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The Alfa Romeo 6C name was used on road, race and sports cars made between 1925–1954 by Alfa Romeo. 6C refers to a straight 6 engine. Bodies for these cars were made by coachbuilders such as James Young, Zagato, Touring, Castagna, and Pininfarina. Starting from 1933 there was also a 6C version with a factory Alfa body, built in Portello.

In the mid-1920s, Alfa's RL was considered too large and heavy, so a new development began. The 2-liter formula that had led to Alfa Romeo winning the World Championship in 1925, changed to 1.5 liter for the 1926 season. The 6C1500 was introduced in 1925 at Milan, production started 1927, with the P2 Grand Prix car as starting point. Engine capacity was now 1487 cc, against the P2's 1987 cc, while supercharging was dropped. First versions were bodied by Young and Touring.

 

In 1928, a 6C Sport was released, with a dual overhead camshafts engine. Its sport version won many races, including the 1928 Mille Miglia. Total production was 3000 (200 with DOHC engine). Ten copies of a supercharged (compressore, compressor) Super Sport variant were also made.

 

Variants:

 

6C 1500, 44 bhp @ 4400 rpm, 109 km/h (68 mph) (1925–1929)

6C 1500 Sport, 54 bhp @ 4500 rpm, 125 km/h (78 mph) (1928–1929)- 171 cars

6C 1500 Super Sport compressore, 76 bhp @ 4800 rpm, 140 km/h (87 mph) (1928–1929)

6C 1500 TF, 84 bhp @ 5000 rpm (1928–1929)

 

Wikipedia

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Museo Storico dell'Aeronautica Militare (Italian Air Force Historical Museum) – Vigna di Valle.

Campini-Caproni CC.2

 

Il Campini-Caproni CC.2 (secondo prototipo, ma primo ad essere completato) fu il primo aereo con propulsione a jet costruito in Italia, ed uno dei primi al mondo. Effettuò il primo volo nell'agosto 1940. Il giudizio sul propulsore è duplice. Da un lato esso non era tecnicamente avanzato, e neanche con elevate prospettive di sviluppo. Dall'altro, però, per la prima volta incorporava un compressore assiale a tre stadi, e, soprattutto, un post-bruciatore che costituiva un notevole avanzamento sul piano tecnico. Per questo, il Campini-Caproni ha comunque notevolmente contribuito allo sviluppo della tecnologia aeronautica.

Il Campini-Caproni esposto a Vigna di Valle è il secondo prototipo (ma primo a volare), ossia il CC.2.

 

Caratteristiche generali

- Lunghezza: 12.10 m

- Apertura alare: 14.63 m

- Superficie alare: 36.03 m^2

- Peso a vuoto: 3639 Kg

- Peso massimo: 4217 Kg

- Motore: Motoreattore Campini, composto da compressore assiale a tre stadi azionato da un motore a 12 cilindri a V Isotta Fraschini Asso L.121 RC.40 raffreddato a liquido (666 KW - 900 CV), e da post-bruciatore. Spinta (con post-bruciatore): 7.3 KN (750 Kgf)

- Velocità max: 360 km/h

  

The Campini-Caproni CC.2 (second prototype, but first to flight) was the first jet aircraft built in Italy, and the third in the world, just after Heinkel He 176 (a rocket plane that flew in June 1939) and Heinkel 178 (a turbo-jet with a centrifugal compressor that flew in August 1939). CC.2 first flew in August 1940. A technical judgment about the powerplant of CC.2 is necessarily twofold. On one hand, it was not technically advanced, because the compressor was operated by a piston engine, and not by a turbine. On the other hand, its three-stage compressor, and mainly its after-burner, were technically innovative. For this reason, the Campini-Caproni significantly contributed to the development of aviation technology.

The Campini-Caproni on display at Vigna di valle Museum is CC.2, namely the second prototype (but first to flight).

 

General characteristics

- Length: 12.10 m

- Wingspan: 14.63 m

- Wing area: 36.03 m^2

- Empty weight: 3639 kg

- Gross weight: 4217 Kg

- Maximum speed: 360 km/h

- Powerplant: Motorjet Campini, composed by 1×670 kW Isotta Fraschini Asso L.121 RC.40 liquid-cooled V12 engine (666 KW – 900 HP) operating a three-stage axial compressor with afterburner; 7.3 KN (750 Kgf) with afterburner

Variants:

 

* 6C 1750 Turismo, 46 bhp @ 4000 rpm, 109 km/h (68 mph) (1929–1933)

* 6C 1750 Sport/Gran Turismo, 55 bhp @ 4400 rpm, 125 km/h (78 mph) (1929–1932)

* 6C 1750 Super Sport/Gran Sport, 64 bhp @ 4500 rpm, 130 km/h (81 mph) (1929–1932)

* 6C 1750 Super Sport/Gran Sport compressore,85 bhp @ 4500 rpm, 145 km/h (90 mph) (1929–1932)

* 6C 1750 Gran Turismo compressore, 80 bhp @ 4400 rpm, 135 km/h (84 mph) (1931–1932)

* 6C 1750 Super Sport/Gran Sport/TF, 85 bhp @ 4800 rpm, 170 km/h (110 mph) (1929–1930)

 

(wikipedia.org)

 

Aziona il sistema di frenatura

The more powerful 6C 1750 (1752 cc actual) was introduced in 1929 in Rome. It was produced in six series between 1929-1933. Base model had a single overhead cam; Super Sport and Gran Sport versions had double overhead cam engine (DOHC). Again, a supercharger was available. Most of hte cars were sold as rolling chassis and bodied by coachbuilders such as Zagato, Touring and James Young. The 1750 was also used in racing, it won eg. the 1929 and 1930 Mille Miglia and 1930 Spa 24 Hours. Total production was 2635.

 

Variants:

 

6C 1750 Turismo, 46 bhp @ 4000 rpm, 109 km/h (68 mph) (1929–1933)

6C 1750 Sport/Gran Turismo, 55 bhp @ 4400 rpm, 125 km/h (78 mph) (1929–1932)

6C 1750 Super Sport/Gran Sport, 64 bhp @ 4500 rpm, 130 km/h (81 mph) (1929–1932)

6C 1750 Super Sport/Gran Sport compressore,85 bhp @ 4500 rpm, 145 km/h (90 mph) (1929–1932)

6C 1750 Gran Turismo compressore, 80 bhp @ 4400 rpm, 135 km/h (84 mph) (1931–1932)

6C 1750 Super Sport/Gran Sport/TF, 85 bhp @ 4800 rpm, 170 km/h (110 mph) (1929–1930)

 

Wikipedia

Kompressor / (Racer Pod)

The more powerful 6C 1750 (1752 cc actual) was introduced in 1929 in Rome. It was produced in six series between 1929-1933. Base model had a single overhead cam; Super Sport and Gran Sport versions had double overhead cam engine (DOHC). Again, a supercharger was available. Most of hte cars were sold as rolling chassis and bodied by coachbuilders such as Zagato, Touring and James Young. The 1750 was also used in racing, it won eg. the 1929 and 1930 Mille Miglia and 1930 Spa 24 Hours. Total production was 2635.

 

Variants:

 

6C 1750 Turismo, 46 bhp @ 4000 rpm, 109 km/h (68 mph) (1929–1933)

6C 1750 Sport/Gran Turismo, 55 bhp @ 4400 rpm, 125 km/h (78 mph) (1929–1932)

6C 1750 Super Sport/Gran Sport, 64 bhp @ 4500 rpm, 130 km/h (81 mph) (1929–1932)

6C 1750 Super Sport/Gran Sport compressore,85 bhp @ 4500 rpm, 145 km/h (90 mph) (1929–1932)

6C 1750 Gran Turismo compressore, 80 bhp @ 4400 rpm, 135 km/h (84 mph) (1931–1932)

6C 1750 Super Sport/Gran Sport/TF, 85 bhp @ 4800 rpm, 170 km/h (110 mph) (1929–1930)

 

Wikipedia

Compressore INGERSOLL - RAND

Killer new designs available at espressoparts.com. The folks at Espressoparts continue to innovate! The black surface treatment of the base is not only a cool look, it ads some nice grip for your thumb and index finger.

The more powerful 6C 1750 (1752 cc actual) was introduced in 1929 in Rome. It was produced in six series between 1929-1933. Base model had a single overhead cam; Super Sport and Gran Sport versions had double overhead cam engine (DOHC). Again, a supercharger was available. Most of hte cars were sold as rolling chassis and bodied by coachbuilders such as Zagato, Touring and James Young. The 1750 was also used in racing, it won eg. the 1929 and 1930 Mille Miglia and 1930 Spa 24 Hours. Total production was 2635.

 

Variants:

 

6C 1750 Turismo, 46 bhp @ 4000 rpm, 109 km/h (68 mph) (1929–1933)

6C 1750 Sport/Gran Turismo, 55 bhp @ 4400 rpm, 125 km/h (78 mph) (1929–1932)

6C 1750 Super Sport/Gran Sport, 64 bhp @ 4500 rpm, 130 km/h (81 mph) (1929–1932)

6C 1750 Super Sport/Gran Sport compressore,85 bhp @ 4500 rpm, 145 km/h (90 mph) (1929–1932)

6C 1750 Gran Turismo compressore, 80 bhp @ 4400 rpm, 135 km/h (84 mph) (1931–1932)

6C 1750 Super Sport/Gran Sport/TF, 85 bhp @ 4800 rpm, 170 km/h (110 mph) (1929–1930)

 

Wikipedia

HAMM roller abandoned near Afandou Beach, Rhodes Island, Greece. Rullo compressore HAMM abbandonato vicino ad Afandou Beach, a Rodi, Grecia.

HAMM roller abandoned near Afandou Beach, Rhodes Island, Greece. Rullo compressore HAMM abbandonato vicino ad Afandou Beach, a Rodi, Grecia.

HAMM roller abandoned near Afandou Beach, Rhodes Island, Greece. Rullo compressore HAMM abbandonato vicino ad Afandou Beach, a Rodi, Grecia.

Ik zal natuurlijk niet goed opgelet hebben, maar ik hoorde pas ongeveer een jaar geleden van het Metropole museum in Druten. Met als aanleiding de speciale Le Mans show van deze maand nu toch maar eens afgereisd.

 

Echt een aangename verrassing! Een enorme collectie, veel variatie en veel kwaliteit. Ik was er wel van onder de indruk …

HAMM roller abandoned near Afandou Beach, Rhodes Island, Greece. Rullo compressore HAMM abbandonato vicino ad Afandou Beach, a Rodi, Grecia.g

HAMM roller abandoned near Afandou Beach, Rhodes Island, Greece. Rullo compressore HAMM abbandonato vicino ad Afandou Beach, a Rodi, Grecia.

Museo Storico dell'Aeronautica Militare (Italian Air Force Historical Museum) – Vigna di Valle.

Campini-Caproni CC.2

 

Il Campini-Caproni CC.2 (secondo prototipo, ma primo ad essere completato) fu il primo aereo con propulsione a jet costruito in Italia, ed uno dei primi al mondo. Effettuò il primo volo nell'agosto 1940. Il giudizio sul propulsore è duplice. Da un lato esso non era tecnicamente avanzato, e neanche con elevate prospettive di sviluppo. Dall'altro, però, per la prima volta incorporava un compressore assiale a tre stadi, e, soprattutto, un post-bruciatore che costituiva un notevole avanzamento sul piano tecnico. Per questo, il Campini-Caproni ha comunque notevolmente contribuito allo sviluppo della tecnologia aeronautica.

Il Campini-Caproni esposto a Vigna di Valle è il secondo prototipo (ma primo a volare), ossia il CC.2.

 

Caratteristiche generali

- Lunghezza: 12.10 m

- Apertura alare: 14.63 m

- Superficie alare: 36.03 m^2

- Peso a vuoto: 3639 Kg

- Peso massimo: 4217 Kg

- Motore: Motoreattore Campini, composto da compressore assiale a tre stadi azionato da un motore a 12 cilindri a V Isotta Fraschini Asso L.121 RC.40 raffreddato a liquido (666 KW - 900 CV), e da post-bruciatore. Spinta (con post-bruciatore): 7.3 KN (750 Kgf)

- Velocità max: 360 km/h

  

The Campini-Caproni CC.2 (second prototype, but first to flight) was the first jet aircraft built in Italy, and the third in the world, just after Heinkel He 176 (a rocket plane that flew in June 1939) and Heinkel 178 (a turbo-jet with a centrifugal compressor that flew in August 1939). CC.2 first flew in August 1940. A technical judgment about the powerplant of CC.2 is necessarily twofold. On one hand, it was not technically advanced, because the compressor was operated by a piston engine, and not by a turbine. On the other hand, its three-stage compressor, and mainly its after-burner, were technically innovative. For this reason, the Campini-Caproni significantly contributed to the development of aviation technology.

The Campini-Caproni on display at Vigna di valle Museum is CC.2, namely the second prototype (but first to flight).

 

General characteristics

- Length: 12.10 m

- Wingspan: 14.63 m

- Wing area: 36.03 m^2

- Empty weight: 3639 kg

- Gross weight: 4217 Kg

- Maximum speed: 360 km/h

- Powerplant: Motorjet Campini, composed by 1×670 kW Isotta Fraschini Asso L.121 RC.40 liquid-cooled V12 engine (666 KW – 900 HP) operating a three-stage axial compressor with afterburner; 7.3 KN (750 Kgf) with afterburner

Mercedes 24/100/140 Compressore

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