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ADVANCED ROTORCRAFT TECHNOLOGY, INC. SBIR Phase II Award, October 2020

A SBIR Phase II contract was awarded to Advanced Rotorcraft Technology, Inc. in October, 2020 for $549,993.0 USD from the U.S. Department of Defense and United States Army.

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sbir.gov/node/2162569
Is a
SBIR/STTR Awards
SBIR/STTR Awards

SBIR/STTR Award attributes

SBIR/STTR Award Recipient
Advanced Rotorcraft Technology, Inc.
Advanced Rotorcraft Technology, Inc.
0
Government Agency
U.S. Department of Defense
U.S. Department of Defense
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Government Branch
United States Army
United States Army
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Award Type
SBIR0
Contract Number (US Government)
W58RGZ-21-C-00340
Award Phase
Phase II0
Award Amount (USD)
549,9930
Date Awarded
October 30, 2020
0
End Date
September 22, 2022
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Abstract

Efficient and accurate analysis is crucial for timely and cost-effective development of emerging vertical lift configurations, including eVTOL. Due to similarities between conventional rotorcraft and eVTOL, many of the critical technologies for analysis of eVTOL are available in existing rotorcraft comprehensive analysis tools. However, existing rotorcraft analysis tools are tailored to the modeling and analysis of conventional rotorcraft, which have important distinctions with eVTOL configurations. Two primary distinctions are eVTOL's use of distributed propulsion (often with 6+ rotors), and the use of electric powertrains with variable rotor speed for thrust control. This contrasts with conventional rotorcraft which typically rely on a main and tail rotor operating at a constant rotor speed.  Therefore, the objective of this effort is to more effectively support the development of emerging vertical lift by enhancing a leading rotorcraft analysis tool (RCAS) for eVTOL's unique needs. Enhancements within this effort include 1) computational efficiency for full vehicles with numerous rotors, each with large numbers of degrees of freedom, through parallelization, 2) aeroelastic full vehicle modeling with complex load paths and mutual interactions between aerodynamics and structure, 3) variable RPM rotors, 4) electric motor dynamics, and 5) trim and control with redundant control options.

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