russianseg, Technika i inne p, SEG Searl Effect Generator Gyro Cell

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Experimental Research of the Magnetic-Gravity Effects.
Full Size SEG tests.
V. V. Roschin, E-mail:
rochtchin@mail.ru
S. M. Godin, E-mail:
serjio@glasnet.ru
Institute for High Temperatures, Russian Academy of Science, Izhorskaya 13/19, Moscow 127412, Russia
Abstract
In the present paper the results of the experimental research of magnetic-gravity effects are presented. Anomalous
magnetic and thermal changes within a radius of 15 meters from the researched device were measured as well.
PACS: 41.20.-q; 44.60.+k; 76.50
.+q
1. Introduction
There has been a great interest in examining non-linear effects in the system of rotating magnetic
fields. Such effects have been observed in the device called Searl's generator or Searl Effect Generator
(SEG) [1-4]. A SEG consists of a series of three concentric rings and rollers that circulate around the
rings. All parts of SEG are based on the Law of the Squares [5]. The rollers revolve around the con-
centric rings, but they do not touch them. There's a primary north-pole and primary south pole on the
rollers and a primary north-pole and primary south-pole on the concentric rings. Obviously, the north-
pole of the roller is attracted to the south-pole of the concentric rings and vice versa.
The rollers have a layered structure similar to the concentric rings. The external layer is titanium,
then iron, nylon and the last internal layer was made from neodymium. John R.R. Searl has supposed
that electrons are given off from the central element (neodymium) and travel out through other ele-
ments. Dr. Searl contends that if nylon had not been used, the SEG would act like a laser and one pulse
would go out and it would stop, build up, and another pulse would go out. The nylon acts as a control
gate that yields an even flow of electrons throughout the SEG [4].
In [4] it was shown that in the process of magnetization of the plate and rollers, the combination of
constant and variable magnetic fields for creating a special wave (sine wave) pattern on a plate surface
and rollers surface was used. The basic effects consist of the rollers self-running around the ring plate
with a concurrent reduction of weight and an increasing occurrence of propulsion. These effects come
about because of a special geometry of experimental setup. It was shown that the operation of the de-
vice in the critical regime is accompanied by biological and real physical phenomena.
Other information where similar effects are be mentioned can be found in the books,
Unconven-
tional Flying Objects
[6] and the
Homopolar Handbook
[7] which includes papers on magnetized di-
electrics. In this paper we present the experimental device the results we have obtained.
2. Description of the Experimental Installation
The basic difficulty arises in choosing the materials and maintaining the necessary pattern imprint-
ing on the plate and roller surfaces. To simplify the technology we decided to use a one-ring design
with one-ring plate (stator) and one set of rollers (rotor). It is obvious, that it was necessary to
strengthen the roller rotor near the bearings and balance the rollers well. In the suggested design, air
bearings were used which provided the minimum losses due to friction.
From the available description [1-4] it was not clear how to build and magnetize a stator with a one-
meter diameter. In order to make the stator, separate magnetized segments of rare earth magnets with a
residual induction of 1T were used. The segments were magnetized in a usual way by discharging a
1
capacitor-battery system through a coil. Afterwards, the segments were assembled and glued together
in a special iron armature, which reduced magnetic energy. To manufacture the stator, 110 kg of neo-
dymium magnets were used and 115 kg of neodymium were used to manufacture the rotor. High-
frequency field magnetization was not applied. It was decided to replace an imprinting technology de-
scribed in [1-5] with cross-magnetic inserts having a flux vector directed at 90 degrees to the primary
magnetization vector of the stator and rollers.
For the cross inserts, modified rare earth magnets with a residual magnetization of 1,2 T and coercive
force a little bit greater than in a base material were used. In Fig.1 and Fig.2 the joint arrangement of
stator 1 and rotor, made up of rollers 2, and a way of their mutual gearing or sprocketing by means of
cross magnetic inserts 19, are shown. Between the stator and roller surfaces the air gap δ of 1-mm is
maintained.
No layered structure was used except a continuous copper foil of 0.8 mm thickness, which wrapped
up the stator and rollers. This foil has direct electrical contact to magnets of the stator and rollers. Dis-
tance between inserts in the rollers is equal to distance between inserts on the stator. In other words,
t
1
=
t
2
in Fig.2.
Fig.1. Variant of one-ring converter.
Fig.2. Sprocket effect of magnetic stator and
roller inserts
.
The ratio of parameters of the stator 1 and the rotor 2 in Fig.2 is chosen so that the relation of stator
diameter D to the roller diameter d is an integer equal to or greater than 12. Choosing such ratio al-
lowed us to achieve a "magnetic spin wave resonant mode" between elements of a working body of the
device since the circumferences also maintained the same integer ratio.
The elements of magnetic system were assembled in a uniform design on an aluminum platform. In
Fig. 3 the general view of the platform with the one-ring converter is displayed. This platform was
supplied with springs and shock absorbers with limited ability to move vertically on three supports.
The system has a maximum value of displacement of about 10 mm and was measured by the induction
displacement meter, 14. Thus, the instantaneous change of the platform weight was defined during the
experiment in real time. Gross weight of the platform with magnetic system in the initial condition was
350 kg.
The stator, 1, was mounted motionlessly, and the rollers, 2, were assembled on a mobile common
separator, 3, also regarded as the rotor, connected with the basic shaft, 4, of the device. The rotary
2
moment was transferred through this shaft. The base of the shaft was connected through a friction
clutch, 5, to a starting motor, 6, which accelerated the converter up to a mode of self-sustained rotation.
The electrodynamics generator, 7, was connected to the basic shaft as a main loading of the converter.
Adjacent to the rotor, electromagnetic inductors, 8, with open cores, 9, were located.
Fig.3. The general view of the one-ring converter and platform.
The magnetic rollers, 2, crossed the open cores of inductors and closed the magnetic flux circuit
through electromagnetic inductors, 8, inducing an electromotive force emf in them, which acted di-
rectly on an active load, 10 (a set of inductive coils and incandescent lamps with a total power load of 1
kW). The electromagnetic inductor coils, 8, were equipped with an electrical drive, 11, on supports,
12. Driven coils for smooth stabilization of the rotor’s rpm were used but the speed of the rotor could
be adjusted by changing the main loading, 10.
To study the influence of high voltage on the characteristics of the converter, a system for radial
electrical polarization was mounted. On the periphery of the rotor ring, electrodes, 13, were set be-
tween the electromagnetic inductors, 8, having an air gap of 10 mm with the rollers, 2. The electrodes
are connected to a high-voltage source; the positive potential was connected to the stator, and the nega-
tive to the polarization electrodes. The polarizing voltage was adjusted in a range of 0-20 kV. In the
experiments, a constant value of 20 kV was used.
In case of emergency braking, a friction disk from the ordinary car braking system was mounted on
a basic shaft of the rotor. The electrodynamics generator, 7, was connected to an ordinary passive re-
sistive load through a set of switches ensuring step connection of the load from 1 kW to 10 kW through
a set of ten ordinary electric water heaters.
The converter undergoing testing had in its inner core the oil friction generator of thermal energy,
15, intended for tapping a superfluous power (more than 10 kW) into the thermo-exchange contour.
But since the real output power of the converter in experiment has not exceeded 7 kW, the oil friction
thermal generator was not used. The electromagnetic inductors were connected to an additional load,
3
which was set of incandescent lamps with total power 1 kW and facilitated complete stabilization of the
rotor revolutions.
3. Experimental results
The magnetic-gravity converter was built in a laboratory room on three concrete supports at a
ground level. The ceiling height the lab room was 3-meters, the common working area of the labora-
tory was about 100 sq. meters. Besides the presence of the iron-concrete ceiling, in the immediate
proximity from the magnetic system there was a generator and electric motor, which contained some
tens of kilograms of iron and could potentially deform the field's pattern.
The device was initially started by the electric motor that accelerated the rotation of the rotor. The
revolutions were smoothly increased up to the moment the ammeter included in a circuit of the electric
motor started to show zero or a negative value of consumed current. The negative value indicated a
presence of back current. This back current was detected at approximately 550 rpm. The displacement
meter, 14, starts to detect the change in weight of the whole installation at 200 rpm. Afterwards, the
electric motor is completely disconnected by the electromagnetic clutch and the ordinary electrodynam-
ics generator is connected to the switchable resistive load. The rotor of the converter continues to self-
accelerate and approach the critical mode of 550 rpm where the weight of the device quickly changes.
Fig. 4. -G, +G changes in weight of the platform vs. rpm
G
of the whole platform (total weight
is about 350 kg), reaches 35 % of the weight in an initial condition
G
i
. Applying a load of more than 7
kW results in a gradual decrease in rotation speed and an exit from the mode of self-generation, with
the rotor coming to a complete stop subsequently.
4
In addition to the dependence on the speed of rotation, the weight differential depends on the gener-
ated power through the load and on the applied polarizing voltage as well. As seen in Fig.4, at the
maximum output power equal to 6-7 kW, the change of weight
The net weight
G
n
of the platform can be controlled by applying high voltage to polarization ring
electrodes located at a distance of 10 mm from external surfaces of the rollers. Under the high 20 kV
voltage (electrodes having negative polarity) the increase of tapped power of the basic generator to
more than 6 kW does not influence
G
(a kind of "residual induction"). The ex-
perimental diagrams given on Fig.4 illustrate the +G and –G modes of the converter operations vs. ro-
tor rpm.
Fig.5 Diagrams of a rotor accelerating and loading of the converter.
The effect of a local change of the platform weight is reversible, relative to the direction of rotor
turning, and has the same hysteresis. A clockwise rotation causes the critical mode to occur in the area
of 550 rpm and the propulsion force against the direction of gravitation vector is created. Correspond-
ingly, a counter-clockwise rotation causes the critical mode to occur the in area of 600 rpm and a force
in the direction of gravitation vector is created. The difference in approach to a critical mode of 50 - 60
rpm was observed. It is necessary to mention that the most interesting region are situated above the
critical area of 550 rpm, but due to of a number of circumstances the implementation of such research
was not possible. It is necessary to note, that probably there are also other resonant modes appropriate
to higher rpm of a rotor and to the significant levels of useful loading and weight changing. Proceeding
from the theoretical assumptions, the dependence of tapped mechanical energy from the parameters of
magnetic system of the converter and rpm of a rotor has a nonlinear character and the received effects
are not optimum. From this point of view, the revealing of the maximal output power, of the maximal
change of weight and resource of the converter represents the large practical and scientific interest. In
tested sample of the converter the using of higher rpm was inadmissible because of unsufficient me-
chanical durability of the magnetic system, which was built from separate pieces.
5
G
if the rotation speed is kept above 400 rpm. "Tightening" of this
effect is observed as well as the effect of hysteresis on
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