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Eagle 20-40 H (1928) The Eagle Manufacturing Company of Appleton, Wisconsin, United States, first entered the farm equipment market in 1906 with a 32-horsepower (24 kW) tractor. In 1899 the company was located at 671 Superior St in Appleton Wisconsin. [1] In 1904 it built a production facility designed by architect Wallace W. De Long. [2]
The DW.1 was designed by Dean Wilson of the Eagle Aircraft Company of Boise, Idaho and the first example first flew in 1977. The Eagle is a single-seat agricultural biplane with tapered long-span wings, an enclosed single-seat cockpit and fixed tailwheel undercarriage.
The Eagle II was developed to take into account the changes wanted by the Swiss Army for the second batch of armoured reconnaissance vehicle it needed. It uses a different chassis and running gear, the one of the Humvee ECV, but all the equipment is the same as for the Swiss Eagle I.
A merger with the Picher Lead Company of Joplin, Missouri occurred in 1906, becoming Eagle–Picher Lead, which evolved into Eagle–Picher Industries, Inc. and finally EaglePicher Technologies. With its merger with the lead mining company owned by Oliver Picher, it was the second largest producer of lead and zinc products in the world. [ 1 ]
The Combat Integrated Releasable Armor System (CIRAS) suite of equipment manufactured by Eagle Industries is currently the new FSBE II system, and has replaced the FSBE AAVs. Prior to this, the FSBE series replaced the older Close Quarters Battle Equipment Assault Vest (CQBE AV) that had been used by Force Recon since 1996.
The Helicycle is a single-seat, semi-rigid two-bladed main rotor, helicopter powered by a Solar T62-32 engine. Manufactured by Helicycle Ventures LLC in Mesilla, New Mexico as a kit, the aircraft is intended to be assembled by the owner and is considered a homebuilt aircraft.
The Eagle has a conversion kit that allows exchanging the parachute wing for a hang glider-style wing to convert the aircraft into an ultralight trike. [ 1 ] With the parachute wing, the standard day, sea level, no wind, take off with a 50 hp (37 kW) engine is 300 ft (91 m) and the landing roll is 100 ft (30 m).