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363. SWAY SPACE - Radial clearance in a foil bearing based on foil and spring material thickness. 364. SWEET GAS – Natural gas with less than 95 ppm of hydrogen sulfide (H2S) will be defined as sweet gas suitable for use in the Capstone Model 330 MicroTurbine system. 365. SWITCHING FREQUENCY FILTER – Filter tuned to reduce IGBT switching frequency (15kHz). 366. Tamb SENSOR – A sensor the measures the inlet temperature of the MicroTurbine. This data is supplied to the controller. 367. TBC – Thermal Barrier Coating. A ceramic based material that is applied to hot section parts to reduce the base metal temperatures. 368. TBD – To Be Determined. 369. Tcd – Compressor discharge temperature. 370. Tci – Compressor inlet temperature. The temperature of the air at the compressor impeller inducer. 371. TECHNOLOGY ROADMAP - Prioritization of technical developments as required by market rollout. 372. TEG - Turbomachinery Engineering Group. 373. TET – Turbine Exit Temperature. The temperature of the exhaust gas, as measured by the thermocouple, at the exit of the turbine rotor. 374. Tex – Exhaust temperature. The temperature of the exhaust gas downstream of the recuperator, at the exit of the exhaust duct. 375. TGNMO – Total Gaseous Non-methane Hydrocarbon. 376. THC - Total Hydrocarbons. 377. THRUST BEARING – A compliant foil bearing deigned to have axial load capacity. The bearing is comprised of multiple levels of under-springs and an aerofoil. The under- springs are of two (2) types: support and springs. The MicroTurbine employs a dual bearing arrangement; forward thrust bearing and aft thrust bearing. Each thrust bearing has load capacity in one direction. 378. TIT – Turbine Inlet Temperature. The temperature of the combustion gases at the entrance to the turbine nozzle. 379. TLA – (1) Top Level Assembly. The configuration that defines the modules and components that comprise a MicroTurbine Generator System. (2) Three Letter Acronym. 380. TRIT – Turbine Rotor Inlet Temperature. The gas temperature at the inducer of the turbine rotor. 381. TROUBLESHOOTING – The process followed to determine the cause of a failure to the unit. 382. TROUBLESHOOTING PROCEDURES - The procedures and processes employed to determine cause of failure. Troubleshooting procedures can be located in the service manual and /or other documentation on the product. 383. TURBINE ROTOR – Also known as a radial inflow turbine. The turbine rotor recovers energy from the combustion gases once the gas has flowed through the turbine nozzle. When the gases, with increased velocity, impinge on the blades, they impart a force that keeps the rotor in motion allowing it to drive the compressor impeller and generator. 384. USER CONNECTION BAY (UCB) - The enclosure assembly where the user connects to the circuit breaker, modem, communication ports and remote control terminals on the enclosure. Other connections such as PC, power meter, and E-stop may also be made. The 215PDF Image | Final Technical Report Advanced MicroTurbine System (AMTS) -C200 MicroTurbine -Ultra-Low Emissions MicroTurbine
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