Rybinsk, Russian Federation
Design technique for technological process of manufacturing body parts of gas turbine aircraft engines is described, taking into account its design workability, technologist and designer's joint work paralleled. The algorithm of ensuring part adaptability to manufacture at the stage of its designing with joint engineering development of the design and manufacturing technology paralleled is given
gas turbine aircraft engine, body part, manufacturability of the part, parallel engineering work of the designer and technologist
1. Kondakov A.I., Vasiliev A.S. Selection of blanks in mechanical engineering, 2007. - 560 p.