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In 1910, Hatz began to produce hot bulb engines for stationary use. Based on that engine, the first Hatz water-cooled diesel engine, the H-series, was developed (max. power: 6 kW; engine speed: 500 rpm; weight: 430 kg). [4] Three years later, a new plant was built at the present location and Hatz started to export engines to South America.
Jacobs was the first to start making engines using forged aluminum alloy pistons, sodium-filled exhaust valves, and magnesium alloy crankcases. The L-4 was used mostly on the Cessna Bobcat, Cessna 195, and Stearman Kaydet. Due to the tendency of the L-4 engine to vibrate heavily at low rpm, it was given the nicknames Shakin' Jake and Shakey ...
John Hatz designed the CB-1 in 1968 as a smaller version of a Waco F series biplane. The CB-1 is a tandem dual-control two-seat biplane with fixed tailwheel landing gear and powered by a variety of nose-mounted small engines. Steel tube fuselage and tail with wooden wings. Plans and kits of parts for the CB-1 are available for amateur construction.
After the war, the French designed and built the AMX-50 series of armoured fighting vehicles, which used a 1000 hp Maybach engine with rear drive, as had been intended for the E-50 and E-75, whilst the idea of external Belleville washer suspension - which was also developed with the Entwicklung series in mind - resurfaced on the Swiss Panzer 61.
The cabin width is 26 in (66 cm). The acceptable power range is 150 to 160 hp (112 to 119 kW) and the standard engine used is the 150 hp (112 kW) Lycoming O-320 powerplant. [1] [2] [3] The Hatz Classic has a typical empty weight of 1,050 lb (480 kg) and a gross weight of 1,700 lb (770 kg), giving a useful load of 650 lb (290 kg).
The Kelly-D is a development of the Hatz CB-1, but with more wingspan and fuselage length, and with more cockpit space for larger pilots. It features a strut-braced biplane layout, two seats in separate tandem open cockpits with individual windshields, fixed conventional landing gear and a single engine in tractor configuration.
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [e] Oxidiser: fuel ratio
The base-line direct drive production version. [2] R-755A2 300 hp variant. R-755A3 Similar to A1 but with Scintilla magnetoes. R-755B1 De-rated version of the R-755A to drive a fixed pitch airscrew. [2] R-755B2 De-rated version of the R-755A to drive a variable or controllable pitch airscrew. [2] R-755E Up-rated engine with reduction gearing ...