Australian tractor biplane designed and constructed by Douglas Sloane. The engine was also of his own design and one of the things that held him up in his attempt to fly. Despite the stage of progress seen in this photo, the plane was eventually covered. It was towed behind a car to give it extra power but the engine just didn’t have the muscle. However the plane did manage a short hop at “Dick’s Plain” swamp in late April 1912.
Douglas Sloane (1890-1917) was killed in an RE8 of 69 (Australian) Sqn RFC headed for France on August 21, 1917. With it was 2AM Sloane (observer/gunner), piloted by 2nd Lt FG Shapira. Having some engine trouble, they landed to have it rectified. This was done and after lunch they set off again. The plane reached about 600 feet when the nose suddenly dropped and it went into a spin from which it never recovered. Shapira and Sloane were the first active service casualties of the squadron.
Designed by Charles H Day and originally known as the Sloane H-2, the Standard H-2 was built by the Standard Aircraft Corporation. Modified from Sloan H-2, three were built by Standard Aircraft Corp, AS82 to 84.
An early American Army reconnaissance aircraft, ordered in 1916, it was an open-cockpit three-place tractor biplane, powered by a 125 hp (90 kW) Hall-Scott A-5 engine. It had swept-back wings and originally had mid-wing ailerons. Only eight were built; AS82 to AS89.
An improved version, the H-3, with the same engine, swept-back, and equal-span wings, earned an order for eight aircraft, AS85 to 93, while the Navy ordered four with floats as the H-4H, 137 to 140.
These, like J-1 and Curtiss JN-4, were the basis of countless modifications as surplus civil aircraft after the war.
H-4H seaplane
Two Standard H-3s were sold by the US Army to Japan, where a further three were built by the Provisional Military Balloon Research Association (PMBRA) in 1917, powered by 150 hp (110 kW) Hall-Scott L-4 engines. They were used as trainers between May 1917 and March 1918, although they were considered dangerous.
H-3 Engine: 1 × Hall-Scott A-5, 135 hp (101 kW) Wingspan: 40 ft 1 in (12.22 m) Wing area: 532 sq ft (49.4 m2) Length: 27 ft 0 in (8.23 m) Empty weight: 2,500 lb (1,134 kg) Gross weight: 3,300 lb (1,497 kg) Fuel capacity: 68 US gal (57 imp gal; 260 L) Maximum speed: 84 mph (135 km/h, 73 kn) Stall speed: 46 mph (74 km/h, 40 kn) Endurance: 6 hr Time to altitude: 10 minutes to 3,400 ft (1,000 m) Crew: 2
1913: (John Eyre) Sloan Aeroplane Co Inc, Company funded by Thomas A Edison. 1733 Broadway, New York NY. USA
In 1913 Déperdussin were manufactured under US license.
Built a military biplane with unusual back-swept wings. Believed to have built aircraft under subcontract for the U.S. government.
1916: Sloan Aero Corp
Sloan Aircraft Co, Bound Brook NJ. USA
On 12 May 1916, Sloane Aeroplane Co. was taken over involuntarily by the newly-formed Standard Aero Corp., which had possession of a majority of Sloane Aeroplane Co.’s shares, and Sloane’s assets became the nucleus of Standard Aero Corp.
The NY Times, 1 May 1917, revealed that John Sloane, who held 26,500 of the 50,000 shares in Sloane Manufacturing Co., had provided his shares as collateral to the Mitsui Co., the large Japanese banking conglomerate, in order to borrow funds from them to finance the manufacture of aeroplanes for the Russian government. Sloane alleged that Mitsui, rather than waiting to be repaid from the profits of this venture, transferred Sloane’s stock shares to Standard Aero Corp., which then stripped the Sloane Co. of its assets and business. Mitsui contended that after Sloane had borrowed funds from Mitsui and been unable to repay the loan, Sloane had adjusted the matter by turning over his stock in payment.
Between 1910 and 1912, American expatriate Jacques-Jules Sloan built a series of biplanes he called Bicurves in his small workshop in the Paris suburb of Charenton-le-Pont. The Bicurve’s fuselage, tail and landing gear were similar to those found on French Blériot monoplanes of that period. As initially constructed, the fuselage terminated in a movable rudder, without a fixed fin, and fixed horizontal stabilizers of flat section without any airfoil. The elevators were originally mounted ahead of the fuselage on struts, in canard fashion. Those struts were subsequently removed and the elevators relocated to a more conventional position at the tail, hinged at the trailing edge of the horizontal stabilizers.
It was in its wing cellule that the Bicurve differed markedly from any of its contemporaries, or from any subsequent biplane designs. The Bicurve’s lower wing attached to the upper fuselage longerons. The lower wing, which was reminiscent of that found on contemporary Antoinette monoplanes, was designed with marked dihedral, transforming to anhedral near the tips, and was fitted with conventional trailing-edge ailerons. The upper wing, on the other hand, was deeply arched, both in section and in span, so much so that the tips curved sharply downward and were attached by struts to the lower wingtips.
The initial version of his Bicurve was fitted with two propellers driven by a single engine via chains and gears. An examination of photographs of the airplane provides a clue as to why he added the additional weight and complexity of such a drive system. The two propellers were clearly arranged to turn in opposite directions, suggesting that Sloan was trying to further improve the airplane’s handling characteristics by canceling out the torque effect imparted by a single propeller.
Lateral control was achieved not by wing-warping but by means of fins installed on the trailing edge of the lower wings, just before the wingtips drooped. Due to the airplane’s inherent natural stability, their surface area was quite small. Vertical control could be achieved any of two ways, depending on the pilot’s preference. One method involved using two elevators, one at the front coupled with another at the rear, acting simultaneously by opposite bearings. This control system was very effective, but some pilots preferred to use only the rear elevator.
The main undercarriage consisted of two forward-facing skids carrying two pairs of wheels, which were equipped with dampers and mounted on a universal joint that could absorb shocks from rough field landings. The undercarriage was secured, as with the fuselage itself, by means of special aluminum fittings. The main gear was complemented by either a rear skid or wheel.
The original Bicurve had a wingspan of 35 feet 11 inches, a length of 37 feet 1 inch and wing area of 161 square feet. Maximum speed was recorded as 46 mph.
Sloan seems to have built and flown at least three different versions of the Bicurve between 1910 and 1912, and it is also reported to have been powered at various times by at least two different engines: a 35-hp Labor-Aviation and, later, a 50-hp Gnome. As was the case with numerous early airplanes, however, there is little documentation as to whether the various Sloan Bicurves were new builds or simply improved versions of the same airframe. For example, while the original airplane had twin propellers driven by a single engine and elevators mounted in front, other versions featured a single propeller and conventional tail-mounted elevators.
A photograph exists of the Bicurve exhibited by Sloan & Company at the Exposition de Locomotion Aérienne in Paris between October 15 and November 3, 1910. In spite of that publicity, the airplane was not a financial success and the design proved to be a dead end. Nevertheless, unlike many strange-looking early airplanes, the Sloan Bicurve actually flew, and apparently flew well. Motion picture footage still exists showing the machine taking off and landing, and it appears to do so quite smoothly.
Originally designed by Chuck Hamilton and prototyped in 1992, the Genesis is a two-place, roomy, side-by-side aircraft for a 2009. Available with a choice of dual yoke controls or center stick, and equipped with the standard Rotax 582, in solo configuration take-off roll is 100 feet, with a 250 foot landing roll and a climb rate of 1,000 fpm. The Genesis base 2009 Price also included dual 10-gallon wing tanks to provide for four hours endurance.
The series were originally produced by Innovation Engineering of Davenport, Iowa and then by SlipStream International of Wautoma, Wisconsin.
Innovation Engineering Genesis
The XL version has extended wings. The kit price in 1997 was US$12,900, including engine.
Optional are “Shark Series” amphibious floats. Computer designed to reduce drag and to provide for rapid hydroplaning, the “Shark Series” floats are built to withstand impacts in excess of 3,000 lbs. per square inch and are rated for up to 1,600 lbs.
With an average empty weight of 565 lbs., the Genesis equipped with the standard Rotax 582 has a useful load of 635 lbs. With any of the larger optional powerplants, and the gross weight capability increases to 1400 lbs., providing for a larger useful load. The HD option has a “beefed up” airframe capable of safely carrying up to 1600 lbs. and a useful load envelope of over 800 lbs.
The Genesis typically will take about 400 hours to complete. All of the welding and fabrication is done before the kits leaves the factory, and the manuals are written with step by step instructions, and numerous photos, illustrations and CAD drawings.
The Genesis airframe sold for US$11,073 in 2009, and includes all of the flight surfaces, fuselage, fiberglass enclosure, landing gear, wheels and tires, control system and doors. Among the options are custom hydraulic brakes, cabin heating, floats, wheel pants, strut fairings, complete instruments packages, and finishing systems.
A complete Genesis aircraft, ready to fly, typically runs from $21,000 to $32,000, depending on your powerplant and choice of options.
In 2001 the Slipstream Industries new trigear Dragonfly Mak III Millennium kit plane was ready for flight testing. Improvements included Hammerhead landing gear, redesigned seatbacks, and a raised panel to accommodate larger pilots.