公开(公告)号：EP3019726A4

公开(公告)日：2016-08-03

申请号：EP14823381

申请日：2014-07-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OTTO JOHN R ,  SHARMA SUNIL

IPC: F02C7/20 ,  F01D25/16 ,  F01D25/28

CPC classification number: F01D15/12 ,  F01D25/164 ,  F01D25/24 ,  F01D25/28 ,  F02C7/20 ,  F02C7/36 ,  F04D25/045 ,  F04D29/053 ,  F04D29/325 ,  F05D2220/323 ,  F05D2230/60 ,  Y02T50/671

Abstract: A gear assembly support for a gas turbine engine includes a first portion engageable to a case of the gas turbine engine and a second portion configured for supporting a gear assembly. The support includes a torque reacting portion for transferring torque from the second portion to the first portion, a forward flange disposed forward of the torque reacting portion, the forward flange defining a first interface to the case and an aft flange disposed aft of the torque reacting portion, the aft flange defining a second interface to the case.

Abstract translation: 一种用于燃气涡轮发动机的齿轮组件支撑件包括第一部分接合，以使燃气涡轮发动机的情况下，并且被配置用于支撑齿轮组件的第二部分。 所述支撑件包括扭矩从第二部分到第一部分起反应为传递环转矩部分，转矩的前凸缘向前设置起反应的部分，前凸缘限定第一接口到壳体和后凸缘的转矩的处理完毕后起反应 部，后凸缘限定第二接口的情况。

公开(公告)号：EP2831403A4

公开(公告)日：2015-12-02

申请号：EP13768646

申请日：2013-03-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： COFFIN JAMES B ,  OTTO JOHN R

IPC: F02K3/00 ,  F02C7/00 ,  F02C7/36 ,  F02K99/00

CPC classification number: F01D15/12 ,  F01D25/04 ,  F02C7/36 ,  F02K3/06 ,  F05D2260/40311 ,  F05D2260/96 ,  Y10T74/19642

Abstract: A gas turbine engine includes a fan section. A turbine section is coupled to the fan section via a geared architecture. The geared architecture includes a torque frame and a flex support spaced apart from one another at a location. A gear train is supported by the torque frame. A damper is provided between the torque frame and the flex support at the location.

公开(公告)号：EP2809889A4

公开(公告)日：2015-11-18

申请号：EP13775951

申请日：2013-01-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OTTO JOHN R

IPC: F01D25/04 ,  F01D25/16 ,  F16H1/28

CPC classification number: F02C7/20 ,  F01D21/045 ,  F01D25/162 ,  F01D25/164 ,  F02C3/107 ,  F02C7/36 ,  F05D2230/53 ,  F05D2230/642 ,  F05D2250/41 ,  F05D2260/40311 ,  F05D2300/501

Abstract: An example turbomachine geared architecture support assembly includes a subpart having a more compliant portion and a less compliant portion. The less compliant portion includes a stop that limits axial movement of a geared architecture within a turbomachine.

公开(公告)号：EP3039276A4

公开(公告)日：2017-04-12

申请号：EP14839045

申请日：2014-08-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OTTO JOHN R ,  COFFIN JAMES B ,  HUSBAND JASON

IPC: F02K3/00 ,  F02C7/36

CPC classification number: F04D25/045 ,  F01D5/02 ,  F01D15/12 ,  F02C3/107 ,  F02C7/36 ,  F02K3/06 ,  F04D25/028 ,  F04D27/004 ,  F04D29/321 ,  F05D2220/32 ,  F05D2260/40311 ,  F05D2270/02

Abstract: A turbofan engine is disclosed that includes a fan rotatable about an axis, a compressor section including a high pressure compressor, a medium pressure compressor and a low pressure compressor and a turbine section including a high pressure turbine, an intermediate turbine and a fan drive turbine. A fan drive gear system is driven by the fan drive turbine for driving the fan. A compressor drive gear system is driven by the intermediate turbine for driving the low pressure compressor. A gear controller controls rotation of at least one of the fan drive gear system and the compressor drive gear system relative to a static structure to vary an effective speed reduction ratio of one of the fan drive gear system and the compressor drive gear system.

Abstract translation: 公开了一种涡轮风扇发动机，其包括可围绕轴线旋转的风扇，包括高压压缩机，中压压缩机和低压压缩机的压缩机部分和包括高压涡轮机，中间涡轮机和风扇驱动涡轮机 。 风扇驱动齿轮系由风扇驱动涡轮驱动，用于驱动风扇。 压缩机驱动齿轮系由驱动低压压缩机的中间涡轮驱动。 齿轮控制器控制风扇驱动齿轮系统和压缩机驱动齿轮系统中的至少一个相对于静态结构的旋转，以改变风扇驱动齿轮系统和压缩机驱动齿轮系统之一的有效减速比。

公开(公告)号：EP3019725A4

公开(公告)日：2016-12-28

申请号：EP14847155

申请日：2014-07-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OTTO JOHN R ,  BAKER STEPHANIE M

IPC: F02C7/06 ,  F01D25/18 ,  F16H57/04

CPC classification number: F01D25/18 ,  B01D29/11 ,  B01D29/52 ,  B01D35/005 ,  F01D9/065 ,  F01D15/12 ,  F01M2001/126 ,  F02C7/06 ,  F05D2220/32 ,  F05D2260/40311 ,  F05D2260/98 ,  F16H57/0404 ,  F16N7/40

Abstract: A lubrication system for gas turbine engine includes a main lubricant passage for providing lubricant from a lubricant supply to a lubricant manifold. The lubricant manifold includes first and second lubricant passages The lubricant manifold is configured to supply lubricant to first and second separate parts of a geared architecture at different first and second lubricant flow conditions. A first filter element is provided within a radial tube for supplying lubricant to the first passage of the lubricant manifold and a second filter element is provided within a second radial tube for supplying lubricant to the second lubricant passage of the lubricant manifold. The first filter element is different than the second filter element.

公开(公告)号：EP3019728A4

公开(公告)日：2016-07-27

申请号：EP14823162

申请日：2014-07-03

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OTTO JOHN R ,  COFFIN JAMES B ,  HUSBAND JASON

IPC: F02C7/36 ,  F01D25/00 ,  F02C3/107 ,  F16H1/34 ,  F16H3/66 ,  F16H57/08

CPC classification number: F02C7/36 ,  F02C3/10 ,  F02C3/107 ,  F02K3/06 ,  F05D2240/40 ,  F05D2260/40311

Abstract: A turbofan engine includes a fan rotatable about an axis and a compressor section including a high pressure compressor and a low pressure compressor. A turbine section includes a high pressure turbine, an intermediate turbine and a fan drive turbine. The high pressure turbine is coupled to drive the high pressure compressor. A fan drive gear system is driven by the fan drive turbine for driving the fan and a compressor drive gear system is driven by the intermediate turbine for driving the low pressure compressor.

Abstract translation: 涡轮风扇发动机包括可围绕轴线旋转的风扇和包括高压压缩机和低压压缩机的压缩机部分。 涡轮机部分包括高压涡轮机，中间涡轮机和风扇驱动涡轮机。 高压涡轮联接以驱动高压压缩机。 风扇驱动齿轮系由风扇驱动涡轮驱动，用于驱动风扇，压缩机驱动齿轮系由驱动低压压缩机的中间涡轮机驱动。

公开(公告)号：EP3004598A4

公开(公告)日：2016-07-06

申请号：EP14836013

申请日：2014-05-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CIGAL BRIAN P ,  OTTO JOHN R

IPC: F02C7/20 ,  F01D25/16 ,  F01D25/28 ,  F02C3/107 ,  F02C7/36 ,  F02K3/04

CPC classification number: F02C7/36 ,  F01D25/164 ,  F02C3/107 ,  F02K3/04 ,  F05D2230/60 ,  F05D2260/30 ,  F05D2260/36 ,  F05D2260/40 ,  F05D2260/40311 ,  F16H57/02 ,  F16H57/025

Abstract: A gear assembly support for a gas turbine engine includes a spline ring configured to fit into a case of the gas turbine engine and a flex support. The flex support includes splines for engaging the spline ring and an inner portion attachable to a portion the gear assembly.

Abstract translation: 用于燃气涡轮发动机的齿轮组件支撑件包括构造成装配到燃气涡轮发动机和柔性支撑件的壳体中的花键环。 柔性支撑件包括用于接合花键环的花键和可附接到齿轮组件的一部分的内部部分。

公开(公告)号：EP2904235A4

公开(公告)日：2015-11-11

申请号：EP13866352

申请日：2013-09-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： OTTO JOHN R ,  SHARMA SUNIL

IPC: F02C7/00 ,  F01D25/00 ,  F02C3/14 ,  F02C7/20 ,  F02C7/36 ,  F16H1/28

CPC classification number: F16H1/2809 ,  F02C7/36 ,  F05D2260/30 ,  F05D2260/40311 ,  Y02T50/671 ,  Y10T29/49231

Abstract: A disclosed gear assembly support for a gas turbine engine includes a first portion configured for attachment to a case of the gas turbine engine and a second portion configured for supporting a gear assembly. The support further includes a snap portion defining a fit within the case. The snap portion includes a tunable feature for adjusting a fit within the case. A torque reacting portion of the support transfers torque from the second portion to the first portion separate from the snap portion and include separately tunable features for adjusting the snap fit independent of the torque transfer portions.

Abstract translation: 公开的用于燃气涡轮发动机的齿轮组件支撑件包括构造成附接到燃气涡轮发动机的壳体的第一部分和被配置为支撑齿轮组件的第二部分。 支撑件还包括限定在壳体内的配合的卡扣部分。 卡扣部分包括用于调节壳体内的配合的可调特征。 支撑件的扭矩反作用部分将扭矩从第二部分转移到与卡扣部分分离的第一部分，并且包括单独的可调谐特征，用于独立于扭矩传递部分而调整卡扣配合。