The OF-2 weighed 2,061 lb (935 kg).This view of a display-quality DB 602 engine shows the four Bosch fuel injection pumps at the rear of the engine. For slow idle (as low as 300 rpm), fuel was cut from one cylinder bank.The DB 602 engine was not supercharged and had a .50 propeller gear reduction that used bevel planetary gears. The engine’s compression ratio was 16.0 to 1, and it was started with compressed air.The DB 602 had a 6.89 in (175 mm) bore and a 9.06 in (230 mm) stroke, both larger than those of the OF-2.

The lower part of the crankcase was finned to increase its rigidity and help cool the engine oil.Originally called the LOF-6, the Daimler-Benz DB 602 was a large 16-cylinder diesel engine built to power the largest German airships. There were 50 passenger sleeping berths in private cabins, with large public areas on the upper, “A” deck, with crew quarters, galley, a public bar and smoking lounge on the lower “B” deck. The engine weighed 4,409 lb (2,000 kg). The engine displaced 5,401 cu in (88.51 L).

Around 1930, Daimler-Benz* developed the F-2 engine, initially intended for aviation use. The engine was available with either direct drive or a .51 gear reduction, and weighed around 1,725 lb (782 kg). However, its capabilities will forever be overshadowed by the *Daimler-Benz was formed in 1926 with the merger of Daimler Motoren Gesellschaft and Benz & Cie.

However, both names were occasionally applied to aircraft engines in the 1930s.Rear view of the DB 602 engine on display in the Zeppelin Museum in Friedrichshafen, Germany. The F-2’s total displacement was 3,288 cu in (53.88 L), and it had a compression ratio of 6.0 to 1. Each injection pump provided fuel at 1,600 psi (110.3 bar) to four cylinders. This arrangement helped eliminate lateral movement of the cylinders and decreased vibrations. Its maximum continuous output was 900 hp (671 kW) at 1,480 rpm, and it could produce 1,320 hp (984 kW) at 1,650 rpm for 5 minutes. Its rigid structure was built of triangular-section duralumin girders (a specially heat-treated alloy of aluminum and copper, and anodized blue for corrosion protection). I have done some research on airships. Fuel consumption at normal power was .392 lb/hp/hr (238 g/kW/hr). The airship was operated by a flight crew of 40, with 12 stewards and cooks. Each pump provided cooling water to one cylinder bank. Small point, but I’m making a 3D virtual model of the ship and wanted to be accurate.As far as I can tell, the engines on the Hindenburg all rotated the same direction. Post was not sent - check your email addresses!

Fuel consumption at cruising power was 0.37 lb/hp/hr (225 g/kW/hr).The ill-fated LZ 129 Hindenburg on a flight in 1936. One question is about the direction of the counter-rotation of the props. Above the engine are the cooling water outlet pipes. Sources disagree on the gear reduction ratio, and it is possible that more than one ratio was offered. When viewed from the rear, the engines turned clockwise. The engine used fork-and-blade connecting rods that rode on roller bearings fitted to the crankshaft. The Daimler-Benz DB 604 was an X-24 engine designed to power aircraft of the Bomber B specification. The fuel was injected into a pre-combustion chamber located between the four valves in the cylinder head.

With the United States unwilling to provide helium because of Germany’s aggression, the airships used inexpensive and volatile hydrogen, as it was readily available. For instance, from the rear, port side props moving counter-clockwise; starboard moving clockwise. Four Bosch fuel injection pumps were located at the rear of the engine and were geared to the camshaft. The 50 degree angle was selected over the 45 degree angle typically used for a V-16 engine.

The DB 602 was 105.9 in (2.69 m) long, 40.0 in (1.02 m) wide, and 53.0 in (1.35 m) tall. Propeller gear reduction was achieved through bevel planetary gears.A single camshaft was located in the Vee of the engine.

The two banks of eight cylinders were positioned at 50 degrees.

Fuel was injected into the center of the pre-combustion chamber, which was situated between the four valves. The runs proved the engine could operate for long periods at 900 hp (671 kW). At the top of the arc, did the blades move outward, or inward.

Listed ratios include .83, .67, and .58.The Daimler-Benz OF-2 engine had a normal output of 700 hp (522 kW) at 1,675 rpm, a maximum output of 750 hp (559 kW) at 1,720 rpm, and it was capable of 800 hp (597 kW) at 1,790 rpm for very short periods of time. The crankcase was made of two pieces and split horizontally through the crankshaft plane. O Daimler-Benz DB 603 foi um motor a pistão desenvolvido e construído na Alemanha e usado em muitas aeronaves da Luftwaffe durante a Segunda Guerra Mundial.Refrigerado a líquido, com 12 cilindros, foi o maior motor V12 construído na Alemanha durante o conflito. The camshaft had two sets of intake and exhaust lobes per cylinder. The ship’s control station was located in a gondola below the forward part of the hull.The airship was designed by Ludwig Dürr. The recovery system would have condensed vapor into water, and the collected water would have been used as ballast to help maintain the airship’s weight and enable the retention of helium.

Designed by Arthur Berger, the Daimler-Benz DB 602 was built upon lessons learned from the OF-2, but it was a completely new engine.


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