DIESEL AIRCRAFT ENGINE
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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Abstract
The present invention is an engine, including two banks of cylinders in a flat, opposed cylinder arrangement and a crankshaft having a plurality of paired throws, the two throws of each respective pair of throws being disposed adjacent to each other and coplanar with respect to each other.
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Citations
7 Claims
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1. An integrated engine comprising:
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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. - View Dependent Claims (2, 3, 4, 5, 6, 7)
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Specification