公开(公告)号：US20050034459A1

公开(公告)日：2005-02-17

申请号：US10638506

申请日：2003-08-11

申请人： Marie McMasters ,  James Cooper ,  Michael Vermeersch ,  Duane Thomsen ,  Allen Danis ,  Gregory Cimmarusti

发明人： Marie McMasters ,  James Cooper ,  Michael Vermeersch ,  Duane Thomsen ,  Allen Danis ,  Gregory Cimmarusti

IPC分类号： F23R3/14 ,  F23R3/00 ,  F23R3/08 ,  F23R3/10 ,  F23R3/50 ,  F23R3/42

CPC分类号： F23R3/002 ,  F23R3/10 ,  F23R3/50

摘要： A combustor dome assembly for a gas turbine engine having a longitudinal centerline axis extending therethrough includes: 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 defined between each of the openings includes a cooling trough formed therein; and, a free floating swirler located upstream of the dome plate in substantial alignment with each of the openings in the dome plate, the swirler including a forward portion and an aft portion. The aft portion of each swirler is configured so as to permit air flow to the cooling trough during operation of the gas turbine engine. In particular, the swirler aft portion includes a substantially annular flange extending adjacent to the forward surface of the dome plate, wherein opposing portions of a circumference for the flange adjacent the radial sections of the dome plate are substantially linear.

公开(公告)号：US20050034460A1

公开(公告)日：2005-02-17

申请号：US10638597

申请日：2003-08-11

申请人： Marie McMasters ,  James Thompson ,  Gregory Cimmarusti ,  James Cooper ,  Glenn Wiehe

发明人： Marie McMasters ,  James Thompson ,  Gregory Cimmarusti ,  James Cooper ,  Glenn Wiehe

IPC分类号： F23R3/14 ,  F23R3/42 ,  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。