NASA: Controlling Combustion Instability
Suppressing Pressure Oscillations
Ultra-low-emission combustors being developed for aircraft gas turbine engines are more susceptible to combustion instabilities. Caused by interaction between fluctuating heat release and naturally occurring acoustic resonances, these instabilities can shorten the life of the engine and result in premature mechanical failure. At the NASA Glenn Research Center, a dSPACE system for real-time data acquisition was integrated in a combustor rig for the control of combustion pressure oscillations. The experiment software of the dSPACE system, ControlDesk, is used to describe how the data for the experiment is to be sampled and where it is to be stored. It also creates an animated data display that runs while the experiment is in progress.
혁신을 추진하세요. 항상 기술 개발의 동향을 주시해야 합니다.
저희 전문 지식 서비스에 가입하세요. dSPACE의 성공적인 프로젝트 사례를 확인해 보세요. 시뮬레이션 및 검증에 대한 최신 정보를 받아보세요. 지금 바로 dSPACE 다이렉트(뉴스레터)를 구독하세요.