A new model of construction of gas turbines (Machine-translation by Google Translate, not legally binding)

摘要

A new mode of construction of gas turbines, especially axial turbines for hot gases for fixed installations, motor vehicles and jet engines in airplanes, characterized in that the turbine disc of each step consists of two halves facing axially and the turbine blades whose part they consist of a central core with two cylindrical or lateral conical spikes of perfectly circular or circular cross section and laterally flattened in tran with reduced play in and suspended from the housings provided in the rim of these half discs that like the feet of blade or blade are cooled by an adjustable pressure air stream; and by the provision of means avoiding vibrations and neutralizing the torsional stresses in the disc means as well as shock absorbing elements of the blades of the blades; means for covering spaces between the feet of the blades and their direction; means for fastening and centering and balancing the discs and driving the cooling air. (Machine-translation by Google Translate, not legally binding)