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Last update 19 november 2006





    Basic formulas are received in the assumption, that working moment of of a drive is constant. Actually, as is known, at reversers of the electric motor the value of the starting moment changes in some range. However, at any law of change of the kind of formulas remain as before. Only numerical factors before them can be changed in appropriate way.
Mechanical devices have big inertia. Even fluctuation frequency of 50Hz is high for them. Selection of the electric motor (or its designing) for inertor on frequency properties can be carried out, using the following formulas (for =130 )
, (14)
, (15)
, (16)
Where f is subcycle frequency, t -subcycle duration. Formulas (14) - (16) are identical to formulas (8), (10), (12).

     Let's carry out numerical parameters calculation of the hypothetical flying device (cosmolet), in which inertor is used as a mover. Let full cosmolet mass is 0 =2000. For the last to overcome gravitation of the Earth and begin momentum, its inertor should develop the traction exceeding all the device weight: F> M0 g, (g is intensity of Earth surface gravitation). Imagine, that cosmolet acceleration, created by inertor, is equal to g = 10 m/c, debalance mass 40kg, its fluctuations radius r = 0,001. We find drive capacity

If drive capacity is known, traction can be calculated, for example, using the formula (10):

Small difference of settlement value starting from 20000 is connected to discrepancy in a rounding off of constant factors before formulas (only two marks after a point).
Drive subcycle frequency can be found from (14)

Debalance fluctuations frequency will be four times less than this value and equal to 97Hz.
Let the gyroscope with kinetic moment of J = 6 gm/ is used in a drive. Such moment creates a gyroscope having mass-1kg, radius of inertia - 0,05 and frequency of rotation-400 . Using the formula (13), we find a drive fluctuation angle around axis Z.

Flight time of the device in a space, according to scheme is as follows: the first half of way is momentum, the second half is braking with identical acceleration. It can be defined, using the formula:
Where S - flight distance, 0- full cosmolet mass, F inertor traction (from the formula 10)
For example, the distance from the Sun up to Jupiter (S=778,3 109) will be overcome by cosmolet for the following time:
In inertor it is possible, moreover, to carry out reversing mode, by current direction change through the electric motor winding, included in a resonant contour of the electronic generator. Efficiency of such device is high. Let us assume, that our cosmolet has such mover. Let its efficiency be = 0, 7. Then the onboard energy source should only compensate capacity losses of 30 % during the whole flight. Taking this into consideration, flight to the Jupiter will require an onboard energy reserve equivalent to burning 190kg of fuel!

     Some more recommendations for those who will want to make inertor by themselves.
At start-up of the asynchronous electric motor with capacity of some kw, its rotor is run up to nominal frequency of rotation (50Hz) approximately for 0,5 seconds. Inertor efficiency is the higher , the less is debalance fluctuation radius, that is why for r = 1 3 mm the value of tangential acceleration will make about 2m/c ?, and traction - about 20H with debalance mass - 10. It is impossible to increase acceleration of a rotor essentially in the asynchronous engine (and this is its basic disadvantage). It does not allow inertor traction to lift considerably. The engine of a direct current has much better starting properties. In all cases it is necessary to reduce the rotor own inertia moment in every possible way, to make it hollow and of greater diameter. For engine to provide curvilinear oscillatory process of debalance movement vaguely long and thus not overheat, it is necessary to observe the following condition: With an increase of the starting (braking) moment, its maximum value should not exceed the nominal (passport) moment of the electric motor.

     The further way of increasing of inertor efficiency is in using molecular and even nuclear fluctuations of a substance. In the numerical example shown above, if we preserve the same small inertor parameters and its capacity and reduce only debalance mass fluctuations radius, for example, up to value about 10-6 m (we assure the reader, that it is far from being a limit ), the mover traction will increase by order (ten times!).

     There are bases to assume, that inertor action principle actually is the universal mechanism of Nature, in particular, in transformation of energy of space (vacuum) to kinetic energy of bodies. From this point of view it is easy to explain goodness knows where from arising increase of energy in super individual gaseous-vortex and liquid heat generators (see for example, [2]).

     As we can see, inertor greatly surpasses any engine or mover in efficiency. It will enable to carry out, in particular, flights to any point of a planet in the course of few minutes and at full absence of discomfort like overloads and weightlessness. Any person will wish to have such machine at his disposal. We are sure, that already in the current century it will be applied as the basic drive in vehicles and power installations.

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