

RECOMMENDATIONS
FOR DESIGNING
Basic
formulas are received in the assumption, that working moment of Ìï
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 ÌÏ 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 Ì0 =2000êã. 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 ò – 40kg, its fluctuations radius r =
0,001ì. 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 20000Í 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 êgm/ñ is used in
a drive. Such moment creates a gyroscope having mass1kg, radius of inertia
 0,05ì and frequency of rotation400 ãö. 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, Ì0
full cosmolet mass, F – inertor traction (from the formula 10)
For example, the distance from the Sun up to Jupiter (S=778,3
•109ì) 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 startup 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  10êã. 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 106 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 gaseousvortex 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.

