LaunchPoint News

LaunchPoint Designs Hybrid Propulsion System for VTOL Aircraft

Posted on Mon, Apr 13, 2015

LaunchPoint Technologies Inc. recently completed a NASA Phase I SBIR* to investigate the design of a “Hybrid Electric Propulsion System for a 4-Passenger VTOL Aircraft”.  The advancement of hybrid-electric propulsion systems for rotorcrafts enables vertical takeoff and landing (VTOL) vehicles to take advantage of aerodynamic efficiencies that can reduce fuel consumption and emissions compared to conventional rotorcraft vehicles.

VTOL Distributed Electric PropulsionVTOL Distributed Electric Propulsion

Unlike conventional internal combustion engines, or high-speed turbine engines, the high power-to-weight ratio and energy efficiency of electric motors is conserved when the motor is scaled to a smaller size.  A distributed electric propulsion system for a VTOL aircraft can exploit aerodynamic benefits that increase the lift to drag ratio by 4- to 5-times that of conventional helicopters (http://ntrs.nasa.gov/search.jsp?R=20140001088).  This yields a fourfold increase in range while maintaining the VTOL and hover capabilities of a conventional helicopter. 

Furthermore, the proposed hybrid electric propulsion system will increase the safety and reliability of the system, while reducing the operating costs compared to a conventional VTOL rotorcraft of a similar payload.  LaunchPoint surveyed concept aircraft designs like the tilt wing vehicle concept images below, and designed the hybrid propulsion system for these types of vehicles, along with all of the hybrid propulsion components, like motors, controllers, battery packs, and generators for the vehicle.  LaunchPoint Technologies applied redundancy management and fault isolation techniques originally developed for “Fly-By-Wire” systems to the design of the hybrid-electric propulsion system.  The result is a propulsion system that can be safer and more reliable than a conventional piston engine propulsion system.

LaunchPoint Technologies is seeking development partners who wish to license the architecture and technology; or who wish to fund the development of custom turn-key hybrid propulsion systems for aircraft.

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*NASA Phase I SBIR: NNX14CC48P titled “Hybrid Electric Propulsion System for a 4-Passenger VTOL Aircraft”

Topics: VTOL, electric propulsion, hybrid propulsion, distributed electric propulsion