WO1989010484A1

WO1989010484A1 - Propulsion method and assemblies using the oscillation of flexible blades rotatingly driven in a force field

Info

Publication number: WO1989010484A1
Application number: PCT/FR1989/000200
Authority: WO
Inventors: Joël Louismarie René MINARD
Original assignee: Minard Joel Louismarie Rene
Priority date: 1988-04-27
Filing date: 1989-04-26
Publication date: 1989-11-02
Also published as: FR2630784A1; FR2630784B1; AU3563889A

Abstract

In a diffrent way from systems used presently for transports and search for energy, the devices of the present invention set in revolution $g(V) elements (r) which, when rotating $g(v) at a characteristical angular speed and due to the phase difference of the law of action of masses along the flexible blades which compose them, generate a propulsion force (F) perpendicular to the centrifugal revolution force and with a linear intensity higher, after a certain lapse of time, than the alternating power consumed by the elements in the direction perpendicular to their translation. Both in this version and in the version using the induction of the gravity effects, these crafts make thus possible the propulsion of vehicles as well as the production of energy, cost free.

Description

a) - Method and propulsion assemblies using the oscillation of flexible blades driven in rotation in a force field. b) -The present invention relates to the propulsion of all mobile land, sea and space vehicles, as well as the production of new energy, both at fixed station, and to provide the energy necessary for the propulsion of the preceding mobiles, while One of the parts of this invention serves as a propellant. c) Up to now, the only mechanical means of moving is the wheel system, propellers which, constrained to rotate, by a motor system, use a reaction, with respect to the ground or with respect to a fluid. There is also the rocket propulsion system, which consists in expelling a gas mass, in order to benefit from the opposite reaction. In the latter case, and more particularly for the propulsion of spacecraft, beyond the Earth's atmosphere, we arrive at an upper speed limit, since, for long journeys, we must first take a mass of gas from more and more important, as one wants to arrive at an increasingly greater speed. It is therefore very interesting to be able to obtain an acceleration economically from an engine internal to the machine that we want to move. As for the problem of energy supply, it is obviously linked to the problem of the risk of an oil shortage. d) The device (I) has an external acceleration, coming from the arrangement of internal forces, which allows it to move outside a fluid, and without using the rocket propulsion system. In addition, under air vacuum, from v = o, at speed v, it has expended an energy kMv, and has an energy that is a

say greater than the energy consumed, from a certain speed in the direction of its propulsion. It therefore gives rise directly to the device (2), capable of recovering excess energy, that is to say of providing free energy, the advantage of which does not require argument. The devices (3) and (4) are modifications of the device (I), which, under the action of gravity, can respectively provide the same advantages as (r) and (2).

1 - According to Figs: (5, 6 and 7), a device (r), forming a rotor, is composed of flat spring blades (Lr), fixed rigidly at their end (C), to an axis (X), rotated, the end (U) of the blades (Lr) being able to vibrate without constraints. The flat spring leaves (Lr) have, according to Fig: (l), a length (L), a width (l), a thickness (e), and elastic properties, such as, rigidly fixed and immobile , by their end (C), and subjected to the force (B) in their free end (U), they return when the force ceases, at their starting point, and enter into oscillation, according to AB, at a frequency (f ), equal to the inverse of the travel time AB, BA; they have these properties in a movement perpendicular to (l), but are not flexible in a movement perpendicular to (e). If (e) is small compared to (l), this last characteristic is realized. Preferably, hardened steel blades are used.

Fig: 2, a rotor (r), set in rotation at the characteristic speed ω _1, ω ₃ , and subjected to the force ^F i, due to zero gravity, or to a centrifugal effect, its axis of rotation (x), being subtracted from ^F i, by the resistance of its support ^R i = - ^F i, is subjected to the force ^F x. nerυendi¬

The blades (Lr), according to a certain embodiment, are provided / at their end (u), with a ballast (m) formed by a metal counterweight. Calculation of the forces at play, according to Fig: 2. Let us consider the vector

The vibrations are transmitted perpendicular to

while

turns, in time according to the unit vector

perpendicular to

F m is the component of ^F i, according to

The impulse arrives at X, with a delay of _

In a rotor with 4 symmetrical blades, forming a 90 ° angle between them, for the second set of blades

In X ', F arrives with phase shift of

(m) being the mass of each blade, ^F i is the force applied to 4 m

One calculates, just as, with the forces of friction near, the average value of ^F r is:

The same effect is obtained with blades (Lr) not fitted with ballast (m); for the calculation of the effect ^F r obtained, we then consider the action of the forces ^F i on each of the parts d (m _j ), such that d (m _j ) = m _r , mass of the leaf spring.

The experiment is easy to carry out, by carrying out the assembly of Fig: 3. Two rotors (r) are rotated at the desired speed, using synchronous electric motors (31), connected to an alternating current generator . The motors are fixed on a rotor (R), using flanges (33); the rotor (R) turns relative to a chassis

(34), using bearings (35). The power supply is réa¬lized by ground and a carbon collector.

We observe the existence of the forces ^F r ₁ to ω ₁ and ^F r ₃ to ω ₃ , by the rotation of the support (R), the force ^F r, being quickly balanced by the friction due to the air.

Fig: 5 shows a rotor (r) with two blades (Lr), the length (L) of which is perpendicular to the axis (x), intended for slow rotational speeds (ω). Preferably the plane of the blades (Lr) formed from the flat of the blade (L × 1) is located in the same plane as the length of the axis of the rotor. When blades of smaller frequency (f) are used, that is to say if rotors (r) rotating at a slow speed ω are used, the elongation AB of the end (U) of the springs becomes significant. It is therefore interesting to use shorter or thicker blades, and rotors (r) rotating faster. In the case of high speeds ω, the centrifugal effect, due to the rotation of the rotor (r), creates harmful tensions on the springs. In order to subtract the flexion AB of the spring blades for this centrifugal effect, the blades (Lr) are preferably arranged, according to Figs: 6 and 7, so that their thickness (e) looks towards the axis of rotation ( X), and that their length (L), forms with the axis (X), an angle (α), such that, during their vibration AB, their distance UO, to the axis (X) is as constant as possible; the angle (α) is determined by the following calculation, according to FIG. 8.

The blade oscillates around the center 0. The position of the center O is determined experimentally by farting the maximum angle of inflection of the blade, UL, the radius of circle described by the blade during its bending, d the mean diameter of the pulley ( p), we set Y = U Sin δ L ^, experience shows that U is close to 0.87, (1-Cos δ)

The angles are such that

According to Fig: 6, representing a rofor (r) with two leaf springs (Lr), and Fig: 1, which represents a rotor (r) with four blades, the pulley (p), is produced in a cylinder, of diameter d ₂ , chamfered (6I), so that the chamfer line (62), forms with the axis (X), an angle the pulley is hollowed out at (63), so that

the face (64) is parallel to the diameter of the pulley, at the distance of this diameter, the number of recesses corresponds to the number

blades (Lr), which is provided with the pulley, which is pierced in its center, so as to receive the key (66) and the axis (X) threaded, provided with the nut (67); the plywoods (68) have a notch (9), of width (1) and depth (e), allowing the blades to be locked (Lr) they are pierced with holes (72), opposite the orifices made in the blades ( Lr) and threaded holes, made in the body of the pulley, intended to receive the screws (70); flat spring leaves (Lr) in hardened steel; are fixed on the faces (64) of the pulley, using the counterplates (68), and screws (70). The blades (Lr) may or may not be provided with a ballast (m) at their end, in order to increase the effect of the induction forces (F _i ).

For reasons of interference, between the different blades (Lr), the rotors (r), having two symmetrical blades, operate at two speeds, ω ₁ , and ω ₃ , while the rotors with more than two blades, are predestined at speed ω ₃ The device (3) ₅ according to Fig: 2, is thus produced; rotors (r) according to Figs: 5, 6 or 7, are arranged on a frame; their axes (X) of rotation are arranged horizontally and perpendicular to the desired direction of propagation; they are coupled to a system motor which drives them at a speed ω ₁ (mod .2π) or ω ₃ depending on the direction of the desired propulsion, under the action of the forces of gravity; the assembly is placed in an enclosure under vacuum. The chassis is fixed to the mobile to be driven horizontally. Calculation of the energies used.

The work provided, E _r , since the elongation a = 0 has power, P _r .

The triavail consumed consists of raising the mass (m), its elongation a ', maximum, against F _i , at each half turn.

l

a power, P _i ,

We see that from a certain time, the propulsion power is greater than the power consumed.

The device (4), according to 1a Fig: 3, makes it possible to recover the excess energy and therefore serves as an energy generator. The rotors (r) are coupled to a motor system which sets them in rotation as shown in Fig: 3, the rotors (r) are located at the ends of the main rotor (R), which can rotate around its vertical axis (Y); the axis of the rotors (r) is horizontal, and directed along a radius of the plane of rotation, perpendicular to the axis (Y), which can rotate relative to the enclosure, under vacuum, forming a frame (34 ), using plate bearings (35); the axis (Y) is coupled to an energy receiver, an alternator, allowing energy to be recovered in electrical form.

The device (I), according to FIGS: I0, II, I2, I3, makes it possible to obtain a propulsion, in the absence of the effect of gravity, it is preferred to the device (3), because it makes it possible to modulate the resulting thrust, by modifying the speed of rotation Ω of the main rotor (R), to obtain values of F _i clearly greater than mg, hence a power gain, and a better function of the rotors; the tendency to phase shift decreasing when F _i increases with respect to m. Rotors (r) of axes of rotation (X) are arranged on a main rotor (R) set in rotation, along its axis (Y) in an enclosure under air vacuum forming a chassis, the axes (X) are orthogonal to the axis (Y) and to a distance (D) from the axis (Y). The rotors (r), coupled to a motor system, rotate at the characteristic speeds, ω ₁ ω ₃ (mod 2π), capable of ensuring propulsion, the rotor (R), rotates at the speed Ω ensuring the production of forces

F _i , by the centrifugal effect. In one embodiment, the rotation of the rotors (r) and (R) is ensured by a single motor (I22) Fig: I2 the connection of the two systems being ensured by a system of axes and gears

(12l); according to another embodiment, the motor of the main rotor (R) is independent (I03) Fig: IC, II, I3; thus ensuring regulation of the nronulsion when

) varies, the motors driving the rotors (r), are then fixed on the rotor (R).

The calculations are identical to systems 3 and 4, the propulsion power can exceed the power consumed, so we have to make an energy generator, device (2), which can operate in the absence of gravity, of higher power 'and modular, relative to the device (4). Several devices (i), according to FIG: I4, are put in circular trajectory; they are arranged at the ends of a rotor (R ''), with a rotational axis Y '', at the distance D '' from Y ''. The rotor (R '') rotates relative to the enclosure (34), under air vacuum using ball bearings (I02); the axis Y of the devices (I) and the direction F of their propulsion are perpendicular to the radius

(D '') of the rotation Ω ", and orthogonal to the axis Y ''. The envelope of the devices (i) is fixed to the rotor (R ''). The energy is recovered on the axis Y" ,

The device (5), Fig: 5 is an energy generator, using the centrifugal force, due to the rotation, of the rotor (R). Rotors (r) are placed on the rotor (R), at the distance (D '') from the Y axis, of rotation of (r), so that their axis of rotation (X) is perpendicular to (D ''), and parallel to (Y). The energy E _r is recovered on the axis Y. In the devices (2), (4), (5), Fig: IA, 3, I5, an alternator (36) is coupled to the axis (Y ''), (Y), (Y), to recover the energy (E _r ), sots electric form.

According to another embodiment, the mechanical energy of rotation of the axes (Y '', Y) is directly recovered the envelope (134,34) is then rotated, relative to a support, the axis (Y '' , Y) being fixed to the envelope.

According to one embodiment, electricity is supplied to the rotor (r) and (R) in the devices (2), using coal collectors, associated with the axes (Y '', Y). According to the different embodiments of the devices (l, 2 and

4), the energy supplied to the rotors (r) can be brought in mechanical form, according to FIG: I2, using axes and conical references, relative to the axes Y of the rotors R, l axis Y then being fixed when the rotors rotate at constant speed.

Rotor drive (r), using rastors attached to the rotors (R) and independent of the motors driving the rotors

(R) is preferred, for regulatory reasons.

The use of electric motors is preferred, due to the vacuum in the envelopes, e) Presentation of the drawings.

Fig: I, represents a flat leaf spring in vibration, in order to define its characteristics.

Fig: 2 shows the force vectors associated with the rotation of a rotor (r) with 4 blades (Lr).

Fig: 3 shows a device (4), allowing the production of electrical energy, under the effect of gravity.

Fig: 4 shows a device (3), allowing horizontal propulsion, under the effect of gravity. Fig: 5 shows a rotor (r) with two blades perpendicular to the axis (X).

Fig: 6 shows a preferred embodiment of a rotor (r) with two blades.

Fig: 7 shows a preferred embodiment of a rotor (r) with four blades.

Fig: 8 shows the graphical way of calculating the angle α in the manufacture of rotors (r).

Fig: 9 represents the calculation of the energies consumed and supplied by the devices of the present invention. Fig: I0, represents an embodiment of the device (I), allowing propulsion.

Fig: II, represents the same device as Fig: I0, seen from below.

Fig: I2, represents a device (i), where the rotation of the rotors (r) is ensured by a system of gears forming bevel gear on the chassis casing.

Fig: I3, represents another embodiment of the device (I) seen from above.

Fig: I4, represents a device (2), composed of several disposi tifs (l) and used to provide energy.

Fig: I5, represents a device (5), which is a modification of the device (I), allowing the production of energy f) According to an exemplary embodiment of the device (I), Fig: I0 and II, a plank in aluminum, hollowed out with two lights (I0I) forms the main rotor (R), integral with the axis (Y), which is driven by the electric motor (I03), fixed to the hollow metallic envelope, of spheroid shape (34 ), in which the air vacuum is produced after assembly, it is formed of two parts, having a return (I05) containing a groove receiving an O-ring and fixed together by bolts. The second end of the Y axis, rotates freely relative to the envelope (34), thanks to the plate bearing (35), contained by the housing provided for this purpose in the envelope. Two synchronous electric motors (3I) are fixed in the lights (I0I); their axis drives the four-blade rotors (r) which rotate in the bearings (I02). A collector (I04) isolated from the axis (Y), provided with chasbons, allows the electrical supply of the motors (3l) with alternating current. The motor (I03) is asynchronous and connected outside the enclosure to a current generator, via a rheostat, making it possible to vary its speed, in order to modulate its propulsion. The collector coals are connected to the outside of the envelope to an alternating current generator; The rotors (r), according to Fig: 7, consist of a pulley (p) made in an aluminum cylinder, chamfer (6l), at an angle with the axis, the angle α being given by the method graph Fig: 8;

the pulley has four recesses (63), the distance between the face / I

(64) is distant from the axis e being thickness of one

blade (Lr); the pulley (p) is pierced in its center (73) and receives the key (66) and the axis (X), threaded at its end, receiving the nut (67); the plywoods (68) have a notch (7I), of width (l) of the blade (Lr), and of depth (e), orifices (72) are drilled there, opposite those made in the blades (Lr ) and those threaded, made in the body of the pulley (69), receiving the screws (70); the blades (Lr) are flat spring blades, of hardened steel having a length (L), a width (l) and a thickness (e), they are fixed on the pulleys, forming with the axis X, l angle α of Fig: 8, they are ballasted at their free end, ballast m, formed of two pieces of steel, riveted on either side of the former blade length (Lr), m, being equal to the weight of the blade (Lr). According to this embodiment, the axis (X) is extended at (74) Fig: 6, this part of the axis of a smaller diameter is housed in the bearing (I02) Fig: 13, according to another embodiment, the rotor (R) has an additional light (l3l), in which is housed the synchronous motor (I32) with 2 output axes, the axis (Y) is fixed with a flange (I34), on each face of the rotor (R), on a metal horseshoe part (I33), having returns, allowing attachment to the rotor; the motor output axes are coupled to the transmission shafts, rotating in the bearings (I02), associated with the bevel gears (l2l); two rotors (r) with four blades are installed on either side of the X axis, driven by the bevel pinion keyed above. In all, the motor drives four rotors (r), the rest conforms to the previous device. Fig: 12, according to another embodiment, the drive of the rotors (r) is ensured by a transmission system using bevel gears (l2l) forming a reference on the Y axis, fixed to the casing (34), while the motor I22 drives the rotor R, at constant speed according to a multiple of ω.

Claims

1 - Method of propulsion and creation of energy, characterized in that it uses the phase shift of the action of a field of acceleration of the masses (Fi) on a rotor (r), in rotation of axis ( X), by means of flexible elements (blades Lr) fixed to the rotor and ensuring the delay of the action of (Fi), necessary to propel the rotor in a direction perpendicular to (Fi) and the setting in convolution of the axis (Y) of the rotors (r) ensuring the recovery of kinetic energy. The assembly is placed under vacuum.

2 - Device according to claim 1, concerning the rotors (r) mentioned therein, characterized in that: the rotors (r), (Fig: 5, 6 and 7), are composed of several blades forming a spring (Lr) symmetrically fixed by one of their ends to an axis of rotation (X) the second end of the blades (Lr), which can vibrate freely; the blades (Lr) have a length (L), a width (l) and a thickness (e), and are such that, immobilized by one of their ends, they oscillate at their natural frequency (f) as soon as they cease to be inflected, they are flexible along the perpendicular to their surface (L × 1) and very little flexible in another direction; the blades (Lr) are fixed to the axis (X) of rotation, that their surface (L × 1) is contained in the same plane as the direction of the axis (X); the free end of the blades (Lr) is provided with a ballast (m) formed of a metal part fixed to this end. 5 - Device according to claims 1 and 2 concerning the rotors (r), characterized in that the blades (Lr) (Fig: 6 and 7) are fixed on the rotor (r) so that their thickness (e) looks towards the axis of rotation (X) and their length (L) forms with the axis (X) a preferential angle (α), such that

the blades (Lr) are mounted on an intermediate piece called a pulley (p) made of a cylinder of diameter (d ₂ ) chamfered (61), so that the chamfer line (62) forms with the axis (X) an angle ; the pulley is hollowed out at (63) so that the face (64)

either parallel to the diameter of the pulley, at the distance ½ e, from this diameter, the number of recesses corresponds to the number of blades (Lr), with which the pulley is provided, which is drilled in its center, so as to receive the key (66) and the threaded axis (X), provided with the nut (67); the plywoods (68) have a notch (9) of width (l) and depth (E), allowing the locking of the blades (Lr) they are pierced with holes (72), opposite the orifices made in the blades (Lr) and threaded orifices, made in the body of the pulley, intended to receive the screws (70); flat spring leaves (Lr) in hardened steel; are fixed on the faces (64) of the pulley, using the counterplates (68), and screws (70).

4 - Propulsion system using the method according to claims 1, 2 and 3, characterized in that the induction forces (F _i ) are formed of centrifugal forces due to the rotation (Ω) of a second rotor (R) (Fig: 10, 11, 12 and 13) on which the rotors (r) are mounted at a distance (D) from the axis (Y) of rotation (Su) from the rotor (H.) the axes (X) are contained in a plane perpendicular to the axis (Y), the axes (X) are perpendicular to their distance (D) from the axis (Y); the rotors (r) are coupled to a motor system which sets them in rotation at a constant speed proportional to the natural frequency of the blades (Lr) which compose them; the rotor (R) is coupled to a motor system, which sets it in rotation at a variable speed; the assembly is placed under vacuum, in an envelope (34).

5 - System according to claims 1, 2, 3 and 4, characterized in that several propulsion systems described in claim 4, are put in circular trajectory (Fig: 14), are located symmetrically on a rotor (R ''), axis of rotation (Y ''), at the distance (D '') from the axis (Y ''); the axes (Y) of the devices described in claim 4 and the direction of their propulsion (F), are contained in a plane perpendicular to the axis (Y '') and are perpendicular to their distance (D '') from the 'axis (Y' '); the assembly is placed under vacuum in an envelope (134), the energy of rotation of the axis (Y '') is recovered.

6 - System for producing energy, according to claims 1, 2 and 3 characterized in that the induction forces

(F.), are formed by the centrifugal forces due to the rotation (Ω) of a second rotor (R) (Fig: 15), several rotors (r) being mounted on the rotor (R), of axis of rotation (Y), at the distance (D ") from the axis (Y), the axis of rotation (X) of the rotors (r) is parallel to the axis (Y); the rotors (r) are coupled to a motor system which sets them in rotation at a constant speed, proportional to the natural frequency of the spring blades (Lr) which compose them; the whole is placed under vacuum, the energy of rotation of the axis (Y) is recovered.

7 - Propulsion system according to claims 1, 2 and 3 characterized by the fact that the induction forces (F _i ) are formed by the action of the forces of gravity (mg), several rotors (r) are placed on a frame (Fig: 4) their axes (X) of rotation are arranged horizontally and perpendicular to the desired direction of propulsion; the rotors (r) are coupled to a motor system which sets them in rotation at a constant speed, proportional to the natural frequency of the blades (Lr) which compose them; the assembly is placed under vacuum.

8 - System used to produce energy, according to claims 1, 2 and 3 characterized in that the induction forces (F _i ) are formed by the action of gravity forces (mg) on the blades ( Lr), several rotors (r) (Fig: 3) are located on a second rotor (R) with an axis of rotation (Y) vertical, the axis (X) of rotation of the rotors (r) is directed horizontally and perpendicularly to the axis (Y); the rotors (r) are coupled to a motor system which sets them in rotation at a constant speed, proportional to the natural frequency of the spring blades (Lr) which compose them; the assembly is placed under vacuum, the energy of rotation of the axis (Y) is recovered.

9 - Device according to claims 1, 2, 3, 5, 6 and 8, characterized in that: the energy of rotation of the axes (Y, Y '') is recovered in the form of electrical energy by a dynamo machine electric coupled to the rotation of the rotors (R).

10 - Device according to any one of the preceding claims, characterized in that (Fig: 3, 4, 10, 11, 13 and 15), the motor systems coupled to the rotors (r) and ensuring their rotation are constituted by motors electric, placed on the rotors (R), powered by charcoal collectors integral with the axes (Y, Y '').

11 - Device according to claims 1, 2, 3, 4, 5 and 8, characterized in that: the motor systems coupled to the rotors (r) and ensuring their rotation consist (Fig: 12) of a device of shafts transmission and bevel gears forming a reference on the axis (Y), then fixed to the casing (34) when the rotor (R) rotates.