Gallaudet D-4
| Gallaudet D-4 | |
|---|---|
| Role | Navy Observation Aircraft |
| Manufacturer | Gallaudet Aircraft Company |
| First flight | 1918 |
| Introduction | 1918 |
| Primary user | United States Navy |
| Produced | 2 |
| Number built | 2 |
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The Gallaudet D-4 was an unusual biplane designed and built by Gallaudet Aircraft Company for the United States Navy. It was powered by a Liberty L-12 engine buried within the fuselage which turned a large, four-bladed propeller attached to a ring around the center fuselage. Only two were constructed, with the second being accepted by the Navy for service as an observation aircraft.
Development
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 was powered by a Duesenberg engine and first flown on 17 July 1916. 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 unconventional 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 supplied by a 360-hp Liberty 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.
Operational history
Two D-4s were built. 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.
Operators
- United States Navy
Specifications
Data from Wagner, Ray. American Combat Planes (1982), p. 118.
General characteristics
- Crew: two (pilot, observer)
- Length: 33 ft 6 in ( m)
- Wingspan: 46 ft 5 in ( m)
- Height: 11 ft 8 in ( m)
- Wing area: 260 ft2 ( m2)
- Empty weight: 4,228 lb ( kg)
- Gross weight: 5,440 lb ( kg)
- Powerplant: 1 × Liberty L-12 V-12 water-cooled piston engine, 360 hp ( kW) each
Performance
- Maximum speed: 119 mph ( km/h)
- Range: 390 miles (628 km)
- Endurance: 3 hours 30 min
- Service ceiling: 14,000 ft ( m)
Armament
- None
- Related development
- Gallaudet D-1
- Gallaudet D-2
- Aircraft of comparable role, configuration and era
- Curtiss R-6
References
- Wagner, Ray (1982). American Combat Planes, Third Edition. USA: Doubleday & Company. ISBN 0-385-13120-8.
External links
- Photos of D-4 at airminded.net. Accessed 2011-09-30.
- Photo of D-4 at earlyaviators.com. Accessed 2011-09-30.
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