Application Guide Model C30 and C60 HEV Application Information

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Application Guide Model C30 and C60 HEV Application Information ( application-guide-model-c30-and-c60-hev-application-informat )

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Capstone Turbine Corporation • 21211 Nordhoff Street • Chatsworth • CA 91311 • USA Application Guide: C30 and C60 Hybrid Electric Vehicle (HEV) Application Information for Capstone Fuel Delivery System to Engine Fuel System Refer to the Fuel Requirements Technical Reference (410002) for detailed fuel requirements and additional information for both C30 and C60 systems. The OEM/Integrator is responsible for providing a fuel delivery system from the fuel tank to the engine fuel system. The MicroTurbine fuel system is basically a metering device and a distribution system for the injectors. It is the OEM/integratorís responsibility to provide the fuel at the required pressure and temperature. For gaseous fuels, the delivery system should consist of, but is not limited to, a fuel filter, coalescing filter (6 micron @95% of particles), regulator, and a shut off valve. The shut off valve should be as close to the MicroTurbine as possible. For liquid fuels, the delivery system should consist of, but be limited to, a boost pump, fuel filter (10 microns@45 of particles), and a shutoff value. For gaseous fuels, it is critical that only vapor be delivered to the MicroTurbine fuel system. The presence of liquid fuel particles in a gaseous fuel will damage the MicroTurbine. A gasification system with a heater will be required for operation with compressed liquid fuels. Particular care must be taken to ensure that fuel in lines after shutdown is conditioned before next start up. Trapped fuel can change phases overnight and cause liquids to form in lines. Air Assist Requirements for Liquid Fuel Systems Refer to the HEV Liquid Fuel Technical Reference (410029) for detailed and updated information. For liquid fuel systems, an external air supply is required for system start-up, low power (idle) and shutdown. This air supply assists the fuel system to atomize the fuel in the combustion chamber. The required air can be supplied from a separate system or from an onboard air system. And in either case, a 10-micron (or less) filter and a coalescing filter/separator should be installed before the turbine system. The air needs to be clean, dry and free of any oils. The following are liquid fuel system air-assist requirements (for reference only): • Start/Cooling mode ñ 80 slpm @ 427.8 kPa (62 psig) for approx. 1.5 minutes • Idle Mode (≤ 6 kW) ñ 60 slpm @ 427.8 kPa (62 psig) for duration of idle NOTE NOTE 480009-001 Rev B (October 2004) Page 33 of 54 This information is proprietary to Capstone Turbine Corporation. Neither this document nor the information contained herein shall be copied, disclosed to others, or used for any purposes other than the specific purpose for which this document was delivered. Capstone reserves the right to change or modify without notice, the design, the product specifications, and/or the contents of this document without incurring any obligation either with respect to equipment previously sold or in the process of construction.

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