The gas turbine has high-temp., high-pressure gas from the combustion chamber (2) taken to a distribution or collection tube (10) via a jet (24). The gas flows through an inlet (21), internal passages or channels (20) and an outlet (22) in the static scoops (15), and then into a subsequent collection tube. The turbine may have a heating medium fluid as well as a working fluid. The heating fluid is delivered to at least one inlet of the static scoop (15). There are channels in these scoops between at least one inlet and one outlet. The heating fluid passes through the channels from inlet to outlet.
申请公布号
DE19501471(A1)
申请公布日期
1995.08.10
申请号
DE19951001471
申请日期
1995.01.19
申请人
HOSHINO, KENZO, HIRATSUKA, KANAGAWA, JP;SIMOES RAPOSO BRUGES DE OLIVEIRA, MANUEL JOSE, HIRATSUKA, KANAGAWA, JP
发明人
HOSHINO, KENZO, HIRATSUKA, KANAGAWA, JP;SIMOES RAPOSO BRUGES DE OLIVEIRA, MANUEL JOSE, HIRATSUKA, KANAGAWA, JP