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Volume 40, Issue 7
1 July 1968
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 40, Issue 7
Review Article| July 01 1968

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

Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1968
Aircraft Engineering (1968) 40 (7): 31–32.
https://doi.org/10.1108/eb034400

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.

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© MCB UP Limited
1968
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