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DIESEL AIRCRAFT ENGINE

  • US 20130019818A1
  • Filed: 05/16/2008
  • Published: 01/24/2013
  • Est. Priority Date: 01/11/2005
  • Status: Active Grant
First Claim
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1. An integrated engine comprising:

  • a unitary structure including at least the components of;

    two banks of cylinders in a flat, opposed cylinder arrangement;

    a crankshaft including multiple paired throws, each of the paired throws supporting a pair of connecting rods, each of the pair of connecting rods associated with an opposing cylinder; and

    first and second heat exchangers arranged above the opposing cylinders and configured to cool the engine.

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