Detonation analyzer for piston engine

Measuring and testing – Engine detonation – Combustion signal compared to reference signal varied by a...

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G01L 2322

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active

040916561

ABSTRACT:
An analyzer adapted to be mounted in a operable aircraft and including an oscilloscopic display of the detonation characteristics of each cylinder of an internal combustion engine. The signal input to the oscilloscope is derived from vibration sensors attached to the engine spark plugs. The synchronizing signal input to the oscilloscope is derived from pulses generated at the primary circuit of the engine magneto. Solid state electronic circuits are used throughout and switching provides the capability to separately study the characteristics of each cylinder.

REFERENCES:
patent: 2518427 (1950-08-01), Lindberg et al.
patent: 2534276 (1950-12-01), Lancor
patent: 2607215 (1952-08-01), DeBoisblanc
patent: 2964939 (1960-12-01), Forrest

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