Spline
Stressing And Wear Project
Computational Mechanics participated in
a collaborative research project with GKN Westland
Helicopter, Rolls Royce, Imperial College, and Nottingham
University. The objective of this project was to
develop a robust computer-based design tool for spline
joints commonly used in gas turbine engines and helicopter
transmissions. The new state-of-the-art computer
code will allow designers to simulate the contact
stress between the spline components. The computer
code is capable of simulating the contact problems
including where friction acts on the contact surfaces.
A simple fretting wear model has also been incorporated
into the software.
Experimental
testing, including extensive strain gage measurements
and photo-elastic modelling were carried out to validate
the computer modelling. Testing work included the
use of a variety of testing machines. These include
a high frequency reciprocating test rig with one
optically transparent contact surface and a 3-tooth
quasi-dynamic spline test rig. These testing machines
are designed to investigate the mechanisms of fretting
wear initiation and progression. The fretting studies
in which specimens are designed to simulate the contact
of a pair of spline teeth have been conducted to
investigate the effect of a wide range of variables.
These variables include material, heat treatment,
coating, machining process (grinding, shaping, broaching),
reciprocating amplitude, contact pressure, temperature,
and type of lubrication.
This new
software tool will have great impact on the design
community because important maintenance and failure
issues can be addressed during the conceptual design
phase without costly experiments. Design to avoid
wear and optimise maximum load carry capacity will
now be possible. |