SBIR-STTR Award

Composite Flywheel Structure
Award last edited on: 5/23/2008

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$1,127,619
Award Phase
2
Solicitation Topic Code
AF00-035
Principal Investigator
Stephen W Tsai

Company Information

Think Composites Inc (AKA: Ilt Corp)

101 Alma Street Suite 703
Palo Alto, CA 94301
   (650) 322-9433
   stevewtsai@aol.com
   N/A
Location: Single
Congr. District: 18
County: Santa Clara

Phase I

Contract Number: ----------
Start Date: ----    Completed: ----
Phase I year
2000
Phase I Amount
$95,501
A new look on materials, geometry and manufacturing processes of flywheels is proposed. Our systems approach relies heavily on analytic modeling of stress analysis, interactive failure criteria, optimization, curing, resin flow, contolled failure progression and life prediction. In particular, the optimum ply stiffness and density variations along the radial direction can significantly reduce radial stress and improve rotor's strength; i.e., a steep increase in hoop stiffness and decrease in density. Addition of radial plies, on the other hand, will increase both radial stiffness and stress. The net effect is low strength and high cost - an approach that we do not recommend. Rotors can be manufactured by cigarette rolling and/or filament winding with prepreg, wet or dry tows. In the last case, a centrifugal resin infusion is a good solution. Instead of the conventional multi-step curing, a single-step cure can produce quality product at reasonable cost. A rotor with graded strength can lead to a controlled failure thus reduce the containment requirement. Only the outer rim of the rotor needs high fiber volume. The goal is to ensure safety while minimize the containment requirement. The ultimate product of this work is a set of guidelines and software to produce rotors with high energy, durability and competitive cost.

Phase II

Contract Number: ----------
Start Date: ----    Completed: ----
Phase II year
2001
Phase II Amount
$1,032,118
Composite flywheel rotors can achieve high performance with new design and manufacturing methods. This is done through novel hybridization of all hoop wound rotors and one stage cure without wrinkles. The rotors will be inspected before static, fatigue and spin tests. The predicted burst speed will be compared with spin test data. A flywheel system will be evaluated using our high performance rotor in a commercial unit.

Keywords:
Composite Materials, Filament Wound Rotors, Hybridization, Spin Tests, One-Stage Cure, Fatigue Life Prediction, Flywheel System Demonstration