The de Monge 7-4 was designed and built to provide aerodynamic information on the three times larger proposed de Monge 72. Each was a twin boom
monoplane with a conventional empennage but no
fuselage. Instead, the wing between the booms was extended in
chord and greatly thickened to provide depth for
cockpits. The smaller aircraft had two engines, mounted just within the booms; the de Monge 72 was to have had a third engine on the central wing
leading edge. It was designed by Belgian pioneer
Louis de Monge. Both the inner and outer sections of the wing were built around two wooden
box spars and wooden ribs. The final ribs of the centre-section extended rearwards to the tail as the booms and the outer panels were bolted to them. An open single cockpit for pilot and passenger in
side-by-side seats was positioned between the spars. In plan the centre-section was rectangular, about in span, in chord (more than half the overall length of the aircraft) and was thick. The outer panels were braced to the lower centre-section outer edge on each side with two steel tube struts. In plan the outer panels were strongly tapering
trapezoids, carrying
ailerons along the entire
trailing edge. The de Monge 7-4 was powered by two
Anzani air-cooled 3-cylinder
radial engines on a girder across the
leading edge of the centre-section. Since they were both just within the centre-section span, they were less than apart and the
propeller disks slightly overlapped; to avoid damage both engines were slightly canted to starboard. The top of the rear ends of the booms were bridged by a near-rectangular plan horizontal tail with a full span
elevator. This had a pair of cut-outs for the deep
rudders, mounted on near triangular
fins; there was another, rudderless fin mounted at the centre of the
tailplane. The de Monge 7-4 had a conventional fixed, split-axle, tailskid
undercarriage. The axles were hinged from a V-strut, mounted on the centreline and braced with transverse wires, with their outer ends mounted on near-vertical rubber
shock absorbing struts and hinged, trailing struts, both to the lower centre-section outer edge. Each boom carried a small tailskid. The exact date of the first flight of the de Monge 7-4 is not known but it was present for the 1923 Coupe de Zenith, piloted by one Brusseaux. However, for unrecorded reasons it failed to depart on the first stage. Its early trials had been flown by
Alexis Maneyrol, who was flying a aircraft at this competition. It competed in the same contest in 1924 but once again was forced to retire. By this time more powerful Anzani engines had been fitted. ==Specifications==