Abstract

Three options for manufacturing of gas turbine engine fan blade blanks are considered. The mechanical properties, macro- and microstructure of the samples are studied. The possibility of replacing blades received from an external foreign supplier with blades of our own production is confirmed.

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.