SBIR-STTR Award

This proposal outlines an innovative parallel hybrid compound differential drive system with infinite variable speed inputs from either the internal combustion/heavy fuel engine (IC/HFE) or the high speed permanent magnet motor (PMM). This variable speed input optimizes propulsion system performance and efficiency. This approach delivers nearly double the peak takeoff/climb power of electrically compounded superchargers and/or PMM direct power (contributing up to 30% of the input power). An innovative direct injected/heterogenous charged IC/HFE with a brake thermal efficiency approaching 50% and the variable compression valves that increase the CI/HFE expansion ratio and efficiency while reducing exhaust energy below propeller noise. The compound differential transmission allows remote, low torque soft/start cabability. Reliability and maintainability are vastly improved using a robust high-speed, multi-fuel combustion system capable of stable operation on JP-8/DF-2 fuels (with the added safety and redundancy inherent with twin pack parallel hybrid propulsion). A hybrid fuel cell assisted battery pack, thermal electric waste heat exhaust recovery, and integrated photo voltaic solar panels are potential sources of supplemental power to extend the electrical energy supply essential to meeting the 24 hour duration program goal.

Benefit:
Maximum hybrid core engine power densities below 1lb/hp. - Double the peak takeoff power by electrically assisted supercharging and/or direct 50% power contribution from the brushless PM motor. - Extended S-UAS range and endurance from an efficient direct injected heterogenous charge combustion system capable lean burn/part load operation on logistically available JP-8/DF-2 fuels. - A reliable means of remote starting through a variable speed differential gear system. - Low noise propulsor for covert missions. Commercial

Benefits:
- Lightweight, multi-fuel hybrid propulsion system suitable for all aspects of ground, marine, and aviation segments in need of improved proulsion system efficiency.

This phase II proposal outlines the necessary innovative technologies that define a revolutionary hybrid turbo-compound hyper bar 2-cycle aero-diesel engine. Technical breakthroughs in multi-fuel combustion supported by innovative high speed pneumatic fuel injection combined with catalytic hot surface ignition systems enable complete freedom of compression ratio essential for effective turbo-compounding. Scavenge air and on demand engine manifold boost pressure is supplied by an electrically assisted, combustion driven hyper bar turbocharger that eliminates the weight and bulk of a positive displacement blower. The high speed permanent magnet motor/generators are independently mounted to the high speed turbochargers as well as the axial gap motor/generator imbedded in the flywheel. The speed differential and turbo compounding is by means of electronic inverter control, thus eliminating the complexity of mechanical transmissions. Variable ratio exhaust valve results in a trapped range from 9-12:1 CR. without compromising the combustion chamber geometry. With the valve closed, the higher 12:1 compression ratio improves cost start, efficient part load and stable combustion during high altitude descent avoiding ignition flame out. This innovative combine cycle engine can be characterized as having the breathing capacity and power density of the gas turbine combined with the fuel economy of the direct injected diesel.

Benefit:
Advanced heterogeneous multi-fuel combustion with favorable peak to mean pressure ratio essential for lightweight and durable engine construction. -Self-running advanced hyper bar turbocharger technology with electrically assisted compressor and on demand combustion driven supercharge independent of main engine exhaust flow. -Maximum hybrid core engine power densities below 1lb/hp. double the peak takeoff power by electrically assisted supercharging and/or direct 50% power contribution from the brushless PM motor. extended UAS range and endurance from an efficient direct injected heterogeneous charge. low noise propulsor for covert missions. Commercial

Benefits:
- lightweight, multi-fuel hybrid propulsion system suitable for all aspects of ground, marine and aviation segments in need of improved propulsion system efficiency.