公开(公告)号：US10443626B2

公开(公告)日：2019-10-15

申请号：US15070418

申请日：2016-03-15

Applicant: General Electric Company

Inventor： Mark Joseph Mielke ,  Peter John Wood ,  Brian Richard Green ,  Steven Mitchell Taylor ,  Curtis Moeckel ,  Mark Joseph Frisch ,  Joseph Michael Bruni

IPC: F04D29/66 ,  F01D9/04 ,  F04D29/54 ,  F04D29/32

Abstract: A circular row of non-uniformally spaced vanes includes only one first group and only one second group of adjacent vanes, unequal first and second spacing between adjacent vanes in the first and second groups, and first spacing greater than second spacing. An embodiment with second group including only three adjacent vanes. Second spacing may be about 25%-35% smaller than a nominal uniform spacing used as a design parameter for designing spacing of the non-uniformly spaced stator vanes. Circular row may be sectored. A gas turbine engine section may include one or more rings or circular rows of fixed and/or variable non-uniformally spaced vanes. Method for designing non-uniform vane spacing for circular row includes determining nominal uniform spacing and forming first spacing and second spacing from nominal uniform spacing of vanes.

公开(公告)号：US20170268537A1

公开(公告)日：2017-09-21

申请号：US15070418

申请日：2016-03-15

Applicant: General Electric Company

Inventor： Mark Joseph Mielke ,  Peter John Wood ,  Brian Richard Green ,  Steven Mitchell Taylor ,  Curtis Moeckel ,  Mark Joseph Frisch ,  Joseph Michael Bruni

IPC: F04D29/66 ,  F04D29/54 ,  F01D9/04

CPC classification number: F04D29/666 ,  F01D9/041 ,  F01D9/042 ,  F04D29/328 ,  F04D29/542 ,  F05D2220/32 ,  F05D2240/12 ,  F05D2240/128 ,  F05D2250/30 ,  F05D2260/961

Abstract: A circular row of non-uniformally spaced vanes includes only one first group and only one second group of adjacent vanes, unequal first and second spacing between adjacent vanes in the first and second groups, and first spacing greater than second spacing. An embodiment with second group including only three adjacent vanes. Second spacing may be about 25%-35% smaller than a nominal uniform spacing used as a design parameter for designing spacing of the non-uniformly spaced stator vanes. Circular row may be sectored. A gas turbine engine section may include one or more rings or circular rows of fixed and/or variable non-uniformally spaced vanes. Method for designing non-uniform vane spacing for circular row includes determining nominal uniform spacing and forming first spacing and second spacing from nominal uniform spacing of vanes.