Wright Aeronautical Corporation, Paterson, N. J., the aircraft engine manufacturing division of the Curtiss-Wright Corporation, announced that during the first six months of 1936 more than 1,300 of their Wright Whirlwinds and Cyclones had been sold to aircraft manufacturers, air line operating companies and military services throughout the world. These orders represented the sale of more than 1,077,000 h.p. More than 1,000 of the 1,300 engines sold were of the Wright Cyclone type, used extensively in large air transports and military aircraft. The orders for 1,000 Cyclones were believed to represent a new peace time sales record for high-powered aircraft engines over a six months period. Of this number over 700 were Cyclones of the 1,000 h.p. type which was released for domestic and commercial sale during the summer. Designated as the Wright Series G Cyclone, the 1,000 h.p. model was introduced to the commercial market on the 10th anniversary of the Cyclone Series. To date the Wright Aeronautical Corporation has produced over 25,000 engines of which over 11,000 were of the radial aircooled type.

Over 600 of the 1,000 h.p. Cyclones on order were scheduled for delivery to the U. S. Army for installation in the new Douglas B-18 twin engine and Boeing B-17 four-engine bombers. Others were used to power the Douglas DC-3 DST transports placed in service by American Airlines. During 1936 the Wright Aeronautical Corporation produced five distinct series of aircraft engines. They were the Wright Cyclones F and F-50 and the Wright Cyclone G Series high-powered, nine cylinder radial aircooled engines; the single-row Whirlwind series of five, seven and nine cylinders; the 14 cylinder Wright double-row Whirlwind Series, and the Curtiss Conquerors.

The Wright G Cyclone Series represented the latest aircooled aircraft engine developed by the company. Although of the same displacement (1,820 cubic inches) as the F and the F-50, the G Series engines incorporated many refinements and improvements in design principal. Among them was a new cylinder which has a cooling fin area of 2,800 square inches against 1,000 square inches in other Cyclone models. Advancement in foundry technique in the Wright Aeronautical foundry, made possible the casting of cooling fins on the G cylinder head as closely spaced as the teeth on a comb and nearly two inches in depth over the combustion chamber. Cylinder barrels were of Nitralloy steel, nitrided to obtain a cylinder bore with a surface with three times the wear resistance of ordinary heat-treated cylinder barrels. Five large nitriding furnaces were installed to accommodate the daily output of Cyclone G cylinders. More accurate fuel control and the improved cylinder heads on the G Cyclone engine permitted a rating of 1,000 h.p. at take-off with a weight in certain models of 1.07 pounds per horsepower and fuel consumption of .43 pounds per horsepower at cruising speed.

Other features of the design and construction of the G Series Cyclones were automatic lubrication of the valve gear from a built-in system devoid of all external lines or tubes, mechanism for the operation of two-position hydro-control and constant speed propellers, an accessory section provided with the driving mechanism necessary to meet all of the requirements of modern military and civil transport service, the dynamic damper counterweight which counteracts torsional vibration at all crankshaft speeds and removes all restrictions in the operating range, full pressure baffling of the cylinders, improved oil seals and refinements in the supercharger and induction systems to increase altitude performance.

The G Cyclone was produced in four geared models and their direct drive counterparts. These were the Cyclone GR-1820-G1 rated at 940 h.p. for take-off, 825 h.p. at sea level, and 850 h.p. at 3,000 feet; the Cyclone GR-1820-G2 rated at 1,000 h.p. for takeoff, 810 h.p. at sea level, and 850 h.p. at 5,500 feet; the Cyclone GR-1820-G3 rated at 875 h.p. for take-off, and 840 h.p. at 8,700 feet; and the Cyclone GR-1820-G6 rated at 820 h.p. for take-off and 815 h.p. at 10,500 feet.

The various G Cyclone models differ only with respect to the amount of supercharging applied. The G-1 has a blower gear ratio of 5.95 to 1; the G-2 a blower ratio of 7 to 1; the G-3 a blower ratio of 8.31 to 1 and the G-6 a blower ratio of 8.83 to 1. All the G Series engines are of the nine-cylinder radial aircooled type and have the following characteristics: bore, 6.125 inches; stroke, 6.875 inches; compression ratio, 6.45 to I; diameter, 54 1/4 inches; length, 43 1/4 inches; dry weight (geared) 1,163 pounds, (direct drive) 1,068 pounds.

The F-50 Series Cyclone was produced in four direct drive models and their geared counterparts. These were the Cyclone R-1820-F52 rated at 890 h.p. for take-off, 745 h.p. at sea level, and 775 h.p. at 5,800 feet; the Cyclone R-1820-F53 rated at 785 h.p. for take-off, 685 h.p. at sea level, and 745 h.p. at 9,600 feet; the Cyclone R-1820-F54 rated at 655 h.p. for take-off, 605 h.p. at sea level, and 690 h.p. at 15,300 feet; and the Cyclone R-1820-F56 rated at 785 h.p. for take-off, 695 h.p. at sea level, and 755 h.p. at 11,300 feet.

Like the engines of the G Cyclone Series, the models of the F-50 Series are identical except for the amount of supercharging applied. All are nine-cylinder radial, aircooled engines. The F-52 has a blower gear ratio of 7 to 1; the F-53, a blower gear ratio of 8.31 to 1; the F-54 a blower gear ratio of 10 to 1, and the F-56, a blower gear ratio of 8.83 to 1. Characteristics common to all F-50 models are: bore, 6.125 inches; stroke, 6.875 inches; compression ratio, 6.40 to I; diameter, 54 1/8 inches; dry weight, (geared) 1,070 pounds, (direct drive) 975 pounds.

This seven-cylinder model has ratings of 235, 250, 285 and 320-350 horsepower.