| Jona J-6 | |
|---|---|
| Role | Experimental sequiplane |
| National origin | Italy |
| Manufacturer | Jona |
| Designer | Alberto Jona |
| First flight | 24 May 1936 |
| Number built | 7, including the J-6S |
The Jona J-6 was an experimental Italian sesquiplane built in 1936 to demonstrate a novel, tilting wing stabilisation system. A military trainer development without the moving wing was produced in small numbers.
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The Jona J-6 was a very unusual design: not only was it a cantilever sequiplane, its lower wing having a span about two thirds that of the upper wing and having narrower chord but, uniquely, the upper plane was mounted to the fuselage so that it could tilt about a longitudinal axis with respect to the rest of the aircraft. The objective was lateral stability; the ailerons were connected together and moved by the motion of the wing with respect to the fuselage so that if the port wing was raised by a gust its aileron was also raised, automatically correcting the roll.[1][2] This system could only be implemented on a biplane, with ailerons on the lower wing under the pilot's control used for turns in the usual way.[3]
Because the upper wing tilted, it had to be a cantilever structure. It was built around two wooden spars, through whose centre passed a circular rod acting as hinge. This rod was held above the fuselage by four pairs of faired V-form struts with their eight ends fixed to it. Control wires from the ailerons were attached to this fixed rod, providing the required automatic deflections as the wing tilted. The rate of tilt was limited by a pair of telescopic, sprung struts from mid-chord quite close to the centre line, which met at the bottom centre of the fuselage after passing in through the upper sides. These could be hydraulically locked for aerobatics and spins or when stabilisation was not wanted. Leading edge automatic Handley Page slots were fitted to prevent spinning via wing tip stalling. The wing was plywood covered and straight tapered in plan, with semi-elliptical tips. The lower wing was generally similar, though much smaller and rigidly mounted.[1][2]
The fuselage was built around a rectangular section steel tube structure, shaped into an oval with metal covering forward of the lower wing leading edge and for the decking behind the cockpit, with fabric elsewhere. At the front a 140 hp (104 kW) Fiat A.54 radial engine was mounted forward of the fuselage within a Townend ring. The tandem cockpits were under continuous glazing with the forward seat under mid-wing, where a large cut-out eased visibility. The glazing was faired into the rear decking. The externally braced tailplane had a swept, straight leading edge and was mounted on top of the fuselage. It carried separate elevators, between which moved a deep, curved edged rudder.[1][2]
The mainwheels of the J-6 were mounted on split axles from the lower central fuselage, with shock absorbers fixed to the upper longerons. The wheels were spatted and the shock absorbers, though not their upper extension rods, were faired. The conventional undercarriage had a steerable, partly faired tailskid.[1][2]
The Jona J-6 first flew on 24 May 1936.[4] Its designer claimed that it could be flown without using the rudder, which was only needed on take-off or landing. It could not be spun or side-slipped when the upper wing was free to move, though with the wing locked it could be spun and looped at will.[1][2]
After successfully completing its flight testing, the J-6 prototype was bought by the Italian government, though no more were built. The prototype of a development, the J-6S, built for Jona by Piero Magni Aviazione was flying by 1938. This aircraft, intended as a military trainer, was powered by a 240 hp (180 kW) Alfa-Romeo D.2C.30 radial engine and did not have the tilting wing but was otherwise closely similar to the J-6.[1] The J-6S lacked a Townend ring cowling on the 9-cylinder radial, had the front cockpit set slightly further aft and had a tail wheel instead of a skid.[5] Six J-6S were ordered but probably not used.[4]
Data from Jane's All the World's Aircraft 1938[1]
General characteristics
Performance
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