
Innovative Approaches in the Design and Fabrication of 3D-Braided Ceramic Matrix Composite FastenersAward last edited on: 9/19/2022
Sponsored Program
SBIRAwarding Agency
DOD : NavyTotal Award Amount
$722,209Award Phase
2Solicitation Topic Code
N202-128Principal Investigator
John E GarnierCompany Information
Advanced Ceramic Fibers LLC
2300 North Yellowstone Highway Suite 210
Idaho Falls, ID 83401
Idaho Falls, ID 83401
(208) 522-6008 |
kkoller@acfibers.com |
www.acfibers.com |
Location: Single
Congr. District: 02
County: Bonneville
Congr. District: 02
County: Bonneville
Phase I
Contract Number: N68335-21-C-0083Start Date: 10/13/2020 Completed: 2/25/2022
Phase I year
2021Phase I Amount
$239,481Benefit:
Offeror will produce a novel ceramic matrix composite fastener which will successfully attach composite and metal aerostructure components. These fasteners will exhibit increased mechanical strength properties, resistance to crack-propagation, engineered thermal conductivity, and a potential for long service-duty performance at ultra-high temperatures.This fastener is lightweight and capable of medium-scale fabrication at reasonable cost. Primary applications are for turbine engines and hot section components as well as missile, hypersonic and space engines and structures.
Keywords:
ceramic matrix composites, ceramic matrix composites, Fasteners Turbine Engines, Ultra-High Temperature, CMC
Phase II
Contract Number: N68335-22-C-0354Start Date: 5/19/2022 Completed: 5/20/2023
Phase II year
2022Phase II Amount
$482,728Benefit:
Offeror will produce a novel ceramic matrix composite fastener which will successfully attach composite and metal aerostructure components. Metal fasteners in current use suffer from several issues including significant strength losses at high temperature, corrosion, high density, galling and high cost. The proposed fasteners will exhibit increased mechanical strength properties, resistance to crack-propagation, engineered thermal management, corrosion-resistance, lower density, favorable wear patterns, and a potential for long service-duty performance at ultra-high temperatures. The proposed fastener is lightweight and capable of medium-scale fabrication at reasonable cost. Primary applications are for turbine engines and hot section components, flaps and seals, as well as missile, hypersonic and space engines and structures, and high-performance ground vehicles. This technology has important dual-use applications including industrial refractory joining mechanisms, ground-based turbine engines for electrical power generation, armor, space propulsion and aero-vehicle components.
Keywords:
Aero-structure Fabrication, High Temperature Components, ceramic matrix composite (CMC), Fasteners, 3D Manufacturing, Space Propulsion Components