| Gyrodyne Company of America XRON-I Rotorcycle | |
|---|---|
| Rotorcycle on display at the Cradle of Aviation Museum | |
| Role | Helicopter |
| National origin | United States of America |
| Manufacturer | Gyrodyne Company of America |
| First flight | 23 November 1955 |
| Number built | 10 |
| Developed from | Gyrodyne Model 2C |
| Developed into | Gyrodyne QH-50 DASH |
The The XRON-I Rotorcycle or YRON-I Rotorcycle (originally designated HOG) was a tiny, single-seat helicopter designed under contract for the U.S. Navy.[1] in the mid 1950s. It later was designed for a United States Marine Corps requirement for a small personal helicopter that would fulfill a number of roles, including observation, liaison, small unit tactical maneuvers, and which could be dropped to downed airmen behind enemy lines to facilitate their escape.[2]
Gyrodyne purchased the asssets of Bendix Helicopters in 1949, including the model 2C coaxial heicopter which provided the technology for the XRON-I. In 1951 the model 2C was demonstrated to the Navy with shortcomings noted in autorotation control. The XRON-I was demonstrated under a new Navy contract NOas 55-388-c for a lightweight single man helicopter.
Gyrodyne's design was an open-framework helicopter with coaxial rotors, which was evaluated with three different power plants (two reciprocating, one turbine).
The XRON-I uses a manually started 40hp two-cycle engine with a gross weight capibility of 500lbs. The fuselage is a simple box-beam construction. The rotor uses co-axial blades which alleviate the need for an anti-torque tail rotor. Yaw control is provided by rotor tip mounted "tip brakes" providing differential speeds between the rotors. Gyrodyne patented the control on 24 October 1954 Patent No. 2,835,331.[3] There is a small inverted V-tail for control at forward speeds. The rotors are laminated wood construction. The mast is pressure lubricated and becomes a cooling surface for oil inflight. The landing gear consists of three small wheels.[4]
The first flight was on November 1955. The two-cycle engine was prone to overheating and other engines were added to the program for testing. The Marine Corps also tested one XRON-I, and three YRON-1 protoypes.[5]
The Marine Corps eventually concluded that both the RON, and the competing Hiller ROE were too heavy and too difficult to fly and abandoned the project. The United States Navy, however, had noticed the compact size and high load-carrying capacity of the RON, and in 1960 awarded a contract to Gyrodyne to produce a radio-controlled drone version of the Rotorcycle, to be used as an Anti-Submarine Warfare (ASW) platform. Using the dynamic components of the RON, this was eventually developed as the Gyrodyne QH-50.
The Rotorcycle went on to win the prize for most maneuverable helicopter at the Paris Air Show in 1961, and was selected for a 1964 trade fair in Morocco by the United States Department of Commerce.
A 2 place enclosed "gyrocycle" commercial variant was proposed after initial tests.[6]
The Cradle of Aviation Museum in New York has a XRON-I on display [7]
General characteristics
Performance
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