公开(公告)号：US11846231B2

公开(公告)日：2023-12-19

申请号：US17560367

申请日：2021-12-23

Applicant: GENERAL ELECTRIC COMPANY

Inventor： William Stanley Adams ,  Victor Alfonso Gonzalez Tellez ,  Jametra Stitt ,  Nileshpuri Goswami

IPC: F02C7/052 ,  F02C7/055

CPC classification number: F02C7/052 ,  F02C7/055 ,  F05D2220/32 ,  F05D2240/14

Abstract: A system and method for preventing icing in the combustion inlet air path of a gas turbine system. An air intake system of the gas turbine system supplies intake air to a gas turbine engine. The air intake system includes an air filter inlet house to filter the intake air. The air filter inlet house includes at least one filter stage having an array of pulse filters, with each of the pulse filters being hydrophobic. A combustion inlet air path is in fluid communication with the air intake system and the gas turbine engine. The combustion inlet air path receives the filtered air from the air filter inlet house and supplies the filtered air as combustion inlet air to an inlet of the gas turbine engine. A surface of at least one component in the combustion inlet air path includes an anti-icing coating to prevent ice from forming thereon.