| 摘要 |
PROBLEM TO BE SOLVED: To provide a gas-liquid centrifuge usable in aerospace where the posture is changed considerably and capable of suppressing a gas following a liquid to a minimum level and also suppressing a liquid following the gas to a minimum level. SOLUTION: The gas-liquid centrifuge is provided with a rotor 12 to be rotated and a housing 14 for housing the rotor while keeping a gap from the rotor. The rotor 12 comprises a center hollow part 12a, a center supply hole 12b, a gas discharge path 12c, and a liquid discharge channel 12. The liquid discharge channel 13 is composed of an inner side channel 13a, an outer side channel 13b, and a middle channel 13c communicating with both channels and having a connection point A with the inner side channel in the outer side in the radius direction than a connection point B with the outer side channel and accordingly, a trap mechanism 4 for holding a liquid by centrifugal force is composed in the middle channel. |
