Abstract: A liquid dispensing element is provided. The element comprising; a dispensing plate comprising a plurality of orifices; the dispensing plate at least partially defining a fluid flow path; a plurality of piezoelectric transducers each comprising a piston configured to move perpendicular to the dispensing plate between a first position wherein the piston is close to the dispensing plate and a second position wherein the piston is further from the dispensing plate. The movement between the first and second positions results in the ejection of a droplet of fluid via a surface cavitation droplet ejection process such that the diameter of the droplet is less than a diameter of the orifice.

Abstract: A turbo-prop driven aircraft has the engines (6) and propeller assemblies (10) spatially separated fore and aft of the wing box (4) and interconnected by a drive shaft (27). This arrangement permits the engine to be located away from the wing box without causing excessive overhang of the turbo-prop installation.