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Gas turbines fuel rates

Gas turbine fuel rates (heat rates) vary considerably, however Evans provides the following fuel rate graph for initial estimating. It is based on gaseous fuels. [Pg.127]

GPSA also provides a table showing 1982 Perfonnance Specifications for a worldwide list of gas turbines, in their Section 15. [Pg.127]

Equipment Design Handbook for Refineries and Chemical Plants, Vol. 1, 2nd Ed., Gulf Publishing Co., 1979. [Pg.127]

GPSA Engineering Data Book, Gas Processors Suppliers Association. Vol. 1, 10th Ed. [Pg.127]

Olefins - [FEEDSTOCKS - COALCHEMICALS] (Vol 10) - [FEEDSTOCKS-PETROCHEMICALS] (VollO) - [HYDROCARBONS - SURVEY] (Vol 13) -m automobile exhaust [EXHAUSTCONTROL, AUTOMOTIVE] (Vol 9) -catalyst for stereospeafic polymerization [TITANIUMCOMPOUNDS - INORGANIC] (Vol 24) -esters from [ESTERIFICATION] (Vol 9) -hydroxylation using H202 [HYDROGEN PEROXIDE] (Vol 13) -luminometer ratings [AVIATION AND OTHER GAS TURBINE FUELS] (Vol 3) -osmium oxidations of [PLATINUM-GROUP METALS, COMPOUNDS] (Vol 19) -polymerization [SULFONIC ACIDS] (Vol 23) -reaction with EDA [DIAMINES AND HIGHER AMINES ALIPHATIC] (Vol 8) -silver complexes of [SILVER COMPOUNDS] (Vol 22)... [Pg.700]

This test method covets the procedure for rating the tendencies of gas turbine fuels to deposit decomposition products within the fuel system. [Pg.527]

This test method for measuring the high temperature stability of gas turbine fuels uses the Jet Fuel Thermal Oxidation Tester (JFTOT) that subjects the test fuel to conditions that can be related to those occurring in gas turbine engine fuel systems. The fuel is pumped at a fixed volumetric flow rate through a beater after which it enters a precision stainless steel filter where fuel d radation products may become trapped. [Pg.527]

A 165-MW-class gas turbine/generator has been introduced by another manufacturer. This machine, also developed by scaling up a proven design, features a simple-cycle efficiency of 37.5% a turbine inlet temperature of 1235°C a pressure ratio of 30 1, up from 16 1 on the previous generation and an output of 165 MW for gas fuel firing under International Standards Organization (ISO) conditions (101 kPa, 15°C (14.7 psia, 59°F)). A combined-cycle facihty based around this machine could achieve efficiencies up to 58% or a heat rate of about 6209 kj/kWh (5885 Btu/kWh). [Pg.16]

See other pages where Gas turbines fuel rates is mentioned: [Pg.122]    [Pg.127]    [Pg.127]    [Pg.134]    [Pg.139]    [Pg.139]    [Pg.122]    [Pg.127]    [Pg.127]    [Pg.122]    [Pg.127]    [Pg.127]    [Pg.134]    [Pg.139]    [Pg.139]    [Pg.122]    [Pg.127]    [Pg.127]    [Pg.271]    [Pg.271]    [Pg.272]    [Pg.281]    [Pg.531]    [Pg.620]    [Pg.626]    [Pg.700]    [Pg.722]    [Pg.938]    [Pg.973]    [Pg.1054]    [Pg.412]    [Pg.271]    [Pg.271]    [Pg.272]    [Pg.281]    [Pg.531]    [Pg.620]    [Pg.626]    [Pg.722]    [Pg.938]    [Pg.188]    [Pg.282]    [Pg.412]    [Pg.414]    [Pg.247]    [Pg.155]    [Pg.3]   


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