A new instrument for fuel consumption measurement in light aircraft and motorgliders

P. Morelli, P. Nuccio
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Abstract

An original instrument for fuel consumption measurement in reciprocating intenal combustion spark ignition engines for light aircraft and motorgliders has been developed and built. It is based on the detection of two parameters. the engine rotational speed and the manifold pressure. The aim of the instrument is to provide a "fuel consumption index" which can be utilized both in "Economy Air Race" competitions and during cruising flight. The instrument is not intended to replace the usual onboard fuel level gauge, but could be used to integrate the flight information with the instantaneous fuel consumption or even with the cruising range indications. Some results of fuel consumption measurements, from both computer simulation and experimental tests, are first presented and then discussed. These were obtained with the instrument installed on the engine during bench tests. Some flight tests were then carried out with the instrument installed on a light aircraft in order to evaluate the instrument response under real operating conditions. The first results thus obtained encourage further development of the instrument.
一种用于轻型飞机和摩托艇燃油消耗量测量的新仪器
研制了一套用于轻型飞机和摩托车用往复式内燃机火花点火发动机油耗测量的独创仪器。它是基于两个参数的检测。发动机转速和歧管压力。该仪器的目的是提供一个“燃油消耗指数”,可用于“经济空中竞赛”比赛和巡航飞行。该仪器不是为了取代通常的机载燃油液位计,但可以用于将飞行信息与瞬时燃油消耗甚至巡航距离指示相结合。首先介绍了计算机模拟和实验测试的一些油耗测量结果,然后对其进行了讨论。这些是在台架试验期间安装在发动机上的仪器获得的。然后,将该仪器安装在一架轻型飞机上进行了一些飞行试验,以评估仪器在实际操作条件下的响应。由此获得的初步结果鼓励了该仪器的进一步发展。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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