avia.wikisort.org - Engine Alfa Romeo built/designed a range of aircraft engines based on the Bristol Jupiter and Bristol Pegasus designs, designated Alfa 125 , Alfa 126 , Alfa 127 , Alfa 128 , Alfa 129 and Alfa 131 . All these essentially similar engines were mainly fitted to Italian bombers in World War II, Alfa Romeo building around 11,000 units between 1934 and 1944
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125, 126, 127, 128, 129 and 131
A 610 kW (820 hp) Alfa Romeo 128 R.C.18 from ca1939.
Type
Piston aircraft engine
Manufacturer
Alfa Romeo
First run
1930s
Major applications
Savoia-Marchetti SM.79
Number built
~11,000
Design and development
Alfa Romeo adapted the Jupiter / Pegasus (which are very closely related) to metric measurements, local materials and indigenous equipment.
Variants
Alfa Romeo 131, 9-cyl radial engine.
(The Italian engine designation system includes a suffix indicating major components or attributes. The most common were R for Riduttore - reduction gear and C for Compressore - compressor/supercharger, followed by a number indicating the rated altitude in hundreds of metres, two speed superchargers were indicated by a double figure such as 10/34).
Alfa Romeo Jupiter
The standard 313 kW (420 hp) Jupiter engine built under licence from the Bristol Aeroplane Company .
Alfa 125 R.C.10 rated at 1,000 m (3,300 ft)
Alfa 125 R.C.35 1934 485 kW (650 hp) rated at 3,500 m (11,500 ft)
Alfa 126 R.C.10 1935 Civilian version of 126 R.C.34 559–597 kW (750–801 hp) rated at 1,000 m (3,300 ft)
Alfa 126 R.C.32 rated at 3,200 m (10,500 ft)
Alfa 126 R.C.34 1935 507–582 kW (680–780 hp) rated at 3,400 m (11,200 ft)
Alfa 127 R.C.50 rated at 5,000 m (16,000 ft)
Alfa 127 R.C.55 1937 560 kW (750 hp) rated at 5,500 m (18,000 ft)
Alfa 128 R.C.18 641–717 kW (860–962 hp) rated at 1,800 m (5,900 ft)
Alfa 128 R.C.21 1938 708 kW (949 hp) rated at 2,100 m (6,900 ft)
Alfa 129 R.C.32 rated at 3,200 m (10,500 ft)
Alfa 131 R.C.14/50 1943 Two speed supercharger, rated at 1,400 m (4,600 ft) in low gear and 5,000 m (16,000 ft) in high gear.
Applications
Breda Ba.64 (Alfa125 R.C.35)
CANT Z.506A Airone (Alfa 126 R.C.10)
CANT Z.506B Airone (Alfa 126 R.C.34 / Alfa 127 R.C.50 / Alfa 127 R.C.55)
CANT Z.506C Airone (Alfa 126 R.C.10)
Caproni Bergamaschi AP.1 (Alfa126 R.C.34)
Caproni Ca.97 (AlfaJupiter)[2]
DAR-10A (prototype) (Alfa126 R.C.34)
Fiat G.12 (Alfa 128 R.C.18)
Junkers Ju 52 (Alfa126 R.C.34)[3]
Macchi M.C.94 (Alfa 126 R.C.10)
Macchi M.C.100 (Alfa 126 R.C.10)[4]
Savoia-Marchetti S.73 (Alfa 126 R.C.10 / Alfa 126 R.C.34)
Savoia-Marchetti S.74 (Alfa126 R.C.34)
Savoia-Marchetti SM.75 Marsupiale (Alfa 128 R.C.18 / Alfa 128 R.C.21)
Savoia-Marchetti S.77 (Alfa 126 R.C.10)
Savoia-Marchetti S.M.79 Sparviero (Alfa 128 R.C.18 / Alfa 125 R.C.35 / Alfa126 R.C.34)[5]
Savoia-Marchetti S.M.79-II Sparviero (Alfa 126 R.C.34)
Savoia-Marchetti S.M.79B Sparviero (Alfa 128 R.C.18)
Savoia-Marchetti S.M.81 Pipistrello (Alfa 125 R.C.35 / Alfa 126 R.C.34)
Savoia-Marchetti S.M.82 Canguru (Alfa 128 R.C.18 / Alfa 128 R.C.21 / Alfa 129 R.C.32)
Savoia-Marchetti S.M.83 (Alfa126 R.C.34)
Savoia-Marchetti S.M.84 (Alfa 128 R.C.21)
Savoia-Marchetti S.M.95 (Alfa 128 R.C.18 / Alfa 131 R.C.14/50)
Specifications (Alfa 128 R.C.21)
Data from Aircraft Engines of the World 1945[6]
Archivio Storico Alfa Romeo - Volume II[7]
General characteristics
Type: 9-cylinder air-cooled radial engine
Bore: 146 mm (5.75 in)
Stroke: 190 mm (7.48 in)
Displacement: 28.6 L (1,745.28 cu in)
Length: 1,329 mm (52.3 in)
Diameter: 1,400 mm (55.1 in)
Dry weight: 516 kg (1,138 lb)
Frontal Area: 1.54 m2 (16.6 sq ft)
Components
Valvetrain: 2 x inlet valves and 2 x exhaust valves per cylinder operated by pushrods and rockers
Supercharger : Gear-driven 1-speed, 8.8:1 ratio, supercharger
Fuel system: 1 x Mona-Hobson AVT85MC updraught carburettor with automatic boost control
Fuel type: 87 octane
Oil system: 551.6 kPa (80 psi), dry sump.
Cooling system: Air-cooled
Reduction gear: Epicyclic bevel reduction gear, 0.65:1 ratio.
Starter: Garelli compressed air starter
Ignition: 2 x Marelli MF9 magnetos, 2 x spark plugs per cylinder, fed by a shielded harness.
Power output: Take-off: 708 kW (950 hp) at 2,300 rpm with 1,000 mm (39.37 in) Hg boostMilitary: 641 kW (860 hp) at 2,300 rpm at 2,100 m (6,900 ft)Cruising: 492 kW (660 hp) at 1,800 rpm at 2,500 m (8,200 ft)
Specific power: 24.57 kW/L (0.54 hp/cu in)
Compression ratio: 7:1
Specific fuel consumption: 0.31 kg/kW/hr (0.51 lb/hp/hr) (take-off)
Oil consumption: 0.0078 kg/kW/hr (0.013 lb/hp/hr)
Power-to-weight ratio: 0.782 kW/kg (0.775 hp/lb)
See also
Comparable engines
Related lists
References
Notes
Bibliography
Wilkinson, Paul H. (1945). Aircraft engines of the World 1945 (2nd ed.). New York: Paul H. Wilkinson. pp. 288–289.
Archivio Storico Alfa Romeo - Volume II. Torino, November 1998
На других языках - [en] Alfa Romeo 125 [es] Alfa Romeo 125 La firma Alfa Romeo construyó/diseñó una gama de motores de avión basados en los diseños de los motores radiales británicos Bristol Jupiter y Bristol Pegasus , designados Alfa 125, Alfa 126, Alfa 127, Alfa 128, Alfa 129 y Alfa 131. Todos estos motores esencialmente similares se instalaron principalmente en bombarderos italianos utilizados durante la Segunda Guerra Mundial. Alfa Romeo construyó alrededor de 11000 unidades entre 1934 y 1944.[1]Alfa Romeo adaptó el diseño Júpiter/Pegasus (que están muy relacionados) al sistema métrico con materiales locales y equipos autóctonos. [it] Alfa Romeo 125 L'Alfa Romeo 125 fu un motore aeronautico radiale 9 cilindri a singola stella e raffreddato ad aria sviluppato dall'azienda italiana Alfa Romeo Milano negli anni trenta. [ru] Alfa Romeo 125 Alfa Romeo 125 — итальянский поршневой 9-цилиндровый авиадвигатель воздушного охлаждения, разработанный
в начале 1930-х годов компанией Alfa Romeo на основе конструкций британских Bristol Jupiter и Bristol Pegasus; выпускался в модификациях AlfaJupiter, Alfa 125, Alfa 126, Alfa 127, Alfa 128, Alfa 129 и Alfa 131. Между 1934 и 1944 годами было произведено около 11000 этих двигателей, преимущественно использовавшихся на трёхмоторных бомбардировщиках итальянских королевских ВВС
[1].
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