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公开(公告)号：WO2015112306A2
公开(公告)日：2015-07-30
申请号：PCT/US2014/072434
申请日：2014-12-26
Applicant: UNITED TECHNOLOGIES CORPORATION
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体护罩段中的周向阵列的叶片。 多个段彼此固定以提供环形发动机静态结构部分。 内壳护罩段和叶片具有彼此不同的材料性质。
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公开(公告)号：WO2015050624A2
公开(公告)日：2015-04-09
申请号：PCT/US2014/046935
申请日：2014-07-17
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： RYAN, Kevin J. , MENTZ, Karl A. , ROGERS, Mark J.
CPC classification number: F01D11/005 , F01D9/041 , F01D11/003 , F01D11/08 , F04D29/083 , F05D2220/32 , F05D2230/60 , F05D2240/11 , F05D2240/24 , F05D2250/232 , F05D2260/98 , F05D2300/17 , F05D2300/611 , F16J15/0887 , F16J15/28
Abstract: A seal assembly arrangement for a gas turbine engine includes first and second non-rotating structures respectively that provide first and second faces. A sealing assembly includes first and second sealing rings respectively that engage the first and second faces. The first and second sealing rings slideably engage one another at a sliding wedge interface.
Abstract translation: 用于燃气涡轮发动机的密封组件装置包括分别提供第一和第二面的第一和第二非旋转结构。 密封组件包括分别与第一和第二表面接合的第一和第二密封环。 第一和第二密封环在滑动楔形界面处可滑动地彼此接合。
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公开(公告)号：WO2014169120A1
公开(公告)日：2014-10-16
申请号：PCT/US2014/033649
申请日：2014-04-10
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： DAVIS, Timothy M. , ROGERS, Mark J. , BROOMER, Mark , MCGARRAH, Craig R. , ROY THILL, Carson A.
CPC classification number: F01D11/005 , F01D9/04 , F01D11/003 , F01D11/08 , F01D25/24 , F05D2220/32 , F05D2240/12 , F05D2240/55 , F05D2260/38 , F05D2300/175 , F05D2300/177 , F05D2300/20 , F05D2300/614
Abstract: A seal for sealing a radially outer component of a gas turbine engine stator to a radially inner component thereof includes an axially resilient seal carrier adapted for mounting the seal carrier and including at a radially inner portion thereof, a pair of radially spaced, axially extending, radially resilient jaws adapted to clamp a sealing element such as a rope seal there between in sealing engagement with a radially inner component of the engine stator.
Abstract translation: 用于将燃气涡轮发动机定子的径向外部部件密封到其径向内部部件的密封件包括轴向弹性的密封载体，其适于安装密封载体并且在其径向内部包括一对径向间隔开的轴向延伸的， 径向弹性夹爪，其适于将密封元件例如其间的绳索密封件与发动机定子的径向内部部件密封接合。
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公开(公告)号：WO2015076889A1
公开(公告)日：2015-05-28
申请号：PCT/US2014/052929
申请日：2014-08-27
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： DAVIS, Timothy M. , ROGERS, Mark J.
IPC: F01D11/00
CPC classification number: F01D11/005 , F01D11/00 , F01D11/003 , F01D11/006 , F01D25/24 , F02C3/04 , F05D2220/32 , F05D2240/55 , F16J15/064 , F16J15/0812 , Y02T50/672
Abstract: A sheath and seal assembly for protecting, containing and insulating a seal is provided. The seal may be installable within the sheath forming a seal-sheath assembly. The assembly may be capable of being installed in the hot section of a gas turbine. The sheath may be a woven, braided, and/or chain link structure. The sheath may be capable of allowing pressure to be conducted to a portion of the seal to load the seal against one or more portions of a housing.
Abstract translation: 提供了用于保护，容纳和绝缘密封件的护套和密封组件。 密封件可以安装在形成密封 - 护套组件的护套内。 组件可以能够安装在燃气轮机的热段中。 护套可以是织造，编织和/或链节结构。 护套可以允许压力被传导到密封件的一部分以将密封件装载到壳体的一个或多个部分上。
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Patent Agency Ranking
公开(公告)号：WO2014150353A1
公开(公告)日：2014-09-25
申请号：PCT/US2014/023017
申请日：2014-03-11
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： BROOMER, Mark , KEENE, Russell E. , DAVIS, Timothy M. , ROGERS, Mark J.
CPC classification number: F16L23/02 , F01D11/003 , F01D11/122 , F01D25/24 , F01D25/246 , F05D2230/642 , F05D2240/11 , F05D2260/38 , F16L23/16 , F16L25/0018
Abstract: A turbine shroud for incorporation in a turbine of a gas turbine engine has a plurality of butted shroud segments circumferentially arrayed to form a ring. Each of the shroud segments has an arcuate main shroud body portion, a radially inward extending annular flange attached to a first end of the main body portion, and a radially outward extending flange with a plurality of mounting apertures attached to a second end of the main shroud body portion. A first mounting aperture is sized smaller than an adjacent second mounting aperture in the radially outward extending flange.
Abstract translation: 用于结合在燃气涡轮发动机的涡轮机中的涡轮机罩具有周向排列以形成环的多个对接护罩段。 每个护罩段具有弓形主护罩主体部分，附接到主体部分的第一端的径向向内延伸的环形凸缘以及径向向外延伸的凸缘，多个安装孔附接到主体的第二端 护罩主体部分。 第一安装孔的尺寸小于径向向外延伸的凸缘中相邻的第二安装孔。
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公开(公告)号：WO2014133958A1
公开(公告)日：2014-09-04
申请号：PCT/US2014/018000
申请日：2014-02-24
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： ROGERS, Mark J. , DAVIS, Timothy M. , BROOMER, Mark , WHITE, Kevin W. , MCGARRAH, Craig , ROY THILL, Carson A.
CPC classification number: F01D11/005 , F01D25/26 , F02C7/28 , F05D2220/30 , F05D2240/11 , F05D2240/55 , F05D2260/97 , F16J15/061 , F16J15/0812
Abstract: An assembly for a turbine engine includes a turbine engine first component, a turbine engine second component and a seal assembly. The first component includes a groove and a groove surface. The second component includes a tongue that extends into the groove to a tongue surface. The seal assembly at least partially seals a gap between the groove surface and the tongue surface. The seal assembly includes a rope seal and a clip that attaches the rope seal to the tongue. The rope seal is arranged within the groove between the groove surface and the tongue surface.
Abstract translation: 涡轮发动机的组件包括涡轮发动机第一部件，涡轮发动机第二部件和密封组件。 第一部件包括凹槽和凹槽表面。 第二部件包括延伸到凹槽中的舌部到舌头表面。 密封组件至少部分地密封槽表面和舌表面之间的间隙。 密封组件包括绳索密封件和将绳索密封件附接到舌头的夹子。 绳密封件布置在槽表面和舌表面之间的槽内。
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公开(公告)号：WO2014123965A1
公开(公告)日：2014-08-14
申请号：PCT/US2014/014811
申请日：2014-02-05
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： ROGERS, Mark J. , BROOMER, Mark , MCGARRAH, Craig R. , DAVIS, Timothy M. , SWIFT, Anthony B. , KEENE, Russell E. , ROY THILL, Carson A. , DUNBAR, Timothy A.
CPC classification number: F01D11/08 , F01D25/246 , F05D2220/32 , F05D2230/60 , F05D2240/10 , F05D2240/20 , F05D2240/55 , F05D2250/14
Abstract: An interface within a gas turbine engine includes a multiple of segmented components, each with a segment flange with a multiple of apertures, at least one of the multiple of apertures a first slot aperture. A full ring component with a ring flange that defines a multiple ring of apertures, at least one of the multiple of ring apertures a second slot aperture, the second slot aperture transverse to the first slot aperture.
Abstract translation: 燃气涡轮发动机内的界面包括多个分段部件，每个部件具有多个孔的段凸缘，多个孔中的至少一个孔是第一槽孔。 具有环形凸缘的整个环形部件，其限定多个孔环，所述多个环形孔中的至少一个具有第二狭缝孔，所述第二狭缝孔横向于所述第一狭缝孔。
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公开(公告)号：WO2015088656A1
公开(公告)日：2015-06-18
申请号：PCT/US2014/062075
申请日：2014-10-24
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： LUTJEN, Paul M. , ROGERS, Mark J.
CPC classification number: F01D11/005 , F01D9/04 , F01D11/08 , F05D2220/32 , F05D2230/54 , F05D2240/11 , F05D2240/80 , F05D2250/70 , F05D2300/10 , F16J15/0887
Abstract: A seal for a gas turbine engine comprises a seal body extending from a first end to a second end. A wrap extends at least partially around the first and second ends of the seal body. A gas turbine engine is also disclosed.
Abstract translation: 用于燃气涡轮发动机的密封件包括从第一端延伸到第二端的密封体。 包装至少部分地围绕密封体的第一端和第二端延伸。 还公开了一种燃气涡轮发动机。
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9.发明申请VANE SEAL SYSTEM HAVING SPRING POSITIVELY LOCATING SEAL MEMBER IN AXIAL DIRECTION 审中-公开具有弹簧位置密封构件的VANE密封系统在轴向方向
公开(公告)号：WO2015050739A1
公开(公告)日：2015-04-09
申请号：PCT/US2014/056864
申请日：2014-09-23
Applicant: UNITED TECHNOLOGIES CORPORATION
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.
Abstract translation: 叶片密封系统包括不可旋转的叶片段，其具有在其一端具有口袋的翼型件。 口袋相对于翼型件在前后两侧之间的轴向方向上跨过敞开的侧边之间的横向方向。 密封件在口袋中延伸。 密封构件包括密封元件和至少一个弹簧部分，其构造成沿着轴向方向将密封构件正确定位在口袋中。 用于将密封构件定位在叶片密封系统中的方法包括使用弹簧部分将密封构件沿轴向方向定位在凹穴中。
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