公开(公告)号：EP1435440A1

公开(公告)日：2004-07-07

申请号：EP03258149.8

申请日：2003-12-24

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Sammann, Bradley C. ,  Twelves, Wendell V. ,  Klein, Harvey L. ,  Jones, James E. ,  Jones, Gary D. ,  Norris, James W. ,  Kramer, Stephen K. ,  Thonebe, Douglas A.

IPC: F02C5/12 ,  F02K3/075 ,  F02K7/02 ,  F02K7/075

CPC classification number: F02C3/165 ,  F02C3/16 ,  F02C5/02 ,  F02C5/04 ,  F02C5/11 ,  F02K3/06 ,  F02K7/02 ,  F02K7/075

Abstract: A pulsed combustion device includes a support structure (25) and a combustor carousel (52) supported by the support structure (25) and rotating relative thereto about an axis (500). The carousel (52) has a number of combustion conduits (50) in a circumferential array. Each conduit (50) cyclically receives a charge and discharges combustion products of the charge.

Abstract translation: 脉冲燃烧装置包括支撑结构（25）和由支撑结构（25）支撑并相对于其围绕轴线（500）旋转的燃烧器转盘（52）。 圆盘传送带（52）具有周向排列的多个燃烧管道（50）。 每个导管（50）循环地接收电荷并排出电荷的燃烧产物。

公开(公告)号：EP1435440B1

公开(公告)日：2006-07-19

申请号：EP03258149.8

申请日：2003-12-24

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Sammann, Bradley C. ,  Twelves, Wendell V. ,  Klein, Harvey L. ,  Jones, James E. ,  Jones, Gary D. ,  Norris, James W. ,  Kramer, Stephen K. ,  Thonebe, Douglas A.

IPC: F02C5/12 ,  F02K3/075 ,  F02K7/02 ,  F02K7/075

CPC classification number: F02C3/165 ,  F02C3/16 ,  F02C5/02 ,  F02C5/04 ,  F02C5/11 ,  F02K3/06 ,  F02K7/02 ,  F02K7/075

公开(公告)号：EP1647673A1

公开(公告)日：2006-04-19

申请号：EP05256247.7

申请日：2005-10-06

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： Swanson, Timothy A. ,  Jones, James E.

IPC: F01D17/14

CPC classification number: F01D17/141 ,  F01D17/145 ,  F05D2250/411

Abstract: A vernier duct blocker (31) comprises a plurality of vanes (21) each having a width and comprising a forward portion (15) and an aft portion (13) defining a plurality of gas paths each of the plurality of vanes being separated by a plurality of widths. It further comprises a rotatably movable ring (11) interposed between the forward portion (15) and the aft portion (13) and comprising a plurality of openings (17) each having a width. The width (W) of one of the plurality of vanes (21) differs from the width (W 1 ) of another one of the plurality of vanes (21).

Abstract translation: 游标管道阻断器（31）包括多个叶片（21），每个叶片具有宽度并且包括限定多个气体路径的前部（15）和后部（13），所述多个叶片中的每一个由叶片 多个宽度。 它还包括置于前部（15）和后部（13）之间的可旋转移动的环（11），并包括多个开口（17），每个开口具有一个宽度。 多个叶片（21）中的一个的宽度（W）与多个叶片（21）中的另一个的宽度（W1）不同。

公开(公告)号：EP1647673B1

公开(公告)日：2009-02-25

申请号：EP05256247.7

申请日：2005-10-06

Applicant: United Technologies Corporation

Inventor： Swanson, Timothy A. ,  Jones, James E.

IPC: F01D17/14

CPC classification number: F01D17/141 ,  F01D17/145 ,  F05D2250/411

公开(公告)号：EP1862660A1

公开(公告)日：2007-12-05

申请号：EP07251290.8

申请日：2007-03-27

Applicant: United Technologies Corporation

Inventor： Jones, James E. ,  Roberge, Gary D. ,  Perkins, Marsha E. ,  Thonebe, Douglas A.

IPC: F02K3/12 ,  F02K7/075

CPC classification number: F02K7/075 ,  F02C5/02

Abstract: A turbine engine (20) has a case (22) with an axis (500). A fan (32) is mounted for rotation about the axis (500). A turbine (42) is mechanically coupled to the fan (32) to drive rotation of the fan (32) about the axis (500). A number of compressor/turbine units (38) are downstream of the fan (32) and upstream of the turbine (42) along a core flowpath (514). A number of combustors (41) are coupled to the compressor/turbine units (38) to receive air and deliver combustion gas to drive the turbine (42).

Abstract translation: 涡轮发动机（20）具有具有轴线（500）的壳体（22）。 安装风扇（32）以围绕轴线（500）旋转。 涡轮（42）机械地联接到风扇（32）以驱动风扇（32）围绕轴线（500）的旋转。 多个压缩机/涡轮机单元（38）沿着芯流道（514）在风扇（32）的下游和涡轮机（42）的上游。 多个燃烧器（41）联接到压缩机/涡轮机单元（38）以接收空气并输送燃烧气体以驱动涡轮机（42）。