Turbine blade and disk Design and Lifing Analysis (Individual effort)
Perform a complete design of the blade-disk assembly using the analytical techniques which were provided from
Sawyers Turbine design manual.
The materials which will be used will be Discaloy for the disk and Alloy X3 first generation single crystal for the
blade. Material Properties are provided.
A) Design of Blade and Disk
Design the airfoil cross section
Design the disc fixing (this should be a three-lobe design, preferably)
Design the blade fir tree
Design the blade platform
Optimize the disc profile to yield a durable and light design using MDIDS-GT by applying a higher
mass at the outer rim to simulate the total mass of the blade, the firtree and platform as well as the
disc tangs. You may alternatively use the finite difference method described in Sawyers notes on
Turbine Disc-Blade design if you wish but it is not mandatory. Using MDIDS-GT with the mass
adjustment should provide the same results.
Perform stress analysis of the critical areas of the disk identified in Sawyers notes (see below).
Perform a disc burst analysis and determine the Burst Margin.
Bu iş için 17 freelancer ortalamada $379 teklif veriyor
Hello I'm Mohamed saeed mechanical engineer with high experin in turbine disk blades design I have checked your job and ready to help you in your project.
Hi. I am a mechanical engineer who has many experiences in aerodynamics. I can provide perfect results according to your proposal. Please open chat window and send me details. Thanks.
HELLO DEAR CLIENT I have gone through your project details and the work is DOABLE since its within my area of EXPERTISE.I will tackle are required guideline to deliver desired goal Please consider my bid. THANKS