Vertipedia is a product of the Vertical Flight Society. With data on 867 aircraft, 620 historical milestones, 597 people, and 395 organizations, Vertipedia is your "one-stop shop" for all things vertical lift.
Our latest featured aircraft for August is the Cierva W.11 Air Horse .
The aircraft was designed to provide viable heavy load lifting capability for commercial operations. It employed 3 main rotors all rotating in the same direction. Torque offset was provided by thrust components from the 3 rotors through built-in shaft tilt. The aircraft had a semi-monoquoque structure, a single engine, and a long-stroke undercarriage (5ft) to cope with high rates of descent. A description of the aircraft and its characteristics can be found in the following references,
Source: "The Cierva W-11 Air Horse", J. Gordon Leishman, VERTIFLITE Spring 2003, Page 52
Source: "Discussing the Helicopter", FLIGHT Staff, FLIGHT, December 2nd 1948, Pages 665-668
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Aircraft dimensions
The layout section for an aircraft includes both 'Overall' and 'Airframe' dimensions. The overall dimensions define the 'box' the rotorcraft would fit into with rotors turning. The airframe dimensions are those of the airframe structure alone minus the rotors (with a few exceptions stated in the aircraft notes). In both cases the aircraft is assumed to be ready for flight. If the aircraft can be folded, these external dimensions are not currently shown.
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