T/CAMS /CICEIA19-2019 Performance test method for rotary internal combustion engines used in drones
T/CAMS /CICEIA19-2019 Performance test method for rotary internal combustion engines used in drones
Basic Information
Scope
Scope: This standard specifies the test methods for the startability, power output, and economic performance of reciprocating internal combustion engines (hereinafter referred to as "engines") for drones under normal temperature and pressure conditions, with dynamometers and propellers as the loads. This standard applies to fixed-wing and rotary-wing drones equipped with spark-ignition engines with a net power of no more than 100kW. Engines with a net power of more than 100kW but no more than 150kW, rotary piston engines, and compression-ignition engines can be used as reference for application. Main technical content: Test methods for the startability, power output, and economic performance of reciprocating internal combustion engines (hereinafter referred to as "engines") for drones under normal temperature and pressure conditions, with dynamometers and propellers as the loads.