Engine Technologies And Repair Development,
I worked in the Engine Technologies and Repair Development Department while at Delta. This department is responsible for developing new repair strategies based on the scrap rate, cost, and estimated increase in service life of a given type of component.I participated in the development of a tip repair for the stage 2 high-pressure turbine blade of the JT8D-219 engine. In order to accomplish this, I scanned the outside of the turbine blades using a white light scanner in order to create a point map of the periphery and used cross sections of the blade to model the interior bleed air channels of the blade. The two aforementioned processes were used to create a FEA model of the blade to simulate the environment over the component's life. The FEA model generated was then used to come up with an experimental protocol for entering these repaired blades back into service.I also taught myself visual basic in order to create a program within excel to determine the natural frequencies of engine rotors, stators, and fan blades. I also came up with a methodology for determining the weight of an approximately 2 gram leading edge coating on a 2+ kilogram fan blade. Due to the change in weight being a thousandth the gross weight of the object, I came up with the idea to use the highly accurate moment weight scale used to balance the fan blades when being installed to estimate the weight of the leading edge coating based on the change in moment.