CENTRAL AIR PASSAGE WITH RADIAL FUEL DISTRIBUTOR

    公开(公告)号:US20240263786A1

    公开(公告)日:2024-08-08

    申请号:US18104899

    申请日:2023-02-02

    发明人: Kian McCaldon

    IPC分类号: F23R3/28 F02C7/22

    摘要: A fuel mixture distribution system for a turbine engine assembly includes a combustor that includes a combustion chamber, a fuel mixture distributor that includes an air conduit defining a mixing chamber between an air inlet and an exit opening to the combustion chamber, and a plurality of fuel passages that are disposed in the air conduit where a fuel flow is introduced and mixed with air in the mixing chamber prior to flowing through the exit opening into the combustion chamber. The air conduit shape is defined to achieve the desired mixing and prevent flashback at all operating conditions.

    GAS TURBINE ALLOWING HYDROGEN TO BE USED AS FUEL

    公开(公告)号:US20240254928A1

    公开(公告)日:2024-08-01

    申请号:US18517621

    申请日:2023-11-22

    IPC分类号: F02C9/40 F02C3/22

    CPC分类号: F02C9/40 F02C3/22

    摘要: A gas turbine is configured such that: in a combustor receiving fuel and compressed air, a compressed air quantity supplied to a primary combustion field in the combustor when the rotation speed of a turbine shaft is a predetermined rotation speed is a quantity causing an equivalent ratio at the primary combustion field to be an equivalent ratio allowing misfire to be avoided in an operation state with a predetermined rotation speed and a predetermined load; fuel supply to the combustor is started when rotation of the turbine shaft is started up; a fuel quantity supplied to the combustor is controlled such that the rotation speed of the turbine shaft rises to the predetermined rotation speed, after ignition within the combustor; and increase in a magnitude of the load to the predetermined load is started before the rotation speed of the turbine shaft reaches the predetermined rotation speed.