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PDE 추진기관 부체계 기술 연구 동향

Research Activities on Subsystem Technologies of PDE Propulsions

  • Jin, Wan-Sung (Department of Aerospace Engineering, Pusan National University) ;
  • Kim, Ji-Hoon (Department of Aerospace Engineering, Pusan National University) ;
  • Hwang, Won-Sub (Department of Aerospace Engineering, Pusan National University) ;
  • Kim, Jeong-Min (Department of Aerospace Engineering, Pusan National University) ;
  • Choi, Jeong-Yeol (Department of Aerospace Engineering, Pusan National University)
  • 투고 : 2015.03.01
  • 심사 : 2015.07.14
  • 발행 : 2015.08.01

초록

펄스데토네이션엔진은 넓은 작동 범위와 높은 열효율로 인하여 잠재력 있는 미래 추진기관 시스템으로 연구되어왔다. 이러한 잠재력을 개선하기 위하여 지난 10여 년간 다양한 요소 기술들에 대한 연구가 진행되었다. 고주파수의 환경에서 PDE를 안정적으로 작동시키기 위하여, inflow-driven 밸브, 회전 밸브 등을 포함하는 새로운 밸브 시스템과 무밸브 시스템이 개발되었다. 작은 점화 에너지로 빠르게 데토네이션을 발생시키기 위하여 플라즈마 점화 방법과 경사 장애물 기술과 같은 DDT 가속 방법이 연구되었다. 또한 PDE 추진 성능 극대화를 위하여 유체노즐 등의 노즐 시스템도 진행 중인 연구 주제의 하나이다. 본 논문에서는 지난 수년간 개발된 PDE의 최신 부체계 핵심 기술에 대하여 소개하고자 한다.

Pulse Detonation Engine (PDE) has been considered as a future propulsion system for broad range of operation and higher thermal efficiency. Various subsystem technologies have been studied for more than decade to improve the performance of the potential system. New valve systems has been developed for the stable operation at high frequency including inflow-driven valve, rotary valve and valveless system. To foster the detonation initiation with a little ignition energy, plasma ignition method and DDT (deflagration to detonation transition) acceleration method such as swept ramp mechanism have been studied. Fluidic nozzle system and other nozzle system are the ongoing research topics to maximize the propulsion performance of the PDE. Present paper introduces the state of the art of PDE subsystem technologies developed in recent years.

키워드

참고문헌

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피인용 문헌

  1. An Experimental Study on Characteristics of Small-scale PDE under Low-frequency Operating Conditions vol.22, pp.3, 2018, https://doi.org/10.6108/KSPE.2018.22.3.081