-
公开(公告)号：US20200248571A1
公开(公告)日：2020-08-06
申请号：US16804641
申请日：2020-02-28
发明人： Christopher David King , David Vickery Parker , John Alan Manteiga , Matthew Brian Surprenant , Megan Lynn Williams , Awot Michael Berhe , Jesse Jacob Ollove
IPC分类号： F01D9/02 , F01D9/04 , B22F3/105 , B22F5/00 , B33Y80/00 , B33Y10/00 , B22F5/10 , F04D29/02 , F04D29/44
摘要： A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.
-
公开(公告)号：US11939880B1
公开(公告)日：2024-03-26
申请号：US17980134
申请日：2022-11-03
发明人： Paul Hadley Vitt , Matthew Brian Surprenant , Brian David Keith , Prem Venugopal , Thomas William Vandeputte
CPC分类号： F01D5/02 , F01D5/14 , F05D2220/30
摘要： A turbine engine stage includes a plurality of airfoils extending between an inner band and an outer band. Each airfoil in the plurality of airfoils can have an outer wall defining a pressure side and a suction side, with the outer wall extending between a leading edge and a trailing edge. An intervening flow passage is defined between two adjacent airfoils in the plurality of airfoils.
-
公开(公告)号：US11098601B2
公开(公告)日：2021-08-24
申请号：US16804641
申请日：2020-02-28
发明人： Christopher David King , David Vickery Parker , John Alan Manteiga , Matthew Brian Surprenant , Megan Lynn Williams , Awot Michael Berhe , Jesse Jacob Ollove
IPC分类号： F01D9/02 , F01D9/04 , F04D29/44 , F04D29/02 , B22F5/10 , B33Y10/00 , B33Y80/00 , B22F5/00 , B22F10/20
摘要： A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.
-
公开(公告)号：US10718222B2
公开(公告)日：2020-07-21
申请号：US15469708
申请日：2017-03-27
发明人： Christopher David King , David Vickery Parker , John Alan Manteiga , Matthew Brian Surprenant , Megan Lynn Williams , Awot Michael Berhe , Jesse Jacob Ollove
IPC分类号： F02D9/02 , F01D9/02 , B22F3/105 , F01D9/04 , F04D29/44 , F04D29/02 , B22F5/10 , B33Y10/00 , B33Y80/00 , B22F5/00
摘要： A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.
-
公开(公告)号：US20180274376A1
公开(公告)日：2018-09-27
申请号：US15469708
申请日：2017-03-27
发明人： Christopher David King , David Vickery Parker , John Alan Manteiga , Matthew Brian Surprenant , Megan Lynn Williams , Awot Michael Berhe , Jesse Jacob Ollove
摘要： A diffuser-deswirler for a gas turbine engine is provided. The diffuser-deswirler includes an inner shell and an outer shell spaced apart and configured for receiving a flow of compressed air from a compressor of a gas turbine engine. A plurality of vanes extend between the inner shell and the outer shell to define a plurality of fluid passageways and a splitter extends along the circumferential direction between adjacent vanes to split the flow of compressed air passing through the each fluid passageway. All of these components are manufactured as a single monolithic piece and are configured for diffusing and deswirling compressor air before passing it to a combustor for an improved combustion process.
-
-
-
-
搜索结果
5 条记录 (耗时 0.013 秒)
