SBIR-STTR Award

Lightweight Composite Launch Fairings with Integrated Damping
Award last edited on: 10/11/05

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$1,018,225
Award Phase
2
Solicitation Topic Code
AF98-067
Principal Investigator
William F Pratt

Company Information

Patterned Fiber Composites Inc

2828 E 2200 South
New Harmony, UT 84757
   (435) 586-3339
   N/A
   N/A
Location: Single
Congr. District: 02
County: Washington

Phase I

Contract Number: F29601-98-C-0138
Start Date: 4/6/98    Completed: 4/12/99
Phase I year
1998
Phase I Amount
$99,645
The objective of the "Lightweight Composite Launch Fairings With Integrated Damping," SBIR proposal is to develop technologies and procedures that merge damping materials with a patent pending wavy composite system, and create lightweight aerospace structures that meet or exceed specified strength, stiffness, damping, and acoustic requirements. Traditional passive noise and vibration control methods for these structures are heavy, bulky and perform only marginally. Based on a design of experiments, panels of highly damped wavy composites will be constructed, staticallu, modally, and acoustically tested and analyzed. Optimized "proof" panels will be built using the results of the experiment and will exceed requirements for weight, stiffness, strength, and damping. Unprecedented improvements in these panel parameters are expected from Phase I funding. This will lead to the design and manufacture of new highly damped space launch vehicle components that exhibit stiffness and strength many times greater than steel at half the weight of aluminum but over 30 times its damping. This research program combines the expertise of aerospace, materials and engineering firms and a university to deliver new methodologies and material systems for the manufacture of improved aerospace vehicles and components.

Phase II

Contract Number: F29601-98-C-0217
Start Date: 2/9/99    Completed: 2/9/01
Phase II year
1998
Phase II Amount
$918,580
The objective of the "Lightweight Composites With Integrated Damping", Phase II SBIR proposal is to develop technologies and procedures that merge damping materials with a patent pending wavy composite system, and create lightweight aerospace structures that meet or exceed the current capabilities of conventional composite materials for strength, stiffness, and damping. Traditional passive noise and vibration control methods for these structures are heavy, bulky, and perform only marginally. Highly damped wavy composite components and structures will be constructed, tested and analyzed. Optimized components will be built using the result of experimentation and integrated with a larger structure. This effor will develop the software analysis tools and methods necessary to analyze this new material system. Unprecedented improvements in structural dynamics are expected from this Phase II project. This will lead to the design and manufacture of new highly damped space launch vehicle components that exhibit high stiffness, strength, and damping that can be tailored by the engineer. This research program combines the expertise of aerospace, materials, and engineering firms and a university to deliver new methodologies and material systems for the manufacture of improved aerospace vehicles and components.

Benefits:
This project will demonstrate the ability of co-cured wavy patterned fiber composites to provide high structural damping without sacrificing stiffness and strength. There are many applications areas that can benefit from this technology including aerospace, automotive, sports, commercial, and civil engineering. In general, any application which uses fiber reinforced plastics (composites), that would benefit from tailorable damping while retaining the lightweight, stiffnes, and strength of composites, is a candidate for this new technology.