A CARBON FIBER REINFORCED SILICON CARBIDE FIBER
Mechanical Engineering
Category
Rest of World
Geographic Coverage
Not Available
Video URL
Not Available
Sale price (USD)
Not Available
Non-exclusive license price (USD)
Not Available
Exclusive license price (USD)
Not Available
Non-exclusive license royalty rate %
Availability
Patent family
Number of members in the patent family
Assignee(s) / Patent owner(s)
To see the additional information details please login and subscribe to a Premium account.

A CARBON FIBER REINFORCED SILICON CARBIDE FIBER

Patent Granted For your reference, I have included a brief summary of the technical details of my patented technology: Tensile strength of 225 Mpa The operating temperature is beyond 1500 degrees Celsius On testing, it was observed that retention of carbon fiber without oxidating at temperatures 1800 degrees Celsius to 2000 degrees Celsius. Proprietary coating was developed to protect carbon fibers from extreme temperatures while maintaining a strength-to-weight ratio. This is also compatible with silica fibers. Any shape and size can be manufactured with conventional tooling. The versatility of the technology allows for coating a surface with silicon carbide particles with a spray paint mechanism. This technology brings together the best of both worlds, the superior strength of carbon fiber and the excellent thermal characteristics of silicon carbide. Possible applications:- Aircraft brake discs(rotors) Rocket engine nozzle lining. Hot section components of a jet engine. Thermal barrier for afterburners. High-temperature coatings. Heat shields. High-Performance CMC with Lower Sintering Temperature My invention addresses the limitations of conventional CF-SiC composites. These materials typically require extremely high sintering temperatures (>1400°C), which limits material options and increases manufacturing costs. Additionally, high temperatures can weaken the bond between the fibers and the matrix, compromising the composite's performance at elevated temperatures, and this material can operate at elevated temperatures without the issue of carbon fiber oxidation. This innovative CMC offers the potential for: Lighter and stronger airframes: Reduced weight translates to improved fuel efficiency and maneuverability. Enhanced heat management in engines and propulsion systems. Improved performance of missile components exposed to high temperatures. TRL Certification and Licensing Opportunity To further support the potential of this technology, I am pleased to include a Technology Readiness Level (TRL) certificate from the National Research Development Corporation (NRDC). This certificate verifies the development stage of my invention, demonstrating its advancement beyond theoretical concepts.

GET LICENSE BROKER APPLY submit an inquiry
photo To see the additional information details please login and subscribe to a Plus or Premium account.