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公开(公告)号：WO2014197042A3
公开(公告)日：2015-03-05
申请号：PCT/US2014023206
申请日：2014-03-11
Applicant: UNITED TECHNOLOGIES CORP
Inventor： EARL JONATHAN J , RICHARDSON CARL S
CPC classification number: F01D9/04 , F01D9/041 , F01D11/005 , F01D25/246 , F05D2230/51 , F05D2240/12 , F05D2240/129 , F05D2240/57 , F05D2250/314 , Y02T50/671
Abstract: One exemplary embodiment of this disclosure relates to a stator segment. The stator segment includes a first circumferential end face, and a second circumferential end face. Further, the first and second circumferential end faces are misaligned relative to one another.
Abstract translation: 本公开的一个示例性实施例涉及定子段。 定子部分包括第一周向端面和第二圆周端面。 此外，第一和第二圆周端面相对于彼此不对准。
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公开(公告)号：WO2015112306A3
公开(公告)日：2015-09-17
申请号：PCT/US2014072434
申请日：2014-12-26
Applicant: UNITED TECHNOLOGIES CORP
Inventor： HAYFORD RICHARD K , ROGERS MARK J , CARMAN KENNETH E , RICHARDSON CARL S , EARL JONATHAN J
CPC classification number: F04D29/542 , F01D9/042 , F04D29/023 , F04D29/522 , F04D29/644 , F05B2220/302 , F05B2240/124 , F05B2280/10743 , F05B2280/50032 , F05D2220/3219 , F05D2230/642 , F05D2240/129 , F05D2300/177 , F05D2300/50212
Abstract: A gas turbine engine includes a circumferential array of vanes slidably supported in an inner case shroud segment. Multiple segments are secured to one another to provide an annular engine static structure section. The inner case shroud segment and the vanes have different material properties than one another.
Abstract translation: 燃气涡轮发动机包括可滑动地支撑在内壳罩段中的周向叶片阵列。 多个部分彼此固定以提供环形发动机静态结构部分。 内壳罩段和叶片具有彼此不同的材料特性。
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公开(公告)号：WO2015076910A3
公开(公告)日：2015-08-06
申请号：PCT/US2014054740
申请日：2014-09-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ROGERS MARK J , RICHARDSON CARL S , HAYFORD RICHARD K , CARMEN KENNETH E , EARL JONATHAN
CPC classification number: F01D11/005 , F01D9/041 , F01D11/001 , F01D11/08 , F01D25/04 , F05D2220/32 , F05D2260/52
Abstract: A vane seal system includes a first non-rotatable vane segment that has a first airfoil with a first pocket at one end thereof. A second non-rotatable vane segment includes a second airfoil with a second pocket at one end thereof spaced by a gap from the first pocket. A seal member spans across the gap and extends in the first pocket and the second pocket. The seal member includes a seal element and at least one spring portion configured to positively locate the seal member in a sealing direction. Also disclosed is a seal for a vane seal system and a method related thereto for damping relative movement between a first pocket and a second pocket.
Abstract translation: 叶片密封系统包括具有在其一端具有第一凹部的第一翼型件的第一不可旋转叶片段。 第二不可旋转的叶片段包括第二翼型件，在其一端具有与第一凹部间隔开的第二凹部。 密封件横跨该间隙并在第一袋和第二袋中延伸。 密封构件包括密封元件和至少一个弹簧部分，其构造成将密封构件主动地定位在密封方向上。 还公开了一种用于叶片密封系统的密封件及其相关方法，用于阻止第一袋和第二袋之间的相对运动。
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公开(公告)号：WO2014197044A3
公开(公告)日：2015-03-05
申请号：PCT/US2014023470
申请日：2014-03-11
Applicant: UNITED TECHNOLOGIES CORP
Inventor： RICHARDSON CARL S , SZYMBOR JOHN A
CPC classification number: F01D9/041 , B23C3/16 , B23C3/18 , B23C2215/04 , B23C2215/045 , B23C2215/44 , B23C2260/68 , B23C2270/08 , B23Q3/06 , B23Q3/062 , B23Q3/063 , B25B11/02 , F01D25/246 , F05D2230/10 , F05D2230/14 , F05D2240/12 , F05D2300/501 , Y02T50/66 , Y02T50/672 , Y10T29/49316 , Y10T29/4932 , Y10T29/49336 , Y10T409/303752 , Y10T409/303808 , Y10T409/30868 , Y10T409/309016
Abstract: A vane tip machining fixture assembly includes a first clamp ring mountable to a fixture, the first clamp ring includes a rigid back ring mounted to a resilient ring.
Abstract translation: 叶片尖端加工夹具组件包括可安装到夹具的第一夹环，第一夹环包括安装到弹性环的刚性后环。
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公开(公告)号：DE60032843D1
公开(公告)日：2007-02-22
申请号：DE60032843
申请日：2000-08-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MCMAHON MICHAEL E , RICHARDSON CARL S , WATSON CHARLES R , TREMBLAY DENNIS R , LESHANE JEFFERY S
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Patent Agency Ranking
公开(公告)号：DE60032843T2
公开(公告)日：2007-06-21
申请号：DE60032843
申请日：2000-08-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： MCMAHON MICHAEL E , RICHARDSON CARL S , WATSON CHARLES R , TREMBLAY DENNIS R , LESHANE JEFFERY S
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公开(公告)号：EP3052766A4
公开(公告)日：2017-08-09
申请号：EP14864145
申请日：2014-09-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ROGERS MARK J , RICHARDSON CARL S , HAYFORD RICHARD K , CARMEN KENNETH E , EARL JONATHAN
CPC classification number: F01D11/005 , F01D9/041 , F01D11/001 , F01D11/08 , F01D25/04 , F05D2220/32 , F05D2260/52
Abstract: A vane seal system includes a first non-rotatable vane segment that has a first airfoil with a first pocket at one end thereof. A second non-rotatable vane segment includes a second airfoil with a second pocket at one end thereof spaced by a gap from the first pocket. A seal member spans across the gap and extends in the first pocket and the second pocket. The seal member includes a seal element and at least one spring portion configured to positively locate the seal member in a sealing direction. Also disclosed is a seal for a vane seal system and a method related thereto for damping relative movement between a first pocket and a second pocket.
Abstract translation: 叶片密封系统包括第一不可旋转的叶片段，该第一不可旋转叶片段具有第一翼型，其一端具有第一凹穴。 第二不可旋转叶片段包括第二翼型件，该第二翼型件在其一端具有与第一凹口间隔开间隙的第二凹口。 密封构件跨越间隙并延伸在第一袋和第二袋中。 密封构件包括密封元件和构造成将密封构件沿密封方向可靠地定位的至少一个弹簧部分。 还公开了一种用于叶片密封系统的密封件及其相关方法，用于阻尼第一袋和第二袋之间的相对运动。
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公开(公告)号：EP3052765A4
公开(公告)日：2017-11-22
申请号：EP14850123
申请日：2014-09-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor： ROGERS MARK J , RICHARDSON CARL S , HAYFORD RICHARD K , CARMAN KENNETH E , EARL JONATHAN J
CPC classification number: F01D11/001 , F01D9/041 , F05D2260/38
Abstract: A vane seal system includes a non-rotatable vane segment that has an airfoil with a pocket at one end thereof. The pocket spans in an axial direction between forward and trailing sides, with respect to the airfoil, and in a lateral direction between open lateral sides. A seal member extends in the pocket. The seal member includes a seal element and at least one spring portion that is configured to positively locate the seal member in the axial direction in the pocket. A method for positioning the seal member in a vane seal system includes positively locating the seal member in the axial direction in the pocket using the spring portion.
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9.发明公开GAS TURBINE ENGINE INNER CASE WITH NON-INTEGRAL VANES 审中-公开INNENGEHÄUSEEINES GASTURBINENMOTORS MIT NICHT-INTEGRIERTEN SCHAUFELN
公开(公告)号：EP3097270A4
公开(公告)日：2017-09-13
申请号：EP14879918
申请日：2014-12-26
Applicant: UNITED TECHNOLOGIES CORP
Inventor： HAYFORD RICHARD K , ROGERS MARK J , CARMAN KENNETH E , RICHARDSON CARL S , EARL JONATHAN J
CPC classification number: F04D29/542 , F01D9/042 , F04D29/023 , F04D29/522 , F04D29/644 , F05B2220/302 , F05B2240/124 , F05B2280/10743 , F05B2280/50032 , F05D2220/3219 , F05D2230/642 , F05D2240/129 , F05D2300/177 , F05D2300/50212
Abstract: A gas turbine engine includes a circumferential array of vanes slidably supported in an inner case shroud segment. Multiple segments are secured to one another to provide an annular engine static structure section. The inner case shroud segment and the vanes have different material properties than one another.
Abstract translation: 燃气涡轮发动机包括可滑动地支撑在内壳罩段中的周向叶片阵列。 多个部分彼此固定以提供环形发动机静态结构部分。 内壳罩段和叶片具有彼此不同的材料特性。
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公开(公告)号：EP2971571A4
公开(公告)日：2016-11-16
申请号：EP14807620
申请日：2014-03-11
Applicant: UNITED TECHNOLOGIES CORP
Inventor： EARL JONATHAN J , RICHARDSON CARL S
CPC classification number: F01D9/04 , F01D9/041 , F01D11/005 , F01D25/246 , F05D2230/51 , F05D2240/12 , F05D2240/129 , F05D2240/57 , F05D2250/314 , Y02T50/671
Abstract: One exemplary embodiment of this disclosure relates to a stator segment. The stator segment includes a first circumferential end face, and a second circumferential end face. Further, the first and second circumferential end faces are misaligned relative to one another.
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