INNOVATIVE DYNAMICS INC. — National Aeronautics and Space Administration SBIR Phase I: A1

Description

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 the rotor surfaces, have a considerable effect on operational and maintenance costs. Another crucial environmental condition that heavily impacts flight safety is ice accretion. This proposal addresses a novel erosion shield system incorporating passive ice-protective technology that can be applied directly to helicopter blades for cost-effective reparability of blades.nbsp;nbsp;The Phase I effort will focus on the design and test of an SMA based erosion tape prototype with natural durability qualities as well as the ability to change phase (strain) for anti-icing properties.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 vehicles. The SMA material is made to perform a thermally activated shape change action that is analogous to a conventional thermal expansion except that it is enhanced to the levels needed to deice.nbsp; Instead of the thermal input being applied via conventional technology, it can be supplied passively from latent heat transfer energy due to the formation of the ice itself to transform the SMA and mechanically debond the ice.nbsp;During Phase II, we will work with NASA and commercial suppliers to define installation and configuration requirements necessary to develop a to-scale SMA based deicing system. Final SMA erosion tape configurations will be tested and validated in natural icing and erosion flight conditions.