FR2630784A1 - METHOD AND PROPULSION ASSEMBLY USING OSCILLATION OF SOFT BLADES DRIVEN IN ROTATION IN A FIELD OF STRENGTH - Google Patents

Abstract

In a diffrent way from systems used presently for transports and search for energy, the devices of the present invention set in revolution OMEGA elements (r) which, when rotating omega 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) I - Device causing a propulsive effect. 2 - Dis-
using the device (I) and serving as an energy generator.

3 - Modified device (I), causing propulsion, under the effect of 1
gravity. 4 - Device (I) modified, serve as a generator of energy
under the effect of gravity. 5 - Device (I) modified, serve as
energy generator.

 b) The present invention relates to the propulsion of mobile land, sea, space, and the supply of new energy.

 c) Until now, there exists as a means to move only the wheel system, propellers which, constrained to rotation, 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 of expelling a gaseous mass, in order to benefit from the opposite reaction. In the latter case, and more particularly for the propulsion of spacious engines, beyond the terrestrial atnosphere, we reach an upper limit of speed, since, for long journeys, we must first bring a mass of gas from more and more important, as one wants to arrive at a speed of greater and greater.It is therefore very interesting to be able to obtain an acceleration of economic way from an engine internal to the machine that one wants to move. When it comes to the problem of energy supply, it is obviously related to the problem of the risk of oil shortage.

d) The device (r) has an external acceleration, originating from the arrangement of internal forces, which allows it to move outside a fluid, and without using the system of rocket propulsion. In addition, under vacuum, from v = o, to speed
I vs he has spent a kNivS energy and has a 2 Mv energy, ie greater than the energy consumed, from a certain speed in the direction of his propulsion. It thus gives rise directly to the device (2), capable of recovering the excess energy, that is to say of providing a free energy, the advantage of which does not require argument. The devices (3) and (4), are modifications of the device (I), which can, under the action of gravity, 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 leaf springs (Lr), fixed rigidly at their end (C), to an axis (X ), rotated, the end (U) of the blades (Lr) can vibrate without constraints.

The flat leaf springs (Lr) have, according to the
Fig: (1), a length (L), a width (1), a thickness (e), and elastic properties, such as, fixed rigidly and immobile, by their end (C), and subjected to the force (B) at their free end (U), they return when the force ceases, at their starting point, and oscillate according to ABS at a frequency (f), equal to the inverse of the travel time AD, BA ; they possess these properties according to a movement perpendicular to (1), but are not flexible in a movement perpendicular to (e). If (e) is small compared to (1), this last characteristic is realized.

 Hardened steel blades are preferably used.

Fig: 2, rotor lin (r), rotated at characteristic speed # 1, # 3, and subjected to force Fi, due to gravity, or to an effect F.

centrifugal, its axis of rotation (X), being subtracted to Fi, by the
RFF with its support Ri = - 1, is subjected to the force Fx perpendicular to Fi.

 The blades (Lr), according to a certain embodiment, are provided at their end (U), a ballast (m) formed of a metal flyweight.

Calculation of the forces involved, according to FIG.

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<tb> X <SEP> - <SEP> Lcoss <SEP> r <SEP> + <SEP> T
<Tb>
your vibrations are transmitted perpendicular to X u, while XU rotates, in time 4T, according to the US unit vector perpendicular to XU

<tb> ic: <SEP> 2eco50c <SEP> E <SEP>
<tb> F <SEP> F <SEP> m <SEP> is <SEP> the <SEP> component <SEP> of <SEP> Fis <SEP> according to <SEP> U
<tb> - <SEP> QS <SEP> o (<SEP> u
<tb><SEP> The impulse <SEP> takes <SEP> in <SEP> X, <SEP> with <SEP> a <SEP> delay <SEP> of
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<Tb>
In a rotor with 4 symmetrical blades, forming between them an anal of 90, for the second set of blades

<tb><SEP> rin <SEP> X '<SEP>, <SEP> F <SEP> arrives <SEP> with <SEP> dephasing <SEP> of <SEP>
<tb><SEP> Fy <SEP> = <SEP> - <SEP><SEP> s <SEP>;<SEP>(<SEP><SEP> 4 <SEP> 81 <SEP>'
<tb><SEP> Sin <SEP> s () <SEP> t <SEP>; (+ 1 <SEP> c5 <SEP> (411 <SEP>) <SEP> g
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<tb> F ': <SEP> Fx <SEP> ì <SEP> FK <SEP> - <SEP> 5 <SEP>(s; nte <+ osL) <SEP>o7t'<SEP> = <SEP>, -4, <SEP> Fs
<tb> (m) being the trap of each blade, Fi is the force appliguce to 4 nn
It is calculated, just as, by rux forces of friction, the average value of Fr is:

 The same effect is obtained with blades (Lr) not provided with ballast (m); for the calculation of the effect r obtained, we then consider the action of the forces Fi on each of the parts d (mj), such that d (m.) = mr, mass of the leaf spring.

J
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) rotates relative to a frame (34) by means of bearings (35). The power supply is made by the mass and a coal collector.

The existence of the forces Fr1 to # 1 and Fr3 to # 3 is observed by the rotation of the support (R), the force Fr being rapidly balanced by the friction caused by the air.

Fig: 5, shows a rotor (r) with two blades (Lr), whose length (L) is perpendicular to the axis (X), for slow speeds (#). Preferably the plane of the blades (Lr) formed of the plate of the blade (Lxl) is located in the same plane as the length of the axis of the rotor. When using blades with a smaller frequency (f), ie using rotors (r) rotating at a speed
# slow, the AB elongation of the (U) end of the springs becomes important. It is therefore interesting to use shorter or thicker blades, and rotating rotors (r) faster. In the case of high speeds W, the centrifugal effect, dl rotation of the rotor (r), creates damaging tensions on the springs.

In order to subtract the flexion AB from the leaf springs for this centrifugal effect, the files (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 (&alpha;), such that, during their vibration AB, their distance UO, to the axis (X) is the most constant possible; the angle (&alpha;) is determined by the following graphical means, according to FIG.

 UC trace, the length (L) of the leaf spring is added EC, the distance (d) from the end C of the blade to the axis (X); at the end Us we draw an arc C ', of radius equal to G, IE L; he cuts UC at the point C '; in c ', we lead the perpendicular C'D to UC.

equal to 0> 54 L; from E, draw the arc of circle DF, of radius ED; we trace EF and FU. (&alpha;) is the desired angle.

Trace UG, perpendicular to UF, and GE, perpendicular to UG, trace CF, perpendicular to EC, LP is the average width (d) of the pulley (p), see Fig. 6.

 According to Fig. 6, showing a rotor (r) with two spring blades (Lr), and Fig: 7, which shows a rotor (r) with four blades the pulley (p), is manufactured in a cylinder, diameter d2, chamfered (61), so that the chamfer line (62) forms with the axis (X), an angle &alpha; '= # / 2- &alpha;; the pulley is recessed in (63), so that the face (64) is parallel to the diameter of the pulley, at the distance 2 e, of this diameter, the number of recesses corresponds to the number of blades (Lr), which is provided the pulley, which is pierced at its center, so as to receive the key (66) and the axis (X) threaded, provided with the nut (67); the counterplaces (68) have a notch (9), width (1) and depth (e), allowing the blocking of the blades (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, for receiving the screws (70); flat leaf springs (Lr) of hardened steel; are fixed on the faces (64) of the pulley, using the plywoods (68), and screws (70). The blades (Lr) may or may not have a ballast (m) at their end to increase the effect of the induction forces (Fi).

 For reasons of interference, between the different blades (Lr), the rotors (r), having two symmetrical blades, operate according to the two speeds, CO1, and # 3, while the rotors with more than two blades, are predestined at speed # 3.

ou selon le sens de la propulsion désirée, sous l'action des forces de la pesanteur; l'ensemble est placé dans une enceinte sous vide d'air. Le chassis est fixé au mobile à entrainer horizontalement.The device (3), according to Fig: 2, is thus formed; 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 motor system that drives them according to a speed

or according to the direction of the propulsion desired, under the action of the forces of gravity; the whole is placed in an enclosure vacuum of air. The chassis is attached to the mobile to drive horizontally.

 Calculation of the energies implemented.

The work provided. E. since the elonzation a = O

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<tb><SEP> i <SEP> L1
<tb> the <SEP> power, <SEP> r
<Tb>
The work consumed consists in raising the mass (m) of its elongation a '. maximum. against B every half every

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<tb> the <SEP> power, <SEP> Pi,
<tb><SEP> D <SEP> 2 <SEP> FL
<tb><SEP> rv
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We see that from a certain time, the power of propulsion is greater than the power consumed.

 The device (4), according to 1ê, Fig 3 s can recover the excess energy and therefore serves as a generator of energy. The rotors (r) are coupled to a motor system which rotates them according to Fig: 3, the rotors (r) are located at the ends of the main rotor (R) s which can rotate about its vertical axis (Y); the axis of the rotors (r) is horiontal, and directed along a radius of the plane of rotation, perpendicular to the axis (T), which can rotate relative to the enclosure, under vacuum, forming a frame ( 34) by means of plate bearings (35); the axis (Y) is coupled to a power receiver, an alternator, for recovering the energy in electrical form.

 The device (i), according to Figs: IOsIII2I3, provides a propulsion, in the absence of the effect of gravity, it is preferred to the device (3), because it allows to modulate the resulting thrust, by changing the rotational speed 52 of the main rotor (R), to obtain values of Fi significantly greater than mg, hence a power gain, and a better function of the rotors; the tendency to phase shift decreasing when Fi believes in relation to m.

Rotors (r) of axes of rotation (X) are arranged on a main rotor (R) rotated, along its axis (Y) in a chassis vacuum chamber, the axes (X) are orthogonal to the axis (Y) and has a distance (D) from the axis (y).

aptes à assurer la propulsion, le rotor (R), tourne à la vitesse #, assurant la production des force par par l'effet centrifuge. Dans une réalisation, la rotation des ro- tors (r) et (R) est assurée par un seul moteur (I22) Fig:I2/la liaison des deux systèmes étant assurée par un système d'axes et d'engrenages (I2I); selon une autre réalisation, le moteur du rotor principal (R) est indépendant (103) Fig:IC,II,I3; assurant ainsi une régulation de la propulsion quand

varie, les moteurs entrainant les rotors (r), sont alors fixés sur le rotor (R). The rotors (r), coupled to an engine system, rotate at characteristic speeds,

suitable for propulsion, the rotor (R) rotates at the speed #, ensuring the production of forces by the centrifugal effect. In one embodiment, rotation of the rotors (r) and (R) is provided by a single motor (I22) Fig: I2 / the connection of the two systems being provided by a system of axes and gears (I2I) ; in another embodiment, the motor of the main rotor (R) is independent (103) Fig: IC, II, I3; thus ensuring a regulation of the propulsion when

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

The calculations are identical to the systems 3 and 4, the power of propulsion, can exceed the power consumed, it is therefore necessary to achieve an energy generator, device (2), can fono tionner in the absence of gravity, higher power and modulable with respect to the device (4) .Several devices (I), according to the
Fig: I4, are placed in circular trajectory; they are arranged at the ends of a rotor (R "), of axis of rotation Y", at the distance D "of Y" .The rotor (R ") rotates relative to the enclosure (34), under air void using ball bearings (I02); the Y axis of the devices (I) and the direction F of their propulsion are perpendicular to the radius (D '') of the rotation g S and orthogonal to the axis Y ".The envelope of the devices (I) is fixed at rotor (R "). Energy is recovered on the Y axis ",.

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 axis
Y, rotation of (r), syrte that their axis of rotation (X) is perpendicular to (D "), and parallel to (Y) The energy E r is recovered on the Y axis.

In the devices (2), (4), (5), Fig. I4, 3, 15, an alternator (36) is coupled to the axis (Y ''), (y), (y), to recover energy (Er) sou; electric form.

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

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

 According to the different embodiments of the devices (1, 2 and 4), the energy supplied to the rotors (r) can be brought into mechanical form, according to FIG. 12, using axes and conical references, relative to to the Y axes of the rotors R, the Y axis then being fixed when the rotors turn constant speed.

 The drive of the rotors (r), using motors fixed on the rotors (R) and independent of the motors driving the rotors (R) is preferred, for reasons of regulation.

 The use of electric motors is preferred because of the air gap in the envelopes.

 e) Presentation of the drawings.

Fig: I, shows a flat leaf spring vibration-, to define its characteristics.

Fig: 2, represents 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 a 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 to calculate the angle o4 in the manufacture of the rotors (r).

Fig. 9 shows the calculation of the energies consumed and provided by the devices of the present invention.

Fig: 10, represents an embodiment of the device (I), allowing propulsion.

Fig: II, shows the same device as Fig: 10, seen from below.

Fig: I2, shows a device (I), where the rotation of the rotors (r) is provided by a gear system forming conical return on the chassis casing.

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

Fig: 14 shows a device (2), composed of several dispos tifs (I) and to provide energy.

Fig: 15, represents a device (5), yes is a modification of the device (I), allowing the production of energy
f) According to an exemplary embodiment of the device (I), Figs: 10 and 11, an aluminum plate, hollowed out by two lumens (ion) forms the main rotor (R), integral with the axis (Y), which is driven by the electric motor (I03), attached to the spheroidally shaped hollow metal casing (34) in which the air vacuum is produced after mounting, it is formed of two parts, having a return (I05) containing a groove receiving an O-ring and fastened to each other by bolts.The second end of the Y-axis, rotates freely with respect to the casing (34), thanks to the bearing plate (35), contained by the housing provided for this effect in the envelope. Two synchronous electric motors (3I) are fixed in the lights (IOI); their axis drives the rotors (r) with four blades which rotate in the bearings (102). A collector (I04) isolated from the axis (Y), provided with good eyes, allows the power supply of the motors (31) in alternating current. The motor (I03), is asynchronous and connected to the outside of the envelope to a current generator, through a rheostat, to vary its speed to modulate its propulsion .The collector coals, are connected outside the envelope to an alternating current generator; the rotors (r), according to Fig: 7, consist of a pulley (p) made in an aluminum cylinder, chamfered (61) at an angle to the axis, &alpha; = # / 2 - &alpha; s the angle X being given by the graphical method Fig: 8; the pulley has four recesses (63), the distance between the face (64) is distant from the axis (X) of I e, e being the thickness of a
2 blade (Lr); the pulley (p) is pierced at 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), width (1) of the blade (Lr), and depth (e), holes (72) Y are drilled, opposite those made in the blades (Lr) ) and those threads, made in the body of the pulley (69), receiving the screws (70); the blades (Lr) are flat spring blades, hardened steel having a length (L), a width (1) and a thickness (e), they are fixed on the pulleys, forming with the X axis, angle &alpha; of FIG. 8, they are weighted at their free end, of the ballast m, formed of two pieces of steel, riveted on either side of the end of the blade (Lr), m, being equal to weight of the soul (Lr) .According to this embodiment, the axis (X) is extended in (74) Fig: 6, this part of the axis of a smaller diameter is housed in the bearing tIOt
Fig: I3, according to another embodiment, the rotor (R) has an additional flyback (131), in which is housed the synchronous motor (I32) with 2 output axes, the axis (Y) is fixed to the using a flange (134), on each face of the rotor (R), on a metal piece horseshoe, (I33), having returns, allowing attachment to the rotor; the output shafts of the motor are coupled to the shafts, rotating in the bearings (I02), associated with the bevel gears (I2I); two rotors (r) with four blades are installed on either side of the X axis, driven by the conical pinion keyed on.

In all, the motor drives four rotors (r), the rest is in accordance with the previous device.

Fig: I2, according to another embodiment, the drive of the rotors (r) is provided by a transmission system using bevel gears (I2I) forming a return 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 CA) i

Claims (10)

 1 - propulsion method using the arrangement of internal forces, for the displacement of any machine, characterized in that it uses the oscillation of flexible blades (Lr), fixed by one of their end to a rotor (r ), rotated (ru3) along an axis (X), in the force field (Fi), such that the blades (Lr) are oscillated under the effect of the force (4), the rotation of ( r) and the time required for the traveling pulse (Fi) (Lr) to arrive on the aie (X), creating a propulsion perpendicular to the initial force (Fi), the assembly being mounted in a vacuum enclosure of 'air.  2 - Device according to claim 1, relating to the rotors (r) mentioned therein, characterized in that: the rotors (r), (Fig: 5, 6 and 7), are composed of several spring blades (Lr) symmetrically fixed by one of their ends to an axis of rotation (X) the second end of the blades (Lr), being able to vibrate freely; the blades (Lr) have a length (L) a width (1) and a thickness (e), and are such that, immobilized by one of their end, they oscillate at their own frequency (f) they cease to be inflected, they are flexible according to the perpendicular to their surface (L x 1) and not very flexible in another direction; the blades (Lr) are fixed to the axis (X) of rotation, that their surface (L x 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 piece attached to this end.  3 - Device according to claims 1 and 2 relating to 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 that their length (L) forms with the axis (X) a preferred angle (C) so that the vibration of the blades (Lr) is very little influenced by the centrifugal force developed by the rotation (cl), the blades (Lr) are mounted on an intermediate piece called pulley (p) made of a chamfered diameter cylinder (d2) (61), so that the cioanfringe line (62) forms with the axis (X) an angle

 the pulley is recessed in (63) so that the face (64) is parallel to the diameter of the pulley, at the distance 1 e, of this dia  2 meters, the number of recesses corresponds to the number of blades (Lr), which is provided with the pulley, which is pierced at 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 locking of the blades (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, for receiving the screws (70); flat leaf springs (Lr) of hardened steel; are fixed on the faces (64) of the pulley, using the plywoods (68), and screws (70).  4 - Propulsion system using the method according to claims 1, 2 and 3, characterized in that the inductive forces (Fi) are formed by centrifugal forces due to rotation (2) of a second rotor (R) ( Fig: 10, 11, 12 and 13) on which are mounted the rotors (r) at a distance (D) from the axis (Y) of rotation (g) of the rotor (R) the axes (X) are contained in a plane perpendicular to the axis (Y), the axes (X) are perpendicular to their distance (D) to the axis (Y); the rotors (r) are coupled to a motor system which rotates them 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 rotates it 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 placed in a circular path (Fig .: 14), are located symmetrically on a rotor (R '' ), axis of rotation (Y ''), at the distance (dol) 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 '') to the axis (Y ''), the assembly is placed under vacuum in an envelope (134), the rotation energy of the axis (yin) is recovered.  6 - System for producing energy, according to claims 1, 2 and 3 characterized in that the induction forces (F.) are formal by the centrifugal forces due to the rotation () of a second rotor (R) (Fig: 15), a plurality of rotors (r) being mounted on the rotor (R), of axis of rotation (Y), at the distance (D ") of the axis (Y), the axis of rotation (X) of the rotors (r) is parallel to the ase (Y), the rotors (r) are coupled to a motor system which rotates them at a constant speed * proportional to the natural frequency of the blades of spring (Lr) that compose them, the whole is placed under vacuum flair, the rotation energy of the axis (Y) is recovered.  7 - propulsion system according to claims 1, 2 and 3 characterized in that the induction forces (Fi) are formed by the action of the forces of gravity (mg), several rotors (r) are pla cés on a chassis (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 rotates them at a constant speed, proportional to the natural frequency of the blades (Lr) which compose them; the whole is placed under vacuum.  8 - A system for producing energy according to claims 1, 2 and 3, characterized in that the inductive forces (Fi) are formed by the action of the forces of gravity (mg) on the blades (Lr), several rotors (r) (Fig: 3) are located on a second rotor (R) of vertical axis of rotation (Y), 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 leaf springs (Lr) which compose them; the assembly is placed under vacuum, the rotation energy of the axis (Y) is recovered  9 - Device according to claims 1, 2, 3, 5, 6 and 8, characterized in that: the rotation energy of the axes (Y, y '') is recovered in the form of electrical energy by a dynamo machine electric coupled to 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), fed by collectors solid carbons axes (Y, Y ") e  il - 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 are constituted (Fig: 12) of a device of trees of transmission and bevel gears forming reference on the axis (Y), then attached.to the casing (34) when the rotor (R) rotates.