BULLGEAR GAS TURBINE WITH INTERCOOLER AND REHEAT

摘要

The invention refers to a bullgear gas turbine with intercooler and reheat, which can be used for driving a payload and/or as burned gases generator. The bullgear gas turbine with intercooler and reheat integrates several turbo-compressor groups each including the compressors (14,16,18,20,22), the shafts (8,9,10,11,12), the pinions (3, 4, 5, 6, 7) and the turbines (24,26,28,30,32). In front of each compressor (16,18, 20, 22) there are placed the intercoolers (15,17,19,21) and in front of each turbine (24,26,28,30,32) there are the combustion chambers (23, 25, 27, 29, 31). The pinions (3,4,5,6,7) of each turbo-compressor group interlock at different speeds (n1, n2, n3, n4, n5) with the bullgear (1) having the speed (n) and delivering the power through the shaft (2) and the coupling (34) to the payload (33). The atmospheric air is admitted through the aspiration filter (13), passes through the compressor (14) and is then delivered to the intercooler (15) and continues its layout through the compressors (16,18, 20, 22) with the intercoolers (17,19, 21). The compressed air is sent into the combustion chamber (23), where the fuel (35) is injected, and then delivered to the turbine (24) following then the layout through the combustion chambers (25, 27, 29, 31), which have the fuel injections (36,37,38,39), with the appointed turbines (26, 28, 30, 32) resulting burned gases exhausted into the atmosphere.