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Volume 45, Issue 7
1 July 1973
This article was originally published in
Aircraft Engineering
Aircraft Engineering Cover Image for Volume 45, Issue 7
Review Article| July 01 1973

Power plant controls Available to Purchase

Author & Article Information
Publisher: Emerald Publishing
Online ISSN: 2059-9366
Print ISSN: 0002-2667
© MCB UP Limited
1973
Aircraft Engineering (1973) 45 (7): 22–23.
https://doi.org/10.1108/eb035049

THE ESSENTIAL CONTROLLABILITY under hover conditions of the VAK 191B is achieved with hot air ducted from the engine compressor tapping through hot air efflux nozzles. Since the temperature of the air bled from the engine's compressor is at 408°C to 440°C and the pressure range is between 12·2 and 15kgf/cm2 (174 to 215lbf/in2), the differential expansion of the hot air pipes relative to the airframe structure is considerable. There are various means of accommodating hot air pipe expansion and aircraft structure:

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© MCB UP Limited
1973
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