Let me do it this way. From a reading of the first two paragraphs of the PATENT application I infer that The Applicant proposes to reduce temperature and Pressure in the compressor, caused by Ram Air effect at high supersonic speeds, by creating a bleeds scheme that redirects some of the gaspath to the Ejector.
That is my conclusion. I am happy with it.
Last edited by Lyman; 14th Feb 2013 at 16:27.