FIELD: measuring equipment.
SUBSTANCE: essence of the invention consists in determining the combustion energy of fuels using a laboratory bypass type installation, taking into account the amount and composition of the combustion products - the adiabatic coefficient k, formed during combustion under conditions close to the engine operating conditions, the mass of incoming fuel mgr into the reaction chamber, which directly depends on the mass mg of the tested fuel and the increase in pressure in the reaction chamber during the combustion of fuel assemblies.
EFFECT: increasing the reliability of the received results due to approach of the test conditions to operating conditions of the air-jet engine on the FA of the given structure.
2 dwg
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Authors
Dates
2017-06-06—Published
2016-07-21—Filed