Had close Fiat links (like Ansaldo and several other Italian companies), and its S.I.A.7 and 9 series of two-seat reconnaissance- bomber biplanes, dating from 1917, were designed by Umberto Savoia and Rodolfo Verduzio. Structural weakness attributed to both, and Type 9 was rejected by Italian Army on this account, though accepted by Navy.
World War 1
Societa Idrovolanti Alta Italia / SIAI
Italy
Forerunner of the Siai-Marchetti organization (see Siai-Marchetti Societa Per Azioni). Founded 1915 by Luigi Cape at Sesto Calende, with a seaplane base on Lake Maggiore. As Idrovolanti Savoia built FBA flying-boats under license. Name “Savoia”had a geographical and historical connotation (House of Savoy), and after the war new flying-boats were known by the name Idrovolanti Savoia, or Savoia. These achieved early distinction, notably in the 1920 Schneider Trophy contest. Names Savoia and Marchetti were linked in 1922, when Alessandro Marchetti became technical director of company renamed Societa Idrovolanti Alta Italia—Savoia-Marchetti. In 1925 the company gained publicity when an S.16ter was flown to Australia and Tokyo and back to Italy by Francesco De Pinedo. Famous types included the twin-hulled S-55 which, though first flown in 1924, is remembered chiefly for General Balbo’s mass-formation flights of 1930 and 1933. Special long-range landplane S-64 broke world’s duration and distance records in June 1930. Initials S. M. for type numbers were not commonly applied until later, and then particularly in association with fast 3-engined civil and military types. Most famous was S.M.79 bomber and torpedo bomber of Second World War. Civil types included the record-breaking S.M.75 of 1939. Last Second World War aircraft was S.M.91 twin-boom fighter-bomber, but S.M.84 bomber served as transport until 1948.
Sloane H-2 / Standard H-2 / H-3 / H-4H

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.

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-2
Engine: 125hp Hall-Scott A-5;
Wingspan: 40’1″
Length: 27’0″
Speed: 84 mph
Range: 350 mi
Seats: 2
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
Sloane H-1
The 1916 Sloane Aircraft Company H-1 was a two-place, open cockpit biplane designed by Charles H Day.
Engine: 180hp Hisso E
Seats: 2
Sloane Aircraft Company Inc
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.
Slesarev Sviatogor

A “Sviatogor” built by Slesarev around 1913-1918. It seems to have been powered with two 300 hp Mercedes engines.
Engines: two 300 hp Mercedes
Wingspan: 36 m
Wing area: 180 sq.m
Length: 21 m
Est max speed: 100 km/h
Ceiling: 2500 m
Weight: 6500 kg
Sikorsky S-22 Ilya Mourometz

In August 1913 a military Voisin biplane broke up in the air over the airfield and its engine fell onto the Grand. Sikorsky subsequently redesigned the aircraft as the Ilya Muromets which was even bigger. Its wing span was 10 ft greater than that of Le Grand and it weighed 10,000 lb.
A four bay biplane with braced extensions of upper wings. With two spar wooden wings and wooden fuselage, all fabric covered, ailerons were fitted to the top wings.
The first flight of Ilya Mourometz No. 1, in January 1914, was made with a skid undercarriage. On 11 February 1914 this machine set a new world record by carrying aloft 16 people and a dog. A familiar picture of it shows the big biplane landing with two fur-coated passengers taking a stroll along its fuselage top promenade. Five months after the first flight, it flew several times as a seaplane.

With the threatened outbreak of hostilities ten were purchased by the Russian Army for military trials.
The Ilya Muromets went into production as a heavy bomber for the Imperial Russian Air Service Eskadra Vozdushnykh Korablei (Squadron of Flying Ships) built at the Russo-Baltic Wagon Works. Seventy three were built, and few of these production aircraft were identical, improvement and developing being continuous, and short engines meant they were flown with a variety of powerplant which, in some cases, involved a mix of engines on one aircraft.
The first version used in combat was the Type B, with Salmson engines of 135-200 hp and an armament of only two machine guns. The largest of the series was the Type IMYe2, with a wingspan of 34.50m and a gross weight of 7,000kg.
After experimenting with various types of armament and bomb racks it was found to be too slow and with limited altitude for offensive purposes. Sikorsky designed a lighter version, the Il’ya Muromets Type V, and deliveries of these began in early 1915.

Sikorsky S-22 Il’ya Murometz Article
They were so effective on more than 400 bombing raids against Germany and Lithua¬nia in 1915 that Great Britain and France sought permission from Czar Nicholas II to produce the design under licence, though nothing came of the scheme before the 1917 Russian Revolution sent Sikorsky fleeing to the United States.
They made 400 successful raids for the loss of only one aircraft, shot down by German fighters after it destroyed three of the enemy aircraft.
Engines: 4 x Argus, 100 hp
Wingspan: 30.9/22.0 m / 101 ft 5 in / 72 ft 2 in
Length: 17.1 m / 56 ft 1 in
Wing area: 148.0 sq.m / 1593.06 sq ft
Max take-off weight: 5100 kg / 11244 lb
Max. speed: 110 km/h / 68 mph
Range: 600 km / 373 miles
Armament: 8 machine-guns, bombs
Crew: 10
Ilya Muromets E
Engines: 4 x Renault, 200 hp
Props: 2 blade
Wingspan: 102 ft 8 in
Wing area: 20050 sq.ft
Length: 59 ft 8 in
Empty weight: 10,600 lb
MTOW: 17,600 lb
Max speed: 85 mph at 5000 ft’
Endurance: 4 hr
Armament: up to 7 mg
Bombload: 1000-1500 lb
Sikorsky IM-W Ilya Muromet
Engine: 4 x Argus, 138 hp
Length: 56.102 ft / 17.1 m
Wingspan: 97.769 ft / 29.8 m
Wing area: 1345.5 sq.ft / 125.0 sq.m
Max take off weight: 9812.3 lb / 4450.0 kg
Max. speed: 67 kts / 125 km/h
Service ceiling: 12139 ft / 3700 m
Wing loading: 7.38 lb/sq.ft / 36.00 kg/sq.m
Endurance: 5 h
Crew: 5
Armament: 3-7x MG, 700kg Bomb.


Sikorsky S-17

1916
Engine: 1 x 150hp Sunbeam Crusader

Sikorsky
Igor Sikorsky
Sikorsky Aero Engineering Corporation

lgor Ivan Sikorsky was born in Kiev, Ukraine, on May 25, 1889. His father was a graduate physician and professor of psychology. His mother also was a physician but never practiced professionally. Her interest in art and in the life and work of Leonardo da Vinci stimulated her son’s early interest in model flying machines; when he was 12 years old he made a small rubber-powered helicopter that could rise in the air.
In 1903 Sikorsky entered the Naval Academy in St. Petersburg, with the intention of becoming a career officer, but his interest in engineering led to his resignation from the service in 1906. After a brief period of engineering study in Paris, he returned to Kiev and entered the Kiev Polytechnic Institute. Following a reasonably successful academic year, however, he concluded that the abstract sciences and higher mathematics as then taught had little relationship to the solution of practical problems, and he left the school, preferring to spend his time in his own shop and laboratory.
A trip through Europe in the summer of 1908 brought him into contact with the accomplishments of the Wright brothers and the group of European inventors who were trying to match their progress in flight. Returning to Kiev, Sikorsky came to the conclusion that the way to fly was “straight up,” as Leonardo da Vinci had proposed, a concept that called for a horizontal rotor. Assisted financially by his sister Olga, he returned to Paris in January 1909 for further study and to purchase a light-weight engine.
Back in Kiev in May of 1909 he began construction of a helicopter, the H-1. Its failure revealed some of the practical obstacles. Powered by a three-cylinder, 25-hp Anzani engine that drove coaxial, twin blade rotors, the H-1 shook wildly but did not have enough power to lift itself off of the ground. A second machine with a larger engine was tested in 1910, but also failed to fly. He then made a major decision: “I had learned enough to recognize that with the existing state of the art, engines, materials, and-most of all-the shortage of money and lack of experience … I would not be able to produce a successful helicopter at that time.” In fact, he had to wait 30 years before all conditions could be met.
For the time being Sikorsky decided to enter the field of fixed-wing design and began construction of his first airplane. His S-1 biplane was tested early in 1910, and, although its 15-horsepower engine proved inadequate, a redesigned airframe with a larger engine (S-2) carried him on his first short flight. The S-3, S-4, and S-5 followed in quick succession, each a refinement of its predecessor, and each adding to his piloting experience. Finally, by the summer of 1911, in an S-5 with a 50-horsepower engine, he was able to remain in the air for more than an hour, attain altitudes of 1,500 feet (450 metres), and make short cross-country flights. This success earned him International Pilot’s License Number 64.
The subsequent S-6 series established Sikorsky as a serious competitor for supplying aircraft to the Russian Army. Characteristically, he soon took a giant step: the first four-engined airplane, called “Le Grand,” the precursor of many modern bombers and commercial transports, which he built and flew successfully by 1913. Among its innovative features, not adopted elsewhere until the middle 1920s, was a completely enclosed cabin for pilots and passengers.
Although he was now an internationally known aircraft designer and pilot, Sikorsky decided to leave Russia for France in 1918 following the Bolshevik Revolution. On Mar. 30, 1919, Sikorsky came to New York City to begin his career anew. Initially unable to land a job with a U.S. airplane manufacturer, Sikorsky supported himself by teaching mathematics to Russian emigees in New York and giving lectures on aviation and astronomy until Mar. 5, 1923, when he received enough financing to launch the Sikorsky Aero Engineering Corp.
They set up shop in an old barn on a farm near Roosevelt Field on Long Island. Sikorsky became a U.S. citizen in 1928. From 1925 to 1926, the company produced one-of-a-kind, fixed-wing designs built to customer needs. In 1924, using junkyard parts and war-surplus materials, Sikorsky constructed his first S-29A, a twin-engine, 14 passenger design. By 1929 the company, having become a division of United Aircraft Corporation, occupied a large modern plant at Bridgeport, Connecticut, and was producing S-38 twin-engined amphibians in considerable numbers. In 1931 the first S-40, the “American Clipper,” pioneered Pan American World Airways mail and passenger routes around the Caribbean and to South America. By the summer of 1937 Pan American began transpacific and transatlantic service with the first four-engined S-42 “Clipper III” the last of the Sikorsky series, the ancestor of which had been “Le Grand” of 1913.
As the era of flying boats faded, lgor Sikorsky revived the idea of developing the helicopter. Once again he was involved in “advanced pioneering work . . . where extremely little reliable information and no piloting experience whatever were available.” By the late 1930s changing requirements for military and commercial air transport forecast the termination of the large flying boat, and Sikorsky returned to his first love, the helicopter. The essential aerodynamic theory and construction techniques that had been lacking in 1910, however, were now available. In a memo to the general manager of Vought-Sikorsky (the new name of the company) dated Aug. 10, 1938, he wrote:
“Besides having considerable possibilities as a privately owned aircraft, the direct-lift ship [helicopter] will be a very important service type for the army and navy. For the army, this type of ship would render excellent services for communication, fire control, short-range reconnoitering and bombing operations. For the navy, the ship would be extremely useful as the only aircraft that could take off and land without catapulting from any surface vessel….”
Even though an official manufacturing order had not been issued to begin work on a “new” type of aircraft, helicopter development continued throughout the fall of 1938. lgor Sikorsky and a handful of engineers and production personnel spent lunch breaks and off hours sketching, designing, fabricating and testing various components and systems for what would become known as the VS-300 (“V’ for Vought, “S” for Sikorsky and “300” for Sikorsky’s third helicopter design).
Rotor tests were encouraging enough for Sikorsky to request a meeting with Eugene Wilson, a senior vice president of United Aircraft, at which he received the go-ahead to construct a prototype helicopter. Sikorsky’s argument for building the rotorcraft had been compelling.
“So important is this development to the future of society that it becomes our responsibility to undertake it. While admittedly radical, and possibly ‘impossible,’ the helicopter is wholly rational. Like no other vehicle, it will operate without regard to prepared landing surfaces. Thus, it will free us of the serious handicap to progress imposed by fixed-wing aircraft-airport limitations. It is not competitive with the airplane, but complementary to it. If Sikorsky does not create this craft of the future, another [company] will. By training and expedence, we are best equipped to do it. And finally, unlike the airplane, the helicopter will be used not to destroy but to save lives!”
Early in 1939, with a well trained engineering group at his disposal, he started the construction of the VS-300 helicopter. As he said later, “There was a great satisfaction in knowing that, within a short period of time, good engineering along a novel line produced encouraging results.” On September 14, 1939, the plane lifted off the ground on its first flight. Its designer was at the controls; during his entire career Sikorsky always insisted on making the first trial flight of any new design himself. On May 6, 1941, in an improved machine, he established an international endurance record of 1 hour, 32.4 seconds.
Sikorsky regarded it as a useful tool for industry and air commerce but primarily as an effective device for rescue and relief of human beings caught in natural disasters, such as fire, flood, or famine. He estimated that over 50,000 lives had been saved by helicopters.
lgor Sikorsky only complained that of all his past predictions, those that he lived to regret were on the “too conservative” side.
Sikorsky retired as engineering manager tor his company in 1957 but remained active as a consultant until his death on October 26, 1972, at Easton, Connecticut. In addition to his wife (married in 1924), he left one daughter and four sons, all of whom have professional careers. Sikorsky received many honorary doctorates in science and engineering, honorary fellowships in leading scientific and technical societies in the United States and Europe, and the highest medals and awards in aviation, including the Cross of St. V1adimir from Russia; the Sylvanus Albert Reed Award for 1942 from the Institute of Aeronautical Sciences in New York; the United States Presidential Certificate of Merit in 1948; the Daniel Guggenheim Medal and Certificate for 1951; the Elmer A. Sperry Award for 1964; and the National Defense Award in 1971.
Apparently, when he checked in for a Sabena S-58 flight, Igor Sikorsky was asked if his name was spelt like the helicopter’s.
Dean C. Borgrnan, who took over as president and CEO of Sikorsky Aircraft in October 1998, said: “As we approach a new millennium, a new generation of helicopter pioneers is designing and building aircraft that will revolutionize the industry. The S-92 and the RAH-66 represent two of the most advanced helicopters in the world today. Technical achievements from these two programs are being incorporated on the Black Hawk and its derivatives.”
Sikorsky also was retooling its design and engineering computers. Sikorsky selected IBM and Dassault Systemes to provide the Enovia PM (Product Manager) solution as its enterprise~wide computer system.
1923: (Igor I) Sikorsky Aero Engr Corp.
1925: Sikorsky Mfg Co, Bridgeport CT (company funded in part by composer-pianist Sergei Rachmaninoff).
1926: Leased former L-W-F plant, College Point, Long Island NY.
1928: Sikorsky Aviation Div, United Aircraft & Transport Corp, Bridgeport.
1939: (Chance) Vought-Sikorsky Div, United Aircraft Corp.
1943: Sikorsky Aircraft Div, United Aircraft Corp.
1975: Sikorsky Aircraft Div, United Technologies Corp, Stratford CT.
199?: Sikorsky Aircraft Corp, United Technologies Corp
Sikorsky was sold to Lockheed Martin in 2015
Siemen Schkukert DDr.I

The Siemens-Schuckert DDr.I was a World War I German twin engine, push-pull configuration triplane fighter aircraft.
The DDr.I was one of the first aircraft to have two engines on the same centre line, one in tractor configuration and the other a pusher. It was a triplane with constant chord, straight edged, square tipped wings of equal span and marked stagger. These were divided into two bays by pairs of near-parallel interplane struts. The upper wing was braced over the fuselage with a pair of N-form struts, leaning inward from the upper fuselage to common mountings on the wing centre line. The middle wing of the triplane was positioned at shoulder height on the fuselage and the lower wing passed unbraced below. There were short span ailerons on each wing.

The smoothly faired and contoured short fuselage of the DDr.I positioned the open pilot’s cockpit between two 110 hp (82 kW) Siemens-Halske Sh.I nine cylinder rotary engines, one with a two blade tractor propeller and the other driving a four blade pusher turning just aft of the lower wing trailing edge. The empennage was mounted on four longitudinal, tubular outrigger beams, braced with vertical and transverse members. There were no fixed rear surfaces; the single piece, constant chord elevator reached between the two upper beams and a pair of similarly shaped rudder went from the upper to the lower beams, hinged further aft than the elevator but with their lower ends on a hinged frame that moved with it. The DDr.I had a fixed conventional undercarriage, with its mainwheels on a single axle mounted on wide spread V-struts attached to the lower fuselage at the lower corner points of each engine’s firewall.
Engine control problems and a lack of stability experienced in the first flight, made on 9 November 1917, led to a crash; the aircraft was not rebuilt and plans for a more powerful version, the DDr.II, powered by two 160 hp (119 kW), Siemens-Halske Sh.III eleven cylinder rotary engines were abandoned.

Powerplant: 2 × Siemens-Halske Sh.1, 82 kW (110 hp) each
Propellers: 2/4-blade; the tractor propeller had two blades and the pusher four.
Wingspan: 10.9 m (35 ft 9 in)
Wing area: 30 m2 (320 sq ft)
Length: 5.8 m (19 ft 0 in)
Empty weight: 680 kg (1,499 lb)
Gross weight: 910 kg (2,006 lb)
Crew: One
Armament: 2×7.9 mm (0.311 in) calibre LMG 08/15 (Spandau) synchronised machine guns
