公开(公告)号：DE69213031T2

公开(公告)日：1997-05-15

申请号：DE69213031

申请日：1992-10-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DUESLER PAUL ,  LOSO WENDELL

IPC: F02C7/00 ,  F02C7/32 ,  F02K3/00 ,  B64D27/00

公开(公告)号：DE60118868T2

公开(公告)日：2006-09-14

申请号：DE60118868

申请日：2001-12-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NICOLSON MATTHEW ,  DUESLER PAUL

IPC: F01D9/02 ,  F01D17/16 ,  F01D5/14

Abstract: A vane 10 having a trunnion portion 12 and an airfoil portion 14 is provided with a stress reducing undercut 24 on the trunnion portion 12 proximate to the transition zone 22 defined between the trunnion portion 12 and the airfoil portion 14 of the vane.

公开(公告)号：DE60118868D1

公开(公告)日：2006-05-24

申请号：DE60118868

申请日：2001-12-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NICOLSON MATTHEW ,  DUESLER PAUL

IPC: F01D9/02 ,  F01D17/16 ,  F01D5/14

Abstract: A vane 10 having a trunnion portion 12 and an airfoil portion 14 is provided with a stress reducing undercut 24 on the trunnion portion 12 proximate to the transition zone 22 defined between the trunnion portion 12 and the airfoil portion 14 of the vane.

公开(公告)号：DE69213031D1

公开(公告)日：1996-09-26

申请号：DE69213031

申请日：1992-10-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DUESLER PAUL ,  LOSO WENDELL

IPC: F02C7/00 ,  F02C7/32 ,  F02K3/00 ,  B64D27/00

公开(公告)号：DE69415696T2

公开(公告)日：1999-07-29

申请号：DE69415696

申请日：1994-10-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BRODELL ROBERT ,  HOVAN EDWARD ,  SELFORS STEVEN ,  LOFFREDO CONSTANTINO ,  DUESLER PAUL

IPC: B64D27/18 ,  B64D29/00 ,  B64D29/06 ,  F02K3/06

公开(公告)号：DE69207773T2

公开(公告)日：1996-09-05

申请号：DE69207773

申请日：1992-09-08

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DUESLER PAUL ,  MANNING FRANK

IPC: B64D27/26 ,  F01D25/28 ,  F02C7/20 ,  F02C7/32 ,  H05K7/12

公开(公告)号：DE69207773D1

公开(公告)日：1996-02-29

申请号：DE69207773

申请日：1992-09-08

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DUESLER PAUL ,  MANNING FRANK

IPC: B64D27/26 ,  F01D25/28 ,  F02C7/20 ,  F02C7/32 ,  H05K7/12

公开(公告)号：DE60118868T3

公开(公告)日：2009-07-09

申请号：DE60118868

申请日：2001-12-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： NICOLSON MATTHEW ,  DUESLER PAUL

IPC: F01D9/02 ,  F01D17/16 ,  F01D5/14

Abstract: A vane 10 having a trunnion portion 12 and an airfoil portion 14 is provided with a stress reducing undercut 24 on the trunnion portion 12 proximate to the transition zone 22 defined between the trunnion portion 12 and the airfoil portion 14 of the vane.

公开(公告)号：DE69504209T2

公开(公告)日：1999-04-29

申请号：DE69504209

申请日：1995-11-20

Applicant: UNITED TECHNOLOGIES CORP

Inventor： DUESLER PAUL

IPC: B64D29/02 ,  B64D27/18 ,  B64D27/40 ,  F02C7/00 ,  F02K3/06 ,  B64D27/26

Abstract: A linkage arrangement (20) joins a nacelle (12) enclosing a gas turbine engine (10) and a pylon (18) suspended from an aircraft wing. The linkage arrangement (20) counteracts the deflections of the nacelle (12) with respect to the free air stream due to the aerodynamic load. The linkage arrangement (20) includes a plurality of links (22, 24, 32, 34) that substantially duplicate the motion of a four bar linkage mechanism.

公开(公告)号：DE69415696D1

公开(公告)日：1999-02-11

申请号：DE69415696

申请日：1994-10-18

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BRODELL ROBERT ,  HOVAN EDWARD ,  SELFORS STEVEN ,  LOFFREDO CONSTANTINO ,  DUESLER PAUL

IPC: B64D27/18 ,  B64D29/00 ,  B64D29/06 ,  F02K3/06