Spray Characteristics of the Rotary Atomizer for the Slinger Combustor

슬링거 연소기의 회전형 분사장치의 분무특성 연구

  • 최현경 (전북대학교 항공우주공학과) ;
  • 이동훈 (삼성테크윈 파워시스템 연구소) ;
  • 유경원 (국방과학연구소) ;
  • 최성만 (전북대학교 항공우주공학과)
  • Published : 2008.09.30

Abstract

An experimental study was performed to understand spray characteristics of the rotary atomizer for the slinger combustor. In this fuel injection system, fuel is injected and atomized in the combustor by centrifugal forces to engine shaft. The experimental apparatus consists of a high speed rotational spindle, rotary atomizer, pressure tank and acrylic case. The droplet size and velocity were measured by PDPA (phase Doppler particle analyzer), and spray was visualized by using high speed camera and Nd:Yag laser-based flash photography. From the test results, the droplet size (SMD) is largely affected by rotational speed, mass flow rate and the number of orifice. As the experimental results, we could understand the spray characteristics of the rotary atomizer for the slinger combustor and obtain the optimum shape of the rotary atomizer which is suitable for the small gas turbine engine.

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