The present invention relates to a droplet combustion test system for a gravity-free aircraft for studying characteristics of combustion phenomenon by simulating a micro-gravity environment of the universe using a weightless airplane on the ground. More specifically, the present invention relates to the droplet combustion test system for the gravity-free aircraft, capable of performing a droplet combustion test in a limited weightless section of the gravity-free aircraft by controlling each of experimental equipment according to a change in gravity of the gravity-free aircraft. The droplet combustion test system for the gravity-free aircraft includes: a chamber; a droplet combustion module; an optical equipment; and a switch unit.
본 발명은 우주의 마이크로 중력환경을 지상의 무중력 비행기로 모사하여 연소현상에 대한 특성을 연구하기 위한 무중력비행기용 액적연소실험시스템에 관한 것으로, 더욱 자세하게는 무중력 비행기의 중력 변화에 따라 실험 장비들을 각기 제어하여 무중력 비행기의 제한된 무중력 구간에서 수행 가능한 무중력비행기용 액적연소실험시스템에 관한 것이다.
The Droplet Combustion Experiment System for parabolic flight
무중력비행기용 액적연소실험시스템
2020-06-15
Patent
Electronic Resource
Korean
The Droplet Combustion Experiment System for parabolic flight
European Patent Office | 2020