EP2987224A2 - Moteur electrique a circuits electriques redondants - Google Patents
Moteur electrique a circuits electriques redondantsInfo
- Publication number
- EP2987224A2 EP2987224A2 EP14719695.0A EP14719695A EP2987224A2 EP 2987224 A2 EP2987224 A2 EP 2987224A2 EP 14719695 A EP14719695 A EP 14719695A EP 2987224 A2 EP2987224 A2 EP 2987224A2
- Authority
- EP
- European Patent Office
- Prior art keywords
- poles
- stator
- pairs
- coils
- electrical circuits
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 239000000696 magnetic material Substances 0.000 claims description 2
- 238000004804 winding Methods 0.000 abstract description 3
- 238000009413 insulation Methods 0.000 description 2
- 239000012212 insulator Substances 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P25/00—Arrangements or methods for the control of AC motors characterised by the kind of AC motor or by structural details
- H02P25/16—Arrangements or methods for the control of AC motors characterised by the kind of AC motor or by structural details characterised by the circuit arrangement or by the kind of wiring
- H02P25/22—Multiple windings; Windings for more than three phases
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/12—Stationary parts of the magnetic circuit
- H02K1/14—Stator cores with salient poles
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/04—Windings characterised by the conductor shape, form or construction, e.g. with bar conductors
- H02K3/28—Layout of windings or of connections between windings
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K1/00—Details of the magnetic circuit
- H02K1/06—Details of the magnetic circuit characterised by the shape, form or construction
- H02K1/12—Stationary parts of the magnetic circuit
- H02K1/14—Stator cores with salient poles
- H02K1/146—Stator cores with salient poles consisting of a generally annular yoke with salient poles
- H02K1/148—Sectional cores
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K2213/00—Specific aspects, not otherwise provided for and not covered by codes H02K2201/00 - H02K2211/00
- H02K2213/06—Machines characterised by the presence of fail safe, back up, redundant or other similar emergency arrangements
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K3/00—Details of windings
- H02K3/32—Windings characterised by the shape, form or construction of the insulation
- H02K3/38—Windings characterised by the shape, form or construction of the insulation around winding heads, equalising connectors, or connections thereto
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K5/00—Casings; Enclosures; Supports
- H02K5/04—Casings or enclosures characterised by the shape, form or construction thereof
Definitions
- the present invention relates to an electric motor, in particular a single-phase motor.
- These single-phase motors are for example used to move flight surfaces in an aircraft with electric flight controls.
- Such an electric motor comprises a stator defining a number, at least two, of pairs of poles and a rotor mounted to pivot in the stator.
- the motor comprises an electrical circuit defining identical bobi ⁇ ns mounted on the poles of the stator to form the phases of the motor.
- the engine can be arranged to have a limited travel. The desired motor travel determines the number of pole pairs: if a pair of poles is sufficient for 180 ° of maximum travel, two pairs of poles are required for a maximum travel of 90 ° and three pairs of poles for a maximum clearance of ⁇ 60 °.
- an actuator having two or three motors having a common output shaft. Three stators are then mounted along the shaft, each facing a section of the shaft which is arranged to form a rotor.
- This solution is less cumbersome and less cumbersome while meeting the same security requirements as the previous solution.
- the object of the invention is to provide a motor having the same safety in case of failure while being even less heavy and less cumbersome.
- an electric motor comprising a stator defining a number N, at least equal to two pairs of poles and a rotor mounted to pivot in the stator.
- the motor comprises a number n of electrical circuits each defining two coils mounted on stator poles and the coils of all the circuits are substantially identical to each other.
- the number n of electrical circuits is greater than the number N of pairs of poles.
- At least a first and a second of the electrical circuits are mounted on a first of the pairs of poles and a third of the electrical circuits is mounted on a second pair of poles.
- the motor of the invention comprises several electrical circuits for controlling the motor so that the failure of one of the circuits does not prevent the operation of the motor.
- the arrangement of the motor thus makes it possible to have a redundancy of the electrical circuits even for motors having a relatively small number of poles. This is particularly interesting for limited travel motors.
- the coils of each of the first and second electrical circuits are mounted on different poles of the first pair of poles.
- the coils of each of the first and second me electrical circuits are mounted on the same pole of the first pair of poles.
- This embodiment is simpler than the first. On the other hand, if the first or the second electrical circuit fails, it will only be possible to supply the motor with half the maximum torque that the motor is capable of supplying when the two electrical circuits are operational.
- each pole is formed of a tooth having an enlarged free end.
- stator is formed of angular sectors each having one pole and are you seem ⁇ each other
- the winding can then be performed on each sector before joining the sectors to each other, which simplifies the manufacture of the stator.
- the number N of pairs of poles is equal to two and the stator has a cross section having an outer contour of square shape.
- the square shape is advantageous because it leaves a relatively large space for the coils.
- FIG. 1 is a schematic half-view in perspective of an engine according to a first embodiment of the invention
- - Figure 2 is a schematic sectional view along the plane II of Figure 1, the engine according to the first embodiment;
- - Figure 3 is a schematic cross-sectional view of a stator according to an alternative embodiment;
- Figure 4 is a view similar to Figure 2 of a motor according to a second embodiment of the invention.
- the invention is here described in connection with a single-phase electric motor having a limited travel for example at 70 °.
- the electric motor comprises a stator 1 and a rotor 2 mounted for pivoting in the stator 1 around an axis A.
- the rotor 2 is known per se and, as the invention relates to not on this one, it will not be described in more detail later.
- the stator 1 has two pairs of teeth 3 symmetrically opposite each other to define two pairs of poles.
- the teeth 3 of one pair extend at 90 ° with respect to the teeth 3 of the other pair.
- Each tooth has an enlarged free end extending in an arc around a portion of the rotor 1.
- the body of the stator 1 comprises, in a manner known per se, sheets which are contiguous with each other along the axis A.
- the body of the stator 1 here has a cross section with the axis A having an outer contour of square shape. .
- the body of the stator 1 is formed of angular sectors which each comprise one of the teeth 3 and which are assembled to each other by a straight tail assembly.
- the pitch of the tails will preferably be of the order of one to two sheets.
- the straight tails assembly increases the overlap surface and makes the engine less susceptible to spurious air gaps.
- the engine having three electrical circuits, generally designated 10, each defining two booster 11, 12 in series (the electrical circuits, and their coils, are differentiated from each other by the numbers 1, 2 and 3 which follow the reference 10, 11, 12 respectively).
- the coils 11, 12 each surround one of the teeth 3 and are substantially identical to each other.
- a first and a second of the electrical circuits 10, respectively referenced 10.1, 10.2, are mounted on one of the two pairs of teeth 3 and a third of the electrical circuits, referenced 10.3 is mounted on the other pair of teeth 3.
- the coils 11 and 12 of each of the first and second electrical circuits 10.1, 10.2 are thus mounted on different poles of the first pair of poles.
- the coil 11.3 and the coil 12.3 of the third electrical circuit 10.3 each surround one of the teeth 3 of the other pair of teeth 3.
- the coils are wound around the teeth 3 before joining the sectors to form the stator 1.
- the coils are each formed of an electrically conductive wire surrounded by an insulator and the coils of the same tooth are separated from one another. the other by insulation and separated from the stator also by an insulator.
- the insulation may be formed of an annular support having a C-shaped cross section defining a peripheral housing receiving the coil.
- the coils 11, 12 have portions extending axially from the body of the stator 1.
- the said protruding portions are covered by a cap 15 (only two of which are visible in Figure 1).
- the Hats 15, made of magnetic material, are arranged in order to channel the leakage flow. This facilitates the filtering of the high frequency currents generated by the switching control of the motor and isolating the coils from each other vis-à-vis these high frequency currents.
- stator 1 is in two parts, namely a tubular inner body 1.1 having teeth 3 projecting outwardly and a tubular yoke 1.2 surrounding the tubular inner body 1.1.
- the motor of Figure 5 is identical to that of the first embodiment except that the coils 11, 12 of each of the first and second electrical circuits 10.1, 10.2 are mounted on the same pole of the first pair of poles.
- the coils 11.1, 12.1 of the first electrical circuit 10. Surround one of the teeth 3 of one of the two pairs of teeth and the coils 11.2, 12.2 of the second electrical circuit 10.2 surround the other of the teeth 3 of this same pair. of teeth 3.
- the coil 11.3 and the coil 12.3 of the third electrical circuit 10.3 each surround one of the teeth 3 of the other pair of teeth 3.
- the number n of electrical circuits and the number N of pairs of poles can be different from three and two.
- the engine may not include hats.
- the stator may comprise portions of Vietnamese ⁇ range extending between adjacent coils of teeth.
- the stator may have other shapes, for example a circular outer shape.
Landscapes
- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Windings For Motors And Generators (AREA)
- Iron Core Of Rotating Electric Machines (AREA)
- Control Of Motors That Do Not Use Commutators (AREA)
Abstract
Description
Claims
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1353538A FR3004864B1 (fr) | 2013-04-18 | 2013-04-18 | Moteur electrique a circuits electriques redondants |
| PCT/EP2014/057836 WO2014170414A2 (fr) | 2013-04-18 | 2014-04-16 | Moteur electrique a circuits electriques redondants |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP2987224A2 true EP2987224A2 (fr) | 2016-02-24 |
Family
ID=48856835
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP14719695.0A Withdrawn EP2987224A2 (fr) | 2013-04-18 | 2014-04-16 | Moteur electrique a circuits electriques redondants |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US20160190968A1 (fr) |
| EP (1) | EP2987224A2 (fr) |
| FR (1) | FR3004864B1 (fr) |
| WO (1) | WO2014170414A2 (fr) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3042077B1 (fr) * | 2015-10-05 | 2019-05-31 | Safran Landing Systems | Moteur electrique. |
| US10686355B2 (en) * | 2016-07-15 | 2020-06-16 | Magnemotion, Inc. | Transport system puck assembly |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1488596A1 (de) * | 1965-11-19 | 1969-04-10 | Licentia Gmbh | Staender fuer Kleinstmotoren |
| US4480203A (en) * | 1982-12-30 | 1984-10-30 | Tokyo Electric Co., Ltd. | Stepping motor |
| DE3521241C1 (de) * | 1985-06-13 | 1986-09-18 | Schabmüller GmbH, 8070 Ingolstadt | Gleichstrommotor |
| US5179308A (en) * | 1992-01-14 | 1993-01-12 | Charles Stark Draper Laboratory, Inc. | High-speed, low-loss antifriction bearing assembly |
| CA2151532C (fr) * | 1994-07-25 | 1998-12-22 | Emerson Electric Co. | Moteur a reluctance commutable muni d'un demarreur auxiliaire |
| US6020711A (en) * | 1998-03-05 | 2000-02-01 | The United States Of America As Represented By The Secretary Of The Air Force | Multiple winding channel, magnetic coupling-alterable reluctance electrical machines and their fault tolerant control |
| DE19820929A1 (de) * | 1998-05-09 | 1999-11-11 | Ako Werke Gmbh & Co | Vorrichtung zum Steuern eines Einphasen-Synchronmotors |
| EP1063753B1 (fr) * | 1999-06-22 | 2009-07-22 | Levitronix LLC | Entraînement électrique rotatif comprenant un rotor suspendu magnétiquement |
| US7382076B2 (en) * | 2003-10-21 | 2008-06-03 | Matsushita Electric Industrial Co., Ltd. | Spindle motor |
| US20060067022A1 (en) * | 2004-09-30 | 2006-03-30 | Valeo Electrical Systems, Inc. | Fail-safe system for electric power steering in vehicles |
| US7095150B2 (en) * | 2004-10-21 | 2006-08-22 | Shop Vac Corporation | Apparatus for securing a bobbin of a reluctance machine |
| US7327066B2 (en) * | 2005-03-01 | 2008-02-05 | Nidec Corporation | Motor and recording disk drive device provided with the same |
| WO2008044740A1 (fr) * | 2006-10-13 | 2008-04-17 | Mitsui High-Tec, Inc. | Noyau en fer stratifié et son procédé de fabrication |
| US20080157622A1 (en) * | 2007-01-03 | 2008-07-03 | General Electric Company | Fault-tolerant permanent magnet machine |
| DE102010064173A1 (de) * | 2010-12-27 | 2012-06-28 | Robert Bosch Gmbh | Wicklungszahn für eine elektrische Maschine, Maschinenkomponente und elektrische Maschine |
| EP2498381B1 (fr) * | 2011-03-08 | 2018-10-10 | Siemens Aktiengesellschaft | Segment de bobine de stator pour transducteur électro-mécanique, en particulier un générateur et transducteur électro-mécanique, en particulier un générateur électrique |
| US8648518B2 (en) * | 2011-10-05 | 2014-02-11 | Rechi Precision Co., Ltd. | Compressor with snug perforated stator end-cover |
-
2013
- 2013-04-18 FR FR1353538A patent/FR3004864B1/fr active Active
-
2014
- 2014-04-16 EP EP14719695.0A patent/EP2987224A2/fr not_active Withdrawn
- 2014-04-16 US US14/785,239 patent/US20160190968A1/en not_active Abandoned
- 2014-04-16 WO PCT/EP2014/057836 patent/WO2014170414A2/fr not_active Ceased
Non-Patent Citations (2)
| Title |
|---|
| None * |
| See also references of WO2014170414A2 * |
Also Published As
| Publication number | Publication date |
|---|---|
| FR3004864A1 (fr) | 2014-10-24 |
| WO2014170414A3 (fr) | 2015-06-11 |
| FR3004864B1 (fr) | 2015-04-24 |
| US20160190968A1 (en) | 2016-06-30 |
| WO2014170414A2 (fr) | 2014-10-23 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
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| 17P | Request for examination filed |
Effective date: 20151015 |
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| AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
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| AX | Request for extension of the european patent |
Extension state: BA ME |
|
| DAX | Request for extension of the european patent (deleted) | ||
| RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: SAFRAN ELECTRONICS & DEFENSE |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
|
| 17Q | First examination report despatched |
Effective date: 20200423 |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
| 18D | Application deemed to be withdrawn |
Effective date: 20200904 |