Gallaudet’s second aircraft, the Model B monoplane flying boat, continued the arrangement of an engine enclosed in the fuselage driving remote propellers, in this case a pusher propeller behind that trailing edge of each wing panel. The Model B was flown several times during 1913 and 1914 with several different engines, but does not appear to have been particularly successful.
The 1912 A-2 Bullet was an evolution of the A-1 with a round, stringer-formed fuselage and variable-incidence wing with single-tube main spar and ribs made of aluminum tubing. Only one was built which crashed during a speed run of 110mph on 24 July 1912.
The A-1 Bullet of 1912 had a streamlined, four-sided, wood fuselage with a three-bladed prop mounted on the tail, driven by extended crankshaft from the fully-enclosed motor. It was twice as fast as biplanes of the era.
The 1926 Gallaudet 59-A of the USN had the propeller mounted amidships in the fuselage. The first flight was on 19 July 1916, piloted by Ltjg G D Murray.
In an effort to produce an aircraft with the best possible forward visibility for the observer, Gallaudet developed the D-2 into the D-4, which placed the observer in the nose, followed by the pilot, with the propeller attached to a ring that circled the fuselage behind the wings. The four blades spun around the fuselage just behind the pilot.
Power for the D-4 was a 360-hp Liberty L-12 engine buried within the fuselage, just behind the pilot. A large pontoon was mounted below the fuselage, and small outboard floats were mounted near the tips of the swept-back wings.
Two D-4 were built for the Navy (A2653, A2654). The prototype crashed during flight testing on 19 July 1918, but the second was accepted by the U.S. Navy. No further aircraft were built, as Gallaudet turned their attention to constructing Curtiss HS-2L flying boats.
Engine: 1 × Liberty L-12, 360 hp ( kW) each Wingspan: 46 ft 5 in ( m) Wing area: 260 sq.ft ( sq.m) Length: 33 ft 6 in ( m) Height: 11 ft 8 in ( m) Empty weight: 4,228 lb ( kg) Gross weight: 5,440 lb ( kg) Maximum speed: 119 mph ( km/h) Range: 390 miles (628 km) Endurance: 3 hr 30 min Service ceiling: 14,000 ft Crew: 2 (pilot, observer) Armament: None
In response to a requirement by the U.S. Navy for light floatplanes capable of being launched off catapults by ships underway, the Gallaudet Aircraft company began development of the “D-4”, based on the earlier Gallaudet D-1. The D-1 (A59) was powered by two 150 hp Duesenberg engines mounted side by side, and first flown on 17 July 1916. Following delivery of the D-1 in January 1917, the firm reorganized as Gallaudet Aircraft Corporation, and moved to Greenwich, Rhode Island.
Despite numerous mechanical difficulties the Army bought four of the improved D-2 version.
In an effort to produce an aircraft with the best possible forward visibility for the observer, Gallaudet developed the D-2 into the D-4.
D-1 Wingspan: 48 ft Length: 33 ft Gross weight: 4,604 lb Max speed: 90 mph
The Gallaudet #1 of 1911 was an open cockpit monoplane with a single float. The 125hp Emerson Aerial engine was mounted amidships turning two props, one at the nose and one at the tail.
Designed by Edson Gallaudet, only one was built, which made test flights only.
Edson Gallaudet was a grandson of Thomas Hopkins Gallaudet, specialist in education of the deaf and co-founder of what evolved into Gallaudet University in Washintgon, D.C. He earned a Ph.D. in electrical engineering in 1896 and was a physics instructor at Yale from 1897 to 1900.
The Gallaudet Kite of 1898 was built by Edson Fessenden Gallaudet, an engineer (PhD) and then working as a physics instructor at Yale, this hydro-bike kite was built to test wing-warping controlled by a system of gears and rods. Its wingspan was 11 and ½ feet, its length just over eight feet.
The original is currently on display at the Early Flight Gallery in the National Air and Space Museum.
Gallaudet worked for several engineering firms from 1900 until 1908. Then he founded Gallaudet Engineering Company in Norwich, Connecticut, and evidently wasted no time. His first airplane came a year later, with others to follow.
1908: (Edson) Gallaudet Engr Co Inc, Norwich CT., USA
His 1912 A-1 Bullet was a sleek monoplane of pusher layout. The motor, a 100-hp Gnome rotary, was enclosed in the fuselage and drove its three-blade rear-mounted prop through a lengthy driveshaft.
In 1916, Gallaudet’s D-1 floatplane optimized ship-catapult launching with its uniquely positioned propulsion. Dual Duesenberg 125-hp 4-cylinder engines were side by side amidships in the D-1’s fuselage. A four-blade propeller was in the middle as well, driven by a 6:5 spur gear and seemingly splitting the fuselage in two.
The U.S. Army bought four of its D-2 variants. A pair of D-4s followed, with the observer given the forward cockpit for a better view. The D-4 swapped dual Duesenbergs for single Liberty power. A prototype crashed in flight testing; the second one was accepted by the U.S. Navy for observation duties.
Gallaudet then turned his company’s attention to constructing Curtiss HS-2L flying boats, many serving in anti-submarine patrols during World War I.
Following delivery of the D-1 in January 1917, the firm reorganized as Gallaudet Aircraft Corporation, and moved to Greenwich, Rhode Island. Later built 5-seat biplane tourer, the Liberty Tourist, and rebuilt 25 DH-4s for U.S. Army.
Aircraft under construction at the Gallaudet Aircraft manufacturing plant at Chepiwanoxet in 1918.
A 1919 catalog for the Gallaudet Aircraft Corporation lists the Chummy Flyabout. This was a two-place land-based monoplane, again with Gallaudet-unique propulsion. Two Indian motorcycle engines, each producing from 18 to 20 hp, were mounted in the nose and drove a pair of pusher props.
Later, in 1923, Gallaudet designed and built an aircraft of all-metal construction.
Gallaudet retired in 1924, keeping scientific memberships and a low profile until his death at age 74 in 1945. His company evolved into Consolidated Aircraft, renowned for the B-24 Liberator heavy bomber and PBY Catalina flying boat.