FA865015C2631

Small Business Innovation Research Program (SBIR) Phase II

Improved Turbo/Superchargers for UAV Applications

Improved Turbo/Superchargers for UAS/UGS Application

The benefits of greater power and efficiency are offered by using turbochargers and superchargers for small UAS propulsion systems which including rotary, piston, and other developing engines. Present day UASs suffer performance losses upon takeoff and at altitude. Therefore, the need for improved, light weight turbo and superchargers which eliminate the use of oil lubrication for the bearing system is needed. Furthermore, current UAS systems are experiencing durability issues with turbochargers due to oil coking. Light weight forced induction systems with improved bearing and lubrication circuits are sought for the 50 to 150 HP UAS class. The bearing systems in turbochargers and superchargers are normally oil-fed from the engine oiling system. The bearings in these systems run in an extremely harsh environment and are subjected to axial, radial and thermal loads that limit the life of the turbocharger system and can cause failures during important mission sorties. The elimination of the pressurized oil bearing system would greatly enhance reliability and durability and decreases losses of aircraft that are employing turbochargers and superchargers. There are a number of engines that could use turbocharger technology but some do not have pressurized oiling systems. Even systems that have pressurized oiling systems suffer from pumping losses due to the oiling system having to supply oil to the turbocharger and supercharger. Additionally, when operating at high angles of attack, the pressurized oil systems may not provide adequate lubrication for the bearing systems. Having a system that optimizes the ability to place the turbocharger or supercharger in airframe positions that are not possible with a pressurized oiling system is a must. Lastly, the forced induction system should be light weight and reliable. The weight should less than 5% of the overall engine system.

The goal of phase II is to continue the R&D efforts initiated in Phase I. Funding is based on the results achieved in Phase I and the scientific and technical merit and commercial potential of the project proposed in Phase II.

OSD13-PR5

F2-8118

2013.3

James Kesseli