公开(公告)号：GB2144492A

公开(公告)日：1985-03-06

申请号：GB8418157

申请日：1984-07-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BARAN WALTER JOSEPH

IPC: F01D9/02 ,  F01D9/04 ,  F01D25/14 ,  F01D25/24 ,  F01D9/00

公开(公告)号：DE3464514D1

公开(公告)日：1987-08-06

申请号：DE3464514

申请日：1984-05-15

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BARAN WALTER JOSEPH

IPC: F01D9/02 ,  F01D11/08 ,  F01D25/24 ,  F02C3/04 ,  F01D9/04

Abstract: The stator vanes (12,14) of an axial flow gas turbine are supported by spaced flanges (4, 6) in the surrounding turbine case one of which flanges (6) supports the upstream end of the outer shroud (10) of the vane (12) radially and also serves to position the blade tip seal segments and the surrounding air seal ring (40). The other flange (4) engages lugs (8) from the vane shroud (10) and also supports clips for the clip seal segments and the upstream edge of the air seal ring (40).

公开(公告)号：DE3563551D1

公开(公告)日：1988-08-04

申请号：DE3563551

申请日：1985-05-13

Applicant: UNITED TECHNOLOGIES CORP

Inventor： COMEAU ROGER JOSEPH ,  BARAN WALTER JOSEPH

IPC: F01D9/02 ,  F01D9/04 ,  F01D25/24

Abstract: The first stage turbine vanes (40) in a gas turbine are supported both axially and for torque control in a sleeve (26) located within the diffuser case (10) such that it is free to expand to minimize thermal stresses. The support sleeve (26) is modified to permit assembly of all the turbine vanes (40) within the sleeve.

公开(公告)号：GB2103295B

公开(公告)日：1984-08-30

申请号：GB8219181

申请日：1982-07-02

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BARAN WALTER JOSEPH

IPC: F02C7/00 ,  F01D21/00 ,  F01D25/00

Abstract: A plug for boroscope access hole located in the turbine section viewing from the outside the internal parts of the engine by cooperating holes formed in concentric casings characterized as free floating and sealing the attendant opening in an axial and radial direction.

公开(公告)号：GB2144492B

公开(公告)日：1988-01-20

申请号：GB8418157

申请日：1984-07-17

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BARAN WALTER JOSEPH

IPC: F01D9/02 ,  F01D9/04 ,  F01D25/14 ,  F01D25/24 ,  F01D9/00

公开(公告)号：GB2103295A

公开(公告)日：1983-02-16

申请号：GB8219181

申请日：1982-07-02

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BARAN WALTER JOSEPH

IPC: F02C7/00 ,  F01D21/00 ,  F01D25/00

Abstract: A plug for boroscope access hole located in the turbine section viewing from the outside the internal parts of the engine by cooperating holes formed in concentric casings characterized as free floating and sealing the attendant opening in an axial and radial direction.