公开(公告)号：EP2809918A4

公开(公告)日：2015-09-16

申请号：EP13774935

申请日：2013-01-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： ACKERMANN WILLIAM K ,  MUNSELL PETER M

IPC: F02C7/12 ,  F01D11/04 ,  F01D25/12 ,  F01D25/16 ,  F02C6/04 ,  F02C6/08 ,  F02C7/06 ,  F02C7/18 ,  F02C7/28 ,  F02C9/18 ,  F02G3/00

CPC classification number: F02C6/08 ,  F01D11/04 ,  F01D25/125 ,  F01D25/16 ,  F02C7/06 ,  F02C7/185 ,  F02C7/28 ,  F02C9/18 ,  F05D2260/202 ,  F05D2260/213 ,  Y02T50/676

公开(公告)号：EP2961944A4

公开(公告)日：2017-01-25

申请号：EP14756696

申请日：2014-02-28

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  ACKERMANN WILLIAM K

IPC: F01D25/30 ,  F02C7/00

CPC classification number: F02C7/18 ,  F01D5/02 ,  F01D9/041 ,  F01D9/065 ,  F01D17/105 ,  F01D25/12 ,  F01D25/24 ,  F02C3/04 ,  F02C6/08 ,  F02C7/04 ,  F02C7/06 ,  F02C7/14 ,  F04D29/541 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/35 ,  F05D2260/20 ,  F05D2260/213 ,  Y02T50/676

Abstract: A gas turbine engine is provided that includes a compressor section, a combustor section with a multiple of pre-swirlers, a diffuser case module, and a manifold. The diffuser case module includes a multiple of struts within an annular flow path from said compressor section to said combustor section, wherein at least one of said multiple of struts defines a mid-span pre-diffuser inlet in communication with said annular flow path. The manifold is in communication with said mid-span pre-diffuser inlet and said multiple of pre-swirlers.

公开(公告)号：EP2961945A4

公开(公告)日：2017-01-18

申请号：EP14756748

申请日：2014-02-28

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  ACKERMANN WILLIAM K

IPC: F01D25/30 ,  F02C7/00

CPC classification number: F02C7/18 ,  F01D5/02 ,  F01D9/041 ,  F01D9/065 ,  F01D17/105 ,  F01D25/12 ,  F01D25/24 ,  F02C3/04 ,  F02C6/08 ,  F02C7/04 ,  F02C7/06 ,  F02C7/14 ,  F04D29/541 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/35 ,  F05D2260/20 ,  F05D2260/213 ,  Y02T50/676

Abstract: A gas turbine engine is provided that includes a compressor section, a combustor section with a multiple of pre-swirlers, a diffuser case module, and a manifold. The diffuser case module includes a multiple of struts within an annular flow path from said compressor section to said combustor section, wherein at least one of said multiple of struts defines a mid-span pre-diffuser inlet in communication with said annular flow path. The manifold is in communication with said mid-span pre-diffuser inlet and said multiple of pre-swirlers.

公开(公告)号：EP2834499A4

公开(公告)日：2015-11-25

申请号：EP13812647

申请日：2013-03-27

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  PICKFORD SIMON ,  ACKERMANN WILLIAM K ,  SNAPE NATHAN ,  HIPSKY HAROLD W

IPC: F02C7/18 ,  B64C11/14 ,  F01D25/02 ,  F02C7/047 ,  F02C7/055 ,  F02C7/12

CPC classification number: F01D25/12 ,  F01D25/02 ,  F01D25/14 ,  F02C7/04 ,  F02C7/047 ,  F02C7/055 ,  F02C7/14 ,  F02C7/18 ,  F02C7/185 ,  F05D2250/141 ,  F05D2250/232 ,  F05D2250/51 ,  F05D2260/213 ,  F05D2260/98 ,  Y02T50/675

Abstract: An example turbomachine assembly includes, among other things, a nose cone of a turbomachine. The nose cone provides an aperture that communicates air to an interior of the nose cone.

公开(公告)号：EP2809911A4

公开(公告)日：2015-09-16

申请号：EP13787586

申请日：2013-01-16

Applicant: UNITED TECHNOLOGIES CORP

Inventor： GLAHN JORN A ,  CRAWLEY CLIFTON J ,  STRIPINIS PHILIP S ,  ACKERMANN WILLIAM K

IPC: F02C6/08

CPC classification number: F02C9/18 ,  F01D11/04 ,  F01D25/00 ,  F01D25/16 ,  F02C6/08 ,  F02C7/06 ,  F02C7/12 ,  F02C7/18 ,  F02C7/28 ,  F05D2260/601 ,  Y02T50/675 ,  Y10T29/49229

Abstract: A gas turbine engine includes a buffer system that can communicate buffer supply air to a portion of the gas turbine engine. The buffer system can include a first circuit and a second circuit. The first circuit selects between a first bleed air supply having a first pressure and a second bleed air supply having a second pressure that is greater than the first pressure to render a first buffer supply air having an intermediate pressure. The second circuit selects between a third bleed air supply and a fourth bleed air supply to communicate a second buffer supply air.

公开(公告)号：EP2809575A4

公开(公告)日：2015-09-16

申请号：EP13775188

申请日：2013-01-21

Applicant: UNITED TECHNOLOGIES CORP

Inventor： SUCIU GABRIEL L ,  SCHWARZ FREDERICK M ,  ACKERMANN WILLIAM K ,  KUPRATIS DANIEL BERNARD

IPC: B63H5/10 ,  B64C11/48 ,  B64C27/10 ,  F02C1/00 ,  F02C1/06 ,  F02C3/00 ,  F02C3/10 ,  F02C6/00 ,  F02K3/00 ,  F02K3/02 ,  F02K3/072

CPC classification number: F02K3/072

Abstract: A gas turbine engine includes a very high speed low pressure turbine such that a quantity defined by the exit area of the low pressure turbine multiplied by the square of the low pressure turbine rotational speed compared to the same parameters for the high pressure turbine is at a ratio between about 0.5 and about 1.5.