My FAA handy dandy bible says that alternators for light airplanes are of the constant voltage type. Airplane alternators being more or less the equivalent of car/truck alternators.
Tests in my laboratory seem to indicate that the output voltage is being held constant as an electrical load is applied and removed. See photos below.
Would you folks agree that boat/car/truck/airplane alternators are doing what they can to maintain a constant voltage? Reason why I ask is that a somewhat reputable authority (or so I thought) said they are not constant voltage.
Tests in my laboratory seem to indicate that the output voltage is being held constant as an electrical load is applied and removed. See photos below.
Would you folks agree that boat/car/truck/airplane alternators are doing what they can to maintain a constant voltage? Reason why I ask is that a somewhat reputable authority (or so I thought) said they are not constant voltage.
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