| 摘要 |
<p>Embodiments of the present invention operate as a mist eliminator (115). Here, at least one magnet (205) is attached to a structure having metallic surfaces that engage an airstream entering an inlet system (100) of a turbomachine. This structure is connected to the inlet system (100) and operates as the mist eliminator (115). Depending on the velocity of the entering airstream, and the orientation of the magnets (200), the mist eliminator (115) may repel the mist particles, which will separate from the airstream. Alternatively, the mist particles may be attracted to the mist eliminator (115). Here, the mist particles may separate from the airstream and then condense.</p> |
