| 摘要 |
According to one aspect of the invention, an ice separating apparatus (106;200) for a gas turbine engine includes a can (202) having a first end (218) and a tangential inlet (204) proximate the first end (218) of the can (202) to receive a fluid flow (210) within the can (202), wherein the fluid flow (210) includes fuel and ice. The apparatus (106;200) also includes a first conduit (206) within the can (202) to receive a separated fuel flow (230) proximate a second end (220) of the can (202), wherein the fluid flow separates ice from fuel to form the separated fuel flow (230). |
