High efficiency low pollution hybrid Brayton cycle combustor
a combustor and high efficiency technology, applied in the direction of engines, machines/engines, mechanical equipment, etc., can solve the problems of limited general adoption, inability of such engines to meet sudden demand and/or maintain a constant working temperature or pressure, and inability to control such engines inefficiently, so as to achieve clean, efficient, pollution-free power
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A. Basic Configuration Of The Present System
[0054]Referring now to FIG. 1, there is shown schematically a gas turbine engine embodying the teachings of the present invention. Ambient air 5 is compressed by compressor to a desired pressure resulting in compressed air 11. In a preferred embodiment, compressor 10 is a typical well-known two or three stage compressor, and the ambient air is compressed to a pressure greater than about four (4) atmospheres, and preferably 10 to 30 atmospheres. The temperature of the compressed air depends on the compression ratio. Al a compression ratio of 30:1 the compressed air temperature is approximately 1424° R (964° F.).
[0055]The flow of the compressed air 11 is controlled by an air flow controller 27 to a combustor 25. Combustors are well-known in the art. However, in the present invention, the compressed air 11 is supplied in a staged, circumferential manner by air flow control 27 to the combustor 200 shown in FIG. 2 and more fully described below...
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