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61.COUNTER-ROTATING LOW PRESSURE TURBINE WITH GEAR SYSTEM MOUNTED TO TURBINE EXHAUST CASE 审中-公开
Title translation: 连续低压管与涡轮排气装置安装的齿轮系统公开(公告)号:EP2820266A4
公开(公告)日:2015-09-16
申请号:EP13793559
申请日:2013-02-15
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MERRY BRIAN D , SUCIU GABRIEL L
IPC: F02C3/067 , F01D1/24 , F01D15/12 , F01D25/12 , F01D25/16 , F01D25/24 , F01D25/30 , F02C3/107 , F02C7/32 , F02K3/072
CPC classification number: F01D15/12 , F01D1/24 , F01D25/162 , F01D25/30 , F02C3/107 , F02C7/32 , F02K3/072 , Y02T50/671
Abstract: A gas turbine engine includes a shaft defining an axis of rotation. An outer rotor directly drives the shaft and includes an outer set of blades. An inner rotor has an inner set of blades interspersed with the outer set of blades. The inner rotor is configured to rotate in an opposite direction about the axis of rotation from the outer rotor. A gear system couples the inner rotor to the shaft and is configured to rotate the inner set of blades at a faster speed than the outer set of blades.
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62.SEGMENTED SEAL FOR GAS TURBINE ENGINE 审中-公开
Title translation: SEGMENTIERTE DICHTUNGFÜRGASTURBINENMOTOR公开(公告)号:EP3068997A4
公开(公告)日:2017-07-05
申请号:EP14881671
申请日:2014-11-11
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HILL JAMES D , SUCIU GABRIEL L , MERRY BRIAN D , ALVANOS IOANNIS
CPC classification number: F01D11/005 , F01D5/06 , F01D5/081 , F01D9/041 , F01D11/001 , F05D2220/32 , F05D2240/57 , F05D2240/80 , F05D2260/30 , Y02T50/676
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公开(公告)号:EP3036416A4
公开(公告)日:2017-03-22
申请号:EP14851172
申请日:2014-07-16
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SCHWARZ FREDERICK M , HASEL KARL L , MERRY BRIAN D
CPC classification number: F02C3/06 , F01D5/14 , F02C3/107 , F02C7/36 , F02K3/06 , F05D2220/32 , F05D2220/36 , F05D2240/30 , F05D2240/303 , F05D2240/307 , F05D2260/40311 , F16H1/28
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64.COUNTER ROTATING LOW PRESSURE COMPRESSOR AND TURBINE EACH HAVING A GEAR SYSTEM 审中-公开
Title translation: 相反低压压气机和涡轮,均与传输系统公开(公告)号:EP2820267A4
公开(公告)日:2015-11-04
申请号:EP13804162
申请日:2013-02-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SUCIU GABRIEL L , MERRY BRIAN D
CPC classification number: F02K3/072 , F02C3/113 , F02C7/36 , F05D2250/36 , F05D2260/40311 , Y02T50/671
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公开(公告)号:EP2809937A4
公开(公告)日:2015-10-07
申请号:EP13805198
申请日:2013-01-29
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MERRY BRIAN D , SUCIU GABRIEL L
CPC classification number: F01D25/162 , F05D2260/53
Abstract: A gas turbine engine includes a shaft supported by first and second bearings for rotation relative to an inlet case. The first and second bearings are positioned within a common bearing compartment.
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公开(公告)号:EP2776677A4
公开(公告)日:2014-10-08
申请号:EP12861657
申请日:2012-12-26
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HASEL KARL L , STAUBACH JOSEPH B , MERRY BRIAN D , SUCIU GABRIEL L , DYE CHRISTOHPER M
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67.GAS TURBINE ENGINE SHAFT BEARING CONFIGURATION 审中-公开
Title translation: KONFIGURATION EINES WELLENLAGERSFÜREINE GASTURBINE公开(公告)号:EP3027864A4
公开(公告)日:2017-03-22
申请号:EP14849357
申请日:2014-06-19
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MERRY BRIAN D , SUCIU GABRIEL L , HASEL KARL L
CPC classification number: F02C7/36 , F01D25/162 , F02C3/107 , F02C7/06 , F05D2260/40311
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68.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: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
CPC classification number: F01D25/162 , F02C3/107 , F02C7/06 , F02K3/06
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69.GEARED TURBOMACHINE ARCHITECTURE HAVING A LOW PROFILE CORE FLOW PATH CONTOUR 审中-公开
Title translation: 带扁平芯流动的GEARBOURNE机器结构公开(公告)号:EP2809888A4
公开(公告)日:2015-12-02
申请号:EP13743906
申请日:2013-01-18
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SUCIU GABRIEL L , MERRY BRIAN D , HASEL KARL L
IPC: F01D15/12 , F01D25/26 , F01D25/28 , F02C3/107 , F02C7/04 , F02K3/06 , F03B11/00 , F03D5/00 , F03D11/02 , F03D11/04 , F04D29/52 , F04D29/54 , F04D29/60
CPC classification number: F02K3/06 , F02C3/107 , F02C7/04 , F04D29/522 , F05D2260/40311 , F05D2270/17
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70.COUNTER ROTATING LOW PRESSURE TURBINE WITH SPLITTER GEAR SYSTEM 审中-公开
Title translation: 带分流器传动系统的连续低压锡公开(公告)号:EP2820265A4
公开(公告)日:2015-11-04
申请号:EP13790583
申请日:2013-02-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SUCIU GABRIEL L , MERRY BRIAN D , MCCUNE MICHAEL E , MAGGE SHANKAR S
CPC classification number: F02C3/107 , F01D1/26 , F02C3/067 , F02C7/36 , F02K3/072 , F05D2250/44 , F05D2260/40311 , Y02T50/671
Abstract: A gas turbine engine includes a shaft defining an axis of rotation. An outer turbine rotor directly drives the shaft and includes an outer set of blades. An inner turbine rotor has an inner set of blades interspersed with the outer set of blades. The inner turbine rotor is configured to rotate in an opposite direction about the axis of rotation from the outer turbine rotor. A splitter gear system couples the inner turbine rotor to the shaft and is configured to rotate the inner set of blades at a faster speed than the outer set of blades.
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