SBIR/STTR Research Award

Lightweight Aluminum Composite Lifting Technologies

Award identifier d9426ba3830f9b5c0ada78278bb98741d36d37eaecf41795ef0abc4b70d03437Awarding agency Department of Defense · Army

Award amount

$250,000

Program and phase

SBIR · Phase I

Award year

2025

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Award details

Awarding agency
Department of Defense
Branch
Army
Recipient company
TOUCHSTONE RESEARCH LABORATORY, LTD.
Proposal award date
2025-04-07
Contract end date
2025-10-10
UEI
FBK3WT3XQVH8
Solicitation number
24.4
Topic code
A244-P056

Research abstract

MetPreg is an aluminum metal matrix composite that will prove to be an excellent fit to provide for ultra-lightweight, field ready hydraulic lifts and portable jacks. MetPreg is comprised of continuous alumina fibers within a pure aluminum matrix. By reinforcing the aluminum matrix with the fibers, a material with the strength of steel but the weight of aluminum is achieved. The feedstock to manufacture equipment is produced in the form of a tape. Touchstone produces the fiber reinforced aluminum (FRA) composite tape by using a low-cost, scalable pultrusion method that is analogous to polymer composite processing. The final pultruded form is achieved through the use of a die that can be tailored to the desired cross-section of the finished part.á Once the fibers pass through the die, the FRA tape is cooled and spooled up. It should be noted that since this is a metal matrix composite, there are no special storage conditions necessary for the material and there is no shelf-life associated with the material, unlike polymer matrix composites.ááTouchstone can then use the MetPreg tape as a feedstock in the filament winding process, allowing for cylindrical fiber reinforced metal matrix composite parts to be made. With this method, the MetPreg tape can be placed in patterns consisting of a helical pattern, a hoop pattern, or a pattern using both helical and hoop. This can allow for parts of various cylindrical and bottle geometries to be fabricated. As with the pultrusion process, no post-processing is needed for the filament wound FRA part to be used, which allows for it to be immediately machined to final design. The current work envelope for this process is set up to be able to produce parts with inner diameters of 1 inch to 21 inches with a maximum length of 60 inches, however, the process was designed to be scalable to whatever end user size is needed. This process also allows for the FRA tape to be wrapped around other materials to improve strength and other properties. The resultant FRA products are able to be machined to final shape and can include threads, bolt holes, and other attachment points. The high strength and lightweight properties of the tape are maintained in the cylindrical form, and high welding and machining capabilities of MetPreg allow for the manufacture of complex structures.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

104 SBIR/STTR records share this UEI (1998–2025). Reported award amounts total $38,514,559. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

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

Agency intelligence

Department of Defense

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