SBIR-STTR Award

Thin-Layer Magnetostrictive Damping for Compressor Blade Damping
Award last edited on: 4/7/2014

Sponsored Program
SBIR
Awarding Agency
DOD : Navy
Total Award Amount
$729,307
Award Phase
2
Solicitation Topic Code
N01-168
Principal Investigator
Wade Pulliam

Company Information

Fortis Technologies Inc (AKA: CEFP Inc~Fortiftek Inc~)

2985 East Hillcrest Avenue Suite 108
Thousand Oaks, CA 91362
   (310) 479-7599
   contact@fortis-tech.com
   www.fortis-tech.com
Location: Single
Congr. District: 26
County: Ventura

Phase I

Contract Number: N68335-02-C-3090
Start Date: 11/13/2001    Completed: 5/13/2002
Phase I year
2002
Phase I Amount
$99,976
Fortis Technology proposes to use their novel manufacturing technique based on magnetic fields to distribute nano-particulate in a polymer resin and apply it in thin-layer on turbomachinery blades for vibration damping. These magnetostrictive particulates, to be included in the resin, provide damping through domain wall switching, a non-conservative action which provides a high loss factor. These nanocomposites can be easily fabricated into thin films, provide stiffness and strength while also incorporating novel damping capabilities which exceed in performance and temperature range viscoelastic materials, the current state of the art for blisk damping. The objective of this program is to demonstrate that magnetic fields can be used to effectively distribute the nano-particles throughout the thin film and produce a composite with properties superior to conventional polymer systems. Once demonstrated, we believe this economical process can easily be scaled up to large structures and commercially implemental for a variety of applications.

Benefits:
The passive damping technology provides extremely large damping losses in a structurally stiff polymer and carbon fiber composites. Currently damping is either active (expensive and complex) or uses viscoelastic materials (poor structural coupling and temperature range). The magnetostrictive particulate composite technology, patent applied and licensed by Fortis Technologies, provides a simple, large temperature range, high stiffness materials to be used in many applications where the current technologies fall short. Fortis sees application of this technology for improvements in sporting goods, power/hand tools, space launch and satellite design, noise abatement and vibration isolation.

Keywords:
Magnetostrictive, composite, damping, vibration, turbines, thin-layer, compressors, high-cycle fatigue

Phase II

Contract Number: N68335-04-C-0001
Start Date: 12/18/2003    Completed: 12/18/2005
Phase II year
2004
Phase II Amount
$629,331
This proposed project will advance the capabilities of Fortis Technologies' patent-pending, magnetostrictive particulate composite dampers. These composites passively (a great advantage in simplicity and effectiveness over other recently developed active material dampers) provide damping through domain wall switching, a non-conservative action which provides a high loss factor (~ 0.40). These dampers can be easily fabricated into complex shapes, provide stiffness and strength while also incorporating novel damping capabilities which exceed in performance and temperature range viscoelastic materials, the current state of the art for damping. Currently, the magnetostrictive material used in these dampers is Terfenol-D, a rare-earth/iron alloy, which was originally developed for sonar applications. The hysteresis of the material is minimal by design. However, by altering the composition of the alloy, i.e. the ratio of rare-earth to iron, the size and activation stress of hysteresis in the material can be changed, increasing loss factors and effective stress ranges. Fortis Technologies proposes to use this new technology in thin-layers on turbomachinery components and measure the vibration mitigation effectiveness on a variety of turbomachinery components susceptible to high-cycle fatigue. We believe this economical process can easily be scaled up and commercially implemental for a variety of applications throughout a turbine engine

Keywords:
DAMPING, HIGH CYCLE FATIGUE, THIN FILM, TERFENOL-D, FAN BLADES, MAGNETOSTRICTION, PASSIVE