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公开(公告)号：US20090085305A1
公开(公告)日：2009-04-02
申请号：US11863729
申请日：2007-09-28
Applicant: Mehmet Demiroglu , Christopher E. Wolfe , Patrick B. Melton , Edip Sevincer
Inventor： Mehmet Demiroglu , Christopher E. Wolfe , Patrick B. Melton , Edip Sevincer
IPC: F16J15/02
CPC classification number: F16J15/0887
Abstract: An apparatus for sealing gas path leakage within a turbomachine is provided. The apparatus may include at least one seal system, which may include at least one sealing shim, at least one spring; and at least one shim protection material. The seal system may be inserted between a first and a second structure of the turbomachine. The seal system may adjust for misalignments between the first and the second structures of the turbomachine.
Abstract translation: 提供一种用于密封涡轮机内的气体通道泄漏的装置。 该装置可以包括至少一个密封系统，其可以包括至少一个密封垫片，至少一个弹簧; 和至少一个垫片保护材料。 密封系统可以插入在涡轮机的第一和第二结构之间。 密封系统可以调节涡轮机的第一和第二结构之间的不对准。
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公开(公告)号：US07827797B2
公开(公告)日：2010-11-09
申请号：US11469952
申请日：2006-09-05
Applicant: Fei Han , Venkatraman Ananthakrishman Iyer , Keith Robert McManus , Edip Sevincer
Inventor： Fei Han , Venkatraman Ananthakrishman Iyer , Keith Robert McManus , Edip Sevincer
IPC: F02C1/00
CPC classification number: F23R3/286 , F23R2900/00014 , F23R2900/03041
Abstract: An injection assembly for use with a combustor is provided. The injection assembly includes an effusion plate that has a plurality of plate openings and a plate sleeve having a sidewall portion that includes a forward edge. The forward edge is coupled to the effusion plate such that the effusion plate is oriented obliquely with respect to a centerline extending through the combustor. The injection assembly also includes a plurality of ring extensions where each of the ring extensions is coupled to one of the plurality of plate openings. Each ring extension extends rearwardly into the plate sleeve.
Abstract translation: 提供了一种与燃烧器一起使用的注射组件。 注射组件包括具有多个板开口的排出板和具有包括前边缘的侧壁部分的板套筒。 前缘连接到渗出板，使得渗出板相对于延伸穿过燃烧器的中心线倾斜地定向。 注射组件还包括多个环延伸部，其中每个环延伸部联接到多个板开口中的一个。 每个环形延伸部向后延伸到板套筒中。
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公开(公告)号：US20100143101A1
公开(公告)日：2010-06-10
申请号：US12329224
申请日：2008-12-05
Applicant: Biao Fang , Christopher Edward Wolfe , Edip Sevincer
Inventor： Biao Fang , Christopher Edward Wolfe , Edip Sevincer
CPC classification number: F16J15/445 , F16J15/3224
Abstract: A compliant foil seal comprises a bottom foil configured to be located circumferentially around at least a portion of a rotor, and one or more upper foils configured to cooperate with a stator to position the bottom foil to compliantly face the rotor and be located between the stator and the rotor. A compliant foil seal assembly and a rotary machine are also presented.
Abstract translation: 柔性箔密封件包括被配置为围绕转子的至少一部分周向定位的底部箔片，以及一个或多个上部箔片，其构造成与定子配合以将底部箔片顺从地面对转子并且位于定子 和转子。 还提供了柔性箔密封组件和旋转机器。
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公开(公告)号：US07125223B2
公开(公告)日：2006-10-24
申请号：US10675364
申请日：2003-09-30
Applicant: Norman Arnold Turnquist , Hamid Reza Sarshar , Biao Fang , Mehmet Demiroglu , Bernard Arthur Couture , Clement Gazzillo , Edip Sevincer
Inventor： Norman Arnold Turnquist , Hamid Reza Sarshar , Biao Fang , Mehmet Demiroglu , Bernard Arthur Couture , Clement Gazzillo , Edip Sevincer
CPC classification number: F01D11/20 , F01D11/22 , F05D2250/42
Abstract: An apparatus for providing active clearance control between blade tips and seals in a turbomachine comprising: a first stator carrier segment, with stator seals centripetally disposed on it; a second stator carrier segment located along a same circumference as the first stator carrier segment, also with stator seals centripetally disposed on it; a shell that adjustably houses the first stator carrier segment and the second carrier segment; at least one displacement apparatus in operable communication with at least one stator carrier segment and configured to position the at least one stator carrier segment to provide active clearance control to the stator seals disposed on the at least one stator carrier segment.
Abstract translation: 一种用于在涡轮机中的叶片尖端和密封之间提供主动间隙控制的装置，包括：第一定子承载段，定子密封件向心地设置在其上; 沿与第一定子承载段相同的圆周定位的第二定子载体段，其中定子密封件向心地设置在其上; 壳体，其可调节地容纳所述第一定子承载段和所述第二载体段; 至少一个位移设备，其与至少一个定子承载段可操作地连通并且被配置为定位所述至少一个定子承载段，以对设置在所述至少一个定子承载段上的所述定子密封件提供主动间隙控制。
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公开(公告)号：US20120119449A1
公开(公告)日：2012-05-17
申请号：US12943978
申请日：2010-11-11
Applicant: Mehmet Demiroglu , Neelesh Nandkumar Sarawate , Edip Sevincer , Benjamin Lacy
Inventor： Mehmet Demiroglu , Neelesh Nandkumar Sarawate , Edip Sevincer , Benjamin Lacy
IPC: F16J15/02
CPC classification number: F01D9/023 , F01D11/005 , F16J15/3288
Abstract: The present application provides a sealing assembly for use with a transition piece and a stage one nozzle of a gas turbine engine. The sealing assembly may include a seal element, an overlay piece positioned on the seal element, and a side seal positioned on the overlay piece.
Abstract translation: 本申请提供了一种用于燃气涡轮发动机的过渡件和一级喷嘴的密封组件。 密封组件可以包括密封元件，定位在密封元件上的覆盖件和位于覆盖件上的侧密封件。
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Patent Agency Ranking
公开(公告)号：US20120119447A1
公开(公告)日：2012-05-17
申请号：US12943981
申请日：2010-11-11
Applicant: Mehmet Demiroglu , Kevin McMahan , Benjamin Lacy , Neelesh Nandkumar Sarawate , Edip Sevincer
Inventor： Mehmet Demiroglu , Kevin McMahan , Benjamin Lacy , Neelesh Nandkumar Sarawate , Edip Sevincer
IPC: F16J15/02
CPC classification number: F01D9/023 , F01D11/003 , F05D2250/75
Abstract: The present application provides a seating assembly for use with a transition piece and a stage one nozzle of a gas turbine engine. The seating assembly may include a support member positioned between the transition piece and the stage one nozzle and a primary spring element positioned on the support member and in contact with the stage one nozzle. The primary spring element may include a single bend therein.
Abstract translation: 本申请提供了一种用于燃气涡轮发动机的过渡件和一级喷嘴的就座组件。 座椅组件可以包括定位在过渡片和舞台一个喷嘴之间的支撑构件和定位在支撑构件上并与舞台一个喷嘴接触的主弹簧元件。 主弹簧元件可以在其中包括单个弯曲部。
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公开(公告)号：US20060228208A1
公开(公告)日：2006-10-12
申请号：US11305905
申请日：2005-12-19
Applicant: Richard Trewin , Jason Mortzheim , Edip Sevincer , Kevin Kirtley , Roointon Pavri , Xiaoyue Liu
Inventor： Richard Trewin , Jason Mortzheim , Edip Sevincer , Kevin Kirtley , Roointon Pavri , Xiaoyue Liu
IPC: F01D5/14
CPC classification number: F01D25/14 , F01D9/065 , F02C7/1435 , F04D29/5846
Abstract: An apparatus for distributing a fluid in a gas flow path inside a turbomachine, comprising: a device for introducing the fluid into the gas flow path; and wherein the device is positioned within the gas flow path. A method for installing an apparatus that will distribute a fluid in a gas flow path inside a turbomachine, the method comprising: machining a casing groove along an inner surface of a casing; machining at least one port into the casing that is in fluid communication with the casing groove; machining an internal cavity in at least one stator blade that is in fluid communication with the casing groove; machining at least one orifice, that is in fluid communication with the internal cavity, on an orifice surface of the stator blade; and coupling a fluid supply to the at least one port.
Abstract translation: 一种用于在涡轮机内的气体流路中分配流体的装置，包括：用于将流体引入气体流路的装置; 并且其中所述装置位于所述气体流动路径内。 一种用于安装在涡轮机内部的气体流路中分配流体的装置的方法，所述方法包括：沿壳体的内表面加工套管槽; 将至少一个端口加工到与壳体槽流体连通的壳体中; 在至少一个与所述壳体沟槽流体连通的定子叶片中加工内腔; 在定子叶片的孔表面上加工至少一个与内腔流体连通的孔口; 以及将流体供应联接到所述至少一个端口。
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公开(公告)号：US20050100438A1
公开(公告)日：2005-05-12
申请号：US10605959
申请日：2003-11-10
Applicant: Richard Trewin , Jason Mortzheim , Edip Sevincer , Kevin Kirtley , Roointon Pavri , Xiaoyue Liu
Inventor： Richard Trewin , Jason Mortzheim , Edip Sevincer , Kevin Kirtley , Roointon Pavri , Xiaoyue Liu
CPC classification number: F01D25/14 , F01D9/065 , F02C7/1435 , F04D29/5846
Abstract: An apparatus for distributing a fluid in a gas flow path inside a turbomachine, comprising: a device for introducing the fluid into the gas flow path; and wherein the device is positioned within the gas flow path. A method for installing an apparatus that will distribute a fluid in a gas flow path inside a turbomachine, the method comprising: machining a casing groove along an inner surface of a casing; machining at least one port into the casing that is in fluid communication with the casing groove; machining an internal cavity in at least one stator blade that is in fluid communication with the casing groove; machining at least one orifice, that is in fluid communication with the internal cavity, on an orifice surface of the stator blade; and coupling a fluid supply to the at least one port.
Abstract translation: 一种用于在涡轮机内的气体流路中分配流体的装置，包括：用于将流体引入气体流路的装置; 并且其中所述装置位于所述气体流动路径内。 一种用于安装在涡轮机内部的气体流路中分配流体的装置的方法，所述方法包括：沿壳体的内表面加工套管槽; 将至少一个端口加工到与壳体槽流体连通的壳体中; 在至少一个与所述壳体沟槽流体连通的定子叶片中加工内腔; 在定子叶片的孔表面上加工至少一个与内腔流体连通的孔口; 以及将流体供应联接到所述至少一个端口。
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公开(公告)号：US20050069406A1
公开(公告)日：2005-03-31
申请号：US10675364
申请日：2003-09-30
Applicant: Norman Turnquist , Hamid Sarshar , Biao Fang , Mehmet Demiroglu , Bernard Couture , Clement Gazzillo , Edip Sevincer
Inventor： Norman Turnquist , Hamid Sarshar , Biao Fang , Mehmet Demiroglu , Bernard Couture , Clement Gazzillo , Edip Sevincer
CPC classification number: F01D11/20 , F01D11/22 , F05D2250/42
Abstract: An apparatus for providing active clearance control between blade tips and seals in a turbomachine comprising: a first stator carrier segment, with stator seals centripetally disposed on it; a second stator carrier segment located along a same circumference as the first stator carrier segment, also with stator seals centripetally disposed on it; a shell that adjustably houses the first stator carrier segment and the second carrier segment; at least one displacement apparatus in operable communication with at least one stator carrier segment and configured to position the at least one stator carrier segment to provide active clearance control to the stator seals disposed on the at least one stator carrier segment.
Abstract translation: 一种用于在涡轮机中的叶片尖端和密封之间提供主动间隙控制的装置，包括：第一定子承载段，定子密封件向心地设置在其上; 沿与第一定子承载段相同的圆周定位的第二定子载体段，其中定子密封件向心地设置在其上; 壳体，其可调节地容纳所述第一定子承载段和所述第二载体段; 至少一个位移设备，其与至少一个定子承载段可操作地连通并且被配置为定位所述至少一个定子承载段，以对设置在所述至少一个定子承载段上的所述定子密封件提供主动间隙控制。
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公开(公告)号：US20090104028A1
公开(公告)日：2009-04-23
申请号：US12119541
申请日：2008-05-13
Applicant: Richard Robert Trewin , Jason Paul Mortzheim , Edip Sevincer , Kevin Richard Kirtley , Roointon Erach Pavri , Xiaoyue Liu
Inventor： Richard Robert Trewin , Jason Paul Mortzheim , Edip Sevincer , Kevin Richard Kirtley , Roointon Erach Pavri , Xiaoyue Liu
CPC classification number: F01D25/14 , F01D9/065 , F02C7/1435 , F04D29/5846
Abstract: An apparatus for distributing a fluid in a gas flow path inside a turbomachine, comprising: a device for introducing the fluid into the gas flow path; and wherein the device is positioned within the gas flow path. A method for installing an apparatus that will distribute a fluid in a gas flow path inside a turbomachine, the method comprising: machining a casing groove along an inner surface of a casing; machining at least one port into the casing that is in fluid communication with the casing groove; machining an internal cavity in at least one stator blade that is in fluid communication with the casing groove; machining at least one orifice, that is in fluid communication with the internal cavity, on an orifice surface of the stator blade; and coupling a fluid supply to the at least one port.
Abstract translation: 一种用于在涡轮机内部的气体流路中分配流体的装置，包括：用于将流体引入气体流路的装置; 并且其中所述装置位于所述气体流动路径内。 一种用于安装将流体分配在涡轮机内部的气体流路中的装置的方法，所述方法包括：沿壳体的内表面加工套管槽; 将至少一个端口加工到与壳体槽流体连通的壳体中; 在至少一个与所述壳体沟槽流体连通的定子叶片中加工内腔; 在定子叶片的孔表面上加工至少一个与内腔流体连通的孔口; 以及将流体供应联接到所述至少一个端口。
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