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Volume 43, Issue 11
1 November 1971
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 43, Issue 11
Review Article| November 01 1971

Increasing efficiency Available to Purchase

Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1971
Aircraft Engineering (1971) 43 (11): 32–33.
https://doi.org/10.1108/eb034833

It was found that the fluorocarbon resins in the hundred or so bearing bushes which support the variable geometry inlet guide vanes in the high pressure compressor of the Rolls Royce Spey gas turbine engine were subject to serious corrosion.

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© MCB UP Limited
1971
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Suggested Reading

The Rolls‐Royce Spey Junior Powerplant
Aircraft Engineering (June,1967)
The Rolls‐Royce Spey Junior Turbofan Engine: The design background to the Spey Junior powerplant for the Fokker F‐28 Fellowship short haul airliner
Aircraft Engineering (May,1967)
Powerplant: A brief description of the Spey 512 and RB.162 booster
Aircraft Engineering (April,1969)
Spey Engine for AMX Combat Aircraft
Aircraft Engineering (September,1983)
Evolution of the hydrofluidic liquid SAS
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