyder ,  Eric J. Heims

IPC: B01D41/00 ,  B64D45/00 ,  F02K3/115 ,  F02C7/055 ,  F02C7/14 ,  B64D33/08 ,  F02C7/052 ,  F02C7/05 ,  B64D33/02 ,  B01D46/10

CPC classification number: B64D45/00 ,  B01D46/10 ,  B01D2273/10 ,  B01D2279/60 ,  B64D33/02 ,  B64D33/08 ,  F02C7/05 ,  F02C7/052 ,  F02C7/055 ,  F02C7/14 ,  F02K3/115 ,  F05D2260/213 ,  F05D2260/607 ,  F05D2260/98 ,  Y02T50/671 ,  Y02T50/675

Abstract: Aspects of the disclosure are directed to a screen configured for use in association with a cooler of an aircraft, the screen comprising: a first portion arranged as a grid and located in a line-of-sight of the cooler with respect to a fluid inlet, and a second portion located out of the line-of-sight of the cooler with respect to the fluid inlet, wherein the second portion is grid-free.

公开(公告)号：US20160312660A1

公开(公告)日：2016-10-27

申请号：US14696615

申请日：2015-04-27

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： James P. Chasse, JR. ,  Ryan K. Snyder ,  William K. Ackermann ,  Pellegrino J. Pisacreta ,  Judith F. Brooks ,  Stephanie Ernst

IPC: F01D25/28 ,  F01D25/12

CPC classification number: F01D25/28 ,  F01D25/12 ,  F01D25/14 ,  F02C7/18 ,  Y02T50/675

Abstract: A fitting according to an exemplary aspect of the present disclosure includes, among other things, a main body portion having a first axial end and a second axial end opposite the first axial end, an inlet provided at the first axial end, and an outlet adjacent the second axial end. The outlet includes a plurality of circumferentially spaced-apart slots formed through the main body portion, and each slot has an area within a range of 0.52 and 0.59 square inches.

Abstract translation: 根据本公开的示例性方面的配件包括主体部分，其具有第一轴向端部和与第一轴向端部相对的第二轴向端部，设置在第一轴向端部处的入口和邻近的出口 第二个轴向端。 出口包括穿过主体部分形成的多个周向间隔开的槽，并且每个槽具有在0.52和0.59平方英寸的范围内的面积。

公开(公告)号：US20160108819A1

公开(公告)日：2016-04-21

申请号：US14891236

申请日：2014-02-27

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Michael Dreher ,  Ryan K. Snyder ,  James M. McPherson ,  Ping Su ,  Fernando Quinones ,  Gabriel Rivera

IPC: F02C7/22 ,  F02C7/06

CPC classification number: F02C7/222 ,  F02C7/06 ,  F02C7/14 ,  F02C7/224 ,  F05D2230/21 ,  F05D2230/53 ,  F05D2260/406 ,  F05D2260/98 ,  F05D2270/64 ,  F05D2300/121 ,  F23K5/04 ,  F23K5/06 ,  Y02T50/675

Abstract: A single, unitary fuel/oil manifold for a gas turbine engine is provided which comprises one or more interfaces for mounting various fuel system and lubricating system components directly to the fuel/oil manifold. The fuel/oil manifold also defines fluid passages for transferring fuel or lubricant from one component to another component. Packing numerous fuel system and lubricating system components within the fuel/oil manifold reduces cost and weight and simplifies maintenance.

Abstract translation: 提供了一种用于燃气涡轮发动机的单一燃料/油歧管，其包括用于将各种燃料系统和润滑系统部件直接安装到燃料/油歧管的一个或多个接口。 燃料/油歧管还限定了用于将燃料或润滑剂从一个部件转移到另一个部件的流体通道。 在燃油/油歧管内包装多个燃油系统和润滑系统部件，降低了成本和重量，简化了维护。