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公开(公告)号：JP2013139782A
公开(公告)日：2013-07-18
申请号：JP2012278774
申请日：2012-12-21
Inventor： SUCIU GABRIEL L , MERRY BRIAN D , DYE CHRISTOPHER M , JOHNSON STEVEN B , SCHWARZ FREDERICK M
Abstract: PROBLEM TO BE SOLVED: To provide a gas turbine engine arrangement in an engine mounting structure for mounting a turbo fan gas turbine engine to an aircraft pylon.SOLUTION: The gas turbine engine includes a spool which drives a gear train along an engine center axis, wherein the spool includes a low pressure compressor with 4 to 8 stages.
Abstract translation: 要解决的问题：提供一种用于将涡轮风扇燃气涡轮发动机安装到飞机塔架的发动机安装结构中的燃气涡轮发动机装置。解决方案：燃气涡轮发动机包括沿发动机中心轴驱动齿轮系的线轴， 其中所述线轴包括具有4至8级的低压压缩机。
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公开(公告)号：JP2013139798A
公开(公告)日：2013-07-18
申请号：JP2012280501
申请日：2012-12-25
Inventor： SUCIU GABRIEL L , MERRY BRIAN D , DYE CHRISTOPHER M , JOHNSON STEVEN B , SCHWARZ FREDERICK M
CPC classification number: F02C3/107 , B64D27/26 , B64D33/04 , F02K1/09 , F02K1/72 , F02K1/763 , F02K3/075 , F05D2240/50
Abstract: PROBLEM TO BE SOLVED: To provide a gas turbine engine which has a low stage count low-pressure turbine.SOLUTION: A gas turbine engine includes a spool which drives a gear train along an engine center axis, wherein the spool includes the low-pressure turbine with 3 to 6 stages.
Abstract translation: 要解决的问题：提供一种具有低阶数低压涡轮机的燃气涡轮发动机。解决方案：燃气涡轮发动机包括沿发动机中心轴驱动齿轮系的阀芯，其中阀芯包括低压 涡轮机3〜6级。
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公开(公告)号：CA2800001C
公开(公告)日：2015-10-13
申请号：CA2800001
申请日：2012-12-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor： SUCIU GABRIEL L , MERRY BRIAN D , DYE CHRISTOPHER M , JOHNSON STEVEN B , SCHWARZ FREDERICK M
Abstract: A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low pressure compressor with four to eight (4-8) stages.
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公开(公告)号：CA2800464C
公开(公告)日：2015-04-07
申请号：CA2800464
申请日：2012-12-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor： SUCIU GABRIEL L , MERRY BRIAN D , DYE CHRISTOPHER M , JOHNSON STEVEN B , SCHWARZ FREDERICK M
Abstract: A gas turbine engine includes a spool along an engine centerline axis which drives a gear train.
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公开(公告)号：BR102012028942A2
公开(公告)日：2016-11-01
申请号：BR102012028942
申请日：2012-11-12
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MERRY BRIAN D , DYE CHRISTOPHER M , SCHWARZ FREDERICK M , SUCIU GABRIEL L , JOHNSON STEVEN B
Abstract: motor de turbina a gás. a presente inven$o se refere a um motor de turbina a gás que inclui um eixo do conjunto compressor-turbina ao longo de um eixo da linha e centro do motor que aciona um trem de engrenagem.
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Patent Agency Ranking
公开(公告)号：RU2747543C1
公开(公告)日：2021-05-06
申请号：RU2019113285
申请日：2012-12-31
Applicant: UNITED TECHNOLOGIES CORP
Inventor： SUCIU GABRIEL L , MERRY BRIAN D , DYE CHRISTOPHER M , JOHNSON STEVEN B , SCHWARZ FREDERICK M
Abstract: Газотурбинныйдвигательсогласноодномуиллюстративномуаспектунастоящегоизобретениясодержитредуктор, расположенныйвдольпродольнойосидвигателя, икаскад, которыйрасположенвдольуказаннойпродольнойосидвигателяи приводитв действиередуктор, приэтомуказанныйкаскадсодержиттурбинунизкогодавленияс небольшимчисломступеней. Вследующемнеограничительномпримереодногоизвышеуказанныхвариантовосуществлениягазотурбинногодвигателянебольшоечислоступенейможетсоставлятьоттрехдошести (3-6) ступеней. Дополнительноилиальтернативно, небольшоечислоступенейможетсоставлятьтри (3) ступени. Дополнительноилиальтернативно, небольшоечислоступенейможетсоставлятьпять (5) илишесть (6) ступеней. Достигаетсяполучениелегкойи эффективнофункционирующейконструкциидвигателяи обеспечениевысокогополетногоКПД. 14 з.п. ф-лы, 15 ил.
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公开(公告)号：BR102012028940A2
公开(公告)日：2015-10-06
申请号：BR102012028940
申请日：2012-11-12
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MERRY BRIAN D , DYE CHRISTOPHER M , SCHWARZ FREDERICK M , SUCIU GABRIEL L , JOHNSON STEVEN B
Abstract: motor de turbina a gás. é descrito um motor de turbina a gás que inclui um eixo do conjunto compressor-turbina ao longo de um eixo geométrico da linha central do motor que aciona um trem de engrenagem, o dito eixo do conjunto compressor-turbina inclui um compressor de baixa pressão com quatro a oito (4-8) estágios
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公开(公告)号：EP2776318A4
公开(公告)日：2014-11-26
申请号：EP12863186
申请日：2012-12-31
Applicant: UNITED TECHNOLOGIES CORP
Inventor： SUCIU GABRIEL L , MERRY BRIAN D , DYE CHRISTOPHER M , JOHNSON STEVEN B , SCHWARZ FREDERICK M
CPC classification number: B64D27/26 , B64D2027/264 , B64D2027/266 , F01D25/162 , F02C3/107 , F02C7/20 , F02K3/06 , F02K3/075 , F05D2260/4031 , F05D2260/40311
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公开(公告)号：CA2849013C
公开(公告)日：2014-11-18
申请号：CA2849013
申请日：2012-12-31
Applicant: UNITED TECHNOLOGIES CORP
Inventor： SUCIU GABRIEL L , MERRY BRIAN D , DYE CHRISTOPHER M , JOHNSON STEVEN B , SCHWARZ FREDERICK M
Abstract: A gas turbine engine according to an exemplary aspect of the present disclosure includes a gear train defined along an engine centeriine axis, and a spool along said engine centeriine axis which drives the gear train, the spool includes a low stage count low pressure turbine. In a further non-limiting embodiment of any of the foregoing gas turbine engine embodiments, the low stage count may include three to six (3-6) stages. Additionally or alternatively, the low stage count may include three (3) stages. Additionally or alternatively, the low stage count may include five (5) or six (6) stages.
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公开(公告)号：DE69518494T2
公开(公告)日：2001-01-04
申请号：DE69518494
申请日：1995-11-29
Applicant: UNITED TECHNOLOGIES CORP
Inventor： JOHNSON STEVEN B , BERGER CURTIS W , GARRIDO MIGUEL A , HOOP WILLIAM G
Abstract: A seal (20) for a gas turbine engine exhaust nozzle comprises a body (26), a spine member (28) attached to one side of the body, and a plurality of face segments (30) attached to the side of the body opposite that to which the spine member is attached. The body (26) includes a length and a width, with a plurality of corrugations (36) being formed in the body extending across the width. First and a second channels (38,40) are formed on respective sides of the body width to receive the ends of the face segments freely so that they may translate within the channels.
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