Flywheel energy can, in principle, be converted into mechanical energy by the spinning rotor blades. This is shown in Figure 1. The two axes in the figure are a, the speed (in radians per hour), and b , the angular displacement (in radians per second). The right-hand side in the figure is the rotational axis. For the rotational axis (b), the rotational velocity is equal to the rotational acceleration. Equation (22) for the free energy will be obtained by replacing the rotational velocity by rotational acceleration in order to make the equation equivelant to the one for rotational velocity. The power of the rotational momentum will be calculated as (22)Where e is the force of gravity, l the rotational diameter and K the rotational mass. If the rotational inertia is less than l, then a negative power will be required. So the power will vary according to the amount of rotational inertia. The energy used in the equation (22) must be equal to the rotational inertia times the torque produced by the rotational inertia. As can be seen, the power necessary to convert the mechanical energy generated by the torque into kinetic energy is equal to:where Pis the rotational diameter; f is the angular momentum; k b is the rotational mass. It can be seen that the energy used in the equation (22) is equal to the kinetic energy and rotational mass times the torque produced by the rotational inertia. Thus to obtain the free energy, one must find the rotational momentum. If the rotational mass is relatively small, a large power of the rotational inertia can be obtained by subtracting the rotational mass from the rotational velocity. Thus the rotational mass is less than the rotational velocity and hence a negative power of the rotational inertia is obtained. Figure 3:

Turbine energy. In Figure 3, the turbine energy can be calculated as (23) The power is obtained by multiplying the rotational momentum of the turbine blades of the thrust-producing rotor with the rotor rotational inertia with a second term to determine the torque produced by the rotational inertia. The torque is obtained from Equation (23). The torque is equal to:where Kis the rotational speed of the turbine blades; l is the rotational diameter of the rotor blades; N is the number of rotating blades; n, p, or q are numbers of rotational stages; and m is the rotor mass. The rotational

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