Effects of Gravity and Flow Velocity on Ignition Characteristics of MMA/Air and DME/Air Mixtures

dc.creatorKobayashi, Yoshinari
dc.creatorNakaya, Shinji
dc.creatorTsue, Mitsuhiro
dc.date.accessioned2016-07-28T19:33:11Z
dc.date.available2016-07-28T19:33:11Z
dc.date.issued2016-07-10
dc.descriptionJapan
dc.descriptionUniversity of Tokyo
dc.description509
dc.descriptionICES509: Fire Safety in Spacecraft and Enclosed Habitats
dc.descriptionVienna, Austria
dc.descriptionYoshinari Kobayashi, University of Tokyo, Japan
dc.descriptionShinji Nakaya, University of Tokyo, Japan
dc.descriptionMitsuhiro Tsue, University of Tokyo, Japan
dc.descriptionThe 46th International Conference on Environmental Systems was held in Vienna, Austria, USA on 10 July 2016 through 14 July 2016.
dc.description.abstractFire safety in spacecraft such as the International Space Station is one of the most important requirements for any manned space activities. It is necessary to understand the fire outbreak mechanism in great detail to prevent fire in space. We have focused on ignition phenomena and conducted various ignition experiments. The ignitability of materials used in space has been evaluated on the ground by NASA-STD-6001. However, combustion behaviors in microgravity are very different from those on the ground due to absence of natural convective flow. Ignition phenomena could be also affected by gravity. Then, in this study, effects of gravity on the ignition limit of flammable mixtures were investigated experimentally by parabolic flight. Furthermore, since flow field could exist in spacecraft due to the movement of crews or air circulation unit, effects of flow velocity on the ignition limit were also investigated. MMA/air mixtures and DME/air mixtures were used as the experimental objects. Laser-induced spark ignition in which minimum ignition energy can be measured constantly regardless of focal length of convex lens was adopted for an ignition method. The ignition energy was calculated by measuring the difference between the incident energy and the transmitted energy. The development of ignited kernels and propagating flames were recorded with a high-speed camera. The ignition energy for the mixtures with various equivalence ratios was measured to identify the ignition limit. The ignition energy in microgravity was lower than that in normal gravity. This tendency was remarkable for mixtures close to the lean ignition limit. This result indicated that the lean ignition limit could expand in microgravity. In shadowgraph images of flame kernel development, local quenching behaviors were observed in normal gravity. On the other hand, they were suppressed in microgravity. Flow velocity of flammable mixtures also affected the ignition energy and flame kernel formation.
dc.format.mimetypeapplication/pdf
dc.identifier.otherICES_2016_395
dc.identifier.urihttp://hdl.handle.net/2346/67705
dc.language.isoeng
dc.publisher46th International Conference on Environmental Systems
dc.subjectFire safety in space
dc.subjectGravity
dc.subjectFlow velocity
dc.subjectLaser-induced spark ignition
dc.subjectIgnition energy
dc.subjectFlame kernel development
dc.titleEffects of Gravity and Flow Velocity on Ignition Characteristics of MMA/Air and DME/Air Mixtures
dc.typePresentation

Files

Original bundle

Now showing 1 - 1 of 1
Loading...
Thumbnail Image
Name:
ICES_2016_395.pdf
Size:
1.03 MB
Format:
Adobe Portable Document Format