发明名称 LIGHTWEIGHT MIST ELIMINATOR FOR AIRCRAFT FUEL TANK INERTING SYSTEMS
摘要 A spiral mist elimination system includes a container with an inlet 64 and a layered assembly 66 in fluid communication with the inlet. The layered assembly contains a spiral shape and is concentric with a central axis of the container. The layered assembly imparts centrifugal motion in the engine bleed air as the engine bleed air travels spirally inward. The first portion of the layered assembly receives the first set of droplets. The layered assembly also includes a mesh matrix 76 that collects a second set of droplets. The second set of droplets impacts the mesh matrix and coalesces to form a third set of droplets. A perforated tube 68 is disposed along the central axis of the container. The perforated tube collects the engine bleed air from the layered assembly. Gravity draws the first and third sets of droplets into a reservoir.
申请公布号 EP3064263(A1) 申请公布日期 2016.09.07
申请号 EP20160158196 申请日期 2016.03.02
申请人 HAMILTON SUNDSTRAND CORPORATION 发明人 CORDATOS, HARALAMBOS
分类号 B01D39/16 主分类号 B01D39/16
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