
Prototyped an electric radial compressor system. System included a compressor stage, gearbox assembly with integral heat exchanger, electric motor and inverter.

Aviation engine manufacturer targeted a 20% power increase to improve aircraft climb rate. A new compressor stage was developed for an existing turbocharger to match other engine modifications and support the new power target.

Aviation engine manufacturer required a turbine stage modification as part of a larger engine power uprate project.
Developed a data acquisition, control system and GUI for onsite compressor map generation.

Turbocharger development that incorporates a dual ceramic ball bearing cartridge; map width optimized compressor, wheel point milled from a forged blank; and investment cast stainless turbine housing.

Rapid prototyped a batch of vacuum investment cast Inconel turbine wheels to accelerate a customer's development program.
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