Morgan Advanced Materials Metals and Joining Centre of Excellence (CoE) is at the forefront of brazing and metallisation technology. Launched in October 2017 the CoE is part of Morgan’s global network of specialised innovation centres delivering new material science. The CoE is a global hub for developing next generation joining solutions that enable progress across aerospace, medical, semiconductor, and other high performance industries.
Our team is continuously developing breakthrough technologies that solve complex joining challenges. Our mission is to deliver differentiated, scalable technologies with measurable customer value.
We work closely with key customers in their R&D programs, delivering collaborative projects to tailor solutions that meet highly specific needs - ensuring that innovation aligns with practical application and commercial requirements.
As a knowledge hub for metallisation and brazing technology, we educate and train both internal and customer personnel while leveraging universities and outside research communities.
Our Centre of Excellence focuses on research and product development support for some of the world’s most demanding applications in Aerospace, Medical, and Semiconductor industries.
Developed a novel patented technology that transforms brittle brazing alloys in flexible wire form, significantly improving application precision in complex applications, including aerospace engine components, heat exchanger systems, and compressor components.
In collaboration with Morgan’s New Bedford facility created a high-density biocompatible feedthrough. This innovation enables greater miniaturisation, reduces invasiveness of surgery, and increases signal transmission for enhanced functionality of implanted devices.
Developed a melt spun foil alloy based on titanium-cobalt-zirconium reducing brazing temperatures for titanium medical implantable devices. Prevents grain growth and distortion while ensuring hermetic integrity.
Created new braze alloy grades for aero engine temperature measurement, extending operational limits from 510°C (950°F) to over 593°C (1100°F). Supporting the increasing thermal demands of modern aero engines.