SBIR-STTR Award

Hal Technology will develop a compact, rugged Multi-angle Optical Dust Sensor (MODS) for real-time engine health monitoring. Prolonged sand and dust exposure leads to gas turbine component degradation and ultimately engine failure. The MODS will measure particulate size, size distributions, and concentration, and eventually chemical composition. This sensor has an extended range for size and concentration measurements when compared with commercially available particle sensors. In the Phase I effort we will produce and demonstrate a prototype sensor capable of measuring load rates which will lay the foundation for development of a composition-capable sensor in Phase II. In Phase II we will develop a detailed design and build an advanced prototype sensor ready for integration into selected engine system(s) for operational assessment. During Phase III we will work with the selected-engine OEM to develop a certification plan, perform Category A (ground) and B (flight) testing. Our MODS can be integrated into an engine control system to allow early warning of excessive dust loading and provide information to help manage the health and durability of an aero-turbine engine.

Benefit:
Although the MODS will be primarily designed for military aero-turbine engines such as the Joint Strike Fighter P&W F135 or GE/RR F136, Sikorsky SH60 GE T700, F/A18E/F GE F414, E-2C RR T56-427, the sensor developed by this contract will also be applicable to civilian aircraft engines and ground-based vehicles such as trucks, tanks, personnel carriers, and automobiles for engine health protection and health management.

Keywords:
turbine blade erosion, turbine blade erosion, Light scattering, particulate load rate, Particle Composition, Optical particle sensor, Particle size, Engine Health Monitoring, Particle concentration

Hal Technology will develop a compact, rugged, fiber-optic, flush-mounted, Multi-angle Optical Dust Sensor (MODS) for real-time engine health monitoring. Prolonged sand and dust exposure leads to gas turbine component degradation and ultimately engine failure. The MODS will measure particulate size, size distributions, and concentration, and eventually chemical composition. This sensor has an extended range for size and concentration measurements when compared with commercially available particle sensors. Our in situ approach with a fiber-optic sensor performs non-intrusive particle measurements with a multiplexed sensor head that has implementation flexibility, reduced thermal management requirements, immunity to electromagnetic interference, and potentially low cost. In the Phase II effort we will ultimately produce and demonstrate an advanced prototype fiber-optic sensor capable of measuring load rates and ready for integration into selected engine system(s) for operational assessment. During Phase III we will work with the selected-engine OEM to develop a certification plan, perform Category A (ground) and B (flight) testing. Our MODS can be integrated into an engine control system to allow early warning of excessive dust loading and provide information to help manage the health and durability of an aero-turbine engine.

Benefit:
Although the MODS will be primarily designed for military aero-turbine engines such as the Joint Strike Fighter P&W F135 or GE/RR F136, Sikorsky SH60 GE T700, F/A18E/F GE F414, E-2C RR T56-427, the sensor developed by this contract will also be applicable to civilian aircraft engines and ground-based vehicles such as trucks, tanks, personnel carriers, and automobiles for engine health protection and health management.

Keywords:
Engine Health Monitoring, Particle Composition, Particle concentration, Particle size, Light scattering, Optical particle sensor, particulate load rate, turbine blade erosion