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A mathematical model of a wind engine unit has been proposed as a system of coupled rigid bodies. Stability conditions of a stationary motion have been obtained by means of linearization. For the case of small blades deviation and large stiffness coefficients, we derive a stability condition in terms of the angular velocity and inertial parameters. Under additional constraints, we obtain a sufficient stability condition for admissible frontal pressure. It is proved that uniform rotation of thedoi:10.1109/romoco.2004.240648 dblp:conf/romoco/SavchenkoZ04 fatcat:rhhdq3u63vfnvgtkfzpi52nrdy