| CPC F02B 37/013 (2013.01) [F02B 29/0412 (2013.01); F02B 37/004 (2013.01); F02B 37/10 (2013.01); F02B 29/04 (2013.01); F02B 39/04 (2013.01); F02B 39/085 (2013.01)] | 17 Claims |

|
1. A low pressure turbo compressor arrangement for an internal combustion engine comprising;
an exhaust gas turbine configured to receive exhaust gas from an internal combustion engine and to discharge the exhaust gas to an ambient environment;
a compressor configured to receive and compress an ambient intake air stream and output a compressed air stream, wherein the compressor and the exhaust gas turbine are mechanically connected to a first motor;
an intercooler coupled to an output of the compressor, wherein the intercooler is configured to receive the compressed air stream from the compressor and discharge a cooled compressed air stream;
an air intake turbine configured to receive the cooled compressed air stream from the intercooler and to discharge an expanded cooled air stream to an internal combustion engine;
a first generator mechanically connected to the air intake turbine; and,
a relief valve in fluid communication with the expanded cooled air stream from the air intake turbine, wherein the relief valve discharges excess expanded cooled air stream.
|