Redundant resolver and rotation angle detection device using same

This application is a National Stage of International Application No. PCT/JP2017/045866, file Dec. 21, 2017, the contents of all of which are incorporated herein by reference in their entirety.

The present invention relates to a redundant resolver that utilizes a change in permeance in a gap between a rotor and a stator, and to a rotation angle detection device in which the redundant resolver is used.

In order to achieve redundancy of a resolver used in a rotation angle detection device, a case wherein two resolvers are stacked in two tiers is disclosed in, for example, JP-A-2009-281818 (Patent Literature 1). Also, a redundant resolver including two pairs of stators and rotors in a radial direction is disclosed in, for example, JP-A-2007-189834 (Patent Literature 2) and JP-A-2009-222435 (Patent Literature 3). Furthermore, a redundant resolver wherein an output winding is configured of a first system winding and a second system winding, and the winding of only either one of the systems is wound around one tooth, is disclosed in, for example, JP-A-2013-247828 (Patent Literature 4) and JP-A-2013-53890 (Patent Literature 5). Also, although not specifically disclosing the present invention, research wherein, when both a four-pole excitation winding and a two-pole output winding are provided in a stator, and a rotor form is such that a change in gap permeance with respect to a position in a circumferential direction is appropriate, a two-phase voltage whose amplitude changes in a sinusoidal waveform in accordance with a position of the rotor, with the whole circumference as one cycle, is obtained in the output winding, with the rotor being of a simple structure of only an iron core with no winding, has been announced by Akira Ishizaki and three others in “The Transactions of the Institute of Electrical Engineers of Japan D”, 1995, Volume 115, Issue 5, pages 598 to 604, “Theory and Characteristics on Novel Variable Reluctance 1X Resolver” (Non-patent Literature 1).

Patent Literature 1: JP-A-2009-281818 Patent Literature 2: JP-A-2007-189834 Patent Literature 3: JP-A-2009-222435 Patent Literature 4: JP-A-2013-247828 Patent Literature 5: JP-A-2013-53890 Non-patent Literature: “The Transactions of the Institute of Electrical Engineers of Japan D”, 1995, Volume 115, Issue 5, pages 598 to 604, “Theory and Characteristics on Novel Variable Reluctance 1X Resolver”, Akira Ishizaki and three others

The redundant resolver disclosed in Patent Literature 1 is such that two resolvers are configured by stators and rotors thereof being stacked in two tiers via a shaft, because of which there is a problem in that an axial direction dimension increases twofold in comparison with that of a one-system resolver.

Also, the redundant resolver disclosed in Patent Literature 2 and 3 is such that redundancy is achieved by a first system rotor, a first system stator, a second system stator, and a second system rotor being disposed in order from an inner side of the resolver, because of which the stator is duplicated and a number of windings increases. Because of this, there is a problem in that manufacturability worsens, and cost increases.

Furthermore, the redundant resolver disclosed in Patent Literature 4 and 5 is such that a first system output winding and a second system output winding are alternately wound around teeth, because of which there is a problem in that an output signal of one of the systems is not an ideal sinusoidal wave, and angle detection accuracy worsens.

The invention, having been contrived in order to resolve the aforementioned problems, has an object of providing a redundant resolver such that a worsening of manufacturability and a cost increase are restricted, and angle detection accuracy is improved, while preventing an increase in an axial direction dimension caused by redundancy, and a rotation angle detection device in which the redundant resolver is used.

A redundant resolver according to the invention is characterized by being configured of a rotor and a stator that form a pair, wherein the rotor is a rotor with a shaft angle multiplier of Nx having Nx (Nx is a natural number) salient poles, the stator is such that n teeth, where n is a natural number, are disposed sequentially in a circumferential direction, configuring M systems by being divided into M in the circumferential direction, and having an angle of 360/M degrees when angles of the teeth configuring one system are totaled, a one-phase excitation winding and a two-phase output winding are wound around each of the n teeth, excitation signals of the same frequency are applied by differing excitation circuits to the respective excitation windings, an output order per system is Nout (Nout is a natural number), and an abnormality is detected based on output signals of the M systems.

The redundant resolver according to the invention is of a structure formed of a stator and a rotor that form a pair, wherein redundancy is achieved by dividing the stator in a circumferential direction, and an output order per system is Nout (Nout is a natural number), because of which a worsening of manufacturability and a cost increase are restricted, and angle detection accuracy can be improved, while preventing an increase in an axial direction dimension caused by redundancy.

FIG. 1 is a drawing showing a configuration of a rotation angle detection device in which a redundant resolver according to a first embodiment of the invention is used.

FIG. 2 is a sectional view of the redundant resolver according to the first embodiment of the invention.

FIG. 3 is a sectional view of a stator of the redundant resolver according to the first embodiment of the invention.

FIG. 4 is a block configuration diagram of the rotation angle detection device in which the redundant resolver according to the first embodiment of the invention is used.

FIG. 5 is a drawing showing numbers of turns of excitation windings of the redundant resolver according to the first embodiment of the embodiment.

FIG. 6 is a drawing showing numbers of turns of output windings of the redundant resolver according to the first embodiment of the embodiment.

FIG. 7 is a drawing showing gap magnetic flux densities of the redundant resolver according to the first embodiment of the invention.

FIG. 8 is a drawing showing output windings of the redundant resolver according to the first embodiment of the invention.

FIG. 9 is a drawing showing output winding interlinkage flux of the redundant resolver according to the first embodiment of the invention.

FIG. 10 is a sectional view of a redundant resolver according to a second embodiment of the invention.

FIG. 11 is a drawing showing numbers of turns of excitation windings of the redundant resolver according to the second embodiment of the invention.

FIG. 12 is a drawing showing numbers of turns of output windings of a redundant resolver according to a third embodiment of the invention.

FIG. 13 is a drawing showing gap interlinkage flux density of the redundant resolver according to the third embodiment of the invention.

FIG. 14 is a drawing showing output windings of the redundant resolver according to the third embodiment of the invention.

FIG. 15 is a drawing showing output winding interlinkage flux of the redundant resolver according to the third embodiment of the invention.

FIG. 16 is a drawing showing a relationship between an excitation signal phase difference and an angle error of a redundant resolver according to a fourth embodiment of the invention.

FIG. 17 is a sectional view of a stator of a redundant resolver according to a fifth embodiment of the invention.

FIG. 18 is a drawing showing numbers of turns of output windings of the redundant resolver according to the fifth embodiment of the embodiment.

FIG. 19 is a sectional view of a stator of a redundant resolver according to a sixth embodiment of the invention.

FIG. 20 is a drawing showing numbers of turns of output windings of the redundant resolver according to the sixth embodiment of the embodiment.

Hereafter, preferred embodiments of a redundant resolver according to the invention, and a rotation angle detection device in which the redundant resolver is used, will be described in detail with reference to the drawings. In the embodiments, identical or corresponding portions are described using the same reference number, but a redundant description may be omitted in one portion.

First Embodiment

FIG. 1 is a drawing showing a configuration of a rotation angle detection device in which a redundant resolver according to a first embodiment of the invention is used, FIG. 2 is a sectional view of the redundant resolver according to the first embodiment, and FIG. 3 is a sectional view of a stator of the redundant resolver according to the first embodiment. Also, FIG. 4 is a block configuration diagram of the rotation angle detection device in which the redundant resolver according to the first embodiment is used.

As shown in FIG. 1 , a rotation angle detection device 100 according to the first embodiment is configured to include an angle computing unit 1 and a redundant resolver (hereafter called simply a resolver) 2 . The resolver 2 is configured of a stator 3 and a rotor 4 , which form a pair, and the stator 3 includes a winding 5 . The rotor 4 of the resolver 2 is connected to a rotating electrical machine 7 , or to rotating units of various devices, via a shaft 6 .

The resolver 2 is such that a number Ns of teeth T 1 to T 14 (hereafter, “to” is represented as “˜”) of the stator 3 is fourteen, and a number Nx of salient poles of the rotor 4 is five, as shown in FIG. 2 . The salient pole number Nx is also called a shaft angle multiplier. Also, the teeth T 1 to T 14 of the stator 3 are divided into two in a circumferential direction, as shown in FIG. 3 , configuring a first system and a second system, as shown in FIG. 4 , and the resolver 2 configures a dual system redundant resolver. That is, a total angle of teeth per system is 360°/2=180°.

The teeth T 1 to T 7 of the stator 3 are first system teeth, and the teeth T 8 to T 14 of the stator 3 are second system teeth, as shown in FIG. 3 . A one-phase excitation winding and a two-phase output winding are wound around each tooth. That is, first system excitation windings R 1 to R 7 , first first system output windings Sa 1 to Sa 7 , and second first system output windings Sb 1 to Sb 7 are wound around the first system teeth T 1 to T 7 , as shown in FIG. 3 and FIG. 4 . In the same way, second system excitation windings R 8 to R 14 , first second system output windings Sa 8 to Sa 14 , and second second system output windings Sb 8 to Sb 14 are wound around the second system teeth T 8 to T 14 .

The first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 are connected to a first system excitation circuit 10 and a second system excitation circuit 11 respectively via an output terminal 9 a provided in an extended portion 8 of the resolver 2 . The first system excitation circuit 10 and the second system excitation circuit 11 provide alternating current voltage of the same amplitude and frequency to the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 respectively. The first first system output windings Sa 1 to Sa 7 , the second first system output windings Sb 1 to Sb 7 , the first second system output windings Sa 8 to Sa 14 , and the second second system output windings Sb 8 to Sb 14 are connected to a first system angle computing unit 1 a and a second system angle computing unit 1 b respectively via an output terminal 9 b provided in the extended portion 8 of the resolver 2 . The arrangement of the output terminal 9 a and the output terminal 9 b is one example, and an arrangement may be arbitrary, such as the output terminal 9 a and the output terminal 9 b being arranged in reverse laterally, or being arranged alternately, in, for example, FIG. 2 .

The first system angle computing unit 1 a and the second system angle computing unit 1 b calculate and output a first system detected angle θ 1 and a second system detected angle θ 2 of the rotor 4 based on output voltages of the two-phase output windings Sa 1 to Sa 7 and Sa 8 to Sa 14 , and Sb 1 to Sb 7 and Sb 8 to Sb 14 , of the resolver 2 . Furthermore, the first system angle computing unit 1 a and the second system angle computing unit 1 b are each connected to an abnormality determiner 12 , and an abnormality such as a failure is detected based on values of the first system detected angle θ 1 and the second system detected angle θ 2 .

The resolver 2 according to the first embodiment is configured in such a way that the one-phase excitation winding, that is, the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 , is wound first around the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 respectively, and the two-phase output winding, that is, the first first system output windings Sa 1 to Sa 7 and the second first system output windings Sb 1 to Sb 7 , and the first second system output windings Sa 8 to Sa 14 and the second second system output windings Sb 8 to Sb 14 , is wound on top of the one-phase excitation winding. The first first system output windings Sa 1 to Sa 7 , the second first system output windings Sb 1 to Sb 7 , the first second system output windings Sa 8 to Sa 14 , and the second second system output windings Sb 8 to Sb 14 may be wound in any order, as may the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 .

Insulation between the windings and an iron core is carried out using an insulator (insulating paper, a coating, or the like) 13 . There is a case in which teeth around which either one-phase output winding of the two-phase output winding is not wound are provided among the teeth T 1 to T 14 of the resolver 2 . Insulation between winding phases is carried out using insulating paper or the like. The first system excitation windings R 1 to R 7 are connected in series, and the first first system output windings Sa 1 to Sa 7 and the second first system output windings Sb 1 to Sb 7 are also connected in series. In the same way, the second system excitation windings R 8 to R 14 are connected in series, and the first second system output windings Sa 8 to Sa 14 and the second second system output windings Sb 8 to Sb 14 are also connected in series.

Herein, it is assumed that the respective windings are connected in series in order of the teeth T 1 to T 7 . However, even if first wound teeth are arbitral teeth, respectively and adjacent teeth are connected in order in series, the same advantage can be obtained.

According to this kind of configuration, redundancy can be achieved with an axial direction dimension equivalent to that of a normal one-system angle detection device. Also, an increase in a number of coils can be restricted, because of which advantages are obtained in that manufacturing is easy, and a cost increase can be restricted.

Also, the resolver 2 according to the first embodiment is such that a one-phase excitation winding and a two-phase output winding are wound aligned in the circumferential direction, but not being limited to this, the same advantages can be obtained by aligning in a radial direction, or changing a winding order for each tooth.

FIG. 5 is a drawing showing a turn number distribution of the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 of the resolver 2 according to the first embodiment. In FIG. 5 , the numbers of turns of the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 wound around the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 respectively are shown consecutively.

Generally, a winding direction (+) and a winding direction (−) are defined for a resolver excitation winding. When a direction of a winding of a certain coil is represented by the winding direction (+), a coil wherein the winding is wound in the reverse direction is expressed as the winding direction (−). Absolute values of a number of turns in the winding direction (+) and a number of turns in the winding direction (−) are the same. That is, when the number of turns in the winding direction (+) is +X turns, the number of turns in the winding direction (−) is −X turns. The number of turns of an excitation winding is standardized by the amplitude of the number of turns.

The resolver 2 according to the first embodiment is such that excitation windings are repeatedly wound Ne times around the stator 3 , wherein the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 are combined, in units of two teeth, a (+) and a (−). That is, as the number of teeth T 1 to T 14 of the stator 3 is fourteen, a spatial order of the excitation windings is Ne=7. Therefore, a spatial order Ne 1 of the first system excitation windings R 1 to R 7 is 3.5, and a spatial order Ne 2 of the second system excitation windings R 8 to R 14 is 3.5.

The resolver 2 according to the first embodiment is such that an excitation order per system is N±0.5 (N is a natural number), and the shaft angle multiplier is an odd number.

According to this kind of configuration, a magnetic flux that interlinks in a gap between the stator 3 and the rotor 4 can have a sinusoidal waveform, because of which rotation angle detection accuracy can be improved.

Also, an example wherein excitation windings are repeatedly wound Ne times around the stator 3 , wherein the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 are combined, in units of two teeth, a (+) and a (−), has been described here, but not being limited to this, the same advantages can be obtained when excitation winding (+) and (−) are repeated with a factor of the number of teeth of the stator 3 as one unit.

FIG. 6 is a drawing showing a turn number distribution of the first first system output windings Sa 1 to Sa 7 , the second first system output windings Sb 1 to Sb 7 , the first second system output windings Sa 8 to Sa 14 , and the second second system output windings Sb 8 to Sb 14 . Herein, in FIG. 6 , the numbers of turns of the output windings wound around the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 are shown consecutively. A number of turns N Sa1i of the first first system output winding and a number of turns N Sb1i of the second first system output winding wound around an i th tooth can each be expressed by Equation (1). Also, a number of turns N Sa1i of the first second system output winding and a number of turns N Sb2i of the second second system output winding can be expressed by the same kind of equation as the number of turns N Sa1i of the first first system output winding and the number of turns N Sb1i of the second first system output winding.

Herein, N 1 is the amplitude of the number of turns of the output winding, and θ teeth represents a circumferential direction position of the tooth.

The output windings are distributed in a sinusoidal waveform in the circumferential direction of the teeth. When the number of turns is a decimal number, this is changed to an integer by rounding down or rounding up. In FIG. 6 , the number of turns of an output winding is standardized by the amplitude thereof, that is, by N 1 .

When the number of pole pairs of the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 is Ne, and the number of salient poles of the rotor 4 is Nx, magnetomotive force is of a space Ne order, and gap permeance is of an Nx order. Herein, the space A order represents a component of an A cycle within a mechanical angle of 360 degrees. The number of pole pairs Ne is the number of magnetic pole pairs of the stator 3 . A magnetic flux is generated in a gap by an alternating excitation current flowing into the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 of the resolver 2 , the magnetic flux interlinks with each output winding, and a voltage is generated in the first first system output windings Sa 1 to Sa 7 , the second first system output windings Sb 1 to Sb 7 , the first second system output windings Sa 8 to Sa 14 , and the second second system output windings Sb 8 to Sb 14 . When the position of the rotor 4 changes, the gap permeance changes, and a voltage change occurs in the first first system output windings Sa 1 to Sa 7 , the second first system output windings Sb 1 to Sb 7 , the first second system output windings Sa 8 to Sa 14 , and the second second system output windings Sb 8 to Sb 14 .

Angle detection is carried out from the output winding wound around each tooth. An envelope curve thereof is called output voltage. A magnetic flux density of a gap can be expressed by the product of magnetomotive force and gap permeance. As both magnetomotive force and permeance are trigonometric functions, the magnetic flux density is in the order of the trigonometric function of the product of the two. That is, it is seen from a trigonometric function product-sum expression that the spatial order of the magnetic flux density of the gap is |Ne±Nx|. Herein, |X| represents an absolute value of X. When the spatial order of the magnetic flux density of the gap and the spatial order of the output winding coincide, output winding interlinkage flux is generated from the orthogonality of the trigonometric functions. As the excitation current is an alternating current, voltage is generated in the output winding, and the angle can be detected.

As previously mentioned, magnetic flux of a spatial order equivalent to |Ne±Nx|, of magnetic flux generated in a gap, needs to be picked up in order to function as the resolver 2 . This is also mentioned in, for example, page 599, “2-1: Principles” of Non-patent Literature 1. As is understood from Equation (7) of Non-patent Literature 1, what changes in accordance with a rotation angle φ is equivalent to |Ne±Nx|. Equation 2 below shows Equation (7) of Non-patent Literature 1, to which remarks have been added.

Math . ⁢ 2 ⁢ B = 6 ⁢ W e ⁢ k w ⁢ ⁢ 1 ⁢ I 4 ⁢ π ⁢ P 01 ⁢ ⁢ sin ⁡ ( θ 1 + ψ ) ⁢ cos ⁡ ( ω ⁢ ⁢ t ) + 6 ⁢ W e ⁢ k w ⁢ ⁢ 1 ⁢ I 2 ⁢ π ⁢ P 00 ⁢ ⁢ sin ⁡ ( 2 ⁢ θ 1 ) ⁢ cos ⁡ ( ω ⁢ ⁢ t ) + 6 ⁢ W e ⁢ k w ⁢ ⁢ 1 ⁢ I 4 ⁢ π ⁢ P 01 ⁢ ⁢ sin ⁡ ( 3 ⁢ θ 1 - ψ ) ⁢ cos ⁡ ( ω ⁢ ⁢ t ) . ( Equation ⁢ ⁢ 2 )

The components of Equation 2 are as below:

B: magnetic flux density,

W e : total number of excitation winding turns,

K ω1 : winding coefficient with respect to fundamental wave,

I: effective value of excitation current,

θ 1 : coordinate set for stator, with origin in center of intermediate tooth of two neighboring excitation winding coils,

ψ: angle between origins of stator and rotor coordinates when rotor is stationary,

P 00 : gap between stator and rotor is gap permeance per unit area in minimum position,

P 01 : gap permeance per unit area when gap between stator and rotor is in other than minimum position.

That is, the resolver 2 in the first embodiment is such that the gap magnetic flux density necessary for angle detection is |7±5 1|=second order or twelfth order (equivalent to second order). Herein, a relationship of |2±Ns|=twelfth order is established between the second order and the twelfth order, which are the spatial orders of the gap magnetic flux density, because of which it can be said that the second and twelfth spatial orders of the gap magnetic flux density are equal. That is, in order to detect the rotation angle of the rotor 4 , it is necessary for the output windings to pick up one of the second or twelfth spatial orders, and herein, the rotation angle of the rotor 4 is detected with the second order as the spatial order of the output windings.

FIG. 7 shows, in simplified form, gap magnetic flux densities according to excitation signals applied to the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 of the resolver 2 according to the first embodiment. Also, FIG. 8 shows, consecutively and in simplified form, the number of turns of an output winding of the first system and the second system.

In FIG. 7 and FIG. 8 , the mechanical angle, which is on the horizontal axis, is such that a range of 0 to 180° represents the first system, and a range of 180 to 360° represents the second system. The resolver 2 is such that an angle is detected by magnetic flux interlinking in a gap being read by an output winding. Because of this, magnetic flux interlinking in the output windings can be calculated by multiplying the spatial interlinkage flux by the number of turns.

The magnetic flux interlinking in the output windings when the spatial interlinkage flux of FIG. 7 is read by the number of turns of FIG. 8 is shown in FIG. 9 . The waveform of the magnetic flux interlinking in the first system output windings of FIG. 9 and the waveform of the magnetic flux interlinking in the second system output windings are inverted. Because of this, offsets with opposite reference signs overlap in output signals from the first system output windings and the second system output windings. When the offsets are corrected in the angle computing unit 1 , the rotation angle can be accurately detected.

The resolver 2 in the first embodiment is such that a first system rotation angle, that is, the first system detected angle θ 1 , and a second system rotation angle, that is, the second system detected angle θ 2 , calculated based on the output signals from the first system output windings Sa 1 to Sa 7 and Sb 1 to Sb 7 and the output signals from the second system output windings Sa 8 to Sa 14 and Sb 8 to Sb 14 are mutually monitored in the abnormality determiner 12 , and an abnormality is detected when a failure such as a disconnection or a short-circuit occurs in an interior of the resolver 2 .

Specifically, the resolver 2 has thresholds α and β in the abnormality determiner 12 . When a relationship between the first system detected angle θ 1 calculated based on the first system output signal and the second system detected angle θ 2 calculated based on the second system output signal satisfies θ 1 +θ 2 >α or θ 1 −θ 2 >β, the abnormality determiner 12 determines that an abnormality such as a disconnection or a short-circuit has occurred in the interior of the resolver 2 .

Further, when a failure occurs in the first system of the resolver 2 , the application of an excitation signal to the first system excitation windings R 1 to R 7 is stopped. According to this kind of configuration, the failed first system is stopped, and the rotation angle can be detected in the same way as at a normal time based on the output signal of the normal second system. In the same way, when a failure occurs in the second system of the resolver 2 , the application of an excitation signal to the second system excitation windings R 8 to R 14 is stopped, whereby an advantage is obtained in that the rotation angle can be detected in the same way as at a normal time based on the output signal of the normal first system.

Heretofore, it has been assumed that there are fourteen slots and that the shaft angle multiplier is five, but this not being limiting, the same advantages can be obtained with other configurations.

Second Embodiment

Next, a rotation angle detection device in which a redundant resolver according to a second embodiment of the invention is used will be described.

FIG. 10 is a sectional view of the resolver 2 used in the rotation angle detection device 100 according to the second embodiment, wherein the number Ns of teeth of the stator 3 is sixteen, and the shaft angle multiplier Nx of the rotor 4 is six.

As shown in FIG. 10 , teeth T 1 to T 16 of the stator 3 are divided in four in a circumferential direction, and are configured of a first system first block B 1 , a second system first block B 2 , a first system second block B 3 , and a second system second block B 4 . The first system first block B 1 and the first system second block B 3 configure first system windings wherein windings wound around the teeth T 1 to T 4 and T 9 to T 12 of the respective blocks are connected in series. In the same way, the second system first block B 2 and the second system second block B 4 configure second system windings wherein windings wound around the teeth T 5 to T 8 and T 13 to T 16 of the respective blocks are connected in series, and the resolver 2 configures a dual system redundant resolver.

According to this kind of configuration, teeth configuring one system are disposed in opposing positions, because of which an imbalance in magnetic flux when the stator 3 is eccentric is moderated, an output signal is of a sinusoidal waveform, and angle detection accuracy can be improved.

FIG. 11 is a drawing showing a turn number distribution of first system excitation windings and second system excitation windings of the resolver 2 according to the second embodiment. Herein, in FIG. 11 , the numbers of turns of the excitation windings wound around the first system teeth T 1 to T 4 and T 9 to T 12 and the second system teeth T 5 to T 8 and T 13 to T 16 are shown consecutively.

Generally, a winding direction (+) and a winding direction (−) are defined for a resolver excitation winding. When a direction of a winding of a certain coil is represented by the winding direction (+), a coil wherein the winding is wound in the reverse direction is expressed as the winding direction (−). Absolute values of a number of turns in the winding direction (+) and a number of turns in the winding direction (−) are the same. That is, when the number of turns in the winding direction (+) is +X turns, the number of turns in the winding direction (−) is −X turns. The number of turns of an excitation winding is standardized by the amplitude of the number of turns.

The resolver 2 according to the second embodiment is such that excitation windings are repeatedly wound Ne times around the stator 3 , wherein the first system teeth T 1 to T 4 and T 9 to T 12 and the second system teeth T 5 to T 8 and T 13 to T 16 are combined, in units of two teeth, a (+) and a (−). That is, as the number of teeth of the stator 3 is sixteen, a spatial order of the excitation windings is Ne=8. Therefore, a spatial order Ne 1 of the first system excitation windings is 4, and a spatial order Ne 2 of the second system excitation windings is 4.

The resolver 2 according to the second embodiment is such that an excitation order per system is N (N is a natural number), and the shaft angle multiplier is an even number.

According to this kind of configuration, a magnetic flux that interlinks in a space between the stator 3 and the rotor 4 can have a sinusoidal waveform, because of which there is an advantage in that rotation angle detection accuracy can be improved.

Herein, it has been assumed that there are sixteen slots and that the shaft angle multiplier is six, but this not being limiting, the same advantages can be obtained with other configurations.

Also, in the same way as in the first embodiment, the resolver 2 according to the second embodiment also has the thresholds α and β in the abnormality determiner 12 , and when the relationship between the first system detected angle θ 1 calculated based on the first system output signal and the second system detected angle θ 2 calculated based on the second system output signal satisfies θ 1 +θ 2 >α or θ 1 −θ 2 >β, the abnormality determiner 12 can determine that an abnormality such as a disconnection or a short-circuit has occurred in the interior of the resolver 2 .

Third Embodiment

Next, a rotation angle detection device in which a redundant resolver according to a third embodiment of the invention is used will be described.

FIG. 12 is a drawing showing a turn number distribution of first first system output windings, second first system output windings, first second system output windings, and second second system output windings of the resolver 2 used in the rotation angle detection device according to the third embodiment.

In the same way as in FIG. 3 described in the first embodiment, the stator 3 of the resolver 2 according to the third embodiment is configured so that the number Ns of teeth is fourteen, wherein the teeth T 1 to T 7 form first system teeth and the teeth T 8 to T 14 form second system teeth, and a one-phase excitation winding and a two-phase output winding are wound around each tooth. That is, the first system excitation windings R 1 to R 7 , the first first system output windings Sa 1 to Sa 7 , and the second first system output windings Sb 1 to Sb 7 are wound around the first system teeth T 1 to T 7 . In the same way, the second system excitation windings R 8 to R 14 , the first second system output windings Sa 8 to Sa 14 , and the second second system output windings Sb 8 to Sb 14 are wound around the second system teeth T 8 to T 14 .

In FIG. 12 , the numbers of turns of the output windings wound around the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 , that is, the first first system output windings Sa 1 to Sa 7 , the second first system output windings Sb 1 to Sb 7 , the first second system output windings Sa 8 to Sa 14 , and the second second system output windings Sb 8 to Sb 14 , are shown consecutively.

Also, the resolver 2 according to the third embodiment is such that winding directions of the first first system output windings Sa 1 to Sa 7 and second first system output windings Sb 1 to Sb 7 and the first second system output windings Sa 8 to Sa 14 and second second system output windings Sb 8 to Sb 14 wound around the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 are mutually opposed. That is, reference signs of the numbers of turns of the first first system output windings Sa 1 to Sa 7 and the first second system output windings Sa 8 to Sa 14 are opposites. In the same way, reference signs of the numbers of turns of the second first system output windings Sb 1 to Sb 7 and the second second system output windings Sb 8 to Sb 14 are opposites.

FIG. 13 shows, in simplified form, gap magnetic flux densities according to excitation signals applied to the first system excitation windings R 1 to R 7 and the second system excitation windings R 8 to R 14 of the resolver 2 according to the third embodiment. FIG. 14 shows, consecutively and in simplified form, the number of turns of an output winding of the first system and the second system, that is, the number of turns of one of the first first system output windings Sa 1 to Sa 7 , the second first system output windings Sb 1 to Sb 7 , the first second system output windings Sa 8 to Sa 14 , or the second second system output windings Sb 8 to Sb 14 .

In FIG. 13 and FIG. 14 , the mechanical angle, which is on the horizontal axis, is such that a range of 0 to 180° represents the first system, and a range of 180 to 360° represents the second system.

Generally, a resolver is such that an angle is detected by magnetic flux interlinking in a gap being read by an output winding. Because of this, magnetic flux interlinking in the output windings can be calculated by multiplying the spatial interlinkage magnetic flux by the number of turns.

The magnetic flux interlinking in the output windings when the spatial interlinkage magnetic flux of FIG. 13 is read by the number of turns of FIG. 14 is shown in FIG. 15 . The waveform of the magnetic flux interlinking in the first first system output windings Sa 1 to Sa 7 and the second first system output windings Sb 1 to Sb 7 , which are the first system output windings of FIG. 15 , and the waveform of the magnetic flux interlinking in the first second system output windings Sa 8 to Sa 14 and the second second system output windings Sb 8 to Sb 14 , which are the second system output windings, are the same. Because of this, offsets with coinciding reference signs overlap in output signals from the first system output windings and the second system output windings. When the offsets are corrected in the angle computing unit 1 , the rotation angle can be accurately detected. According to this kind of configuration, there is an advantage in that detecting an abnormality becomes easier.

Heretofore, a case wherein the resolver 2 is such that the number Ns of teeth of the stator 3 shown in FIG. 3 described in the first embodiment is fourteen, and the teeth T 1 to T 14 are divided in two in the circumferential direction, has been described as an example. In the third embodiment, however, the resolver 2 such that the number Ns of teeth of the stator 3 shown in FIG. 10 described in the second embodiment is sixteen, and the teeth T 1 to T 16 are divided in four in the circumferential direction, is also applicable.

Fourth Embodiment

Next, a rotation angle detection device in which a redundant resolver according to a fourth embodiment of the invention is used will be described.

FIG. 16 is a drawing showing a relationship between an angle error and a phase difference between a first system excitation signal and a second system excitation signal of the resolver 2 used in the rotation angle detection device according to the fourth embodiment.

Herein, an angle error is the difference between an angle detected by the resolver 2 and a true value of the rotation angle of the rotor 4 , wherein a small angle error indicates that angle detection accuracy is good. The angle errors of FIG. 16 are shown standardized by a value when the phase difference is 0°. When the phase difference between the two excitations signals is within 60°, angle detection accuracy of an extent equivalent to that when the phase difference is 0° is obtained.

Also, the angle error is smallest when the phase difference is 45°. That is, by restricting the phase difference between the first system excitation signal and the second system excitation signal to 60° or less, an advantage of improving angle detection accuracy can be obtained. Also, the phase difference between the first system excitation signal and the second system excitation signal is desirably synchronized at 0° for practical purposes.

Fifth Embodiment

Next, a rotation angle detection device in which a redundant resolver according to a fifth embodiment of the invention is used will be described.

FIG. 17 is a sectional view showing the stator 3 of the resolver 2 used in the rotation angle detection device according to the fifth embodiment.

The teeth T 1 to T 14 of the stator 3 according to the fifth embodiment are divided in two in the circumferential direction, configuring a first system and a second system, whereby a dual system redundant resolver is configured. That is, the total angle of teeth per system is 360°/2=180°.

The teeth T 1 to T 7 of the stator 3 are the first system teeth, and the teeth T 8 to T 14 of the stator 3 are the second system teeth. Of the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 , the tooth T 1 and the tooth T 8 are auxiliary teeth around which only an excitation winding is wound, with no output winding being wound. A one-phase excitation winding and a two-phase output winding are wound around the other teeth T 2 to T 7 and T 9 to T 14 . That is, the first system excitation winding R 1 is wound around the first system tooth T 1 , while the first system excitation windings R 2 to R 7 , the first first system output windings Sa 2 to Sa 7 , and the second first system output windings Sb 2 to Sb 7 are wound around the first system teeth T 2 to T 7 .

In the same way, the second system excitation winding R 8 is wound around the second system tooth T 8 , while the second system excitation windings R 9 to R 14 , the first second system output windings Sa 9 to Sa 14 , and the second second system output windings Sb 9 to Sb 14 are wound around the second system teeth T 9 to T 14 .

By configuring in this way, there is no place in which output windings of the first system and the second system are disposed neighboring, because of which an advantage can be obtained in that magnetic interference is restricted, whereby angle detection accuracy is improved.

FIG. 18 is a drawing showing a turn number distribution of the first first system output windings Sa 2 to Sa 7 , the second first system output windings Sb 2 to Sb 7 , the first second system output windings Sa 9 to Sa 14 , and the second second system output windings Sb 9 to Sb 14 according to the fifth embodiment.

Herein, in FIG. 18 , the numbers of turns of the output windings wound around the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 , including the auxiliary teeth T 1 and T 8 , are shown consecutively. Also, the numbers of turns are standardized by the number of turns when not having the auxiliary teeth T 1 and T 8 .

The first first system output windings Sa 2 to Sa 7 and the second first system output windings Sb 2 to Sb 7 of the resolver 2 according to the fifth embodiment are designed so that when the number of turns of both of the auxiliary teeth T 1 and T 8 is zero, the phase difference is 90°, and the amplitudes are equal. Because of this, the number of turns amplitudes appear to differ. In the same way, the first second system output windings Sa 9 to Sa 14 and the second second system output windings Sb 9 to Sb 14 are designed so that when the number of turns of both of the auxiliary teeth T 1 and T 8 is zero, the phase difference is 90°, and the amplitudes are equal. Because of this, the number of turns amplitudes appear to differ.

By configuring in this way, an output signal can be of a sinusoidal waveform, because of which an advantage can be obtained in that angle detection accuracy is improved.

Sixth Embodiment

Next, a rotation angle detection device in which a redundant resolver according to a sixth embodiment of the invention is used will be described.

FIG. 19 is a sectional view showing the stator 3 of the resolver 2 used in the rotation angle detection device according to the sixth embodiment.

The teeth T 1 to T 14 of the stator 3 according to the sixth embodiment are divided in two in the circumferential direction, configuring a first system and a second system, whereby a dual system redundant resolver is configured. That is, the total angle of teeth per system is 360°/2=180°.

The teeth T 1 to T 7 of the stator 3 are the first system teeth, and the teeth T 8 to T 14 of the stator 3 are the second system teeth. Of the first system teeth T 1 to T 7 and the second system teeth T 8 to T 14 , the teeth T 1 , T 7 , T 8 , and T 14 are auxiliary teeth around which only an excitation winding is wound, with no output winding being wound. A one-phase excitation winding and a two-phase output winding are wound around the other teeth T 2 to T 6 and T 9 to T 13 . That is, the first system excitation windings R 1 and R 7 are wound around the first system teeth T 1 and T 7 , while the first system excitation windings R 2 to R 6 , the first first system output windings Sa 2 to Sa 6 , and the second first system output windings Sb 2 to Sb 6 are wound around the first system teeth T 2 to T 6 .

In the same way, the second system excitation windings R 8 and R 14 are wound around the second system teeth T 8 and T 14 , while the second system excitation windings R 9 to R 13 , the first second system output windings Sa 9 to Sa 13 , and the second second system output windings Sb 9 to Sb 13 are wound around the second system teeth T 9 to T 13 .

By configuring in this way, a tooth that has no output winding is disposed at either end of the teeth around which the first system and second system output windings are wound, and there is no place in which output windings of the first system and the second system are disposed neighboring, because of which an advantage can be obtained in that magnetic interference is restricted, whereby angle detection accuracy is further improved.

FIG. 20 is a drawing showing a turn number distribution of the first first system output windings Sa 1 to Sa 7 , the second first system output windings Sb 1 to Sb 7 , the first second system output windings Sa 8 to Sa 14 , and the second second system output windings Sb 8 to Sb 14 according to the sixth embodiment.

Herein, in FIG. 20 , the numbers of turns of the output windings wound around the first system teeth T 2 to T 6 and the second system teeth T 9 to T 13 , including the auxiliary teeth T 1 , T 7 , T 8 , and T 14 , are shown consecutively. Also, the numbers of turns are standardized by the number of turns when not having the auxiliary teeth T 1 , T 7 , T 8 , and T 14 .

The first first system output windings Sa 1 to Sa 7 and the second first system output windings Sb 1 to Sb 7 of the resolver 2 according to the sixth embodiment are designed so that when the number of turns of both of the auxiliary teeth T 1 and T 7 is zero, the phase difference is 90°, and the amplitudes are equal. Because of this, the number of turns amplitudes appear to differ. In the same way, the first second system output windings Sa 8 to Sa 14 and the second second system output windings Sb 8 to Sb 14 are designed so that when the number of turns of both of the auxiliary teeth T 8 and T 14 is zero, the phase difference is 90°, and the amplitudes are equal. Because of this, the number of turns amplitudes appear to differ.

By configuring in this way, an output signal can be of a sinusoidal waveform, because of which an advantage can be obtained in that angle detection accuracy is improved.

Multiple embodiments of the invention are described above, but the invention not being limited to this, the embodiments can be freely combined, and each embodiment can be modified or abbreviated as appropriate, without departing from the scope of the invention.

1 angle computing unit, 1 a first system angle computing unit, 1 b second system angle computing unit, 2 redundant resolver, 3 stator, 4 rotor, 5 winding, 6 shaft, 7 rotating electrical machine, 8 extended portion, 9 a , 9 b output terminal, 10 first system excitation circuit, 11 second system excitation circuit, 12 abnormality determiner, 13 insulator, 100 rotation angle detection device, T 1 to T 14 tooth, R 1 to R 14 excitation winding, Sa 1 to Sa 14 , Sb 1 to Sb 14 output winding, B 1 first system first block, B 2 second system first block, B 3 first system second block, B 4 second system second block.