Patent search ap:("UNITED TECHNOLOGIES CORP") AND inv:"SUCIU GABRIEL" Page 1

1.

发明专利
GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES 未知

公开(公告)号：CA2854077A1

公开(公告)日：2013-08-08

申请号：CA2854077

申请日：2013-01-18

Applicant: UNITED TECHNOLOGIES CORP

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

IPC: F04D29/04

Abstract: A gas turbine engine includes a very high speed fan drive turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5. The high pressure turbine is mounted by bearings positioned at an outer periphery of a shaft driven by the high pressure turbine.

2.

发明专利
DICHTUNGSANORDNUNG FÜR EINE GEBLÄSEROTORANORDNUNG EINER SPITZENTURBINE 未知

公开(公告)号：DE602006014269D1

公开(公告)日：2010-06-24

申请号：DE602006014269

申请日：2006-03-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NORRIS JAMES W , NORDEEN CRAIG A , ROBERGE GARY , SUCIU GABRIEL

IPC: F02K3/068 , F01D11/00 , F02C3/073

3.

发明专利
TURBINE WHEEL VANE FOR A TURBINE ENGINE 未知

公开(公告)号：PL357125A1

公开(公告)日：2003-05-19

申请号：PL35712502

申请日：2002-11-14

Applicant: UNITED TECHNOLOGIES CORP A USA

Inventor： SUCIU GABRIEL , BABU MICHAEL , MURDOCK JAMES R

IPC: F01D5/14 , F01D5/30 , F02K3/06 , F04D29/34 , F04D29/38

4.

发明专利
GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES 未知

公开(公告)号：CA2854077C

公开(公告)日：2021-03-16

申请号：CA2854077

申请日：2013-01-18

Applicant: UNITED TECHNOLOGIES CORP

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

IPC: F02C3/113 , F02C7/06 , F02C7/20 , F02K3/06

Abstract: A gas turbine engine includes a very high speed fan drive turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5. The high pressure turbine is mounted by bearings positioned at an outer periphery of a shaft driven by the high pressure turbine.

5.

发明专利
GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES 未知

公开(公告)号：SG11201403615QA

公开(公告)日：2014-10-30

申请号：SG11201403615Q

申请日：2013-01-18

Applicant: UNITED TECHNOLOGIES CORP

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

IPC: F02K3/06 , F02C7/06 , F04D29/056

Abstract: A gas turbine engine includes a very high speed fan drive turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5. The high pressure turbine is mounted by bearings positioned at an outer periphery of a shaft driven by the high pressure turbine.

6.

发明专利
Verdichtergehäuse einer Gasturbine mit Zapfluftöffnungen 未知

公开(公告)号：DE602004031915D1

公开(公告)日：2011-05-05

申请号：DE602004031915

申请日：2004-11-11

Applicant: UNITED TECHNOLOGIES CORP

Inventor： CUMMINGS KEVIN J , DEMERS CHRISTOPHER G , HODGSON JAMES C , SUCIU GABRIEL , MERRY BRIAN

IPC: F01D17/10 , F01D17/16 , F01D17/14 , F01D25/16 , F02C6/08 , F04D27/02 , F04D29/54

7.

发明公开
GAS TURBINE ENGINE WITH HIGH SPEED LOW PRESSURE TURBINE SECTION AND BEARING SUPPORT FEATURES 审中-公开
Title translation: 具有快速低压涡轮部分和贮水池特点的燃气涡轮发动机

公开(公告)号：EP2809953A4

公开(公告)日：2015-11-25

申请号：EP13743282

申请日：2013-01-18

Applicant: UNITED TECHNOLOGIES CORP

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

IPC: F04D29/04 , F02C7/06 , F02C7/20 , F02K3/06 , F04D29/056

CPC classification number: F04D29/056 , F02C7/06 , F02C7/20 , F02K3/06

Patent Agency Ranking