The Dair 100 engine is a twin-cylinder two-stroke, opposed-piston, 18101NaN1 displacement, liquid-cooled, diesel engine direct drive design. It produces 1000NaN0 at 2500 rpm, with a compression ratio of 18:1.[1] The engine has two cylinders and two crankshafts linked to four pistons, the combustion chamber formed between the crowns of the pistons. There are no poppet valves, each cylinder having a ring of ports at each end. In this "one-direction (uniflow)" engine these ports, respectively, admit air and expel exhaust gases. This design eliminates the need for a cylinder head and camshafts. Scavenging is assisted by a centrifugal air pump, the pump also serving to provide a mild supercharging effect. Fitment of an exhaust-driven turbocharger is permissible.[2]
The engine may use either diesel fuel (DERV) or Jet-A1 kerosene (AVTUR). Jet-A1 is more readily available at airfields, but its reduced lubricity (compared to diesel fuel) could mean that additional cylinder lubrication may be required. Fuel is directly injected into each cylinder, pressure being supplied by a hydraulically-governed mechanical fuel pump.[2]
Dry sump lubrication is by high pressure pump delivering oil to plain main bearings and con-rod bearings.[2]