Air Engine Control Principles270VDirect Current Power Supply
Basic Requirements for Aviation Engine Control Systems:
Jinfei discusses maximizing the potential of the engine itself when external flying conditions change, increasing engine thrust to high levels when acceleration is needed, and adjusting the fuel consumption to low during cruising to ensure long-duration endurance.;
The engine ensures stable operating parameters during slow-speed or high-power operations, and the adjustment process must be sensitive during transient states.
Prevent engine surge and excessive exhaust temperatures under various flight conditions. During ground testing, utilize28VDirect current or270VDirect current and400HZPower Supply Communication. The control system of modern aviation engines is primarily used to control the fuel supply to the combustion chamber, thereby regulating other operating parameters of the engine, such as speed and thrust. Its structure is large and complex.
