US2911550A - Eddy current brakes - Google Patents

Eddy current brakes Download PDF

Info

Publication number
US2911550A
US2911550A US673331A US67333157A US2911550A US 2911550 A US2911550 A US 2911550A US 673331 A US673331 A US 673331A US 67333157 A US67333157 A US 67333157A US 2911550 A US2911550 A US 2911550A
Authority
US
United States
Prior art keywords
core elements
armature
core
electro
support
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.)
Expired - Lifetime
Application number
US673331A
Inventor
Bessiere Pierre Etienne
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Telma SA
Original Assignee
Telma SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Telma SA filed Critical Telma SA
Application granted granted Critical
Publication of US2911550A publication Critical patent/US2911550A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K49/00Dynamo-electric clutches; Dynamo-electric brakes
    • H02K49/02Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type
    • H02K49/04Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type
    • H02K49/046Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type with an axial airgap
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K49/00Dynamo-electric clutches; Dynamo-electric brakes
    • H02K49/02Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type
    • H02K49/04Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type
    • H02K49/043Dynamo-electric clutches; Dynamo-electric brakes of the asynchronous induction type of the eddy-current hysteresis type with a radial airgap

Definitions

  • Such a device includes a frame carrying an inductor essentially constituted by a plurality of electro-magnets distributed about the axis of a part rotatable with respect to saidframe so as to create a magnetic field in an armature made of a piece of a conducting material rigid with said part so as to set up therein eddy currents which brake the relative movement of rotation between said part and said frame.
  • the object of this invention is to provide a device of this kind which is better adapted to meet the requirements of practice than those existing at the present time.
  • the cores of the electro-magnets each include two core elements insulated from each other, from a magnetic point of view, by a non magnetic space, each of said two core elements of one core being connected with the adjoining core element of opposed polarity of the core of the next electro-magnet through magnetic means extending between the ends of said core elements located on the other side thereof from the armature, the core elements being rigid with a support from which they project in a direction transverse to the portion of the armature adjacent to them, and the electro-magnet coils surrounding the respective pairs of core elements forming the electro-magnet cores and having their turns substantially .at right angles to the direction in which said core elements are projecting from said support.
  • Fig. 1 is a half elevational view with parts in crosssection of a braking device according to the invention.
  • Fig. 2 is a similar view of a modification.
  • Fig. 3 is a perspective view of the framework of the inductor of the braking device of Fig. 2, and Fig. 4 shows the arrangement of the electro-magnets of these inductors.
  • Figs. 5 and 6 show respectively in axial section on the line V--V of Fig. 6 and in cross-section on the line VI--VI of Fig. 5 (the armature being cut away) a braking device made according to another embodiment of the invention.
  • Figs. 7 and 8 show, respectively in axial section on the line VlIVII of Fig. 8 and in cross-section on the line VIE-VIII of Fig. 7, a braking device made according to still another embodiment of the invention.
  • the braking or slowing down device essentially comprises a fixed inductor or stator including electro-magnets constituted by coils 1 surrounding cores 2, 3, 4, 5 projecting from a support 6.
  • a rotating armature or rotor, constituted by a piece 7 of a conducting material is located close to said inductor, so that the magnetic fields created by said electro-magnets can close through said armature.
  • Cooling means are provided for evacuating the heat created by this braking system.
  • Every electro-magnet core such as 2, 3, 4, 5 is constituted by two core elements In and 1b, 2a and 2b, 3a and 3b, 4a and 412 respectively, the two core elements of every pair being practically insulated from each other from a magnetic point of view and being, for this purpose, separated from each other by a non magnetic space such as 20, 30, 4c, '50, forming a gap which may be an air gap or be made of a solid material.
  • Every core element is magnetically connected with the root of the adjacent core element of opposed polarity of the next electro-magnet, so that the inductor flux such as 11 (Fig. 1) can pass through the magnetic path thus produced.
  • a magnetic connection may be constituted by individual bridges .12 (Fig. 2), the whole of two core elements and of such a bridge having the shape of a horseshoe. It may be constituted by a single piece or by the juxtaposition of identical sheets (laminated core). Every bridge element 12 may also be screwed or otherwise fixed to the corresponding core element.
  • the magnetic connection between the root portions of the core elements may also be achieved by magnetic portions 13 (Fig. 1) of support 6 on which the cores are secured, for instance by screwing.
  • these portions 1 3 are separated from one another by parts 14, made of a non magnetic material, located opposite the non magnetic spaces such as 2c, 30, 4c, 5c above referred to, which are provided between the two core elements of every core.
  • Fig. 1 shows a braking device in which the armature 7 is constituted by a hollow tube coaxially located inside the annular inductor.
  • This inductor includes a cylindrical support 6 from which the core elements 2a and 2b, 3a and 3b, 4a and 4b, rigidly fixed thereto, project radially toward the axis of shaft 8.
  • a cooling air circulation is, for instance, obtained in this case by a fan (not shown) mounted at the end of shaft 8 and carrying blades rigid therewith which send cooling air into recesses provided in the mass of the rotor in radial, longitudinal or other directions.
  • Figs. 2, 3 and 4 show a modification in which the inductor is located inside the armature 7.
  • the rotor including said armature is for instance bell-shaped. It is rigid with shaft 8 which is journalled in bearings 15 carried by the stator.
  • the support member 6b of the inductor is constituted by a kind of cage, the longitudinally extending bars 16 of which are made of a magnetic material, said bars being separated by slots 17 containing a non magnetic material (air, in this case).
  • Each of these slots or air gaps 17 is located opposite the non magnetic interval, such as 30, which separates from each other the two core elements of every core.
  • the unit constituted by two core elements of two consecutive electro-magnets, said core elements being connected together by a part 12 of a magnetic material, are made separately. Then the coils 1 are mounted around the adjacent core elements of two consecutive units and the ring-shaped structure thus formed (Fig. 4) is stretched and slipped longitudinally on support 6:: (Fig. 3) on which it is then fixed.
  • the cores may be mounted around the two core elements of every pair before fixing said core elements to the support.
  • the core elements instead of being mounted on a cylindrical-support may be fixed on the end discs of said support.
  • cooling air circulation is ensured by blades 18 (Fig. 2) fixed to the outer face of the rotor and sending air into holes 19 provided in said rotor.
  • the rotor in order to obtain a better'transformation of the mechanical energy into eddy currents, the rotor is advantageously coppered either wholly or partly.
  • the armature 7 consists of a disc fixed on shaft 8 and the inductor includes two bell-shaped supports 6b opposed to each other and located on either side of said disc 7, each of said supports '61) carrying electro-magnets the cores of which project toward disc 7 and extend to a close dis* tance therefrom, the electro-magnet coils 1 surround pairs of core elements such as 2a and 2b extending in directions parallel to the axis of disc 7.
  • shaft 8 extends through at least one of the bell-shaped sup ports 6b, so as to be secured to the part to be braked.
  • every support 612 is made of a nonmagnetic material (for instance aluminium or an alloy thereof) or it is separated from said bridge elements '12 by a layer of non magnetic material.
  • the armature 7 consists of two external annular discs fixed on shaft 8.
  • the inductor includes electro-magnets disposed between said discs 7 and constituted by coils 1, each surrounding a pair of core elements such as 2a and 2b projecting from supports 60 in a direction parallel to the axis of the shaft.
  • Supports 60 may be made of a magnetic material, provided that non magnetic gaps (for instance air gaps) 117 are supplied opposite the spaces such as 2c provided between the two core elements of every core.
  • These air gaps 17 may be constituted by radial slots in support 6c, as shown on Fig. 8.
  • the cooling air circulation is indicated by arrows in the top portions of Figs. 5 and 7.
  • both the inductor and the armature might be rotatable or the armature might be fixed and theinductor rotatable with respect'thereto.
  • An eddy current brake for retarding the movement of a rotating part journalled in a frame about an axis which comprises, in combination, an inductor rigid with one of the two above mentioned elements, an armature constituted by a piece of a conducting material rigid with the other of said elements, so that said annatureand said inductor have a relative movement of: rotation with respect to each other about the axis of said rotating part, said inductor including a support rigid with said frame and extending around said axis and a plurality of electro-magnets carried by said support and distributed about said axis, each of said electro-magnets comprising two core elements insulated from each other from a magnetic point of view by an air.
  • said two core elements being rigid with said support and projecting therefrom-in a direction transverse to the portion of the armature adjacent to them, and acoil surrounding both of said core elements and the turns of which are substantially at right angles to the direction in which said core elements are projecting from said support, and magnetic means for connecting together every two consecutive core elements of opposed polarities belonging to two consecutive electro-magnets, said magnetic connecting means being interposed between the ends of the core elements located on the otherside thereof from said armature, said armature and said support being provided with passages for the circulation of air through said air gaps, and means for causing air to C11! eulate through said apertures and said air gaps for cooling purposes.

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Dynamo-Electric Clutches, Dynamo-Electric Brakes (AREA)

Description

Nov. 3, 1959 P. E. BESSIERE 7 2,911,550
EDDY CURRENT BRAKES Filed my 22, 1957 2 Sheets-Sheet 1 HWENTOR PIERRE Emzwwa (5E S$\ER ATTORNEY Nov. 3, 1959 P. E. BESSIERE 2,911,550
EDDY CURRENT BRAKES Filed July 22, 1957 2 Sheets-Sheet 2 //\/VEN7'UR Plrmz ETHENNE aessl ERE k WEAK ATTORNEY United States Patent EDDY CURRENT BRAKES Pierre Etienne Bessiere, Paris, France, assignor to Compagnie Telma, Paris, France, a society of France Application July 22, 1957, Serial No. 673,331 Claims priority, application France August 23, 1956 2 Claims. 01. 310-93) The present invention relates to braking or slowing down devices of the eddy current type.
Such a device includes a frame carrying an inductor essentially constituted by a plurality of electro-magnets distributed about the axis of a part rotatable with respect to saidframe so as to create a magnetic field in an armature made of a piece of a conducting material rigid with said part so as to set up therein eddy currents which brake the relative movement of rotation between said part and said frame.
The object of this invention is to provide a device of this kind which is better adapted to meet the requirements of practice than those existing at the present time.
For this purpose, according to the present invention, the cores of the electro-magnets each include two core elements insulated from each other, from a magnetic point of view, by a non magnetic space, each of said two core elements of one core being connected with the adjoining core element of opposed polarity of the core of the next electro-magnet through magnetic means extending between the ends of said core elements located on the other side thereof from the armature, the core elements being rigid with a support from which they project in a direction transverse to the portion of the armature adjacent to them, and the electro-magnet coils surrounding the respective pairs of core elements forming the electro-magnet cores and having their turns substantially .at right angles to the direction in which said core elements are projecting from said support.
Preferred embodiment of this invention will be hereinafter described with reference to the accompanying drawings, given merely by way of example and in which:
Fig. 1 is a half elevational view with parts in crosssection of a braking device according to the invention.
Fig. 2 is a similar view of a modification.
Fig. 3 is a perspective view of the framework of the inductor of the braking device of Fig. 2, and Fig. 4 shows the arrangement of the electro-magnets of these inductors.
Figs. 5 and 6 show respectively in axial section on the line V--V of Fig. 6 and in cross-section on the line VI--VI of Fig. 5 (the armature being cut away) a braking device made according to another embodiment of the invention.
Figs. 7 and 8 show, respectively in axial section on the line VlIVII of Fig. 8 and in cross-section on the line VIE-VIII of Fig. 7, a braking device made according to still another embodiment of the invention.
The braking or slowing down device according to the present invention essentially comprises a fixed inductor or stator including electro-magnets constituted by coils 1 surrounding cores 2, 3, 4, 5 projecting from a support 6.
A rotating armature or rotor, constituted by a piece 7 of a conducting material is located close to said inductor, so that the magnetic fields created by said electro-magnets can close through said armature.
Said fields produce eddy currents in the conducting Patented Nov. 3, 1959 mass of the rotating armature 7. The electric energy spent by these eddy currents, which is transformed into heat, is supplied from the mechanical energy of the rotor and therefore of the shaft 8 to be braked (which is rigid with said rotor), thus causing said shaft to be braked.
Cooling means are provided for evacuating the heat created by this braking system.
Every electro-magnet core such as 2, 3, 4, 5 is constituted by two core elements In and 1b, 2a and 2b, 3a and 3b, 4a and 412 respectively, the two core elements of every pair being practically insulated from each other from a magnetic point of view and being, for this purpose, separated from each other by a non magnetic space such as 20, 30, 4c, '50, forming a gap which may be an air gap or be made of a solid material.
The root of every core element is magnetically connected with the root of the adjacent core element of opposed polarity of the next electro-magnet, so that the inductor flux such as 11 (Fig. 1) can pass through the magnetic path thus produced. Such a magnetic connection may be constituted by individual bridges .12 (Fig. 2), the whole of two core elements and of such a bridge having the shape of a horseshoe. It may be constituted by a single piece or by the juxtaposition of identical sheets (laminated core). Every bridge element 12 may also be screwed or otherwise fixed to the corresponding core element. The magnetic connection between the root portions of the core elements may also be achieved by magnetic portions 13 (Fig. 1) of support 6 on which the cores are secured, for instance by screwing. In order to prevent the formation of an armature flux, these portions 1 3 are separated from one another by parts 14, made of a non magnetic material, located opposite the non magnetic spaces such as 2c, 30, 4c, 5c above referred to, which are provided between the two core elements of every core.
Fig. 1 shows a braking device in which the armature 7 is constituted by a hollow tube coaxially located inside the annular inductor.
This inductor includes a cylindrical support 6 from which the core elements 2a and 2b, 3a and 3b, 4a and 4b, rigidly fixed thereto, project radially toward the axis of shaft 8.
A cooling air circulation is, for instance, obtained in this case by a fan (not shown) mounted at the end of shaft 8 and carrying blades rigid therewith which send cooling air into recesses provided in the mass of the rotor in radial, longitudinal or other directions.
Figs. 2, 3 and 4 show a modification in which the inductor is located inside the armature 7. The rotor including said armature is for instance bell-shaped. It is rigid with shaft 8 which is journalled in bearings 15 carried by the stator.
As shown by Fig. 3, the support member 6b of the inductor is constituted by a kind of cage, the longitudinally extending bars 16 of which are made of a magnetic material, said bars being separated by slots 17 containing a non magnetic material (air, in this case). Each of these slots or air gaps 17 is located opposite the non magnetic interval, such as 30, which separates from each other the two core elements of every core.
The unit constituted by two core elements of two consecutive electro-magnets, said core elements being connected together by a part 12 of a magnetic material, are made separately. Then the coils 1 are mounted around the adjacent core elements of two consecutive units and the ring-shaped structure thus formed (Fig. 4) is stretched and slipped longitudinally on support 6:: (Fig. 3) on which it is then fixed.
If the core elements are made individually, the cores may be mounted around the two core elements of every pair before fixing said core elements to the support.
The core elements, instead of being mounted on a cylindrical-support may be fixed on the end discs of said support.
In this embodiment, cooling air circulation is ensured by blades 18 (Fig. 2) fixed to the outer face of the rotor and sending air into holes 19 provided in said rotor.
In this case, as in the preceding embodiment, in order to obtain a better'transformation of the mechanical energy into eddy currents, the rotor is advantageously coppered either wholly or partly.
In the embodiment of Figs. 5 and 6, the armature 7 consists of a disc fixed on shaft 8 and the inductor includes two bell-shaped supports 6b opposed to each other and located on either side of said disc 7, each of said supports '61) carrying electro-magnets the cores of which project toward disc 7 and extend to a close dis* tance therefrom, the electro-magnet coils 1 surround pairs of core elements such as 2a and 2b extending in directions parallel to the axis of disc 7. Of couse, shaft 8 extends through at least one of the bell-shaped sup ports 6b, so as to be secured to the part to be braked. In this construction the adjacent core elements of opposed polarities are connected together by bridge elements 12 and every support 612 is made of a nonmagnetic material (for instance aluminium or an alloy thereof) or it is separated from said bridge elements '12 by a layer of non magnetic material.
In the construction of Figs. 7 and 8, the armature 7 consists of two external annular discs fixed on shaft 8. The inductor includes electro-magnets disposed between said discs 7 and constituted by coils 1, each surrounding a pair of core elements such as 2a and 2b projecting from supports 60 in a direction parallel to the axis of the shaft. Supports 60 may be made of a magnetic material, provided that non magnetic gaps (for instance air gaps) 117 are supplied opposite the spaces such as 2c provided between the two core elements of every core. These air gaps 17 may be constituted by radial slots in support 6c, as shown on Fig. 8.
The cooling air circulation is indicated by arrows in the top portions of Figs. 5 and 7.
Of course, both the inductor and the armature might be rotatable or the armature might be fixed and theinductor rotatable with respect'thereto.
What I claim is:
1. An eddy current brake for retarding the movement of a rotating part journalled in a frame about an axis which comprises, in combination, an inductor rigid with one of the two above mentioned elements, an armature constituted by a piece of a conducting material rigid with the other of said elements, so that said annatureand said inductor have a relative movement of: rotation with respect to each other about the axis of said rotating part, said inductor including a support rigid with said frame and extending around said axis and a plurality of electro-magnets carried by said support and distributed about said axis, each of said electro-magnets comprising two core elements insulated from each other from a magnetic point of view by an air. gap between them, said two core elements being rigid with said support and projecting therefrom-in a direction transverse to the portion of the armature adjacent to them, and acoil surrounding both of said core elements and the turns of which are substantially at right angles to the direction in which said core elements are projecting from said support, and magnetic means for connecting together every two consecutive core elements of opposed polarities belonging to two consecutive electro-magnets, said magnetic connecting means being interposed between the ends of the core elements located on the otherside thereof from said armature, said armature and said support being provided with passages for the circulation of air through said air gaps, and means for causing air to C11! eulate through said apertures and said air gaps for cooling purposes.
2. An eddy current brake according to claim 1, in which said support is made of a magnetic material provided with slots forming air gaps located in line with the air gaps between said core elements.
References Cited in the file of this patent UNITED STATES PATENTS 2,556,013 Thomas June 3, 1951 2,617,052 Bessiere Nov. 4, 1952 2,640,941 Winther -June 2, 1953 2,643,351 'Feiertag June 23, 1953
US673331A 1956-08-23 1957-07-22 Eddy current brakes Expired - Lifetime US2911550A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2911550X 1956-08-23
FR834847X 1956-08-23

Publications (1)

Publication Number Publication Date
US2911550A true US2911550A (en) 1959-11-03

Family

ID=26223754

Family Applications (1)

Application Number Title Priority Date Filing Date
US673331A Expired - Lifetime US2911550A (en) 1956-08-23 1957-07-22 Eddy current brakes

Country Status (2)

Country Link
US (1) US2911550A (en)
GB (1) GB834847A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3045197A (en) * 1959-06-15 1962-07-17 Honeywell Regulator Co Rotary electromagnetic pickoff device
US3396289A (en) * 1965-07-16 1968-08-06 Hayasaka Enakichi Infinitely variable speed drive
WO1990005690A1 (en) * 1988-11-21 1990-05-31 Heino Hautio Roll brake
CN108313322A (en) * 2017-12-22 2018-07-24 清华大学天津高端装备研究院 Integrated structure liquid electricity composite braking aircraft carrier arresting engine and obstruction system

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2598270B1 (en) * 1986-04-30 1988-08-12 Labavia IMPROVEMENTS TO THE INDUCED ROTORS OF ELECTROMAGNETIC RETARDERS
DE202012000897U1 (en) * 2012-01-31 2012-02-28 Kendrion Magneta Gmbh Spring-loaded brake with a magnet housing

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2556013A (en) * 1949-03-29 1951-06-05 Gen Electric Stator for universal electric motors
US2617052A (en) * 1949-10-22 1952-11-04 Electro Mecanique De Laveyron Electric brake
US2640941A (en) * 1951-01-18 1953-06-02 Eaton Mfg Co Eddy current mechanism
US2643351A (en) * 1952-06-05 1953-06-23 Gen Electric Dynamoelectric machine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2556013A (en) * 1949-03-29 1951-06-05 Gen Electric Stator for universal electric motors
US2617052A (en) * 1949-10-22 1952-11-04 Electro Mecanique De Laveyron Electric brake
US2640941A (en) * 1951-01-18 1953-06-02 Eaton Mfg Co Eddy current mechanism
US2643351A (en) * 1952-06-05 1953-06-23 Gen Electric Dynamoelectric machine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3045197A (en) * 1959-06-15 1962-07-17 Honeywell Regulator Co Rotary electromagnetic pickoff device
US3396289A (en) * 1965-07-16 1968-08-06 Hayasaka Enakichi Infinitely variable speed drive
WO1990005690A1 (en) * 1988-11-21 1990-05-31 Heino Hautio Roll brake
CN108313322A (en) * 2017-12-22 2018-07-24 清华大学天津高端装备研究院 Integrated structure liquid electricity composite braking aircraft carrier arresting engine and obstruction system
CN108313322B (en) * 2017-12-22 2021-04-09 清华大学天津高端装备研究院 Integrated structure hydraulic-electric composite brake aircraft carrier arrester and arresting system

Also Published As

Publication number Publication date
GB834847A (en) 1960-05-11

Similar Documents

Publication Publication Date Title
US2903610A (en) Dynamo-electric machine field magnet construction with split poles
KR960003205B1 (en) Full flux reversal variable reluctance machine
US3469134A (en) Electrical machines
US9997982B2 (en) Rotating electrical machine comprising at least one stator and at least two rotors
KR920001804A (en) Stator cooling system for electric machines
GB1140021A (en) Electrical machine of disc-type construction
US4031422A (en) Gas cooled flux shield for dynamoelectric machine
JP2019044964A (en) Active radial magnetic bearing with yoke winding
US5886449A (en) Electrical machine
US2911550A (en) Eddy current brakes
US3418506A (en) Axial airgap motors and generators
US2702004A (en) Linear polyphase electromagnetic pump
GB1204444A (en) Improvements in or relating to electromagnetic stepping motors
US3396325A (en) Voltage control of permanent magnet generators
US3432706A (en) Rotary electric machine
US2836742A (en) Foucault current braking devices
US2986663A (en) Rotor construction for dynamoelectric machines
US2852711A (en) Electrical rotor apparatus
US3293469A (en) Electrical alternator
US3233132A (en) Inductor alternator
US3238402A (en) Electromagnetic clutch
US2872604A (en) Dynamoelectric machine structure
US2131035A (en) Magnetic speed changer
US3031592A (en) Eddy-current brakes
US2617052A (en) Electric brake