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The business field of Hatz Components produces high precision engine and drive elements such as conrods, crankshafts, casings and rotating and control parts for engine manufacturers throughout the world. The focus here is on commercial vehicle, automobile, motorcycle, agriculture and printing machine industries as well as the branches of racing ...
This category lists multi-engine passenger airline accidents involving loss of all engines in flight and subsequent gliding flight. Causes of these rare situations have included fuel exhaustion or starvation, multiple bird strikes, volcanic ash, extreme weather and hijacking.
Print/export Download as PDF; Printable version; In other projects ... Help. Pages in category "Engine problems" The following 13 pages are in this category, out of ...
Diesel engine runaway is an occurrence in diesel engines, in which the engine draws extra fuel from an unintended source and overspeeds at higher and higher RPM, producing up to ten times the engine's rated output until destroyed by mechanical failure or bearing seizure due to a lack of lubrication. [1]
Compressor stalls were a common problem on early jet engines with simple aerodynamics and manual or mechanical fuel control units, but they have been virtually eliminated by better design and the use of hydromechanical and electronic control systems such as full authority digital engine control. Modern compressors are carefully designed and ...
The Hatz Classic is a development of the Hatz CB-1. The major differences from the CB-1 are that the fuselage is more rounded, it mounts a larger engine, it uses push-pull tubes instead of control cables for the ailerons and elevators and it has aluminum ailerons. As well the seats are relocated in the fuselage and reclined to provide more leg ...
Pogo oscillation is a self-excited vibration in liquid-propellant rocket engines caused by combustion instability. [1] The unstable combustion results in variations of engine thrust, causing variations of acceleration on the vehicle's flexible structure, which in turn cause variations in propellant pressure and flow rate, closing the self-excitation cycle.
The Daihatsu 2HA engine is a horizontal engine that was developed for Daihatsu Bee (1951-1952). The 2HA engine was available in two version, 540 cc and 804 cc. The earlier version was a 540 cc, with output 13.5 PS (13.3 hp; 9.9 kW) and the larger 804 cc available shortly, with output increased to 18 PS (17.8 hp; 13.2 kW). [17]