German Patent Abridgements

Abstract

The horizontal stream 9 of exhaust gases coming from the gas turbine, which flows out of the lateral openings 3 and 4 for torque compensation, is used for driving an additional small turbine connected to an airscrew 8 with horizontal axis by the gearing 5. The deflector vanes 6, 7 are opened by control means when the aircraft has reached a certain forward velocity.

Citation

(1958), "German Patent Abridgements", Aircraft Engineering and Aerospace Technology, Vol. 30 No. 2, pp. 62-62. https://doi.org/10.1108/eb032937