The paper presents general information about the new microprocessor-based FADEC control system for the PZL-10WM engine used on the W-3 “Sokół” helicopter. It demonstrates the possibilities of using phase mapping to analyze the basic operating parameters of turbine engines. It has been proven that with the help of phase mapping, already in the qualification testing phase (and even at the preliminary testing stage), it is possible to monitor the technical condition and fine-tune the fuel systems of aircraft engines, as well as identify gas-dynamic loads that may pose a significant threat to safe operation.The propulsion system of the W-3 “Sokół” helicopter consists of two PZL-10W engines with a single-stage power turbine and a WR-3 main gearbox. The power of this engine and (…)
The article contains 19,139 characters.
Source: Logistyka Magazine