Editing Straight engine (section)

=== Inverted engines ===
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Some straight aircraft engines have used an ''inverted engine'' configuration, whereby the crankshaft is at the top of the engine and the pistons hang downwards from it. Advantages of the inverted arrangement include a raised thrust line for improved clearance for the propeller, which either allows for the use of a larger, more efficient propeller, or for shorter undercarriage. Since the thrust line is higher, the engine can be mounted lower in the airframe, improving visibility forward, which is no longer blocked by the cylinder heads. It also allows for a simpler exhaust to keep gasses clear from the cockpit.