公开(公告)号：EP2820264A4

公开(公告)日：2015-11-18

申请号：EP13790528

申请日：2013-02-22

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  KUPRATIS DANIEL BERNARD ,  SUCIU GABRIEL L

IPC: F02C3/067 ,  F01D25/16 ,  F02C3/107 ,  F02K3/072

CPC classification number: F01D25/162 ,  F02C3/107 ,  F02K3/072 ,  F05D2260/40311

Abstract: A turbine engine includes a fan, a compressor section having a low pressure compressor section and a high pressure compressor section, a combustor in fluid communication with the compressor section and a turbine section in fluid communication with the combustor. The turbine section includes a low pressure turbine section and a high pressure turbine section. The low pressure compressor section, the low pressure turbine section and the fan rotate in a first direction whereas the high pressure compressor section and the high pressure turbine section rotate in a second direction opposite the first direction.

Abstract translation: 涡轮发动机包括风扇，具有低压压缩机部分和高压压缩机部分的压缩机部分，与压缩机部分流体连通的燃烧器和与燃烧器流体连通的涡轮部分。 涡轮部分包括低压涡轮部分和高压涡轮部分。 低压压缩机部分，低压涡轮部分和风扇沿第一方向旋转，而高压压缩机部分和高压涡轮部分沿与第一方向相反的第二方向旋转。

公开(公告)号：EP2809940A4

公开(公告)日：2015-11-18

申请号：EP13777804

申请日：2013-01-29

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KUPRATIS DANIEL BERNARD ,  SCHWARZ FREDERICK M

IPC: B63H5/10 ,  B64C11/48 ,  B64C27/10 ,  F01D25/16 ,  F02C1/00 ,  F02C1/06 ,  F02C3/00 ,  F02C3/10 ,  F02C6/00 ,  F02C7/06 ,  F02K3/00 ,  F02K3/02 ,  F02K3/06 ,  F02K3/072

CPC classification number: F02C7/06 ,  F02K3/06 ,  F05D2260/40311 ,  Y02T50/671

公开(公告)号：EP2809934A4

公开(公告)日：2015-10-14

申请号：EP13775036

申请日：2013-01-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  ACKERMANN WILLIAM K ,  KUPRATIS DANIEL BERNARD ,  SCHWARZ FREDERICK M

IPC: F02K3/06 ,  F02C3/107 ,  F02C7/36

CPC classification number: F02K3/06 ,  F02C3/107 ,  F02C7/36 ,  F05D2220/323 ,  F05D2250/44

公开(公告)号：EP2834469A4

公开(公告)日：2015-06-24

申请号：EP13813216

申请日：2013-03-28

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  KUPRATIS DANIEL BERNARD

IPC: F01D5/02 ,  F01D15/12 ,  F02C3/067 ,  F02C7/00 ,  F02C7/36 ,  F02K3/072

CPC classification number: F16J15/0887 ,  F01D15/12 ,  F02C3/067 ,  F02C7/36 ,  F02K3/072 ,  Y02T50/672

Abstract: A seal for use between a first duct and a second duct and, the ducts having relative motion therebetween, includes a first plurality of fingers for attachment to the first duct to be disposed about one of the first duct and the second duct, a seal land attaching to about an other of the first duct and the second duct, and a seal attaching to the seal land and in contact with the plurality of fingers wherein one of the plurality of fingers and the seal is metallic and an other of the seal land or the plurality of fingers is non-metallic.

公开(公告)号：EP2834505A4

公开(公告)日：2015-04-29

申请号：EP13877780

申请日：2013-03-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KUPRATIS DANIEL BERNARD ,  SCHWARZ FREDERICK M

IPC: F02C7/36 ,  F02C7/00 ,  F02K3/06

CPC classification number: F02K3/06 ,  F02C7/36 ,  F05D2260/40311

Abstract: A gas turbine engine includes first and second shafts rotatable about a common axis. A first turbine section is supported on the first shaft. Second compressor and turbine sections are supported on the second shaft. The gas turbine engine includes a fan. A first compressor section is arranged in an axial flow relationship with the second compressor and the first and second turbines. A geared architecture operatively connects the first shaft and the fan. An inducer operative couples to the gear train.

公开(公告)号：EP3090160A1

公开(公告)日：2016-11-09

申请号：EP14877384

申请日：2014-12-19

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KUPRATIS DANIEL BERNARD ,  HASEL KARL L

IPC: F02C3/04 ,  F02C7/00 ,  F02K3/06

CPC classification number: F02C3/04 ,  F02K3/06 ,  F05D2220/321 ,  F05D2220/3216

Abstract: A turbine engine includes at least a compressor section and a turbine section, each having at least a first and second portion. A ratio of turbine section second portion stages to compressor section second portion stages is less than or equal to 1.

Abstract translation: 涡轮发动机包括至少一个压缩机部分和一个涡轮部分，每个部分至少具有第一部分和第二部分。 涡轮机段第二部分段与压缩机段第二部分段的比率小于或等于1。

公开(公告)号：EP2820255A4

公开(公告)日：2015-12-23

申请号：EP13785331

申请日：2013-02-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  KUPRATIS DANIEL BERNARD

IPC: F01D17/16 ,  F02C7/042 ,  F02C9/22

CPC classification number: F01D17/162 ,  F02C9/22 ,  F05D2270/112 ,  F05D2270/3032

Abstract: A gas turbine engine includes a shaft and a turbine configured to drive the shaft. The turbine has at least one stage comprising a plurality of turbine vanes interspersed with a plurality of turbine blades. The plurality of vanes includes at least one variable vane movable between a closed position to reduce air flow and an open position to increase air flow. Movement of the at least one variable vane is controlled based on an engine limiting condition.

公开(公告)号：EP2820249A4

公开(公告)日：2015-12-23

申请号：EP13784211

申请日：2013-02-14

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  KUPRATIS DANIEL BERNARD

IPC: F02C3/107 ,  F02C7/36 ,  F02K3/06

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

公开(公告)号：EP2834496A4

公开(公告)日：2015-12-09

申请号：EP13772321

申请日：2013-03-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： KUPRATIS DANIEL BERNARD ,  SCHWARZ FREDERICK M

IPC: F02C7/00 ,  F02C7/36 ,  F02C9/00 ,  F02K3/00

CPC classification number: F02C7/36 ,  F02C3/113 ,  F05D2260/40311

Abstract: A gas turbine engine includes first and second shafts rotatable about a common axis. A first turbine section is supported on the first shaft. Second compressor and turbine sections are supported on the second shaft. The gas turbine engine includes a fan, a first compressor section, and a differential gear train that couples the fan and the first compressor section to the first shaft.

公开(公告)号：EP2820250A4

公开(公告)日：2015-12-09

申请号：EP13784828

申请日：2013-02-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  KUPRATIS DANIEL BERNARD

IPC: F01D15/12 ,  F01D5/02 ,  F02C7/047 ,  F02C7/36 ,  F02K3/072

CPC classification number: F01D15/12 ,  F02C7/047 ,  F02C7/36 ,  F02K3/072 ,  F05D2260/40311

Abstract: A gas turbine engine includes a shaft, a speed change device driven by the shaft, and a fan including a fan rotor driven by the speed change device. At least one inducer stage is positioned aft of the fan and is coupled for rotation with the fan rotor.