Fiat 4700
| 4700 | |
|---|---|
| Type | |
| National origin | Italy |
| Manufacturer | Fiat Aviazione |
| First run | 1960 |
| Major applications | Fiat 7002 |
| Developed from | Fiat 4002 |
The Fiat 4700 was an Italian turbo-generator developed by Fiat Aviazione under contract to the Italian Defence Ministry and used to power the experimental Fiat 7002 helicopter.[1]
Contents
Design and development
The Fiat 4700 was developed to provide power in cold-jet driven helicopters.[1] The 4700 was a turbo-driven air compressor driven by the primary engine, a turbojet engine based on the Fiat 4002.[1] The compressor and primary engine are mechanically independent.[1] The engine is mounted vertically to reduce the length of the compressed-air ducts to the rotor.[1] The engine was used on the Fiat 7002 helicopter which first flew on 26 January 1961 where the Fiat 4700 was used to power the cold tip-jets on the two-blade rotor.[2]
Applications
Specification
Data from Jane's All the World's Aircraft 1962-63.[3]
General characteristics
- Type: Gas generator
- Length: 1,300 mm (51.18 in) (height)
- Diameter: 612 mm (24.09 in)
- Dry weight: 152 kg (335.10 lb)
Components
- Compressor: Single-sided centrifugal flow + gas generator single sided centrifugal flow compressor driven by the free power turbine
- Combustors: Annular with 16 burners
- Turbine: 1-stage axial flow (gas trubine power) + 1-stage axial flow free power turbine (Gas generator power)
- Fuel type: Aviation kerosene to MIL-F-5624 (JP-4)
- Oil system: Re-circulating pressure system with one pressure pump adnthree scavenge punmps, oil grade DERD 2479.
Performance
- Maximum power output: 454.88 kW (610 hp) (gas hp for take-off), 376.58 kW (505 hp) (ghp max continuous)
- Overall pressure ratio: 4:1
- Air mass flow: 5.1 kg (11.24 lb)/sec at 25,000 rpm at sea level, 3.34 kg (7.36 lb)/sec (max continuous)
- Power-to-weight ratio: 2.99 kW/kg (1.82 hp/lb
See also
- Comparable engines
- Related lists
References
Notes
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