Hovering on One Engine: Reduced diametral clearance eliminates problem of bearing roller skid during no load running

Abstract

An important operational feature of the Bristol Siddeley Gnome type H1200 turboshaft helicopter engine, is the way in which it can be used in coupled installations.

Citation

(1968), "Hovering on One Engine: Reduced diametral clearance eliminates problem of bearing roller skid during no load running", Aircraft Engineering and Aerospace Technology, Vol. 40 No. 7, pp. 31-32. https://doi.org/10.1108/eb034400