• 대한기계학회논문집B
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• 제24권10호
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• pp.1300-1308
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• 2000

The objectives of this study was to investigate the spray characteristics of single spray and twin spray in the overlap region such as mean axial velocity, mean radial velocity, mean droplet size and probability density function of droplet size. A phase doppler anemometer was used as the measurement system for droplet size and velocity. In case of single spray, injection pressure was varied from 0.2MPa to 0.7MPa. Mean axial velocity, mean radial velocity and droplet size were decreased as the distance below nozzle tip was increased. In case of twin spray, the spray characteristics were measured by varying the distance between two nozzles from 127mm to 155mm. In the overlap region, the boundary of the overlap region was determined by obtaining the distribution of mean axial and radial velocity. Droplet size was increased as the distance from nozzle tip was increased. It was found that the distribution of droplet size for twin spray in the overlap region was different to single spray.

• 한국추진공학회지
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• 제12권1호
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• pp.29-36
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• 2008

APU 가스터빈에 적용되는 연료노즐의 분무특성을 확인하였다. 분무시험은 항공기의 비행조건에 따라 4개의 작동조건에 대하여 수행하였으며 각 분무조건은 지상에서의 무부하 및 통합부하 조건과 고도 20,000 feet에서의 무부하 및 통합부하에 대해서 실험을 수행하였다. 분무특성은 레이저 빔을 이용한 가시화와 PDPA 시스템을 이용하여 SMD 및 속도측정을 수행하였으며 노즐출구에서 $20{\sim}100\;mm$지점에서 측정하였다. 연구결과 20,000 feet 무부하 조건의 경우 $90{\sim}95\;{\mu}m$ 정도의 SMD를 나타내었고 지상무부하의 경우 약 $60{\sim}75\;{\mu}m$로 측정되었으며 20,000 feet 통합부하의 경우 약 $55{\sim}65\;{\mu}m$ 지상 통합부하의 경우 $30{\sim}70\;{\mu}m$의 값을 나타내었다. 20,000 feet 무부하의 경우 화염 불안정이 발생할 가능성이 있으므로 연료분무입자의 크기를 감소하는 다양한 노력이 요구된다.