公开(公告)号：CA2845618A1

公开(公告)日：2014-05-22

申请号：CA2845618

申请日：2014-03-10

Applicant: UNITED TECHNOLOGIES CORP

Inventor： MCCUNE MICHAEL E ,  HUSBAND JASON ,  SCHWARZ FREDERICK M ,  KUPRATIS DANIEL BERNARD ,  SUCIU GABRIEL L ,  ACKERMANN WILLIAM K

IPC: F02C7/36 ,  F01D25/24 ,  F02C7/00 ,  F16H1/48 ,  F16H57/021

Abstract: A gas turbine engine includes a flex mount for a fan drive gear system. A very high speed fan drive turbine drives the fan drive gear system.

公开(公告)号：DE69107988T2

公开(公告)日：1995-11-02

申请号：DE69107988

申请日：1991-12-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  CANDELORI DAVID J ,  BROOKE RICHARD D

IPC: F01D9/02 ,  F01D5/08 ,  F01D11/00 ,  F01D11/02 ,  F01D11/06 ,  F01D17/08 ,  F02C7/18 ,  F02C7/28

Abstract: Cooling air to the 1-2 turbine stage seal is supplied in parallel with air to the vane (52) between the turbines (42, 48) from a plenum (24). A modulatable valve in the supply line to the plenum (24) regulates the air flow in response to a gas temperature sensed in the seal area by a thermocouple (26). Valve and thermocouples are checked for proper operation. Immediate alerts and maintenance messages are established along with fail safe operating conditions upon fault detection. Over cooling of the seal area during low power operation, in anticipation of a power increase, is used to improve low cycle fatigue life of the turbine disk and seal runner.

公开(公告)号：GB2168760A

公开(公告)日：1986-06-25

申请号：GB8529998

申请日：1985-12-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  GRIFFIN JAMES G

IPC: F01D5/08 ,  F02C7/18

公开(公告)号：EP3087267A4

公开(公告)日：2017-09-27

申请号：EP14885127

申请日：2014-12-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  SUCIU GABRIEL L

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

CPC classification number: F02C3/107 ,  F02C7/36 ,  F02K3/06 ,  F05D2260/4031

公开(公告)号：EP3058202A4

公开(公告)日：2017-06-28

申请号：EP14870182

申请日：2014-09-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M

IPC: F02C7/36 ,  F02K3/06

CPC classification number: F02C3/107 ,  F01D5/142 ,  F02K3/06 ,  F05D2220/327 ,  F05D2220/36 ,  F05D2260/40311 ,  Y02T50/671 ,  Y02T50/673

Abstract: A turbofan engine includes a fan section including a fan blade having a leading edge and hub to tip ratio of less than about 0.34 and greater than about 0.020 measured at the leading edge and a speed change mechanism with gear ratio greater than about 2.6 to 1. A first compression section includes a last blade trailing edge radial tip length that is greater than about 67% of the radial tip length of a leading edge of a first stage of the first compression section. A second compression section includes a last blade trailing edge radial tip length that is greater than about 57% of a radial tip length of a leading edge of a first stage of the first compression section.

Abstract translation: 涡轮风扇发动机包括风扇部分，风扇部分包括风扇叶片，风扇叶片具有在前缘处测量的小于大约0.34且大于大约0.020的前缘和毂到尖端比率以及具有大于大约2.6比1的齿轮比的变速机构。 第一压缩区段包括最终叶片后缘径向末端长度，该长度大于第一压缩区段的第一级的前缘的径向末端长度的约67％。 第二压缩区段包括最终叶片后缘径向末端长度，该长度大于第一压缩区段的第一级的前缘的径向末端长度的约57％。

公开(公告)号：EP3084174A4

公开(公告)日：2017-01-25

申请号：EP14881900

申请日：2014-11-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  SUCIU GABRIEL L

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

CPC classification number: F02C3/107 ,  F02C7/36 ,  F02K3/06 ,  F05D2250/30 ,  Y02T50/671

公开(公告)号：EP2971664A4

公开(公告)日：2016-11-16

申请号：EP13878400

申请日：2013-12-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  PICKFORD SIMON

IPC: F02C7/12 ,  F01D25/12 ,  F01D25/24 ,  F02C3/04 ,  F02C3/107 ,  F02C6/08 ,  F02C7/04 ,  F02C7/14 ,  F02C7/18 ,  F02C9/18 ,  F02K3/06 ,  F02K3/115

CPC classification number: F02C7/185 ,  F01D25/24 ,  F02C3/04 ,  F02C3/107 ,  F02C6/08 ,  F02C7/04 ,  F02C7/12 ,  F02C7/14 ,  F02C7/18 ,  F02C9/18 ,  F02K3/06 ,  F02K3/115 ,  F05D2260/4031 ,  F05D2260/98 ,  Y02T50/675

公开(公告)号：EP2954212A4

公开(公告)日：2016-05-25

申请号：EP14748753

申请日：2014-02-04

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  PICKFORD SIMON

IPC: F04D29/06 ,  F01D25/12 ,  F01D25/18 ,  F01D25/20 ,  F02C7/06 ,  F02C7/14 ,  F02K3/06

CPC classification number: F01D25/20 ,  F01D1/02 ,  F01D15/10 ,  F01D15/12 ,  F01D25/08 ,  F01D25/125 ,  F01D25/16 ,  F01D25/18 ,  F02C3/107 ,  F02C7/14 ,  F05D2220/30 ,  F05D2260/20 ,  F05D2260/213 ,  F05D2260/40311 ,  F05D2260/98 ,  Y02T50/676

Abstract: A turbine engine system includes a first lubricant circuit, a second lubricant circuit, a plurality of engine stages and a shaft. The first lubricant circuit includes a first turbine engine component that is fluidly coupled with a first lubricant heat exchanger. The second lubricant circuit includes a second turbine engine component that is fluidly coupled with a second lubricant heat exchanger, wherein the second lubricant circuit is fluidly separate from the first lubricant circuit. The first turbine engine component includes a gear train, which connects a first of the engine stages to a second of the engine stages. The second turbine engine component includes a bearing. The shaft is supported by the bearing and connected to one of the engine stages.

公开(公告)号：EP2841718A4

公开(公告)日：2016-03-02

申请号：EP13822569

申请日：2013-04-23

Applicant: UNITED TECHNOLOGIES CORP

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

IPC: F01D25/16 ,  F02C7/06

CPC classification number: F01D25/162 ,  F02C3/107 ,  F02C7/06 ,  F02K3/06

公开(公告)号：EP2935791A4

公开(公告)日：2016-01-20

申请号：EP13864578

申请日：2013-12-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SCHWARZ FREDERICK M ,  WEISSE MICHAEL A

IPC: F01D5/22 ,  F02C7/00

CPC classification number: F04D29/326 ,  F01D5/225 ,  F01D11/02 ,  F02C3/107 ,  F04D27/004 ,  F04D27/0261 ,  F04D29/164 ,  F04D29/321 ,  F05D2220/36 ,  F05D2300/603 ,  Y02T50/673 ,  Y10T29/49229

Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a fan section including a fan with a plurality of fan blades rotatable about an axis and a shroud and a speed change device in communication with the fan.