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In these pages,
you will find a century’s worth of
proof that Man has had the ability to
create and control the crafts and lights
seen in the sky. This evidence comes from
the most reliable source available:
the Patent Office.
These patents are included in this Series as the evidence
to show that man has had the ability to be behind the flying saucer phenomena.
Within this encyclopedic series you will be exposed to the technology that
gives YOU the power to seize and manifest the New Space Age.
The information is presented to stimulate your
thoughts, and to help acquaint you with the field of non-airplane-non-helicopter flying craft,
of the aerial and space varieties.
Excerpts from 10 of the 40 entries taken at random from Volume I of the UFO How-To series,
and in no particular order:
1) The object of my invention is to produce a machine, which, though heavier
than air,
can raise itself from the ground, without a running start, to any desired
height, to remain, as a humming bird, hovering over any given spot, at any
desired altitude, in spite of the strongest wind; to raise or lower itself, at
will, while in the air; and to propel itself in any desired direction; all at a
rate of speed entirely under the control of the operator.
2) The present invention is directed to a space propulsion system that is
propellantless. The propelling force of a space vehicle is generated by means of
generating asymmetric gravitation waves, thus creating a momentum imbalance
through the center of mass of the radiating system. This causes a force to act
upon said center of mass, resulting in motion in the direction of the least
intense gravitational wave.
3) The Flying Saucer is a vertical take off and landing vehicle for space
flight. The vehicle comprises a metal sphere rotating around a hub to which are
affixed four magnetic coils in a circle equidistantly with a fifth coil at the
center which is surrounded by a hollow circular glass tube filled with rubidium
gas, tube and magnets with axes vertical The inner wall of the tube is made of
more dense glass with a phosphor coating, and the top of the tube has a less
dense glass outer coating on top of the more dense glass. When an electric motor
rotates a vertical column, supported by a bearing at the center of the hub which
is attached to the top and bottom of the sphere, the metal sphere rotating
around the magnetic coils causes a continuous buildup of electric charge on the
sphere and magnetic field, which heats and excites the rubidium gas in the tube
so it interacts with the phosphor layer to produce light which is slowed down by
the hot rubidium gas; causing a radial Einstein time change over distance,
causing increased centrifugal force radially, causing acceleration of sphere
rotation, resulting in more mechanical energy than needed to produce the slowed
light by the previously mentioned process, with excess energy turning the
electric motor as a generator to charge the battery. The slowed light reflected
down vertically produces vertical thrust from the light (force of light equals
wattage divided by velocity), and vertical thrust from Einstein time change over
distance. Hinged mirrors at exhaust at bottom of sphere deflect the vertical
light at an angle for horizontal thrust. The part of the hub which the tube
rests on, and the exhaust at the bottom of the sphere, are transparent.
4) The embodiments of the invention in which an exclusive property or privilege
is claimed are defined as follows:
1. A rotaplane comprising a hollow rotatable discus-like body having an inclined
surface which, upon rotation of the body, is operable to force the surrounding
air mass downward, a cabin carried by said body within the body and around which
the body is rotatable relative to the cabin, and an engine carried by said cabin
and operatively connected to said body for rotating the body to sustain the same
in the air.
5) The present description generally relates to a vehicle capable of flight and,
more particularly, to an aircraft with vertical takeoff and landing and high
maneuverability characteristics which can be operated inside and outside of
Earth's atmosphere.
6) The present invention is related to discoidal shaped aircraft. The
aerodynamic advantages of saucer shaped craft have been sought after in
commercial, private and military aircraft design. Discoidal flight is
known and particular reference is made to it in U.S. Pat. No. 3,359,678.
This flight principle is claimed to be put to use in an invention disclosed in
U.S. Pat. No. 3,946,970 in combination with vertical thrust means. The
disclosure relates to a "gyroscopically stabilized vertical takeoff and landing
aircraft". The craft includes an outer spinning ring thrust that does not, of
itself, produce vertical lift during takeoff or hovering of the craft. Instead,
lift is provided by downwardly directed thrust produced by conventional jet or
rocket engines. Part of the engine thrust is diverted through a complex ducting
arrangement to produce rotation of the ring. Thus, the craft has the advantage
of the spinning disk principle during horizontal flight but necessarily relies
solely upon the downward thrust of its engines to accomplish vertical takeoff or
for hovering.
7) An aircraft with automated means to transport. Spherical or one of its
segments, without airfoils for lift or guidance. Means for flight are housed
within the aircraft. The outermost surface is configured to disrupt the
air-flow, over its surfaces, in flight. This, to reduce skin-friction and drag
coefficients, and mollify heat build-up on the skins outer surfaces as speeds
increase to and beyond mach 1. The weight of gas per unit volume, with
temperature variations, is the means to reduce the gross-weight and adjust for
temperature and weight changes during flight. Propulsion, within the propulsion
component, is provided by turbojet engines. They are secured within an inner
compression pod and an outer combustion pod. The compression pod and the
attached vertical-air-duct, rotate through three hundred sixty degrees, as the
means for directional guidance and direct thrust. Augmented power-thrust-tubes
extend outward from the combustion pod to the mid-horizontal circumference of
the aircraft. Control baffles, on each thrust-tube, check, deflect and regulate
the engines' thrust to control the motivity of the aircraft. Struts retract for
flight and are extended for landing. These electro-hydraulic struts, level,
raise and lower the aircraft for direct ground level support operations. The
aircraft has the means to maintain a horizontal flight attitude. For flight
aptness the aircraft has an internal, mechanical and scientific means, for
vertical ascent and vertical descent without horizontal motivity, to hover and
maintain a position and altitude. And during horizontal flight, climb and
descend, and perform heading changes. These flight means are all performed in
the aircrafts' horizontal attitude.
8) A disk-shaped vertical take-off and landing aircraft having a centrally
arranged fan chamber, a plurality of radially arranged trunk ducts for
conducting pressured air outwardly toward the circular periphery of the
aircraft, and includes at the outer end of each trunk duct a pair of vertically
spaced thrust nozzles; one nozzle being a lift nozzle for projecting air
downwardly, the other nozzle being a forward thrust nozzle for projecting air
rearwardly and for propelling the aircraft forwardly in flight. The aircraft
includes valve means for directing the air through either the lift thrust
nozzles or the forward thrust nozzles or simultaneously through both nozzles.
The aircraft also includes thin flat annular plane means arranged about the
circular periphery of the body of the craft for stabilizing and controlling the
craft in rapid forward flight.
9) The invention refers to a proceeding that lies at the basis of the building,
working and the shifting of some flying saucers that are characterized by having
an original propulsion system of a new type, capable to shift in any direction
(including the zigzag way of shifting), to ensure by centrifugal motion both the
annulment of the earth gravity, an sustentation in the air due to the permanent
depressurization from the upper exterior side and changing at every moment the
ways of working of the propulsion,- respectively from the combustion under
constant pressure to the combustion overfeed by static reactor or by rocket
engine used at movement in the outer space, having the feature that can be
produced at wide range, means of transportation of a new type, capable to ensure
the ultra rapid transport of goods and persons both in the atmosphere and in
cosmos as well and at such speeds that can overpass the light speed, - complying
with the laws from Physics (utilizing also the theorem of Steiner - from the
Physics) - using the possibility of shifting in a zigzag, concomitantly
overlapped to the basically propulsion.
10) It is the broad object of this invention to provide for flying apparatus
capable of leaving the ground and starting on a vertical or very steep path, of
hovering in the air under its own power, of executing fast flights efficiently
and economically, and to glide down without power at a reasonably low velocity.
It is another object "of the invention to provide for flying apparatus without a
rotating propeller, eliminating thereby the aerodynamic power loss of such
propeller, its noise, and the danger associated therewith on the ground.
This volume has been revised to include 120+ new pages of UFO technology with the additions placing an emphasis on gravitational wave generation technology.
650 pages
99% patents - 1% commentary
Perfect Binding, black and white ink
8.5 x 11 inches
$29.99
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