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1. 发明申请

US20130004906A1 COMBUSTOR DOME WITH COMBINED DEFLECTOR/MIXER RETAINER 有权
标题翻译： COMBUSTOR DOME与组合式定位器/混合器保持器
公开(公告)号：US20130004906A1
公开(公告)日：2013-01-03
申请号：US13174027
申请日：2011-06-30
申请人： Daniel Dale Brown , Glenn Edward Wiehe , Michael Terry Bucaro , Stephen William Freund
发明人： Daniel Dale Brown , Glenn Edward Wiehe , Michael Terry Bucaro , Stephen William Freund
IPC分类号： F23D14/62 , B21D53/00
CPC分类号： F23R3/283 , F23R3/14 , F23R2900/00017 , Y02T50/675 , Y10T29/49348
摘要： A combustor dome assembly includes a dome plate with upstream and downstream faces and an aperture therein; a deflector with body and a tube section, the deflector fixedly attached to the dome plate adjacent the downstream face with the tube section in the aperture; a retainer having an annular body with a central opening therein, an annular flange, and at least one hook defining a slot, the retainer being fixedly attached to the dome plate adjacent the upstream face of the dome plate with the flange received in the aperture; and an annular mixer with a radial array of swirl vanes and an annular mounting flange, with a retention tab extending radially outward from the mounting flange. The mixer is disposed adjacent the upstream face with the mounting flange against the retainer. The retention tab is engaged in the slot to prevent axial withdrawal of the mixer from the retainer.
摘要翻译：燃烧器穹顶组件包括具有上游和下游面的圆顶板和其中的孔; 具有主体和管部分的偏转器，偏转器固定地附接到邻近下游面的圆顶板，孔中的管部分; 保持器，其具有在其中具有中心开口的环形体，环形凸缘和限定狭槽的至少一个钩，所述保持器固定地附接到邻近圆顶板的上游面的圆顶板，凸缘容纳在孔中; 以及具有旋转叶片的径向阵列和环形安装凸缘的环形混合器，其具有从安装凸缘径向向外延伸的保持翼片。混合器邻近上游面设置有安装凸缘抵靠保持器。保持片接合在槽中以防止混合器从保持器轴向退出。

2. 发明授权

US08726669B2 Combustor dome with combined deflector/mixer retainer 有权
标题翻译：具有组合偏转器/混合器保持架的燃烧器穹顶
公开(公告)号：US08726669B2
公开(公告)日：2014-05-20
申请号：US13174027
申请日：2011-06-30
申请人： Daniel Dale Brown , Glenn Edward Wiehe , Michael Terry Bucaro , Stephen William Freund
发明人： Daniel Dale Brown , Glenn Edward Wiehe , Michael Terry Bucaro , Stephen William Freund
IPC分类号： F23R3/14
CPC分类号： F23R3/283 , F23R3/14 , F23R2900/00017 , Y02T50/675 , Y10T29/49348
摘要： A combustor dome assembly includes a dome plate with upstream and downstream faces and an aperture therein; a deflector with body and a tube section, the deflector fixedly attached to the dome plate adjacent the downstream face with the tube section in the aperture; a retainer having an annular body with a central opening therein, an annular flange, and at least one hook defining a slot, the retainer being fixedly attached to the dome plate adjacent the upstream face of the dome plate with the flange received in the aperture; and an annular mixer with a radial array of swirl vanes and an annular mounting flange, with a retention tab extending radially outward from the mounting flange. The mixer is disposed adjacent the upstream face with the mounting flange against the retainer. The retention tab is engaged in the slot to prevent axial withdrawal of the mixer from the retainer.
摘要翻译：燃烧器穹顶组件包括具有上游和下游面的圆顶板和其中的孔; 具有主体和管部分的偏转器，偏转器固定地附接到邻近下游面的圆顶板，孔中的管部分; 保持器，其具有在其中具有中心开口的环形体，环形凸缘和限定狭槽的至少一个钩，所述保持器固定地附接到邻近圆顶板的上游面的圆顶板，凸缘容纳在孔中; 以及具有旋转叶片的径向阵列和环形安装凸缘的环形混合器，其具有从安装凸缘径向向外延伸的保持翼片。混合器邻近上游面设置有安装凸缘抵靠保持器。保持片接合在槽中以防止混合器从保持器轴向退出。

3. 发明授权

US08893382B2 Combustion system and method of assembling the same 有权
标题翻译：燃烧系统及其组装方法
公开(公告)号：US08893382B2
公开(公告)日：2014-11-25
申请号：US13249868
申请日：2011-09-30
申请人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe , Donald Scott Yeager , Mark Willard Marusko , Michael Joseph Zerbe
发明人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe , Donald Scott Yeager , Mark Willard Marusko , Michael Joseph Zerbe
IPC分类号： B23P17/00 , F23R3/50 , F23R3/00 , F23R3/60
CPC分类号： F23R3/50 , F23R3/002 , F23R3/60 , Y02E20/16 , Y10T29/49229 , Y10T29/4932
摘要： A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.
摘要翻译：一种组装燃气涡轮发动机的燃烧系统的方法包括提供燃烧室框架，内壳结构和外壳结构。该方法还包括将燃烧室框架安装在内壳结构和外壳结构之间，使得燃烧室框架联接到内壳结构和外壳结构。

4. 发明申请

US20130081270A1 COMBUSTION SYSTEM AND METHOD OF ASSEMBLING THE SAME 有权
标题翻译：燃烧系统及其组装方法
公开(公告)号：US20130081270A1
公开(公告)日：2013-04-04
申请号：US13249868
申请日：2011-09-30
申请人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe
发明人： David Bruce Patterson , Donald Michael Corsmeier , Craig Douglas Young , Donald Lee Gardner , James Edward Thompson , Daniel Dale Brown , Glenn Edward Wiehe
IPC分类号： B23P17/00 , F02C3/14
CPC分类号： F23R3/50 , F23R3/002 , F23R3/60 , Y02E20/16 , Y10T29/49229 , Y10T29/4932
摘要： A method of assembling a combustion system for a gas turbine engine includes providing a combustion chamber frame, an inner casing structure, and an outer casing structure. The method also includes mounting the combustion chamber frame between the inner casing structure and the outer casing structure such that the combustion chamber frame is coupled to the inner casing structure and the outer casing structure.
摘要翻译：一种组装燃气涡轮发动机的燃烧系统的方法包括提供燃烧室框架，内壳结构和外壳结构。该方法还包括将燃烧室框架安装在内壳结构和外壳结构之间，使得燃烧室框架联接到内壳结构和外壳结构。

5. 发明授权

US07596949B2 Method and apparatus for heat shielding gas turbine engines 有权
标题翻译：燃气涡轮发动机的保温方法和装置
公开(公告)号：US07596949B2
公开(公告)日：2009-10-06
申请号：US11360205
申请日：2006-02-23
申请人： Shaun Michael DeVane , Erika Suzanne Show , Glenn Edward Wiehe , Timothy Glen Umbaugh , James Neil Cooper , Mateusz Pawel Wenclik , Marek Krzysztof Krol
发明人： Shaun Michael DeVane , Erika Suzanne Show , Glenn Edward Wiehe , Timothy Glen Umbaugh , James Neil Cooper , Mateusz Pawel Wenclik , Marek Krzysztof Krol
IPC分类号： F02C7/00
CPC分类号： F23R3/002 , F23R3/14 , F23R3/283 , F23R3/286 , F23R2900/00005 , F23R2900/00017 , F23R2900/03044
摘要： A method for fabricating a gas turbine engine combustor that includes a domeplate and at least one fuel injector extending through an opening in the domeplate. The method includes fabricating a heatshield that includes a threaded collar extending upstream from the heatshield, positioning the heatshield on a downstream side of the domeplate such that the threaded collar is received within the domeplate opening, and coupling a retainer to the collar on an upstream side of the domeplate such that the domeplate is securely coupled between the heat shield and the retainer.
摘要翻译：一种用于制造燃气涡轮发动机燃烧室的方法，该燃气涡轮发动机燃烧器包括一个三脚架和至少一个燃料喷射器，该燃料喷射器延伸穿过该多孔板中的一个开口。该方法包括制造遮光罩，该遮光罩包括从挡风玻璃上游延伸的螺纹轴环，将遮光板定位在该多孔板的下游侧，使得螺纹轴环容纳在该多孔板开口内，并且将保持器连接到上游侧的轴环以使得三脚架牢固地联接在隔热罩和保持器之间。

6. 发明授权

US07062920B2 Combustor dome assembly of a gas turbine engine having a free floating swirler 有权
标题翻译：具有自由浮动旋流器的燃气涡轮发动机的燃烧器顶盖组件
公开(公告)号：US07062920B2
公开(公告)日：2006-06-20
申请号：US10638597
申请日：2003-08-11
申请人： Marie Ann McMasters , James Edward Thompson , Gregory Allen Cimmarusti , James Neil Cooper , Glenn Edward Wiehe
发明人： Marie Ann McMasters , James Edward Thompson , Gregory Allen Cimmarusti , James Neil Cooper , Glenn Edward Wiehe
IPC分类号： F23R3/60
CPC分类号： F23R3/14 , F23D2211/00 , F23R3/10 , F23R3/60
摘要： A combustor dome assembly for a gas turbine engine having a longitudinal centerline axis extending therethrough, including: an annular dome plate having an inner portion, an outer portion, a forward surface and a plurality of circumferentially spaced openings formed therein, wherein a radial section is defined between adjacent openings; an annular outer cowl connected to the outer portion of the dome plate; an annular inner cowl connected to the inner portion of the dome plate; and, a swirler located between the forward surface of the dome plate and the inner and outer cowls in substantial alignment with each of the openings in the dome plate. Each swirler further includes a forward portion and an aft portion and is retained by at least one tab member located upstream thereof so as to be movable in a radial and axial direction.
摘要翻译：一种用于燃气涡轮发动机的燃烧器圆顶组件，其具有延伸穿过其中的纵向中心线轴线，包括：环形圆顶板，其具有形成在其中的内部部分，外部部分，前表面和多个周向间隔开的开口，限定在相邻的开口之间; 连接到圆顶板的外部的环形外罩; 连接到圆顶板的内部的环形内罩; 以及位于圆顶板的前表面和内外罩之间的旋流器，其与圆顶板中的每个开口基本对准。每个旋流器还包括前部和后部，并且由位于其上游的至少一个突片构件保持以便在径向和轴向方向上可移动。

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