International Journal of Microgravity Science and Application
Online ISSN : 2188-9783
航空機実験による微小重力環境下の固体燃料揮発成分の希薄限界付近に おける点火挙動
中谷 辰爾 小林 芳成津江 光洋
著者情報
ジャーナル オープンアクセス

2015 年 32 巻 4 号 p. 320404-

詳細
抄録
An Experimental setup was designed to conduct ignition experiments for mixtures of the polymethyl methacrylate (PMMA) pyrolyzed gas and air. Suitable ignition methods for microgravity experiments were reviewed, and the laser induced spark ignition was employed to investigate the ignition limit of the mixture. The pyrolyzed gas of PMMA was produced under an emission of the halogen lamp in a vessel filled with nitrogen and air. The gaseous components were sampled and analyzed by a gas chromatograph. Most pyrolyzed component was methyl methacrylate (MMA). Therefore, ignition process of MMA/air mixtures was experimentally investigated under a microgravity condition available from parabolic flights. Ignition tests were performed at 0.1MPa under microgravity and normal gravity conditions. The results indicated that the minimum ignition energy in microgravity decreased compared with that in normal gravity. Initial flame kernel formation and the growth had the preferable direction due to flow fields induced by gravity, resulting in the local quenching phenomena.
著者関連情報
© 2015 日本マイクログラビティ応用学会
前の記事 次の記事
feedback
Top