公开(公告)号：US10920155B2

公开(公告)日：2021-02-16

申请号：US16511658

申请日：2019-07-15

Applicant: General Electric Company

Inventor： Baha Mahmoud Suleiman ,  Obulesu Chatakonda ,  Eric William Cottell

IPC: C10G31/06 ,  C10G33/06

Abstract: A system that includes a fuel treatment system. The fuel treatment system includes a hydrodynamic cavitation reactor that receives a fluid that includes fuel from a fuel supply and water from a water supply. The hydrodynamic cavitation reactor cavitates the fluid. Cavitation of the fluid cracks the fuel and forms radicals that combine with one or more substances in the fuel. A separator receives the fluid and separates the fluid into water, fuel, and one or more substances.

公开(公告)号：US20210017456A1

公开(公告)日：2021-01-21

申请号：US16511658

申请日：2019-07-15

Applicant: General Electric Company

Inventor： Baha Mahmoud Suleiman ,  Obulesu Chatakonda ,  Eric William Cottell

IPC: C10G31/06 ,  C10G33/06

Abstract: A system that includes a fuel treatment system. The fuel treatment system includes a hydrodynamic cavitation reactor that receives a fluid that includes fuel from a fuel supply and water from a water supply. The hydrodynamic cavitation reactor cavitates the fluid. Cavitation of the fluid cracks the fuel and forms radicals that combine with one or more substances in the fuel. A separator receives the fluid and separates the fluid into water, fuel, and one or more substances.

公开(公告)号：US09803552B2

公开(公告)日：2017-10-31

申请号：US14927578

申请日：2015-10-30

Applicant: General Electric Company

Inventor： Yuxin Zhang ,  Obulesu Chatakonda ,  Soumya Gudiyella ,  Narendra Digamber Joshi ,  Venkat Eswarlu Tangirala ,  Matthieu Marc Masquelet ,  Shashank Yellapantula

IPC: F23R3/28 ,  F02C7/22 ,  F02C7/04

CPC classification number: F02C7/222 ,  F02C7/04 ,  F23R3/28 ,  F23R3/286 ,  F23R2900/00004

Abstract: A fuel injection system for use in a combustor of a turbine assembly includes a substantially annular fuel injection housing at least partially defining an annular cavity. The fuel injection system also includes a fuel manifold and an air manifold. The fuel manifold includes a plurality of fuel injection ports extending through the fuel injection housing. The air manifold includes a first plurality of air injection ports and a second plurality of air injection ports that each extends through the fuel injection housing.

公开(公告)号：US20170122211A1

公开(公告)日：2017-05-04

申请号：US14927578

申请日：2015-10-30

Applicant: General Electric Company

Inventor： Yuxin Zhang ,  Obulesu Chatakonda ,  Soumya Gudiyella ,  Narendra Digamber Joshi ,  Venkat Eswarlu Tangirala ,  Matthieu Marc Masquelet ,  Shashank Yellapantula

IPC: F02C7/22 ,  F23R3/28 ,  F02C7/04

CPC classification number: F02C7/222 ,  F02C7/04 ,  F23R3/28 ,  F23R3/286 ,  F23R2900/00004

Abstract: A fuel injection system for use in a combustor of a turbine assembly includes a substantially annular fuel injection housing at least partially defining an annular cavity. The fuel injection system also includes a fuel manifold and an air manifold. The fuel manifold includes a plurality of fuel injection ports extending through the fuel injection housing. The air manifold includes a first plurality of air injection ports and a second plurality of air injection ports that each extends through the fuel injection housing.