- Source: Kayaba Heliplane
The Kayaba Heliplane Type-1 (Japanese: ヘリプレーン 1型) was a gyrodyne (compound autogyro) designed by Shiro Kayaba and prototyped by Kayaba Industry in Japan during the early 1950s.
Design and development
In March 1952, Kayaba Industry began the development of the Heliplane, a Gyrodyne, which combines the advantages of autogyro and helicopter. Kayaba took advantage of experience producing the Ka-Go Ka-1 and Ka-2 autogyros, intended for reconnaissance, artillery-spotting and anti-submarine use, developed during World War II.
Kayaba received a subsidy of 2 million yen from the government of Japan for the development of the aircraft, as well as 1.2 million yen from Ishikawajima Heavy Industries (IHI) for development of the rotor-tip ramjets. The aircraft was modified from Cessna 170B. The wing was removed, and a three-blade main rotor with support structure was installed on the upper part of the fuselage. In addition, short-span fixed wings were fitted to either side of the lower fuselage. For initial testing the fixed pitch wooden propeller of the Cessna 170 was retained, but a 3-bladed variable-pitch propeller was to be fitted for flight testing. Ishikawajima had developed the Ne-0 (Japanese: 石川島 ネ-0) ramjet during the war and tested it in flight beneath a Kawasaki Ki-48-II. A development of this ramjet was envisaged as the power source for the rotor drive. At takeoff, the rotor was to be started using the tip mounted ramjet engines, then transition to an autogyro powered by the propeller engine after the ramjets were stopped.
One prototype unit was produced and almost completed in March 1954 (Showa 29), but was damaged in July 1954 during tie-down testing. Further development was cancelled before the aircraft was flown.
Specifications (Heliplane)
Data from sjac.or.jp, Handbook of Japanese Aircraft and Model Art General characteristics
Crew: 1 or 2
Capacity: 1 or 2
Length: 7.4 m (24 ft 3 in) fuselage
Wingspan: 2.74 m (9 ft 0 in) stub wings
Height: 2.83 m (9 ft 3 in)
Airfoil: NACA 2412
Powerplant: 1 × Continental Motors air-cooled 6-cylinder horizontally-opposed piston engine E-190, 130 kW (180 hp)
Powerplant: 3 × unknown rotor tip ramjet, 0.245 kN (55 lbf) thrust each
Main rotor diameter: 11 m (36 ft 1 in)
Main rotor area: 95 m2 (1,020 sq ft) three-bladed bonded metal rotor rotating at 310 rpm
Propellers: 2-bladed wooden fixed pitch propeller
Performance
Maximum speed: 170 km/h (110 mph, 92 kn) projected
Cruise speed: 120 km/h (75 mph, 65 kn) projected
Range: 360 km (220 mi, 190 nmi) projected
Service ceiling: 4,000 m (13,000 ft) projected
References
External links
Attempt at the dawn of the helicopter in our Japan Aviation Now / Modern aeronautics (rewritten draft of the 37th Airplane Symposium hosted by the Japan Aviation Space Association). 1999, November 26, 2015. Retrieved February 10 2017.
The birthplace collection / The birthplace of the jet engine in Japan. Retrieved February 11 2017.
Gas turbine gallery _ Public benefit organization The Japan Gas Turbine Society. Retrieved February 11 2017.
Kata Kunci Pencarian:
- Kayaba Heliplane
- KYB Corporation
- Gyrodyne
- Kayaba Ka-1
- Cessna 170
- Kayaba Ku-4
- Kayaba Ku-2
- Kamov Ka-22
- Fairey FB-1 Gyrodyne
- Kayaba Ku-3
