公开(公告)号：DE602004031067D1

公开(公告)日：2011-03-03

申请号：DE602004031067

申请日：2004-05-05

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SYNDER TIMOTHY S ,  BUEY JOHN R ,  BRDAR CHRISTOPHER R

IPC: F02K3/00 ,  F02K3/11 ,  F02K3/10 ,  F23D11/12 ,  F23D11/38 ,  F23R3/20 ,  F23R3/28

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：CA2462753A1

公开(公告)日：2004-11-13

申请号：CA2462753

申请日：2004-04-01

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER TIMOTHY S ,  BRDAR CHRISTOPHER R ,  BUEY JOHN R

IPC: F02K3/00 ,  F02K3/10 ,  F23D11/12 ,  F23R3/20 ,  F23R3/28

Abstract: A gas turbine engine augmentor nozzle has an inlet for connection to an augmentor fuel conduit and an outlet for expelling a spray of fuel. A passageway betwe en the inlet and outlet is at least partially bounded by outlet end surface portions divergin g from each other. The nozzle may be used as a replacement for a non-divergent nozzle and may reorient a fuel jet centerline toward radial.

公开(公告)号：AU2004201436A1

公开(公告)日：2004-12-02

申请号：AU2004201436

申请日：2004-04-06

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BUEY JOHN R ,  BRDAR CHRISTOPHER R ,  SNYDER TIMOTHY S

IPC: F02K3/00 ,  F02K3/10 ,  F23D11/12 ,  F23R3/20 ,  F23R3/28 ,  F02C7/22

Abstract: A gas turbine engine augmentor (72) nozzle has an inlet (104) for connection to an augmentor fuel conduit and an outlet (106) for expelling a spray of fuel. A passageway (110) between the inlet (104) and outlet (106) is at least partially bounded by outlet end surface portions (126,128) diverging from each other. The nozzle (70) may be used as a replacement for a non-divergent nozzle and may reorient a fuel jet centerline (150) toward radial.

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.

公开(公告)号：NO20041064A

公开(公告)日：2004-09-14

申请号：NO20041064

申请日：2004-03-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BUEY JOHN R ,  BONELL JOHN M

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

CPC classification number: F23R3/343 ,  F02K3/10 ,  F05D2250/232 ,  F05D2250/323 ,  F05D2250/324 ,  F05D2260/85 ,  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：SG144719A1

公开(公告)日：2008-08-28

申请号：SG2004027124

申请日：2004-04-23

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER TIMOTHY S ,  BRDAR CHRISTOPHER R ,  BUEY JOHN R

IPC: F02K3/00 ,  F02K3/10 ,  F23D11/12 ,  F23R3/20 ,  F23R3/28 ,  F02K3/11 ,  F23D11/38

Abstract: AUGMENTOR PILOT NOZZLE A gas turbine engine augmentor nozzle has an inlet for connection to an augmentor fuel conduit and an outlet for expelling a spray of fuel. A passageway between the inlet and outlet is at least partially bounded by outlet end surface portions diverging from each other. The nozzle may be used as a replacement for a non-divergent nozzle and may reorient a fuel jet centerline toward radial.

公开(公告)号：PL367932A1

公开(公告)日：2004-11-15

申请号：PL36793204

申请日：2004-05-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SNYDER TIMOTHY S ,  BRDAR CHRISTOPHER R ,  BUEY JOHN R

IPC: F02K3/00 ,  F02K3/10 ,  F23D11/12 ,  F23R3/20 ,  F23R3/28 ,  F02C3/00

Abstract: A gas turbine engine augmentor (72) nozzle has an inlet (104) for connection to an augmentor fuel conduit and an outlet (106) for expelling a spray of fuel. A passageway (110) between the inlet (104) and outlet (106) is at least partially bounded by outlet end surface portions (126,128) diverging from each other. The nozzle (70) may be used as a replacement for a non-divergent nozzle and may reorient a fuel jet centerline (150) toward radial.

公开(公告)号：NO20041951A

公开(公告)日：2004-11-15

申请号：NO20041951

申请日：2004-05-12

Applicant: UNITED TECHNOLOGIES CORP

Inventor： BUEY JOHN R ,  SNYDER TIMOTHY S ,  BRDAR CHRISTOPHER R

IPC: F02K3/00 ,  F02K3/10 ,  F23D11/12 ,  F23R3/20 ,  F23R3/28 ,  F02K1/10 ,  F02K1/00 ,  F02K1/30

CPC classification number: F23R3/20 ,  F02K3/10 ,  F05D2250/324