NOZZLE ASSEMBLY FOR A SMALL GAS TURBINE

Abstract : An Author Certificate has been issued for a nozzle assembly for a small gas turbine with nozzles having an annular cross section whose leading or trailing edges are intersected by the corresponding edges of the preceding nozzle. To secure a uniform supply of the working fluid to the inlet section of the rotor blades, the nozzles are arranged in two or several rows. (Author)