This application is a U.S. National Stage Application of International Application No. PCT/JP2012/082566 filed on Dec. 14, 2012, and published in Japanese as WO 2013/089248 A1 on Jun. 20, 2013. This application claims priority to Japanese Application No. 2011-275628 filed on Dec. 16, 2011. The entire disclosures of the above applications are incorporated herein by reference.
This invention relates to an electric generator.
An electric generator comprising a rotor having a magnet such as a permanent magnet and a stator having a coil may be improved in power generation efficiency as the number of turns of the coil is large. However, increasing of the number of turns of the coil enlarges size of the electrostatic generator.
On the other hand, JP 2006-340425 A, for example, discloses a motor reduced in size and improved in output by arranging the magnet of the rotor side and the coil of the stator side in a predetermined positional relationship. Therefore, it is considered to obtain an electric generator with high power generation efficiency by adopting the positional relationship between the magnet and coil of such a motor.
Further, in the electric generator as described above, it is known that when the rotor rotates cogging torque is generated in relation to the core. Such cogging torque is caused by attractive force or repulsive force generated between the magnetic poles of the rotor and the core and would cause cogging on rotation of the rotor. Therefore, the rotation of the rotor becomes unstable by the cogging torque. Regarding such a point, JP 2006-101695 A, for example, discloses a mean for suppressing cogging by making the shape of the part for mounting the magnet of the rotor into a predetermined shape to moderate the change in magnetic flux at the rotor rotating.
However, the conventional technologies described above have problems that the structures are complicated and cannot suppress cogging sufficiently.
Accordingly, this invention aims to provide a power electric generator which has not a complex structure and achieves sufficient suppression of cogging.
An electric generator according to this invention comprises a rotor portion and a stator portion in which: the rotor portion includes: a rotor yoke which made of soft magnetic material and which has a cylindrical non-magnetic portion and one or more pairs of grooves towards the non-magnetic portion; annular rotor side permanent magnets each of which is arranged in each of the grooves and magnetized as north and south poles in an axial direction; and a plurality of rotor side protrusions which protrude over the rotor side permanent magnet to the stator portion side and are arranged linearly with a constant pitch at mutually separated positions sandwiching the rotor side permanent magnets; the stator portion includes a stator member made of soft magnetic material having: a stator yoke; annular stator side permanent magnets being opposed to the rotor side permanent magnets; and stator side protrusions arranged linearly with the constant pitch at mutually separated positions sandwiching the stator side permanent magnets; wherein the stator members are arranged to shift the stator side protrusions by a half of the pitch between the neighboring stator members.
It is preferable for the electric generator according to this invention that non-magnetic portions a number of which is equal to the multiple of two are provided instead of the non-magnetic portion wherein each of the non-magnetic portions extends in axial direction to connect between neighboring ones of the rotor side permanent magnets and has a length longer than the axial distance between the both end faces of the corresponding both rotor side permanent magnets.
According to another aspect of this invention, an electric generator comprises a rotor portion and a stator portion in which: the rotor portion includes: a rotor yoke which made of soft magnetic material and which has a cylindrical non-magnetic portion and one or more pairs of grooves towards the non-magnetic portion; annular rotor side permanent magnets each of which is arranged in each of the grooves and magnetized as north and south poles in an axial direction; and a plurality of rotor side protrusions which protrude over the rotor side permanent magnet to the stator portion side and are arranged at mutually separated positions sandwiching the rotor side permanent magnets; wherein one of the rotor side protrusions located between two of the rotor side permanent magnets is shift by a half of the pitch at the position where the length of the one of the rotor side protrusions in the axial direction is equally divided by two; and in which: the stator portion includes a stator member made of soft magnetic material having: a stator yoke; annular stator side permanent magnets being opposed to the rotor side permanent magnets; and stator side protrusions arranged linearly with the constant pitch at mutually separated positions sandwiching the stator side permanent magnets.
It is also preferable for the electric generator according to the another aspect of this invention that non-magnetic portions a number of which is equal to the multiple of two are provided instead of the non-magnetic portion wherein each of the non-magnetic portions extends in axial direction to connect between neighboring ones of the rotor side permanent magnets and has a length longer than the axial distance between the both end faces of the corresponding both rotor side permanent magnets.
In these configurations, it is preferable that areas of the opposing parts of the rotor protrusions and the stator side protrusions and non-opposing part thereof are set constant respectively regardless of the positional relationship between the rotor portion and the stator portion in the rotation direction.
According to further aspect of this invention, non-magnetic portions are provided instead of the stator side permanent magnets.
Preferred embodiments of the present invention will now be described with reference to the drawings. In the following description, the term “flux” means a flux of magnetic field lines and the term “magnetic path” means a path of the magnetic field lines. Further, notation of “a magnetic path is formed by the magnetic flux” may be read as “a magnetic path is formed by the magnetic field lines.”
As shown in
The rotor yoke 4 has a plurality of rectangular-shaped protrusions 8U made of magnetic material at the axially upward side of the permanent magnet 7U shown in
The outer periphery “a” has an arc-shaped cross section for each of the protrusions 8U, 9 and 8L. Supposing the length of a part of the outer periphery “a” for one protrusion being L, the span of a virtual outer periphery “a” with the neighboring protrusion 8U, 9 or 8L is set as L. At the center of the rotor yoke 4, a rotation shaft 10 is provided. The portion the rotation shaft 10 contacts with the rotation shaft 10 is joined so that the rotor yoke 4 can rotate integrally in accordance with the rotation shaft 10 rotating.
In a housing of the electric generator 1, which is not show in
In the example shown in
On the rotor portion 2 itself, the magnetic flux of the upper-side permanent magnet 7U is to pass from the lower end of the projecting portions 8U through the outside of the rotor part 2, direct to the upper end of the protrusions 9 shown in
In the rotor portion 2 according to the preferred embodiment of the present invention having such a configuration, magnetic flux always directs from the protrusions 8U, 9 and 9L to themselves. By forming such protrusions 8U, 9 and 8L, it is possible to increase the density of the magnetic flux to increase the attractive force.
The stator portion 3 has a double decker construction of stator yokes 12U and 12L being piled in the axial direction, wherein the stator yokes 12U and 12L are made of a soft magnetic material in a cylindrical shape with a cylindrical hole portion 11 in the center for inserting the rotor portion 2. In this description, it is explained, for the purpose of illustration, that the stator yokes 12U and 12L are constructed as the “double decker construction.” Practically, these may be constructed from one yoke member to form one part corresponding to the stator yoke 12U and another part corresponding to the stator yoke 12L. Two stator yokes 12U and 12L may be formed separately and joined in double decker.
In the stator yoke 12U and 12L of the stator portion 3, there are provided annular hollow portions 13U and 13L each having a square cross-section, and annular grooves 14U and 14L penetrating from the inner periphery (facing to the hole portion 11) of the stator yoke 12U and 12L to the hollow portions 13U and 13L. An annular permanent magnet 15U is attached on the groove 14U of the stator yoke 12U and an annular permanent magnet 15L is attached on the groove 14L of the stator yoke 12L. Protrusions 16U1, 16U2, 16L1 and 16L2 made f magnetic material arranged in two stages by two longitudinally are provided on the hole portion 11 or the inner-side surface of the stator yoke 12U and 12L so as to sandwich the permanent magnet 15U and 15L in the axial direction. The inner periphery “b” of the protrusions 6U1, 16U2, 16L1 and 16L2 are configured so as to be opposed to the outer periphery “a” of the rotor yoke 4 and each part of the inner periphery “b” for the protrusions 6U1, 16U2, 16L1 and 16L2 is slightly longer than the length L of the outer periphery “a” in the circumferential direction.
Protrusions 16U1 and 16U2 of the stator yoke 12U and protrusions 16L1 and 16L2 of the stator yoke 12L are arranged so as to shift by a half pitch each other in the circumferential direction with respect to the central axis of the stator yokes 12U and 12L. The protrusions 16U1, 16U2, 16L1 and 16L2 are also arranged so as to form equally-spaced angular intervals along the inner-side face of the stator yokes 12U and 12L in the circumferential direction about the center axis of the stator yokes 12U and 12L and be spaced in the same length with the width of each inner periphery “b” of the protrusions 16U1, 16U2, 16L1 and 16L2. In the hollow portions 13U and 13L, there are provided wound portions 17U and 17L respectively. The wound portion 17U has a wound in the circumferential direction multiply and both ends of the wire (not shown) are drawn from the stator yoke 12U to the outsid. The wound portion 17L similarly has a wound and both ends of the wire (not shown) are drawn from the stator yoke 12L to the outside. Each of the wires leads electric current generated by the electric generator 1 to the outside.
In the example shown in
At the same time, in the example shown in
The protrusions 16U1 and 16U2 of the stator portion 3 shown in
In the electric generator 1, as shown in
As shown in
In such a state S1, since the stator yoke 12U of the stator portion 3 is not affected so much by the attractive force from the protrusions 8U and 9 of the rotor portion 2, most of the magnetic flux from the permanent magnet 15U of the stator yoke 12U forms, as shown in
Consequently, as shown in
In the state S1 as described above, changes are happened on the wound portions 17U and 17L such that most of the magnetic flux of the permanent magnet 15L having passed around the wound portion 17L until just before the state S1 is absorbed into the rotor portion 2 side to become weak and that the magnetic flux of the permanent magnet 15U having directed to the rotor portion 2 side until just before the state S1 returns to the wound portion 17 U of the stator portion 3 to become intensive. Accordingly, an electric current flows through the wound portions 17U and 17L so as to generate magnetic lines counteracting the changes of the magnetic flux. It will be describe in detail about the current flowing through the wound portion 17U and 17L.
As shown in
In the state S2, a part of magnetic flux of the permanent magnet 7L of the rotor portion 2, which has directed to the stator yoke 12 side of the stator portion 3 in the state S1, passes through the hollow portion 5 to return the rotor 2 side. A part of the magnetic flux of the permanent magnet 15L also becomes to pass around the wound portion 17L. That is, compared to the state S1, a magnetic path M6 is formed by weak magnetic lines directing from the north pole of the permanent magnet 7L of the rotor portion 2 side to the south pole of the permanent magnet 15L of the stator portion 3 side and from the north pole of the permanent magnet 15L of the stator portion 3 side to the south pole of the permanent magnet 7L of the rotor portion 2 side. The magnetic flux of the magnetic path M7 passing around the wound portion 17 is made intensive as compared to the state S1 (shown as S1: thick dashed-dotted lines to S2: thin dashed-dotted lines). The magnetic path M2 described above is yielded in the rotor portion 2 opposing to the protrusions 16L1 and 16L2 of the stator portion 3 and its intensity becomes weak. In the state S1, a magnetic path M9 described below is also yielded and its intensity is becoming intensive.
In the state S2 as described above, compared to the state S1, changes are happened such that the magnetic flux passing around the wound portion 17U is made weak and that the magnetic flux passing around the wound portion 17L is made intensive. so that an electric current flows so as to generate magnetic lines counteracting L the changes of the magnetic flux. Since the permanent magnets 7U and 7L of the rotor portion 2 are arranged for opposing portions to be different and to be connected by the hollow portion 5, the magnetic flux of the respective permanent magnets 7U and 7L directs to the stator portion 3 effectively.
As shown in
As shown in
A magnetic path M10 is also formed such that the magnetic flux of the permanent magnet 15U of the stator yoke 12U of the stator portion 3 directs to the protrusion 9 of the rotor portion 2 and the magnetic flux of the permanent magnet 7U of the rotor portion 2 directs from the protrusion 8U of the rotor portion 2 to the protrusion 16U1 of the stator portion 3.
In the state S3 as described above, changes are happened on the wound portions 17U and 17L such that most of the magnetic flux of the permanent magnet 15U having passed around the wound portion 17U until just before the state S3 is absorbed into the rotor portion 2 side to become weak and that the magnetic flux of the permanent magnet 15L having directed to the rotor portion 2 side until just before the state S3 returns to the magnetic path passing around the wound portion 17 U of the stator portion 3 to become intensive to form a magnetic path M8. Accordingly, an electric current flows through the wound portions 17U and 17L so as to generate magnetic lines counteracting the changes of the magnetic flux.
In
Therefore, at time t1, as shown in
In
Therefore, at the time t5 as shown in
The time t3 corresponds to the state S2 shown in
The times t2 and t4 correspond to transitions from the state S1 to the state S2 and from the state S2 to the state S3 respectively. Therefore, at the time t2 as shown in
In this way, at the times t1 to t5, a current occurs in a quarter cycle of a sinusoidal waveform to be generated on the wound portions 17U and 17L. That is, when the rotation shaft 10 of the electric generator 1 is rotating in a constant rate, one cycle part of the sinusoidal current waveform to be generated on the wound portion 17U and 17L is completed in four times periods of the times t1 to t5.
Here, considering the reason why cogging is generated in a general electric generator, cogging would be caused by changing of attractive or repulsive force between a rotor side and a stator side according to the rotor position. According to the electric generator 1 of this embodiment on the other hand, the attractive force will be constant between protrusions 8U, 8 and 8L of the rotor portion 2 and protrusions 16U1, 16U2, 16L1 and 16L2 of the stator portion 3 in any positional relationship of the rotor portion 2 and the stator portion 3 at the times t1 to t5.
For example, at the time t1 (the state S1), the lower half of the protrusion 9 of the rotor portion 2 and the protrusion 8L of the same are fully opposed to the protrusions 16L1 and 16L2 of the stator portion 3 and are attracting them in the maximum attractive force. On the other hand, the protrusion 16U1 and 16U2 of the stator portion 3 are not opposed to any of the protrusions 8U, 9 and 8L of the rotor portion 2 and the attractive force therebetween becomes a minimum. Therefore, it can be considered that the strength of the attractive force between the protrusions 8U, 9 and 8L of the rotor portion 2 side and the protrusions 16U1, 16U2, 16L1 and 16L2 of the stator portion 3 side depend on the total of the strengths of the opposing and non-opposing areas therebetween.
Supposing Q cm2 (square centimeter) as a maximum value of an area where the protrusion 16U1, 16U2, 16L1 or 16L2 of the stator portion 3 is opposed to the protrusions 8U, 9, and 8L of the rotor portion 2, and P1 as strength of attractive force per 1 cm2 unit, then, at the time t1, the opposing area between the lower half of the protrusion 9 of the rotor portion 2 and the protrusion 16L1 of the stator portion 3 becomes Q cm2 and the attractive force becomes Q×P1. The opposing area between the protrusion 8L of the rotor portion 2 and the protrusion 16L2 of the stator portion 3 also becomes Q cm2 and the attractive force becomes Q×P1. The non-opposing area between the protrusion 8L of the rotor portion 2 and the protrusion 16U1 of the stator portion 3 and the non-opposing area between the upper half of the protrusion 9 of the rotor portion 2 and the protrusion 16U2 of the stator portion 3 are Q cm2 respectively and the attractive forces become Q×P2 respectively where P2 is strength of attractive force per 1 cm2 unit. Therefore, the attractive force between the rotor portion 2 and stator portion 3 becomes 2Q×P1+2Q×P2=2Q(P1+P2) at the time t1 on each of the protrusions 8U, 9, 8L, 16U1, 16U2, 16L1 and 16L2.
Similarly, at the time t2, the protrusion 8U of the rotor portion 2 is opposed to the protrusions 16U1 of the stator portion 3 at respective quarters in the circumferential direction, the protrusion 9 of the rotor 2 is opposed to the protrusion 16U2 of the stator portion 3 at a quarter in the circumferential direction of the upper half of the former and a quarter in the same direction of the latter, the protrusion 9 of the rotor 2 is opposed to the protrusion 16L1 of the stator portion 3 at three quarters in the circumferential direction of the lower half of the former and three quarters in the same direction of the latter, and the protrusion 8L of the rotor 2 is opposed to the protrusion 16L2 of the stator portion 3 at three quarters in the circumferential direction of the former and three quarters in the same direction of the latter to attract each other.
In this case, the opposing areas are (¼)Q cm2 for between the protrusion 8U of the rotor portion 2 and the protrusion 16U1 of the stator 3 and for between the upper half of the protrusion 9 of the rotor portion 2 and the protrusion 16U2 of the stator 3 respectively, and (¾)Q cm2 for between the lower half of the protrusion 9 of the rotor portion 2 and the protrusion 16L1 of the stator 3 and for between the protrusion 8L of the rotor portion 2 and the protrusion 16L2 of the stator 3 respectively. Therefore, at the time t1, the total attractive force between the rotor portion 2 and stator portion 3 on the opposing parts of each of the protrusions 8U, 9, 8L, 16U1, 16U2, 16L1 and 16L2 becomes as follows:
On the other hand, the attractive force of the non-opposing parts can be similarly calculated to become 2Qcm2×P1. Therefore, the attractive force at the time 2 becomes 2Q×P1+2Q×P2=2Q(P1+P2) same as that at the time t1.
Similarly, at time t3, the protrusion 8U of the rotor portion 2 is opposed to the protrusions 16U1 of the stator portion 3 at respective halves in the circumferential direction, the protrusion 9 of the rotor 2 is opposed to the protrusion 16U2 of the stator portion 3 at a half in the circumferential direction of the upper half of the former and a half in the same direction of the latter, the protrusion 9 of the rotor 2 is opposed to the protrusion 16L1 of the stator portion 3 at a half in the circumferential direction of the lower half of the former and a half in the same direction of the latter, and the protrusion 8L of the rotor 2 is opposed to the protrusion 16L2 of the stator portion 3 at respective halves in the circumferential direction to attract each other.
In this case, the opposing areas are (¼)Q cm2 for between the protrusion 8U of the rotor portion 2 and the protrusion 16U1 of the stator 3, for between the upper half of the protrusion 9 of the rotor portion 2 and the protrusion 16U2 of the stator 3, for between the lower half of the protrusion 9 of the rotor portion 2 and the protrusion 16L1 of the stator 3 and for between the protrusion 8L of the rotor portion 2 and the protrusion 16L2 of the stator 3 respectively. Therefore, at the time t3, the total attractive force between the rotor portion 2 and stator portion 3 on the opposing parts of each of the protrusions 8U, 9, 8L, 16U1, 16U2, 16L1 and 16L2 becomes as follows:
On the other hand, the attractive force of the non-opposing parts, which are parts of the stator portion 3 other than the protrusions 16U1, 16U2, 16L1 and 16L2 being opposed to the protrusions 8U, 8 and 8L, becomes 2Qcm2×P2 as the area of the non-opposing parts becomes Q2 cm2. Therefore, the total attractive force at the time t3 becomes 2Q(P1+P2) same as that at the times t1 and t2.
Similarly, at time t4, the protrusion 8U of the rotor portion 2 is opposed to the protrusions 16U1 of the stator portion 3 at respective three quarters in the circumferential direction, the protrusion 9 of the rotor 2 is opposed to the protrusion 16U2 of the stator portion 3 at three quarters in the circumferential direction of the upper half of the former and three quarters in the same direction of the latter, the protrusion 9 of the rotor 2 is opposed to the protrusion 16L1 of the stator portion 3 at a quarter in the circumferential direction of the lower half of the former and a quarter in the same direction of the latter, and the protrusion 8L of the rotor 2 is opposed to the protrusion 16L2 of the stator portion 3 at respective quarters in the circumferential direction to attract each other.
In this case, the opposing areas are (¾)Q cm2 for between the three quarters of the protrusion 8U of the rotor portion 2 and the three quarters of the protrusion 16U1 of the stator 3 and for between the three quarters of the upper half of the protrusion 9 of the rotor portion 2 and the three quarters of the protrusion 16U2 of the stator 3 respectively, and (¼) Q cm2 for between the quarter of the lower half of the protrusion 9 of the rotor portion 2 and the quarter of the protrusion 16L1 of the stator 3 and for between the quarter of the protrusion 8L of the rotor portion 2 and the quarter of the protrusion 16L2 of the stator 3 respectively. Therefore, at the time t4, the total area of the fully opposing parts of the protrusions 8U, 9, 8L, 16U1, 16U2, 16L1 and 16L2 between the rotor portion 2 and stator portion 3 is as follows:
Therefore, the attractive force caused by the protrusions being opposed each other becomes 2Q×P1. On the other hand, the area of the protrusions 8U, 9 and 8L of the rotor portion 2 being opposed to the protrusions 16U1, 16U2, 16L1 and 16L2 of the stator portion 3 becomes 2Qcm2 so that the total attractive force becomes 2Q(P1+P2) same as that at the times t1, t2 and t3.
Similarly, at time t3 (the state S3), the upper half of the protrusion 9 of the rotor 2 and the protrusion 8U of the same is opposed to the protrusions 16U1 and 16U2 of the stator portion 3 and attract therebetween, but the protrusions 16L1 and 16L2 of the stator portion 3 are not opposed to any of the protrusions 8U, 9 and 8L of the rotor portion 2. In this case, the opposing areas are Q cm2 for between the upper half of the protrusion 9 of the rotor portion 2 and the protrusion 16U2 of the stator 3 and for between the protrusion 8U of the rotor portion 2 and the protrusion 16U1 of the stator 3 respectively. Therefore, at the time t5, the total area of the fully opposing parts of the protrusions 8U, 9, 8L, 16U1, 16U2, 16L1 and 16L2 between the rotor portion 2 and stator portion 3 is as follows:
Qcm2+Qcm2=2Qcm2
Therefore, the attractive force caused by the protrusions being opposed each other becomes 2Q×P1. On the other hand, the area of the protrusions 8U, 9 and 8L of the rotor portion 2 being opposed to the protrusions 16U1, 16U2, 16L1 and 16L2 of the stator portion 3 becomes 2Qcm2 so that the total attractive force becomes 2Q(P1+P2) same as that at the times t1, t2, t3 and t3.
As described above, the total attractive force between the rotor portion 2 and the stator portion 3 on each of the protrusions 8U, 9, 8L, 16U1, 16U2, 16L1 and 16L2 does not change at any of the times t1 to t5 shown in
The electric generator in which no cogging occurs as described above can generate power in high efficiency because rotation torque applied on the rotation shaft 10 from outside is not reduced by cogging torque and most of it is used a torque for electric generation.
In the electric generator 1, the hollow portion 5 of the rotor portion 2 is continuously passing through the two permanent magnets 7U and 7L. According to this, as shown in
The embodiment described above can be modified in various ways without departing from the scope of the invention. For example, the hollow portion 5 may not be hollow and be embedded by non-magnetic material such as aluminum or resin material. Although it has been described that each of the protrusions 8U, 9 and 8L is formed integrally with the body of the yoke 4 and each of the protrusions 16U1, 16U2, 16L1 and 16L2 is formed integrally with the body of the yoke 12U and 12L, each protrusion may not be formed integrally but be made as a separated member and fixed on the respective body by such as glue.
In the embodiment shown in
In this case, the rotor portion 2B may be configured by arranging to pile one rotor member having protrusions 8U1 and 8U2 along the central axis direction with a same pitch and another rotor member having protrusions 8L1 and 8L2 with the same pitch linearly arranged in the axial direction, in two stages, such that the protrusion 8U1 and 8U2 are shifted a half pitch with the protrusions 8L1 and 8L2. The stator portion 3B may also be configured by arranging to pile one stator member having protrusions 16U and 16M1 with a same pitch linearly arranged in the axial direction and another stator member having protrusions 16M2 and 16L with the same pitch linearly arranged in the axial direction, in two stages, such that the protrusion 16U, 16M1, 16M2 and 16L are linearly arranged in the axial direction and have the same pitch. The rotor portion 2B and/or the stator portion 3B may be made from on yoke member by, for example, cutting out.
Although it has been described that each of the electric generators 1 and 1B comprises the stator portion 3 having a two stage piled structure of the stator yokes 12U and 12L, the number of the piled stages may be any even number. In this case, the rotor portion part 2 preferably has a construction in that the structure shown in
Although it has been described that each of the electric generators 1 and 1B is an inner rotor type generator, an outer rotor type generator may be adopted. Although the rotor yoke 4 and the stator yokes 12U, 12L are preferable made of soft magnetic material, these may be made by simple magnetic material. Grooves 6U, 6L, 14U and 14L may not be grooved if each of them is formed integrally with the permanent magnet but these are called as “grooves” including ones formed integrally. Although the axial length of the hollow portion 5 as a non-magnetic portion is set equal or longer than the axial distance between the outer ends of the combination of the permanent magnetics 7U and 7L, it may be equal to, slightly longer or slightly shorter that the axial distance between the outer ends of the permanent magnetics 7U and 7L. Although the width of each protrusion and the distance between protrusions are preferably equal for cogging to be suppressed, the width the distance may not be equal and be set slightly different by another requirement.
As shown in
The state shown in
Similarly, in the electric generator 1, since the permanent magnet 15U is provided on the stator yoke 12U, the magnetic flux of the permanent magnet 15U forms the magnetic path M1 around the wound portion 17U on the state S1 so that the magnetic flux around the wound portion becomes intensive. On the other hand, in the electric generator 1C, since the permanent magnet 15U is not provided on the stator yoke 12CU, the magnetic flux of the permanent magnet 7U of the rotor portion 2U extends into the stator yoke 12CU side to form the magnetic path M16 but the protrusions 16U1 and 16U2 of the stator portion 3C are not opposed to the protrusions 8U and 9 so that the magnetic flux around the wound portion 17U becomes weak.
As described above, it can been seen that the intensity states of the magnetic flux on the wound portion 17U and 17L are reversed between the electric generators 1 and 1C. Thus, the waveform shown in
Number | Date | Country | Kind |
---|---|---|---|
2011-275628 | Dec 2011 | JP | national |
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/JP2012/082566 | 12/14/2012 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2013/089248 | 6/20/2013 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
4920294 | Christiaens et al. | Apr 1990 | A |
7057323 | Horst | Jun 2006 | B2 |
7088029 | Hiramatsu | Aug 2006 | B2 |
7365472 | Hiramatsu | Apr 2008 | B2 |
20020175580 | Ogino | Nov 2002 | A1 |
20060006744 | Nashiki | Jan 2006 | A1 |
20110070108 | Arita et al. | Mar 2011 | A1 |
Number | Date | Country |
---|---|---|
1615572 | May 2005 | CN |
2706952 | Jun 2005 | CN |
1986-052488 | Apr 1986 | JP |
H08-214519 | Aug 1996 | JP |
09131040 | May 1997 | JP |
2002-191160 | Jul 2002 | JP |
2002-247818 | Aug 2002 | JP |
2006-025559 | Jan 2006 | JP |
2006-101695 | Apr 2006 | JP |
2009-033930 | Feb 2009 | JP |
WO-2009-136574 | Nov 2009 | WO |
Entry |
---|
Chinese Office Action (with English Translation) for Chinese Application No. 201280068570.3 dated Dec. 29, 2015 (11 pages). |
Number | Date | Country | |
---|---|---|---|
20150200573 A1 | Jul 2015 | US |