Some manufacturers utilize certain of the advantages of the aero-derivative machines, i.e. high powerto- weight ratio and easy maintenance. The high power-to-weight ratios are achieved by running the machines with high combustion and exhaust temperatures and by operating the primary air compressors at reasonably high compression ratios i.e. above 7.
Year: 2013
Aircraft engines are used as ‘gas generators’, i.e. as a source of hot, high velocity gas. This gas is then directed into a power turbine, which is placed close up to the exhaust of the gas generator. The power turbine drives the generator. The main advantages of Aero-derivative Gas Turbines are:- •
For an individual generator that is rated above 1000 kW, and is to be used in the oil industry, it is usual practice to use a gas turbine as the driving machine (also called the prime mover). Below 1000 kW a diesel engine is normally preferred, usually because it is
In the first few weeks of a new project the engineer will need to roughly draft a key single-line diagram and a set of subsidiary single-line diagrams. The key single-line diagram should show the sources of power e.g. generators, utility intakes, the main switchboard and the interconnections to the subsidiary
The capacity of the battery is determined by the capacity of the individual series connected cells. Parallel connection of cells can be made to increase capacity. In the past this practice was discouraged because a weak or defective cell in one of the batteries means that this battery on discharge