公开(公告)号：DE602004026953D1

公开(公告)日：2010-06-17

申请号：DE602004026953

申请日：2004-03-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BUEY JOHN R ,  BONNELL JOHN M

IPC: F02C3/16 ,  F23R3/34 ,  F02K1/04 ,  F02K3/10 ,  F23D14/74

公开(公告)号：AT467089T

公开(公告)日：2010-05-15

申请号：AT04251281

申请日：2004-03-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BUEY JOHN R ,  BONNELL JOHN M

IPC: F02C3/16 ,  F23R3/34 ,  F02K1/04 ,  F02K3/10 ,  F23D14/74

Abstract: A turbine engine has a centerbody (38) within a gas flowpath and a downstream tailcone (58) and a pilot (56) at an upstream end of the tailcone (58). A flameholder (82) is positioned in the flowpath outboard of the centerbody (38). The pilot (56) has a first surface (64) diverging in a downstream direction.

公开(公告)号：AU2004200934A1

公开(公告)日：2004-09-30

申请号：AU2004200934

申请日：2004-03-08

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BONNELL JOHN M ,  BUEY JOHN R

IPC: F02C3/16 ,  F02K1/04 ,  F02K3/10 ,  F23D14/74 ,  F23R3/34 ,  F02C7/32 ,  F02C1/00

Abstract: A turbine engine has a centerbody (38) within a gas flowpath and a downstream tailcone (58) and a pilot (56) at an upstream end of the tailcone (58). A flameholder (82) is positioned in the flowpath outboard of the centerbody (38). The pilot (56) has a first surface (64) diverging in a downstream direction.

公开(公告)号：AU2004200934B2

公开(公告)日：2006-05-25

申请号：AU2004200934

申请日：2004-03-08

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BONNELL JOHN M ,  BUEY JOHN R

IPC: F02C3/16 ,  F02K3/10 ,  F02K1/04 ,  F23D14/74 ,  F23R3/34

Abstract: A turbine engine has a centerbody (38) within a gas flowpath and a downstream tailcone (58) and a pilot (56) at an upstream end of the tailcone (58). A flameholder (82) is positioned in the flowpath outboard of the centerbody (38). The pilot (56) has a first surface (64) diverging in a downstream direction.

公开(公告)号：CA2458280A1

公开(公告)日：2004-09-13

申请号：CA2458280

申请日：2004-02-23

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BUEY JOHN R ,  BONNELL JOHN M

IPC: F02C3/16 ,  F02K1/04 ,  F02K3/10 ,  F23D14/74 ,  F23R3/34

Abstract: A turbine engine has a centerbody within a gas flowpath and a downstream tailcone and a pilot at an upstream end of the tailcone. A flameholder is positioned in the flowpath outboard of the centerbody. The pilot has a first surface diverging in a downstream direction.

公开(公告)号：PL365623A1

公开(公告)日：2004-09-20

申请号：PL36562304

申请日：2004-02-26

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BUEY JOHN R ,  BONNELL JOHN M

IPC: F02C3/16 ,  F02K1/04 ,  F02K3/10 ,  F23D14/74 ,  F23R3/34 ,  F02C3/00

Abstract: A turbine engine has a centerbody (38) within a gas flowpath and a downstream tailcone (58) and a pilot (56) at an upstream end of the tailcone (58). A flameholder (82) is positioned in the flowpath outboard of the centerbody (38). The pilot (56) has a first surface (64) diverging in a downstream direction.