The development of design of experimental perspective generator was a first project from non-aviation industry and first project when customer was a company not linked to Airbus.
The project was developed in accordance with separate contracts in 2010, 2011 and 2012.
The project task was the following:
The provision of sufficient strength of generator rotor (the provision of stress level in the elastic region) and to secure the deformation of rotor components for provision of generator work on the nominal loads were as customer criteria.
Two prototypes of generator with maximum speed of 3000 rpm were developed. After this both of them were tested on the stand.
In addition the stress analysis of rotor for 2 new generators for 8 500 rpm and 24 000 rpm speed was done, necessary actions were developed and proposed to the customer for sufficient strength provision. Customer received 3D models of modified design.