公开(公告)号：EP2864612A4

公开(公告)日：2015-07-08

申请号：EP13807202

申请日：2013-06-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEBLANC RYAN EDWARD ,  CUMMINGS KEVIN J

IPC: F02C7/00 ,  F01D17/14 ,  F01D17/16 ,  F02C7/20 ,  F02C7/32 ,  F02C9/18 ,  F02K3/075

CPC classification number: F02C9/18 ,  F01D17/162 ,  F04D27/0215 ,  F04D27/023 ,  F05D2240/91 ,  F05D2260/50 ,  F05D2260/56 ,  Y10T74/20

Abstract: A bracket for use with a four bar linkage, has a head portion having a triangular shape, and a shank extending from a corner of the triangular head portion, the shank thickening depthwise and narrowing widthwise along its length.

Abstract translation: 用于四杆连杆的支架具有三角形形状的头部，以及从三角形头部的角部延伸的柄部，该柄部沿着其长度沿深度方向变宽并沿宽度方向变窄。

公开(公告)号：EP2864597A4

公开(公告)日：2016-06-15

申请号：EP13807208

申请日：2013-04-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEBLANC RYAN EDWARD ,  CUMMINGS KEVIN J ,  FORD BARRY M

IPC: F01D17/00 ,  F04D29/02

CPC classification number: F04D27/0215 ,  F02C6/08 ,  F02C9/18 ,  F04D27/023 ,  F04D29/023 ,  F04D29/522 ,  F05D2230/10 ,  Y02T50/671 ,  Y10T29/49234

Abstract: An air bleed system for a jet engine is provided. The air bleed system is located in the low pressure compressor chamber and comprises a movable bleed valve and a stationary, annular bleed case having a forward section and an aft section and ligaments connecting the two sections and providing structural support to the bleed case. The ligaments are machined from the bleed case into an aerodynamic shape that maximizes the flow of air through the bleed ports.

公开(公告)号：EP2864610A4

公开(公告)日：2015-07-22

申请号：EP13806251

申请日：2013-06-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEBLANC RYAN EDWARD ,  CUMMINGS KEVIN J

IPC: F02C7/00 ,  F01D17/10 ,  F01D17/20 ,  F02C6/08 ,  F02C7/20 ,  F02C7/32 ,  F04D27/02 ,  F04D29/02

CPC classification number: F02C6/08 ,  F01D17/105 ,  F01D17/20 ,  F04D27/0215 ,  F04D27/023 ,  F04D29/023 ,  F04D29/545 ,  F05B2280/10304 ,  F05D2230/21 ,  F05D2260/50 ,  F05D2260/941 ,  F05D2300/121 ,  F05D2300/133 ,  Y10T29/49236

Abstract: A duct assembly for venting flow from an internal portion of a gas turbine engine, has a first piece having a first duct portion extending therethrough, the first piece configured to withstanding backbone loads of the engine, the first piece having a first portion of a duct passing therethrough, and a second piece, the second piece having a second portion of the duct passing therethrough, the second portion and the first portion aligning, the second piece constructed of a lighter material than the first piece.

公开(公告)号：EP2864613A4

公开(公告)日：2015-07-15

申请号：EP13807735

申请日：2013-06-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEBLANC RYAN EDWARD ,  CUMMINGS KEVIN J

IPC: F02C7/00 ,  F01D17/10 ,  F01D17/20 ,  F02C6/08 ,  F02C7/20 ,  F02C7/32

CPC classification number: F02C7/00 ,  F01D17/105 ,  F01D17/20 ,  F02C6/08 ,  F02C7/20 ,  F02C7/32 ,  F04D27/0215 ,  F04D27/023 ,  F05D2260/50

Abstract: An actuation system for a bleed valve includes first and second bell cranks connected by a connecting link. The first bell crank has a first arm that is coupled to a bleed valve and a second arm that is coupled to the connecting link. The connecting link has a first end coupled to the second arm of the first bell crank and a second end coupled to a first arm of the second bell crank. A second arm of the second bell crank is coupled to an actuating element. Input is communicated through the actuating element to move the bleed valve between open and closed positions via the first and second bell cranks.

Abstract translation: 用于放气阀的致动系统包括通过连接连杆连接的第一和第二钟形曲柄。 第一钟形曲柄具有联接到排放阀的第一臂和耦合到连接链节的第二臂。 连接连杆具有联接到第一钟形曲柄的第二臂的第一端和联接到第二曲柄的第一臂的第二端。 第二钟形曲柄的第二臂联接到致动元件。 输入通过致动元件传递，以便通过第一和第二钟形曲柄使放气阀在打开和关闭位置之间移动。

公开(公告)号：EP2904213A4

公开(公告)日：2016-04-27

申请号：EP13844023

申请日：2013-09-25

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEBLANC RYAN EDWARD ,  CUMMINGS KEVIN ,  ALI AMR

IPC: F01D5/22 ,  F01D5/12 ,  F01D17/10 ,  F01D25/06 ,  F02C6/08 ,  F02C7/00 ,  F02K3/00 ,  F04D27/02 ,  F04D29/52 ,  F04D29/66

CPC classification number: F01D5/10 ,  F01D17/105 ,  F01D25/06 ,  F02C6/08 ,  F04D27/023 ,  F04D29/526 ,  F04D29/668 ,  F05D2220/3216 ,  F05D2260/606 ,  F05D2260/96 ,  F05D2260/963 ,  Y10T29/49236

Abstract: A system for minimizing non-integral vibrations in rotor blades located in a compressor section of a gas turbine engine includes a casing having a plurality of bleed slots, at least one of the bleed slots being located in close proximity to a row of rotor blades, a plurality of structural ligaments, at least one of the structural ligaments extending between two adjacent ones of the bleed slots; and a channel for reducing the height of at least one of the structural ligaments so as to minimize the non-integral vibrations in the rotor blades in the row.

公开(公告)号：EP2864611A4

公开(公告)日：2016-03-23

申请号：EP13806497

申请日：2013-06-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： LEBLANC RYAN EDWARD ,  CUMMINGS KEVIN J

IPC: F02C9/00 ,  F01D17/14 ,  F02C7/042 ,  F02C7/20 ,  F02C9/18

CPC classification number: F02C9/18 ,  F01D17/141 ,  F04D27/0215 ,  F04D27/023 ,  F05D2250/711 ,  F05D2260/30 ,  F05D2260/50 ,  F05D2260/56 ,  F05D2260/606 ,  F05D2260/96 ,  F05D2300/431 ,  F05D2300/501 ,  Y10T74/2142