Proceedings of the JFPS International Symposium on Fluid Power
Online ISSN : 2185-6303
ISSN-L : 2185-6303
PERFORMANCE OF A POWER TRANSFER UNIT FOR AIRCRAFT APPLICATIONS
John WATTON
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Keywords: PTU, pump, motor, direct coupling
JOURNAL FREE ACCESS

2008 Volume 2008 Issue 7-1 Pages 155-160

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Abstract
This paper considers power transfer between two fluid power circuits such that a failing pressure in one of them is improved by power transfer from the other circuit. The two coupled axial piston machines are effectively driven by the pressure differential across the two machines and particular features are required for the unit to operate successfully. Steady state theory is presented that may be used to select the relative displacement ratios and the range predicted is compared with those typically found in aircraft applications.
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