公开(公告)号：WO2014058710A1

公开(公告)日：2014-04-17

申请号：PCT/US2013/063288

申请日：2013-10-03

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： LEVASSEUR, Glenn ,  SUCIU, Gabriel L. ,  STETSON, Gary M.

IPC: F02C9/22 ,  F01D17/16

CPC classification number: F01D17/162 ,  F02C7/36 ,  F02C9/20 ,  F05D2260/4031

Abstract: A gas turbine engine has a fan which includes a plurality of fan blades that are rotatable about an axis, and a compressor section, where the combustor section includes a first compressor and a second compressor aft of the first compressor. At least one first variable guide vane controls operation of the first compressor and at least one second variable guide vane controls operation of the second compressor. A combustor is in fluid communication with the compressor section and a turbine section is in fluid communication with the combustor. A geared architecture is driven by the turbine section for rotating the fan about the axis.

Abstract translation: 燃气涡轮发动机具有风扇，该风扇包括可围绕轴线旋转的多个风扇叶片和压缩机部分，其中燃烧器部分包括第一压缩机和第一压缩机的第二压缩机。 至少一个第一可变导向叶片控制第一压缩机的操作，并且至少一个第二可变导向叶片控制第二压缩机的操作。 燃烧器与压缩机部分流体连通，并且涡轮部分与燃烧器流体连通。 齿轮架构由涡轮部分驱动，用于围绕轴线旋转风扇。

公开(公告)号：EP2788603A1

公开(公告)日：2014-10-15

申请号：EP12787998.9

申请日：2012-10-31

Applicant: United Technologies Corporation

Inventor： NORRIS, James W. ,  KUPRATIS, Daniel B. ,  STETSON, Gary M.

IPC: F02C7/36 ,  F02C3/14 ,  F02C7/32 ,  F02K3/105

CPC classification number: F02C7/36 ,  F02C3/145 ,  F02C7/32 ,  F02K3/105 ,  F05D2220/76 ,  F05D2260/4023 ,  F05D2260/96

Abstract: A gas turbine engine has a variable overall pressure rate ("OPR."). The engine includes a high pressure compressor having at least a primary stage having a set of primary rotors and a secondary stage having a set of secondary rotors. A clutch is provided to selectively engage the secondary rotors with the primary rotors. Engagement of the clutch may be controlled based on the vehicle travel mode, such as disengaging during a takeoff mode to reduce turbine entry temperature and engaging during a loiter mode to increase OPR.

公开(公告)号：EP2788603B1

公开(公告)日：2016-04-27

申请号：EP12787998.9

申请日：2012-10-31

Applicant: United Technologies Corporation

Inventor： NORRIS, James W. ,  KUPRATIS, Daniel B. ,  STETSON, Gary M.

IPC: F02C7/36 ,  F02C3/14 ,  F02C7/32 ,  F02K3/105

CPC classification number: F02C7/36 ,  F02C3/145 ,  F02C7/32 ,  F02K3/105 ,  F05D2220/76 ,  F05D2260/4023 ,  F05D2260/96

公开(公告)号：EP2909460A1

公开(公告)日：2015-08-26

申请号：EP13845694.2

申请日：2013-10-03

Applicant: United Technologies Corporation

Inventor： LEVASSEUR, Glenn ,  SUCIU, Gabriel L. ,  STETSON, Gary M.

IPC: F02C9/22 ,  F01D17/16

CPC classification number: F01D17/162 ,  F02C7/36 ,  F02C9/20 ,  F05D2260/4031

Abstract: A gas turbine engine has a fan which includes a plurality of fan blades that are rotatable about an axis, and a compressor section, where the combustor section includes a first compressor and a second compressor aft of the first compressor. At least one first variable guide vane controls operation of the first compressor and at least one second variable guide vane controls operation of the second compressor. A combustor is in fluid communication with the compressor section and a turbine section is in fluid communication with the combustor. A geared architecture is driven by the turbine section for rotating the fan about the axis.