公开(公告)号：US20190162188A1

公开(公告)日：2019-05-30

申请号：US15827940

申请日：2017-11-30

申请人： Rayne Sung

发明人： Rayne Sung

IPC分类号： F04D3/02 ,  F04D19/02 ,  F04D23/00

CPC分类号： F04D3/02 ,  F02C3/08 ,  F04D17/02 ,  F04D17/025 ,  F04D19/02 ,  F04D23/005 ,  F04D29/442 ,  F05D2250/232

摘要： A gas turbine engine, with a conical screw integrated compression system, that utilizes at least one conical screw as an intermediary fluid transport device to facilitate the multi-staging of non-axial compressors, such as centrifugal and diagonal compressors, as well as or alternatively to combine non-axial compressors to axial compressors and to the fan. The conical screw in the compression system applies axial flow translation and funnels, as necessary, the exit flow of the impeller, fan or compressor into the next impeller or compressor.

公开(公告)号：US10598181B2

公开(公告)日：2020-03-24

申请号：US15827940

申请日：2017-11-30

申请人： Rayne Sung

发明人： Rayne Sung

IPC分类号： F02C3/05 ,  F04D3/02 ,  F04D23/00 ,  F04D19/02 ,  F04D29/44 ,  F04D17/02 ,  F02C3/08

摘要： A gas turbine engine, with a conical screw integrated compression system, that utilizes at least one conical screw as an intermediary fluid transport device to facilitate the multi-staging of non-axial compressors, such as centrifugal and diagonal compressors, as well as or alternatively to combine non-axial compressors to axial compressors and to the fan. The conical screw in the compression system applies axial flow translation and funnels, as necessary, the exit flow of the impeller, fan or compressor into the next impeller or compressor.