SBIR/STTR Research Award

Novel Parfoil Construction using 3D Weaving Techniques

Award identifier eedec7b1c361bbf6d626e514a5cb06bbeb10993b1a06c564061886d556baa7a1Awarding agency Department of Defense · Army

Award amount

$100,000

Program and phase

SBIR · Phase I

Award year

1998

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Award details

Awarding agency
Department of Defense
Branch
Army
Recipient company
Federal-Fabrics-Fibers, Inc.
Proposal award date
Not reported
Contract end date
Not reported
UEI
V5PDWML2J195
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Ram air paragliders offer the advantage of relatively safe and quiet insertion of cargo that can be remotely guided to within 100 meters of the target point. Fabrication of cargo ram air parafoils however involves cumbersome cut-and-sew processes which is labor intensive leading to high cost. Weaving the ram air parafoil fabric in Net Shape Three Dimensions (NS3D) will eliminate the labor intensive cut-and-sew method. Two methods will be investigated and the best method will be used for the deliverable. Current parafoils are made of non-porous materials with ribs cut and sewn into the top and bottom of the canopy forming cells, into which the air flows. Moving through the air, filling each cell in the parafoil creates lift. This mechanism forms an aerodynamic wing-like structure. The cut and sewing process can be replaced however by other structural designs which can be manufactured cheaper and can carry heavier loads. One such design is a series of arched and tapered tubes sandwiched on the top and bottom with flat woven material. The real challenge in the airfoil project is creating an arched and tapered tube that contains no seams. Arched tubes are fairly routine in practice using NS3D weaving. However, weaving of the tapered tube requires more research for perfecting the technique (Fig. 1). FFF has the necessary technology and skill in order to successfully complete the task. BENEFITS: In addition to military and sport paragliders, this structure can be rigidized. The rigid parafoil form can be used to construct wings for military and sport gliders as well as motorized aircraft that are either heavier or lighter then air. For the same reasons that such structure can be used in an efficient aircraft, it can be used for watercraft structures as well. This can be accomplished by fitting the hydro surface with structural beams-ribs.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

32 SBIR/STTR records share this UEI (1993–2021). Reported award amounts total $6,548,469. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy

Agency intelligence

Department of Defense

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