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CHAPTER 7 Capstone PERFORMANCE Elevation Derating Elevation affects power output by changing the density of the air. Figure 7-2 provides expected maximum power output for several elevations versus ambient temperature. Values shown assume nominal engine output, and are based on the 1976 US Standard Atmosphere model to correlate air density to elevation. Electrical efficiency is not strongly dependent on elevation, so the nominal efficiency values listed in Table 7-2 can be used to estimate fuel consumption at any elevation for a given ambient temperature. A method to estimate exhaust characteristics is provided below. Ambient Temperature/Pressure Derating Nominal C200 Engine 200 180 160 140 120 100 80 60 40 20 0 -20 -10 0 10 20 30 40 50 Ambient Temperature [°C] Figure 7-2. Ambient Elevation vs. Temperature Derating Inlet Pressure Loss Correction Factors Air inlet design can affect engine performance. The amount of air inlet filter debris can also affect engine performance for all engine applications. The maximum allowable inlet pressure loss is 10 inches of water. Table 7-3 presents the nominal fraction of ISO zero inlet pressure loss power and efficiency versus inlet pressure loss at ISO ambient conditions for the Model C200 microturbine. These values are estimated from nominal performance curves. Interpolate, if needed, for inlet pressure losses between those listed in Table 7-3. 410066 Rev C (June 2009) 7-8 Capstone reserves the right to change or modify, without notice, the design, specifications, and/or contents of this document without incurring any obligation either with respect to equipment previously sold or in the process of construction. 0 ft 1,500 ft 3,000 ft 4,500 ft 6,000 ft 8,000 ft Net Power [kW]PDF Image | CAPSTONE C200 MICROTURBINE TECHNICAL REFERENCE
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