公开(公告)号：DE69404610D1

公开(公告)日：1997-09-04

申请号：DE69404610

申请日：1994-11-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NORRIS JAMES W ,  MATHENY ALFRED P

IPC: F01D5/22 ,  F01D9/04

Abstract: The inner shroud (48) of the vane of a vane assembly for the compressor section of a gas turbine engine is fabricated from a composite material preferably carbon fibers and imide resin and is formed into an open ended box-like member segment supporting no less than two vanes or airfoils (44,46). The segments are interlocked by a necked down edge adapted to slip into the open end of the adjacent inner shroud of the stator vane that serve to seal the gas path and provide damping. Rub strips (66,68) may be integrally formed on the bottom surface of the inner shroud.

公开(公告)号：DE602004032186D1

公开(公告)日：2011-05-19

申请号：DE602004032186

申请日：2004-12-01

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  NORRIS JAMES W ,  NORDEEN CRAIG A

IPC: F02K3/068 ,  F01D5/22 ,  F01D5/30 ,  F02C3/073 ,  F02C3/08

公开(公告)号：DE602004028528D1

公开(公告)日：2010-09-16

申请号：DE602004028528

申请日：2004-12-01

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NORRIS JAMES W ,  NORDEEN CRAIG A ,  ROBERGE GARY

IPC: F02C3/073 ,  F02C3/067 ,  F02C3/14 ,  F02K3/068 ,  F02K3/072

公开(公告)号：DE60306879T2

公开(公告)日：2007-02-15

申请号：DE60306879

申请日：2003-12-24

Applicant: UNITED TECHNOLOGIES CORP

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 ,  F02C3/16 ,  F02C5/02 ,  F02C5/04 ,  F02C5/11 ,  F02K3/06 ,  F02K3/075 ,  F02K7/02 ,  F02K7/075

公开(公告)号：DE60307033T2

公开(公告)日：2006-12-21

申请号：DE60307033

申请日：2003-12-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NORDEEN CRAIG A ,  NORRIS JAMES W ,  TWELVES WENDELL V

IPC: F02K9/66 ,  F02C3/16 ,  F02C5/02 ,  F02C5/04 ,  F02C5/11 ,  F02C5/12 ,  F02K3/06 ,  F02K7/02 ,  F02K7/06 ,  F02K7/075 ,  F02K7/20

Abstract: Distributed initiation (e.g., multipoint or continuous) is utilized to obtain constant volume-like combustion performance in a pulse combustion device (20) in the absence of detonation. A number of such devices (20) may be utilized as turbine engine combustors. The device comprises, in one embodiment, a tube (22) having a valve (30) for admitting gas to the tube, and a plurality of igniters (32) spaced along the tube.

公开(公告)号：DE69404610T2

公开(公告)日：1998-03-05

申请号：DE69404610

申请日：1994-11-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NORRIS JAMES W ,  MATHENY ALFRED P

IPC: F01D5/22 ,  F01D9/04

Abstract: The inner shroud (48) of the vane of a vane assembly for the compressor section of a gas turbine engine is fabricated from a composite material preferably carbon fibers and imide resin and is formed into an open ended box-like member segment supporting no less than two vanes or airfoils (44,46). The segments are interlocked by a necked down edge adapted to slip into the open end of the adjacent inner shroud of the stator vane that serve to seal the gas path and provide damping. Rub strips (66,68) may be integrally formed on the bottom surface of the inner shroud.

公开(公告)号：SG11201500961RA

公开(公告)日：2015-04-29

申请号：SG11201500961R

申请日：2013-08-06

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  NORRIS JAMES W

IPC: F01D5/02 ,  F01D11/00 ,  F02C7/28 ,  F04D29/08

公开(公告)号：DE602004028297D1

公开(公告)日：2010-09-02

申请号：DE602004028297

申请日：2004-12-01

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  NORRIS JAMES W ,  NORDEEN CRAIG A ,  MERRY BRIAN

IPC: F02K3/068 ,  F02C3/073 ,  F02C3/14

公开(公告)号：DE60307033D1

公开(公告)日：2006-09-07

申请号：DE60307033

申请日：2003-12-24

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NORDEEN CRAIG A ,  NORRIS JAMES W ,  TWELVES WENDELL V

IPC: F02K9/66 ,  F02C3/16 ,  F02C5/02 ,  F02C5/04 ,  F02C5/11 ,  F02C5/12 ,  F02K3/06 ,  F02K7/02 ,  F02K7/06 ,  F02K7/075 ,  F02K7/20

Abstract: Distributed initiation (e.g., multipoint or continuous) is utilized to obtain constant volume-like combustion performance in a pulse combustion device (20) in the absence of detonation. A number of such devices (20) may be utilized as turbine engine combustors. The device comprises, in one embodiment, a tube (22) having a valve (30) for admitting gas to the tube, and a plurality of igniters (32) spaced along the tube.

公开(公告)号：DE60306879D1

公开(公告)日：2006-08-31

申请号：DE60306879

申请日：2003-12-24

Applicant: UNITED TECHNOLOGIES CORP

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 ,  F02C3/16 ,  F02C5/02 ,  F02C5/04 ,  F02C5/11 ,  F02K3/06 ,  F02K3/075 ,  F02K7/02 ,  F02K7/075