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Saunders Severn
The Saunders Severn was a three-engined biplane flying boat intended for maritime patrol duties. It performed well but was fragile and unreliable. Only one was built.
==Design and development==
The Saunders A.7 Severn was the last flying boat designed by S.E. Saunders Ltd before the take-over by A.V. Roe and John Lord late in 1928 that produced the Saunders-Roe, or "Saro", company. Its first flight was two years after this change of ownership and so it has been alternatively referred to as the Saunders/Saro Severn, the Saunders-Roe A7 and the Saro A7. It was designed to Air Ministry specification R.4/27 for a maritime patrol aircraft.
It was the second Saunders aircraft to use their patented "corrugated" structure for the hull, first trialled on the Saunders A.14, in which longitudinal external corrugations in the skin replaced internal riveted stringers. Full trials of the A.14, revealing both the strengths and weaknesses of this technique were not made until after the Severn had flown. Like the A.14 the Severn's construction largely avoided doubly curved hull plating, so the planing bottom was strictly V-shaped and the upper hull rather slab sided. The hull was a two-step design with tumble-home sides above the chines. There was a gunner's position in the nose and a side-by-side open cockpit for the pilots ahead of the engines and wing. Behind the cockpit and within a windowed part of the hull were crew positions and accommodation and from which a dorsal gunner's position just aft of the wings could be accessed. There was an isolated rear gunner's position in the extreme rear of the upswept rear fuselage, above the braced tailplane and between the two braced fins. Twin balanced elevators projected beyond the tailplane and the fins carried balanced rudders. Early flight trials showed the Severn to be heavy on the rudder, so separate servo-rudders were soon fixed on struts behind the main rudder surfaces. It was also heavy on elevators, which were increased in area.
The Severn was a three-engined sesquiplane, the lower wing having a span of only 58% of the upper one and about 52% of the chord. This small lower wing was mounted just below the hull decking. Both wings were made of fabric-covered duralumin. The upper wing, which carried the ailerons, was joined at its centre line to the upper edges of the fuselage by a tandem pair of inverted V-struts, the forward one supporting the central engine, which was faired into the underside of the wing. Single vertical struts held the outer engines in similar positions, with single inward leaning struts at the rear. There were outboard outwardly splayed interplane struts with the braced stabilising single stepped floats mounted below. The three 490-hp (365 kW) Bristol Jupiter XI radial engines each had their nine uncowled cylinders forward of the wing leading edge, driving two-bladed propellers.〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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