The operating point where the compressor speed lines, and the engine’s operating line meet is critical. Thus, improvement of the efficiency at that point is of paramount importance. Through systematic development of the single-stage supercharger by (i) incremental improvements to the compressor impeller, (ii) the arrangement and development of the diffuser vanes, and (iii) the shape of the outer volute/spiral, significant gains in the performance of the single-stage compressor have been made.
This chapter contains the references listed by Dr. Kollmann himself. Some of the cited books can be found on the used book market, e.g., https://www.abebooks.com/books/used-books.shtml (in original German only). They can also be located in big libraries, e.g., the British Library in London.
No abstract
The idea of precompression of the cylinder charge air is as old as the internal combustion itself. It is generally accepted that the first supercharger design in the modern sense was actually a turbocharger, patented in 1905 by the Swiss engineer Alfred Büchi (1879-1959). It comprised an axial compressor, an aftercooler and an exhaust gas turbine applied to a radial piston-cylinder engine as shown in the German patent drawings in Figure 8-1. Not surprisingly, it took him more than two decades to make the system work due to low component efficiencies, i.e., the problem that bedeviled all early gas turbine inventors due to the insufficient knowledge of aerodynamics.
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