Rotary Device, for Instance an Air Mover Such as a Fan, a Propeller or a Lifting Rotor, a Water Turbine or a Wind Turbine

Abstract

A rotary device comprises a frame with a guide for flowing medium, a rotor with a number of blades, whereby a relation is obtained between the flowing medium and the rotation of the rotor, and energy converting means, the one part of which is connected to the frame and the other part to the rotor. The device has the feature that the end zones of the blades are connected to a ring, the ring has a radial section with the shape of an isosceles triangle or trapezium, the medium guide has an encircling recess, the form of which corresponds to the form of the ring and the ring fits with clearance into the recess, permanent magnets are added to the truncated conical surfaces, electromagnets debouch on both the corresponding surfaces of the recess, this such that the ring and the frame together form an annular induction motor or an electric generator.

Claims

1. A rotary device for converting one form of energy to another form of energy, which forms of energy are electrical energy and the energy of a flowing medium, the device comprising: a frame with an inlet and an outlet and a rotation-symmetrical guide for the flowing medium extending between the inlet and the outlet; a rotor supported rotatably at least during operation by said frame and having a central hub and a number of blades which are connected to said hub in angularly equidistant arrangement and which extend at least more or less in radial direction, which blades all have a form such that a relation between the flowing medium and the rotation of the rotor is obtained; energy converting means, one part of which is connected fixedly to the frame and another part is connected fixedly to the rotor; the rotor comprising a concentric ring to which end zones of the blades are connected; the ring has at least one outer surface; the medium guide has an encircling recess, the form of which corresponds to that of the ring such that the ring fits with clearance into the recess; magnets on the at least one outer surface, which magnets are placed angularly equidistant and the poles of which debouch on the at least one outer surface; electromagnets having poles, the poles of the electromagnets being placed equidistantly on a surface of the recess facing the ring; and wherein: the ring with the magnets and the frame with the electromagnets together form an annular induction motor or an electric generator; and the frame is provided with a collar of openings at a first side of a clearance between the ring and the walls of the recess, the openings being connected to the recess at the first side of the recess via a collar of channels.

2. The device as claimed in claim 1, wherein the rotor ring is assembled from: two identical part-rings which each comprise a strip of material with the shape of a part of a circular arc, the free ends of which are connected to each other such that each strip has the form of the outer surface of a truncated cone, which thus modelled strips are connected with their outer circular peripheral zone to each other; and a third part-ring, the third part-ring comprising a strip of material which is curved to a round form and mutually connects the respective free circular inner edges and outer edges of the first two part-rings; and the end zones of the blades are connected to the third part-ring.

3-4. (canceled)

5. The device as claimed in claim 1, wherein each electromagnet comprises a coil comprising: a stack of electrically insulating carriers disposed in register, each with at least one electrically conductive track present thereon which forms at least one winding of the coil, which tracks debouch on the outer side of the respective carriers and are connected to each other electrically such that the windings formed by the tracks together form the coil, which carriers have registered through-holes through which a ferromagnetic core extends.

6-8. (canceled)

9. The device as claimed in claim 1, further comprising an inflow grill which is placed upstream of the inlet and which comprises a pattern of baffles placed and formed such that the channels bounded by these baffles have directions corresponding to the directions of the relevant local part-flows of the medium.

10. The device as claimed in claim 1, wherein the blades are connected under bias to the hub and to the ring.

11-13. (canceled)

14. The device as claimed in claim 1, wherein an upstream part of an active surface of the guide has a radial sectional form largely corresponding to a quarter of an ellipse, a longitudinal axis of which extends parallel to a central axis of the rotor.

15. (canceled)

16. The device as claimed in claim 1, further comprising a stationary, substantially rotation-symmetrical nose element which is disposed fixedly relative to the frame or forms part of the rotor and which is disposed upstream relative to the hub and has an outer surface which widens from its front side to its rear side and which connects at its rear side to the hub in rheologically smooth manner.

17. The device as claimed in claim 16, wherein a longitudinal section of the outer surface has more or less the form of a parabola, an extreme of which is situated at an upstream end of the nose element.

18. The device as claimed in claim 16, wherein the nose element is disposed fixedly relative to the frame and is supported by the frame via spokes.

19. (canceled)

20. The device as claimed in claim 1, the channels guide medium part-flows from an area of a downstream medium flow at increased pressure into the clearance such that these part-flows flow along the poles of the electromagnets and the magnets and thus cool these electromagnets and the magnets and leave the clearance at reduced pressure in the area of the upstream medium flow.

21. (canceled)

22. The device as claimed in claim 1, wherein the rotor is supported by the frame via auxiliary bearing means.

23. The device as claimed in claim 2, wherein each peripheral zone has on an outflow side a convergent annular protrusion which is formed by two mutually connecting concave surfaces which on their sides remote from the protrusion transpose smoothly into a largely toroidal, convex other surface of the peripheral zone.

24. (canceled)

25. The device as claimed in claim 23, wherein the downstream part of the hub has a gently tapering rotation-symmetrical form, the end surface of which has an encircling concave form such that the peripheral zone is sharp and in the centre is situated a tip, an apex of which lies at least roughly in the plane of the peripheral zone.

26-36. (canceled)

37. The device according to claim 1, wherein: the ring has two equal truncated conical surfaces with mutually opposite orientations, having a radial section with at least partially the general shape of an isosceles triangle or trapezium, the base of which extends parallel to central axis, also the rotation axis, of the rotor and the sides of which converge outward; the magnets are added to each of the truncated conical surfaces corresponding to said sides; and the poles of the electromagnets are equally placed equidistantly on the magnets debouch on both the corresponding surface or surfaces of the recess.

38. The device according to claim 1, wherein the frame further comprises an outflow zone at a second side of the recess, opposite to the first side of the recess and connected to the recess at the second side of the recess.

39. Device as claimed in claim 38, wherein the outflow zone has a deflection zone by which the part-flows are deflected such that they acquire a radial directional component and a longitudinal directional component in the direction of the medium flow through the device.

40. A system for operating a device according to claim 1, comprising an electronic unit which is configured to: supply the electromagnets with alternating currents such that through the electromagnetic interaction between the electromagnets and the magnets the rotor is driven rotatingly; or convert the currents induced in the electromagnets by throughflowing medium during rotating drive of the rotor to a form of electric current suitable for a user; wherein the electronic unit is further configured to supply the electromagnets with alternating currents such that the rotor is suspended magnetically during operation.

Description

[0090] The invention will now be elucidated with reference to the accompanying figures. In the drawings:

[0091] FIG. 1 shows a perspective view of a rotor according to the invention;

[0092] FIG. 2 shows an axial section through a device according to the invention;

[0093] FIG. 3 shows the detail III according to FIG. 2;

[0094] FIG. 3A shows the detail IIIA according to FIG. 3;

[0095] FIG. 4 shows a view corresponding to FIG. 2 of a variant in which positioning bearings are present in the area of the hub;

[0096] FIG. 5 shows an axial section through an embodiment with a medium guide and an inflow grill;

[0097] FIG. 6A shows a partially cut-away perspective view of an assembly of fans according to the prior art;

[0098] FIG. 6B shows a perspective view of a functionally similar assembly of fans according to the invention, wherein broken lines indicate the dimensions relative to FIG. 6A;

[0099] FIG. 7 shows a perspective view of a drone in a first exemplary embodiment;

[0100] FIG. 8 shows a perspective view of a drone in a second exemplary embodiment;

[0101] FIG. 9 shows a perspective view of a drone in a third exemplary embodiment;

[0102] FIG. 10A shows a helicopter with two lifting rotor devices according to the invention in a first embodiment;

[0103] FIG. 10B shows a helicopter with two lifting rotor devices according to the invention in a second embodiment;

[0104] FIG. 10C shows a cross-section of the helicopter according to FIG. 10B through the wing with rotary device close to the fuselage;

[0105] FIG. 11A shows a helicopter platform or quadcopter according to the invention which is equipped with four lifting rotor devices according to the invention;

[0106] FIG. 11B shows the cross-section along the broken line X-X through the quadcopter according to FIG. 11A;

[0107] FIG. 12A shows a ferromagnetic core of an electromagnet;

[0108] FIG. 12B shows a coil assembled from stacked electrically insulating carriers with electrically conductive tracks for co-action with the ferromagnetic core according to FIG. 12A;

[0109] FIG. 13A shows a view corresponding to FIG. 12A of a ferromagnetic core of an electromagnet which comprises through-holes intended for passage of medium for cooling purposes;

[0110] FIG. 13B shows a view corresponding to FIG. 12B of a coil assembled from stacked electrically insulating carriers with electrically conductive tracks which is likewise provided with continuous cooling channels;

[0111] FIG. 14 shows a view corresponding to FIGS. 12B and 13B of a variant in which the conductive tracks extend over the whole relevant surfaces of the carriers and the number of cooling channels is increased compared to the embodiment according to FIG. 13B;

[0112] FIG. 15 shows a structure of carriers with conductors zigzag foldable in concertina manner and thus stackable for the purpose of manufacturing a stack of windings;

[0113] FIG. 16 shows a view corresponding to FIGS. 12B, 13B and 14 of an embodiment obtained with the structure according to FIG. 15;

[0114] FIG. 17 shows a top view of an adhesive strip with permanent magnets which can be adhered to the truncated conical surfaces in the peripheral direction of the rotor according to for instance FIG. 1;

[0115] FIG. 18 shows a perspective partial view of half of two rotor halves manufactured by injection moulding prior to assembly thereof to form one rotor; and

[0116] FIG. 19 shows a perspective partial view corresponding to FIG. 18 of a rotor assembled from the two rotor parts according to FIG. 18;

[0117] FIG. 20 shows a diametric section through a device according to the invention, in particular an air moving device, in which the directions of the local median flows are indicated with arrows;

[0118] FIG. 21 shows a diametric section through a further embodiment in which the peripheral zone has a form such that the flow pattern is greatly improved;

[0119] FIG. 22 shows a diametric section through a variant in which the flow pattern is improved still further;

[0120] FIG. 23 shows on larger scale the detail XXIII according to FIG. 22;

[0121] FIG. 24 shows a schematic, locally cut-away perspective view of a rotary transformer;

[0122] FIG. 25 shows a cross-section through a fan-rotor with heating means powered by a rotary transformer; and

[0123] FIG. 26 shows a view corresponding to FIG. 3 of a detail of a device according to the invention with a rotary transformer for electrical heating of the blades.

[0124] FIG. 1 shows rotor 1 of a rotary device according to the invention for converting one form of energy to another form of energy, these forms of energy being electrical energy and the energy of a flowing medium. Rotor 1 comprises a central hub 2 bearing on the entry side a more or less parabola-shaped nose element 3 as well as a number of blades 4 connected to hub 2 in angularly equidistant arrangement and extending at least more or less in radial direction, which blades 4 all have the same form, i.e. a form such that a relation is obtained between the flowing medium, designated on the entry side with 5 and on the exit side with 6, and the rotation of rotor 1.

[0125] Rotor 1 further comprises a concentric ring 7 to which the end zones 8 of blades 4 are connected.

[0126] As shown particularly clearly in FIG. 3, the ring 7 in this embodiment has a radial section with the general shape of an isosceles triangle, the base 9 of which extends parallel to the central axis 10 (FIG. 1), also the rotation axis, of rotor 1 and the sides 11, 12 of which converge toward the apex 13 lying radially furthest outward of triangle 13.

[0127] Rotor 1 according to FIG. 1 is designed such that it is suitable for use as fan or as rotor of a wind turbine. The blades have an aerodynamic form suitable for this purpose.

[0128] Added to each of the truncated conical surfaces 14, 15 corresponding to said sides 11, 12 are permanent magnets which are placed angularly equidistant and the respective poles 16, 17 of which debouch on said surfaces.

[0129] As shown clearly in FIG. 1, the magnets are placed in such that the groups of poles 16 are offset half a pitch distance relative to poles 17.

[0130] FIGS. 2, 3 and 3A show an exemplary embodiment of rotor 1 which is suspended magnetically during operation in a rotation-symmetrical medium guide 18 with an inlet opening 19 and an outlet opening 20. Ring 7 is received fittingly with clearance in a triangular encircling recess 21. The respective poles 24, 25 of respective electromagnets 26, 27 debouch on the two corresponding surfaces 22, 23 of recess 21 which each take the form of a truncated cone, wherein poles 24, 25 of each collar have the same mutual angular distance as poles 16 and 17 of the two collars of poles of rotor 1. Each electromagnet 26, 27 comprises a core 28 and a coil 29.

[0131] It is important for the magnetic suspension that the ring has two truncated cones which are the same but oriented in opposite directions. The desired balance of forces can hereby be achieved in forward and backward direction.

[0132] The arrangement is such that ring 7 with the permanent magnets with poles 16, 17 and the frame or the medium guide with electromagnets 26, 27 together form an annular induction motor or an electric generator.

[0133] Not shown is that an electronic unit is added to electromagnets 26, 27 which is configured to supply electromagnets 26, 27 with alternating currents such that, due to the electromagnetic interaction between the electromagnets and the permanent magnets, the rotor is driven rotatingly, and which in this case is configured to convert the electric currents induced in electromagnets 26, 27 by throughflow medium during rotating drive of rotor 1 to a form of electric current suitable for a user, for instance for exporting back to the electricity grid.

[0134] The upstream part 30 of the active inner surface 31 of guide 18 has a radial sectional form as shown in FIGS. 2, 3 and 4 which largely corresponds to a quarter of an ellipse, the longitudinal axis of which extends parallel to the central axis 10 of rotor 1.

[0135] In the embodiment according to FIGS. 1 and 2 the more or less semi-elliptical nose cone 3 is fixedly connected to hub 2 and so forms part of the rotor.

[0136] FIG. 4 shows an embodiment in which a nose cone 32, which has the same form as nose element 3, is supported via four spokes 33 by medium guide 18. Connected to nose element 32 are ball bearings 34 which position the hub 2 relative to the frame, i.e. the medium guide 18.

[0137] As described above, rotor 1 is preferably suspended magnetically relative to medium guide 18 during operation. Under these conditions the bearings 34 are unnecessary. As a result of the magnetic suspension, particularly the axial forces to which prior art bearings are subjected are practically absent. However, when not in use the surfaces 14 or 15 of ring 7 do lie against the corresponding surfaces 22, 23 of recess 21. It is practical, for instance for maintenance purposes, for an engineer to be able to rotate the rotor by hand. This can take place easily in the embodiment according to FIG. 4, since under these conditions the rotor 1 is supported in more or less freely rotatable manner by bearings 34.

[0138] FIG. 5 shows an embodiment wherein the basis corresponds to that according to FIG. 2. Frame 18 is however provided in this embodiment with an inflow grill 35 which is placed upstream of inlet opening 19 and which comprises a pattern of baffles 36 placed and shaped such that the channels 37 bounded by these baffles 36 have directions corresponding to the directions of the associated local part-flows 38 of the medium.

[0139] In the embodiment according to FIG. 5 flow guide 38 further has a guide surface 39 on the downstream side with a shape such that the downstream airflow 6 through device 40 is free of dead zones.

[0140] All embodiments according to FIGS. 1, 2, 3, 4 and 5 have in common that the number of blades 4 amounts to fourteen, that inner surface 41 of the ring is streamlined and that end zones 8 of blades 4 connect smoothly to inner surface 41 of ring 7. Blades 4 are connected under bias to hub 2 on one side and to ring 7 on the other.

[0141] In the embodiment according to FIG. 4 spokes 33 have an aerodynamic or generally rheological form.

[0142] The embodiments according to FIGS. 2, 3, 4 and 5 further have in common that frame 18 is provided with a collar of channels 42 with inflow openings 92 which guide medium part-flows 43 from the area of the downstream medium flow at increased pressure into the clearance between ring 7 and the walls of recess 21 such that these part-flows 43 flow along poles 16, 17 of electromagnets 26, 27 and poles 24, 25 of the permanent magnets and thus cool these electromagnets 26, 27 and the permanent magnets and leave the clearance in the area 44 at reduced pressure.

[0143] Recess 18 has in the area of outflow zone 44 an encircling deflection surface 45 by which the part-flows 43 are deflected such that they acquire a radially inward directional component and a longitudinal directional component in the direction of the medium flow through the device.

[0144] FIG. 6A shows a prior art fan assembly 46 with an arrangement of 24 fans, to each of which fans is added a second fan with opposite rotation direction placed downstream. The rotation component is hereby effectively removed from the outlet flow of the fans.

[0145] It will be apparent from FIG. 6A, which represents the prior art, that the space taken up by the sets of cascaded fans is substantial compared to the volume of the object 47 for cooling, for instance a server area.

[0146] When the space taken up by assembly 46 is compared to the space taken up by fan assembly 48 according to the invention on the basis of the four parallel broken lines as shown in FIG. 6B, it will be immediately obvious that the space taken up in this latter case is very substantially smaller.

[0147] Only six fans, for instance of the type as shown in FIG. 5, are necessary according to the invention instead of sixteen prior art fans. All outer edges of fan assembly 48 and the edges adjoining the actual fans are rounded such that a very smooth and controlled laminar airflow is ensured. Although owing to the low rotation speed of the fans the rotation component on the outflow side is not zero, it is technically negligible and the sound levels generated by the fans during operation are in the order of magnitude of 20 dB SPL lower than according to the prior art as shown in FIG. 6A.

[0148] Fan assembly 48 comprises spaces for accommodating the six fans, which for the sake of convenience are all designated 49. Are these fans can slide into and out of the associated spaces, wherein electric coupling means are added to each space and to each fan, whereby each inserted fan can be coupled electrically to the above described electronic unit (not shown). FIGS. 7, 8 and 9 show three exemplary embodiments of drones. These are small unmanned aircraft which can be remotely controlled and carry for instance cameras and the like for the purpose of inspecting farmland, carrying out investigations by police units, or traffic surveillance.

[0149] These three drones according to FIGS. 7, 8, 9 designated with reference numerals 50, 51 and 52 have in common that they have a fuselage 53, 54, 55 which is configured to carry for instance the inspection equipment. Each drone further comprises wings, all designated with 56, and two propellers of the type according to the invention. These propellers are all designated with reference numeral 57. The foremost zone of each propeller can correspond to the embodiment of the device according to the invention as shown in FIG. 4, while a lengthened guide connects to the rear zone and ensures that flowing air is able as far as possible to impart a forward thrust to drone 50, 51, 52.

[0150] FIG. 10A shows a perspective view of a helicopter 136 with two lifting rotor devices 137, 138 according to the invention. For the purpose of supporting the forward thrust the helicopter also comprises a schematically designated jet engine 139.

[0151] The lifting rotor devices 137 and 138 can be of type applied in quadcopter 58 according to FIGS. 11A and 11B, with the proviso that the lifting rotor devices 137 and 138 must be configured to lift a heavier load and are therefore driven with greater power, have a larger diameter and operate at a higher rotation speed.

[0152] Connected to jet engine 139 is an electric generator (not shown) which serves to supply power to the lifting rotor devices 137, 138 via a computer-controlled electronic control unit.

[0153] In the embodiment according to FIG. 10A the helicopter 136 has a vertical tail surface 140 and two horizontal tail surfaces 141, 142. The outlet of jet engine 139 is situated at the rear end 143.

[0154] The helicopter according to FIG. 10A is designed such that it is suitable for speeds up to a maximum of 250-300 km/h.

[0155] FIGS. 10B and 10C show a helicopter 144, the fuselage 155 of which displays a high degree of rotation symmetry. Such a shape contributes toward a very low air resistance, also in the case where the horizontal speed in the direction 91 is high. The target maximum speed is in the order of magnitude of 500 km/h.

[0156] Other than in the embodiment according to FIG. 10A, the lifting rotor devices 138 in the embodiment according to FIGS. 10B and 10C are not placed horizontally but incline forward through an angle of about 10. This is indicated by the rotation axes 145 of rotors 1 which extend at 10 to the vertical. As shown schematically in FIG. 10C, rotors 1 can pivot through an angular range of about 30 in total. The maximum angle of inclination to the rear amounts to about 5 and the maximum angle of forward inclination amounts to about 25. A forward thrust can hereby be obtained which is substantially higher than with the classical horizontal arrangement according to FIG. 10A.

[0157] During flight the stability is ensured by computer control through dynamic control of the stepping motors (see FIGS. 11A and 11B and the associated description) for pivoting the lifting rotor devices 137, 138 in two independent directions.

[0158] It will be apparent that it is also of great importance that the annular structure 146 is modelled such that, in the case of a forward speed as according to arrow 91, the lift realized by this generally annular wing structure 146 is as great as possible.

[0159] Use is preferably made for this purpose of a structure such as the annular frame 124 with the specific aerodynamic profile shown in FIG. 23. Reference is made to this figure for the description hereof.

[0160] Of further importance is the fact that helicopter 144 is provided with two jet engines 147, 148 with outlets 149, 150. An electric generator is added to each of the jet engines 147, 148. In the case of possible failure of one of the jet engines the lifting rotor devices can still be driven electrically, albeit with less power. This enhances safety.

[0161] Helicopters 136 and 144 need not be provided with an anti-rotation rotor in the tail zone. As a result they are in principle about 15% more energy-efficient than usual helicopters and they make considerably less noise. The anti-rotation rotor, as irksome disruptive factor in respect of the aerodynamic properties of the helicopter as a result of asymmetrical airflows in transverse direction, is moreover hereby eliminated.

[0162] It is finally noted that helicopter 144 comprises on its rearmost zone four tail surfaces 151, 152, 153, 154 disposed in the form of a cross at 45. This guarantees great stability, even at a high speed.

[0163] FIGS. 11A and 11B show a quadcopter 58. This quadcopter comprises a more or less square plate-like frame 59, all corners and edges of which have a rounded form.

[0164] Frame plate 59 carries four devices 60 according to the invention which serve in this embodiment as lifting rotors.

[0165] As in the fan assembly of FIG. 6B, all relevant corners and edges are embodied such that an aerodynamically efficient shape is obtained. An important consideration here is that the airflows generated by the lifting rotors may not interfere with each other to any appreciable extent.

[0166] There is another reason why the four edges 61 and the corner zones 62 mutually connecting these edges also have a rounded shape. These shapes are designed such that in the case of a horizontal movement of quadcopter 58 the frame plate 59 is subjected, in the manner of an aircraft wing, to a lift force as a result of its horizontal speed. The quadcopter can in this way remain airborne with a relatively low engine power during its horizontal movement. The flight direction is indicated with an arrow 91.

[0167] FIG. 11B shows the shape of corner zones 62 with which the described effect is realized.

[0168] FIG. 11B likewise shows schematically that lifting rotors 60 are pivotable relative to the main plane of frame plate 59. The pivoting range is indicated with arrows 63.

[0169] Situated in the central part of quadcopter 58 is a compartment 64 in which the electronic unit is housed, while the batteries, sensors, cameras and other load to be carried are accommodated in the compartment 65 located thereunder. A low centre of gravity is realized with this construction. This contributes toward the stability of quadcopter 58 during flight.

[0170] Pivoting a minimum of one of the lifting rotors 60 out of the main plane, though preferably all four at the same angle, achieves that the quadcopter is not only subjected to a vertical lift force but also a force with a horizontal component, whereby the quadcopter begins to move in horizontal direction. The described streamlined form is of essential importance, and certainly when reaching substantial speeds.

[0171] In FIG. 11B an arrow 93 indicates a force directed obliquely upward which is caused by the combination of the flying speed in the direction 91 and the specific aerodynamic form of edges 61. The occurrence of this obliquely upward directed force 93 is generally known per se from aerodynamics. Aircraft wings, rotor blades of wind turbines and the like are designed such that the path length of the air flowing along the convex upper side of the associated profile is greater than that on the concave lower side of the profile. An upward directed force occurs as a result during a horizontal movement.

[0172] The force 93 can be separated into a horizontal force component 94 and a vertical force component 95. Seen over the whole periphery, the horizontal force components 94, shown only toward the right-hand side in the schematic view of FIG. 11B, cancel each other out; this is because forces in the opposite direction occur on the left-hand side. The vertical force components 95 likewise occur over the whole of the relevant surfaces and add together. A substantial lift is hereby obtained as a result of the horizontal speed in direction 91.

[0173] This lift can be very substantial and even reach values in practice which are greater than the lift realized by the difference in air pressure generated by the rotation of the lifting rotors 60. It will be apparent that particularly for lifting rotor devices of the type according to the invention this aspect can be of exceptionally great importance since on the basis hereof a great upward force can be realized with a relatively limited power during flight.

[0174] Anticipating the discussion of FIGS. 20, 21, 22 and 23, attention is now drawn to the fact that the principles outlined, except for the lifting rotor devices, can also be important in the case of for instance fans. A comparison of the respective FIGS. 20, 21 and 22 particularly shows that, as a result of the specific measures characteristic for the relevant exemplary embodiments, the flow pattern becomes increasingly better in the sequence of these figures and that, particularly in the embodiment of FIG. 22, the flow pattern very closely approximates the ideal of a completely smooth inflow and a smooth outflow without disruptive vortices and turbulences.

[0175] In addition to the already stated advantage of a low energy consumption, the great advantage can also be noted that the quadcopter according to the invention makes in the order of magnitude of 20 dB SPL less noise than usual quadcopters.

[0176] An exactly adjustable pivoting of lifting rotors 60 is realized by means of stepping motors. Added to each lifting rotor 60 are stepping motors operating at mutual angles of 90. Any direction can hereby be realized within the limits of the pivoting range 63. FIG. 11B shows two stepping motors 66. The spherical segments 67 indicate schematically that the lifting rotors can pivot in the manner of a sphere in a correspondingly shaped cup.

[0177] FIG. 11A shows access hatches 68. Opening hereof makes the stepping motors 66 accessible, for instance for maintenance or repair.

[0178] As shown particularly in FIG. 11B, the transition zones between compartments 64 and 65 and frame plate 59 also have smooth forms. This choice is also made with a view to the best possible aerodynamics.

[0179] FIG. 12A shows a core 69 as component of an electromagnet 26, 27. The core is for instance embodied as a granular and/or powder-form ferromagnetic material, for instance niobium, iron, ferrite or the like, embedded in polyetherimide.

[0180] FIG. 12B shows a coil 29 comprising a stack of thin printed circuit boards 72, for instance with a thickness in the order of a maximum of 0.1 mm, in which is present a through-hole 70 around which extends a loop-like copper track 71. Printed circuit boards 72 are stacked onto each other in the manner shown in FIG. 12B such that the free connections 73, 74 of copper track 71 can all come into contact with two electrical conductors 75, 76. Core 69 fits into the through-hole in the stack of printed circuit boards 72. An electromagnet 26, 27 is in this way realized.

[0181] FIG. 13A shows a ferromagnetic core 96 with the same general form as core 69 according to FIG. 12A. Core 96 differs from core 69 in the presence of continuous channels 97. Cooling medium can be guided through channels 97. The increase in temperature of core 96 can hereby remain limited to a chosen maximum value during operation.

[0182] FIG. 13B shows a coil 98 which, like coil 29 (FIG. 12B), comprises a stack of winding elements which each consist of an electrically insulating carrier and a loop-like conductor, for instance of copper, aluminium or other suitable material, present thereon. Situated in die four corner zones of each winding element 100 is a through-hole 99. These holes 99 are registered in coil 98, which comprises a stack of winding elements 100, and thus form four continuous cooling channels through which cooling medium can be guided for the purpose of cooling coil 98.

[0183] The conductive loop-like tracks 71 are situated around the registered through-holes 70 into which, as in the embodiment according to FIGS. 12A, 12B, the ferromagnetic core 96 fits.

[0184] FIG. 14 shows a coil 102 which differs from coils 29 according to FIG. 12B and 98 as according to FIG. 13B in the sense that the whole surface on one side of the electrically insulating carrier is provided with an electrically conductive layer, for instance of copper. Extending in this embodiment through both layers are ten cooling channels, all designated 101 here for the sake of convenience. The degree of cooling can hereby be substantially improved. It will be apparent that it is necessary to ensure in both the embodiment according to FIG. 13B and the embodiment according to FIG. 14 that the medium flowing through the cooling channels must only be in thermally conductive contact with the winding elements and that the cooling medium must be electrically separated therefrom. The cooling medium can optionally be guided via tubes through channels 97, which are formed by the registered holes 99, and the channels 101. It is for instance possible to envisage thermally conductive tubes, for instance of copper, provided on their outer side with an electrically insulating coating.

[0185] FIG. 15 shows schematically a strip of winding elements, all designated 104 and mutually connected via hinge zones 103. These elements can be laid on each other pivoting zigzag-wise in the manner indicated schematically with arrows 105. A stack 106 according to FIG. 16 can hereby be formed which corresponds functionally to the coil 29 according to FIG. 12B.

[0186] FIG. 17 shows an adhesive strip 107 in which permanent magnets 108 are embedded. Situated at the one end zone of adhesive strip 107 is an undercut recess 109, while at the other end zone is situated an undercut protrusion 110 which fits exactly into recess 109. By depositing the adhesive strip 109 in the correct manner on one of the truncated conical surfaces 14, 15 of ring 7 as according to FIG. 1 the magnets can be attached in the correct manner to these surfaces. This is a highly reliable and simple way of mounting the permanent magnets on rotor ring 7. Attention is drawn to the fact that FIG. 17 is schematic in the sense that the number of magnets 108 does not correspond to the number of magnetic poles 16, 17 according to FIG. 1. It should be therefore be understood that FIG. 17 serves only to elucidate the use of an adhesive strip provided with permanent magnets.

[0187] FIG. 18 shows two parts 77, 78 for assembling a rotor 79 according to FIG. 13.

[0188] Both rotor parts are manufactured by injection moulding of plastic. Each rotor part 77, 78 comprises eight blades. During assembly these equidistant sets of blades are placed such that a rotor is created with sixteen equidistantly placed blades.

[0189] Rotor parts 77, 78 can each be manufactured by injection moulding. The manufacture of a monolithic rotor by injection moulding is found to result in a very complicated and costly mould design. The proposed solution according to FIGS. 12 and 13 therefore has a very significant economic advantage.

[0190] The hub pans 80, 81 can be slid together and subsequently locked to each other by means of a jam jar-like screw closure to form the rotor 79 as shown in FIG. 19. Hub parts 80 and 81 comprise for this purpose stop surfaces 82, 83 which can co-act with the respective mutually facing end surfaces 84, 85 of the other hub part. With rotation through a small angle a screw-tightening axial displacement takes place through co-action between the four partially helical protrusions 86 and the correspondingly shaped partially helical recesses 87. Rotor parts 77 and 78 are connected inseparably to each other along the associated adjacent surfaces of the ring, which are designated 88, 89, corresponding to the main plane of ring 7, and also along the described adjacent surfaces 82, 83, 84, 85 of hub parts 80, 81.

[0191] FIG. 20 shows a separately drawn lifting rotor in the device 111. This comprises an annular frame 112. The structure of device 111 corresponds largely to the four lifting rotors 60 forming part of quadcopter 58 as according to FIGS. 11A and 11B. It is important to note that the more or less Y-shaped central hub 113 co-rotates with the rotor.

[0192] The local flow directions of the lifting rotor device 111 operating as air mover are drawn with the arrows. It is noted that this lifting rotor device could also be used as fan.

[0193] The flow pattern on the entry side 114 gives a smooth impression. This is due to the fact that, because of the nature of the invention and the superior aerodynamic qualities of the lifting rotor device 11, the rotor 1 can rotate substantially more slowly than functionally similar prior art rotors. It is otherwise noted here that the flow pattern according to FIG. 20 (and also the FIGS. 21, 22, 23 to be discussed below) is not completely two-dimensional but is essentially three-dimensional and dynamic. This is not however of prima relevance for the basic principles of the invention and the effects thereof.

[0194] The flow pattern on the exit side 115 gives a somewhat less smooth impression. It will be apparent that downward directed and upward directed flows are in the vicinity of each other. Partly as a result the occurrence of systematic vortices, for instance the more or less toroidal vortex system 116, cannot be prevented. It is not possible as a result to avoid the upward force caused directly by the rotor leaving something to be desired.

[0195] FIG. 21 shows a lifting rotor device 117 comprising an annular frame 118 having on its underside a convergent annular protrusion 119 which is formed by two mutually connecting concave surfaces 120, 121 which transpose smoothly on their sides remote from the protrusion into the largely toroidal convex other surface 122 of the annular frame 118.

[0196] Attention is drawn to the fact that the flow pattern on the downstream side, so the exit side of device 117, is considerably smoother than that in device 111 according to FIG. 20. This is because of the specific form of the annular frame 118 with protrusion 119. Compared to device 111, device 117 already gives a substantially improved aerodynamic result.

[0197] FIG. 22 shows a lifting rotor device 123 which differs in a number of important respects from device 117 according to FIG. 21.

[0198] The annular frame 124 has a form which clearly differs from that of annular frame 118 according to FIG. 21. Outer surface 125 has a somewhat more vertical position and the annular protrusion 126 protrudes little or not at all beyond the plane 127 defined by the lower part 128 of the convex surface 129 of the annular frame.

[0199] The more or less parabolic nose element 130 is further stationary relative to the rotating hub 131. The downstream part of hub 131 has a gently tapering, rotation-symmetrical form, the end surface of which has an encircling concave shape 132 such that peripheral zone 133 is sharp and in the centre is situated a tip 134, the apex of which lies roughly in the plane 135 of peripheral zone 133. Reference is also made in this respect to FIG. 23 which shows this on enlarged scale.

[0200] It is of great importance to note that both on the upstream side, or the entry side 114, and on the downstream side, or exit side 115, the flow pattern is exceptionally smooth. As shown clearly in FIG. 22, the medium flow is directed substantially wholly downward on the exit side 150. This greatly enhances the aerodynamic performance.

[0201] Attention is drawn to FIG. 23 which shows on enlarged scale a Von Karman vortex street system 136 present as wake in the more or less conical shape under the downstream end of hub 131. The vortices are to some extent elongate and are not in a strictly stationary state. The vortex speed is low and the disruption of the overall downstream flow is negligible. As a result the aerodynamic efficiency of device 123 is not disrupted, or hardly so, by any vortex system or turbulence. The device is therefore extremely low-noise and has an exceptionally high aerodynamic efficiency.

[0202] The height of the vortex cone according to FIG. 23 lies in the order of magnitude of three times the diameter of peripheral edge 133.

[0203] FIG. 24 shows a rotary transformer 155 comprising an annular stator 156 and an annular rotor 157, in this embodiment placed therein and co-acting electromagnetically therewith.

[0204] Stator 156 and rotor 157 both consist of electromagnetic elements, designated respectively 158 and 159.

[0205] Stator 156 and rotor 157 are each constructed from thirty-six of such elements. Another number can be chosen subject to the dimensioning of the device.

[0206] Each element comprises a respective ferromagnetic core 160, 161, in this embodiment with a general U-shape.

[0207] FIG. 25 shows the manner in which the cores 160 and 161 are relatively positioned.

[0208] Added to stator core 160 is a coil 162 which, when powered by an alternating current, provides for an alternating magnetic field between the poles, i.e. the end zones of the legs, of stator core 160. Owing to the momentary position of two cores 160, 161 shown in FIG. 25 an alternating magnetic field is generated in core 161 which generates an electromagnetic force (EMF) over rotor coil 163.

[0209] It should be understood that all electromagnetic elements of 158 of the stator each generate a magnetic field which varies in time, for instance varies in sinusoidal manner, but which are equal to each other. These fields together form a homogenous annular alternating magnetic field. An equal EMF is hereby generated over all rotor coils 163. By connecting the terminals of rotor coils 163, for instance in series, to each other these EMFs are added together and the cumulative voltage can be applied over heating elements forming part of blades 164 of rotor 165.

[0210] It will be apparent that the primary or stator coils 162 and the secondary or rotor coils 163 connected in series as described above can together behave as coils of one unitary stationary transformer.

[0211] A parallel connection or a combination of serial connections and parallel connections of the elements is also possible.

[0212] It is however important that the distances between the end zones of cores 160 and 161, or the so-called air gaps, are as small as possible and as constant as possible. This can be realized according to the invention by the embodiment according to FIG. 26 in which, as already described with reference to, among others, FIG. 3, the rotor is magnetically suspended during operation.

[0213] FIG. 26 shows a more realistic view of a detail corresponding to FIG. 3 which differs from FIG. 3 only in the sense that in device 166 the rotor ring 167 does not have a sharp apex but a flattened apex which is modelled such that it carries the electromagnets 161, 163 in a more or less cylindrical configuration. These co-act with stator elements 160, 162 which are likewise disposed in a more or less cylindrical configuration.

[0214] FIGS. 24, 25 and 26 show that the primary coils 162 are powered via terminals 169 by for instance a mains voltage of 230 V, 50 Hz.

[0215] It should be understood that, due to the assembly of the annular stator 156 from thirty-six electromagnetic elements 158, in the case of serial connection or parallel connection the magnetic field generated by the stator can be annular and stationary. This field is transmitted to the thirty-six electromagnetic rotor elements 159 which, likewise through serial connection or parallel connection, can generate an alternating voltage which is stationary, i.e. constant over time, in the manner of a stationary transformer. Reference is made once again in this latter respect to FIG. 26.

[0216] FIG. 26 shows schematically that in this embodiment of the invention the rotor coils 163, for instance connected to each other in series, supply power to cover layers 168 of resistance material, for instance of constantan or inconel, present on rotor blades 4, i.e. provide for conduction of alternating current therethrough cover layers 168, which serve as heating elements, are hereby heated to for instance the temperature in the order of magnitude of 70-80 C. The inflowing unheated airflow 5 is hereby heated and a heated airflow 6 is emitted. Cover layers 168 are embedded or lie recessed relative to the aerodynamic basic profile of each blade 4 such that this profile is not disrupted or obstructed thereby in any way whatsoever, nor does it display transition zones or transition edges which could cause vortices or turbulences.

[0217] Indicated as application for a heating element as shown in and described with reference to FIGS. 24, 25 and 26 are a space heater for household use, i.e. a fan heater, a hairdryer or other air heating device which must heat air at a temperature in the order of 20 C. to a temperature in the order of magnitude of 60 to 70 C.

[0218] It is noted that ring 167 has a cross-section with the form of an isosceles trapezium. A stable magnetic suspension can be realized owing to the symmetrical structure of the truncated conical sides 11, 12.