Automatic matching control method for variable propeller pitch rotorcraft accelerator propeller pitch
A control method, rotorcraft technology, applied in the direction of control starting method, rotorcraft, motor vehicles, etc., to achieve the effect of increased margin, good engine speed, and reduced vibration
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[0031] Such as figure 1 Shown, a kind of variable-pitch rotorcraft throttle pitch automatic coordination control method comprises the following steps:
[0032] Step 1. After the aircraft takes off, detect the current pitch and the output speed of the engine through the speed sensor. Pitch Relationship Table", and estimate the current lift through these two data:
[0033] L=f(ω,α);
[0034] In the formula, ω is the engine output speed; α is the pitch; L is the generated lift;
[0035] Through the function relationship and the actual measurement of the currently used engine, a table of the relationship between the rotational speed and the pitch is made. The relationship table is roughly as follows
[0036] Rotation speed (r / min)\propeller pitch (degrees)
0
1
…
1000
Xx
xx
…
1200
Xx
xx
…
…
….
…
…
[0037] The current lift force can be obtained by interpolation through this table, and the interpolation ope...
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