SBIR/STTR Research Award

Erosion Tolerant Passive Anti-icing Materials for UAM Rotor Blades

Award identifier 5a57e9624c61f3d3d14b64567b868f6c734671893844c40170086bd7be2ede73Awarding agency National Aeronautics and Space Administration

Award amount

$849,077

Program and phase

SBIR · Phase II

Award year

2024

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
INNOVATIVE DYNAMICS INC.
Proposal award date
2024-07-08
Contract end date
2026-07-07
UEI
FT3JFDDDKLA4
Solicitation number
SBIR_23_P2
Topic code
A1

Research abstract

ldquo;Weather-Tolerant Capabilityrdquo; is considered essential in the expanding urban air mobility vehicle industry. Erosion effects of rain, dust, and sand on vehicle surfaces, especially rotor surfaces, have a considerable effect on operational and maintenance costs. Another crucial environmental condition that heavily impacts flight safety is ice accretion. This project addresses a novel erosion shield system incorporating nbsp;ice-protective technology that can be applied directly to helicopter blades.nbsp; The innovation is based on the concept of Super Elasticity in certain metals known as Shape Memory Alloys (or SMA#39;s) that allow the material to elastically deform over 4% strain, making themnbsp;very durable and erosion resistant. The Phase I effort focused on the design of an SMA based erosion tape with natural durability qualities as well as the ability to change phase (strain) for anti-icing properties. nbsp;Superior erosion resistance was demonstrated in the superelastic material Austenite phase. The material was also demonstrated to strain when activated by heat, and break the ice bond strength with a combination of surface strain and temperature, making this a very efficient electro-thermal de-ice mechanism. nbsp;Its unique nature of high stress output rate and low power requirements is a promising material to meet the need for energy savings required for electric vertical take-off and landing (eVTOL) vehicles. Phase II will continue the development of an extremely efficient rotor blade de-icing actuator, with superior erosion resistance properties. Optimal actuator materials will be selected such that the SMA will self activate in the lower temp extremes, as well as be pulse activated electrically in a power assist mode, when the rotorcraft is in extreme icing environments. A final Proof of Concept demonstration will be perfromed at the Penn State AERTS Icing Faciity to evaluate SMA perfromance at representative temperature and cloud moisture (LWC) conditions.

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

69 SBIR/STTR records share this UEI (1985–2024). Reported award amounts total $19,527,165. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

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

Agency intelligence

National Aeronautics and Space Administration

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