The flow conversion becomes effective at different places in the rotor 5 and, due to the uniform compact construction of the whole rotor system, finally is fully effective without losses. Due to the spiral build-up of pressure of the rotor 5 over the individual stories, the multi-compartment operation of the admission compartments 16, the different wind energy conversion possibilities, the different attack angles, the sliding aerodynamics in the rotation, the support of the initial velocity of all driving components in the individual operating cycles as well as in conjunction with the effects, working behind the facility, a collaboration to achieve maximum wind power conversion while utilizing the smallest to the larges wind forces, is achieved. A particularly advantageous and effective division of the wing positions is possible already with four stories. By means of an attack angle A of the vertical admission surface elements of about 36° to 38°, the wind is prepared already in the ramp for the subsequent rotation R. If there are twelve vertical admission elements 12, the attack angle A is established in such a manner that the first and fourth of the vertical admission area elements 12 form an angle of 90° and comprise three admission compartments 16. In the attack field of the wind surface at the facility, each wing 1, 2, and 3 in the rotor 5 works consecutively over four admission compartments 16. This has the advantage that each admission compartment 16 receives a new and higher initial velocity.
- Mala memoria
- FIG. 4A depicts a perspective view of an embodiment of a kinetic energy conversion system
- Ayuda a combatir los problemas del tinnitus
- Distorsión de voces o sonidos
- (8) if EcCapture>EcMax then EcMax=EcCapture and Coptimal=Ctest
- Disminución de la presión arterial alta
If subsequently, the first wing moves somewhat further into the admission compartment, the work of aerodynamics commences. The aerodynamics work with a different power of about 75% of the path in admission compartment. The field of use for the inventive wind power facility with a vertical rotor is the home area as well as the industrial area. However, this becomes effective only when the wind power facility is installed on a ship. Dolor de espalda alta lado izquierdo . The rotor wings are disposed ideally in such a manner to one another, that the sail pull and the aerodynamics ensure the best possible flow-through of the wind velocity without obstruction, which basically is possible only if there are three wings in the rotor, since they have the best angle of attack for the flow-through. On the other hand, subsequently, in the rear region of the facility averted from the wind, the diffuser effect is seen, which is a consequence of the Magnus effect.
Dolor De Estomago
No matter which wing is working, two admission compartments 16 are constantly served by the Magnus affect flow. For this variation, only the angle of incidence and the curvature of the wing are changed. The line, drawn from the leading edge of the wing up to the center of the axle and of the outwardly going line to 90° from the axle, provides the average measured value of the wing depth of the profile. The whole curvature of the wing up to the leading edge corresponds to the line shape of the high-speed engine of Schulz.
The second initial velocity is realized by the first operating cycle of the wing 1 in the first admission compartment 16. The third initial velocity is realized by the second operating cycle of the wing 1 in the second admission compartment 16. The fourth initial velocity is realized by the third operating cycle of the wing 1 in the third admission compartment 16. An increase in the energy potential of the wind power conversion is noted in the four admission compartments 16 of the wing working region. The inventive wind power facility shown can also be installed on a roof or a ship. The angle, with which the wind flows against the wing 1 and which results from the flow-through direction from the compartment, commences from 0° to 90° and after the rotation of the wing 1, from 90° to 0°. From 0° to 90°, the subsequent wing 2 is also blown against at 45°, the maximum flow-thorough, however, falling back to 0. The strongest flow through at 0° incident flow at the inner arc of the wing 1 acts on the subsequent wing 2. In the last phase of the third operation cycle, wing 1 still carries out 50% of its pressure processing.
Dolores Musculares Remedios
It is the only situation in which the flow incident on the wing is so steep. The DE 88 04 674 discloses a further variation of the solution with a vertical rotor, which operates according to the Savonius principle. The curved shape with the aerodynamically arched head shape, which must not in any way correspond to the curved leading edge shape of the rotor wings, serves as preferred variation of an optimally functioning vertical admission surface element.
This can be hollowed out at the underside to such an extent that a regular leading edge, opposite to the direction of rotation, results at its front edge. Dolor lumbar espalda . Due to the aerodynamics at wing 1, the wind velocity increases in the interior of the rotor 5. As a result, the subsequent wing 2 is tilted rapidly from 90° to 0° to the direction of flow and, with that, realizes the necessary flow-through for maintaining the optimum possible wind velocity. The incident flow on the second wing, with an inclination of 45° is also from 0° to 90°. However, the incident flow on the second wing is constant at 45°, because the wind direction leads through the center of the rotor and varies only in the force of the incident flow.
Dolor Espalda Baja
If the number of stories is different, the whole rotor has a differently selected offset of the wing groups. An octagon al machine space 8 and a cylindrical admission surface construction 11, consisting of several stories, are disposed on a foundation 9. In the center of the facility, there is a rotor 5, which has stories, which are parallel to the admission surface construction 11. The cylindrical admission surface construction 11 rests on the roof 18 of the machine space 8. The cylindrical admission surface construction 11 consists of a cylindrical admission surface outer ring 14, which may have a different number of stories. With this solution also, the disadvantage may be noted that the output abates very rapidly and the utilization of a wind velocity of the order of only 1 m/s to about 3 m/s is not possible.
Especially in this case, it may appropriately have an elevator for extending or retracting it. When used on a ship, the Flettner effect may, under some circumstances, even have a positive effect on the traveling speed. Even if the rotor barely commences to run at a wind velocity of about 0.5 m/s, the flow-through commences to build up immediately. If a two-wing rotor is selected as a variation and, in addition, the position and the shape of the wing are disadvantageous, the wind flows through these even without carrying out any work or bestowing any energy. Residual work is performed by the second wing in the rotor in the tenth and eleventh admission compartment. The compressive force works in the rotor wings only up to the end of the deflecting vane and transfers the pressure subsequently into the next, compartment, where it then undesirably becomes a counterpressure.
Dolor Muscular Bayer
Consequently, only the wind pressure and the sail pull are working in this equipment, the aerodynamics not being advantageous. The guide vanes, disclosed in the VALSAMIDIS solution, moreover have the pressure side tangents of the aerodynamic configuration disposed structurally on the wrong side. The dimensions of the profile of the vertical admission surface elements arise out of the relative dimension of 70 cm length, to the lower curvature of 6 cm and the thickest aerodynamic formation of 7 cm, which runs out into a uniform tapering.
Tipos De Dolor Lumbar
The whole system is to be regarded as a unit, which is directed to a complex collaboration. In this way, the generator is around the core of the axle and extends over the whole length of the latter. In the center of the facility, there is a cylindrical shaft, which extends through the whole of the facility down into the machine space. For the rotor wing shape selected, these wings are constructed too short, as a result of which the path of work of the wind is also too short. Where the back of the rotor wing enters the incident flow field of the admission surface, it is attracted by suction by the sail pull. Since the attack surface of the wind on the facility always serves four admission compartment 16, there is flow support and maximum utilization of the capacities of the wings 1, 2, and 3 and of the flow-through.
The rotor axle extends as far as the bottom of the machine space.
Due to the subsequent aerodynamics at the first wing, the wind velocity in the interior of the rotor increases. Due to the greater projection in the lower region, the known variation of the energy fir also has the function of a pre-compressor. 3 is not greater than that of the rotor wings 1, 2, 3. At the front side of the vertical admission surface elements 12, there is an aerodynamic curvature 19. Dolor en la parte posterior de la pierna derecha . However, at least a temporary curvature is produced. The floors of the stories are connected reliably, preferably by welding, with the associated admission surface elements and are seated on the roof of the machine space. The rotor axle extends as far as the bottom of the machine space. Pedestals for a preferably polygonal construction of the machine space are disposed in the foundation. Between these, a total of twelve vertical admission surface elements are disposed. The vertical admission elements and the rotor are designed so that the rotor runs counterclockwise.
The vertical and horizontal admission surface elements and the wings are constructed rigid and immovably. FIG. 7 shows a section of the vertical admission surface element. In the case of a total of twelve vertical admission surface elements, the angle of attack is such that the first vertical admission surface element and the fourth admission surface element enclose an angle of 90° and comprise three surfaces. This means that 10 percent in the plus range and 10 percent in the minus range, that is 100° and 80° give the range of the ideal length of the wing depth. The frequency stability is achieved by the offsetting of the wing groups in the stories and by the fly-wheel effect. This makes a balanced distribution of forces at the rotor possible and ensures an optimum frequency stability. 3 and have an aerodynamic configuration of FIG.