The invention discloses an electromechanical integrated reaction
momentum flywheel structure based on an
air bearing, and belongs to the technical field of
spacecraft attitude control equipment. Comprising a structure base, a rotating shaft, a porous
air bearing, a motor rotor magnetic ring, a motor
stator coil, an
encoder magnetic ring, an
encoder reading head, a bearing pressing ring, a
flywheel and a shell, the structure base comprises a bottom base, a sleeve part and a bearing installation opening, and the rotating shaft comprises a
flange, a magnetic ring installation shaft neck and a bearing installation shaft neck. The bearing installation shaft neck is arranged in a center hole of the porous
air bearing in a penetrating mode, the motor rotor magnetic ring is tightly sleeved on the magnetic ring installation shaft neck, the motor
stator coil is embedded between the sleeve portion and the motor rotor magnetic ring, a uniform gap is formed between the motor
stator coil and the motor rotor magnetic ring, and the
encoder magnetic ring is tightly sleeved on the lower end portion of the magnetic ring installation shaft neck. The encoder reading head is sleeved outside the encoder magnetic ring and is fixed with the bottom base; and a uniform gap is formed between the encoder reading head and the encoder magnetic ring. The device has the advantages of high reliability, long service life, low
power consumption and high control precision.