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Energy Harvesting from Thermal and Vibration Loads due to High Temperature, High Speed Impinging Jets
Navy SBIR 2010.1 - Topic N101-093 ONR - Mrs. Tracy Frost - [email protected] Opens: December 10, 2009 - Closes: January 13, 2010 N101-093 TITLE: Energy Harvesting from Thermal and Vibration Loads due to High Temperature, High Speed Impinging Jets TECHNOLOGY AREAS: Ground/Sea Vehicles ACQUISITION PROGRAM: PEO (Ships) OBJECTIVE: Perform laboratory scale experimental study to understand and characterize the vibrational and thermal effects of impinging jets on surfaces. Develop computational tools and models to evaluate thermoelectric and piezoelectric materials for absorbing this wasted energy and to convert to useful power. Provide information to utilize this methodologies to simulated carrier deck conditions. DESCRIPTION: Due to the conditions created by the takeoff and landing of various fixed wing and rotor aircraft, the operational environment on an aircraft carrier flight deck is very harsh, both for the personnel and the structural components of the deck itself. For example, the high-temperature, high velocity jet exhaust from the F/A-18E/F during takeoff and landing produces very high noise levels that may compromise the performance and safety of the flight crew personnel operating in proximity to the aircraft. These high noise levels also propagate through the flight deck, thus making the environment hostile even for personnel below the deck. The problems associated with jet impingement will be exacerbated with the introduction of the F-35B, which is a vertical takeoff and landing (VTOL) aircraft. The near-vertical impingement of the lift jets results in a number of adverse ground effects, including ground/surface erosion of the landing surface due to the high-temperature, highly unsteady impinging jets; significantly higher noise levels; enhanced unsteady heat transfer through the deck surface, and vibration. These conditions pose an additional risk to the crew operating near such aircraft and under the deck, and also affect the integrity of the carrier flight deck. This SBIR topic addresses the thermal and vibration effects, to damp/absorb them and to convent to useful energy, as well as to reduce the noise. Accomplishments from this SBIR effort will complement to other noise reduction efforts to harvest the wasted energy in the unsteady thermal load and vibrations. This in turn helps to reduce cost of operation. PHASE I: Experimental and/or numerical study at laboratory scale to understand the thermal load fluctuations and vibration due to impingement of unsteady hot jet on a flat surface. Develop numerical models and codes to predict and evaluate the various parameters involved. PHASE II: Evaluate properties of thermoelectric, piezoelectric of similar materials for heat and vibrations absorption. Develop experimental rig to examine effectiveness of noise isolation, and vibration and thermal energy utilization from hot jet impingement on walls (double). PHASE III: Under simulated conditions of engine exhaust jet impinging deck, conduct parametric study, develop user-friendly predictive tools, and optimize isolation and energy management for transition to real deck environment. PRIVATE SECTOR COMMERCIAL POTENTIAL/DUAL-USE APPLICATIONS: The methodologies developed in this SBIR program will generally be applicable to noise reduction and energy absorption from walls on engine rooms in commercial ships. Any energy harvesting technology developed will have a wide range of commercial applications in areas where vibrations and thermal loading are present. REFERENCES: 2. Maillard, J.P, Fuller, C. "Active Control of Sound Radiation from Cylinders with Piezoelectric Actuators and Structural Acoustic Sensing", J. Sound Vibration, 1997 KEYWORDS: High Speed Jet noise, Flow-structure interaction, piezoelectric materials, pyroelectric materials, vibration, thermal loads, energy conversion, energy harvesting
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