IP Library Granted Patent US 6,900,569
Granted Patent B2
US 6,900,569 · App. 10/244,989 · Granted May 31, 2005

Increased torque in retarder brake system through use of conductive layer

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Quick Facts
Patent No.
US 6,900,569
App. No.
10/244,989
Granted
May 31, 2005
Kind
B2
Abstract

Electromagnetic retarder brake systems, and methods for their use, are provided utilizing specified thickness conductive layers. The specified thickness of the conductive layer in each system is determined to obtain a certain desired torque at a certain desired low rotational frequency. The specified thickness conductive layer is disposed between a winding and a rotor within each system. By utilizing a specified thickness conductive layer, torque on the rotor at low rotational frequencies is increased, thereby improving deceleration capabilities.

Claims (24)

1. An eddy current braking system in a vehicle comprising:

a rotor defining a generally cylindrical inner pocket extending axially along the rotor;

a stator assembly at least partially disposed within the generally cylindrical inner pocket of the rotor, the stator assembly comprising a winding, the winding capable of inducing a magnetomotive force capable of slowing rotation of the rotor; and

a conductive layer having a thickness in the range of about 0.125 mm to 2 mm disposed between an inner surface of the rotor and the winding, wherein at said thickness, a rotational frequency in the range of a bout 200 revolutions per minute to approximately 2000 revolutions per minute, a torque larger than about 200 Nm is produced on the rotor.

2. The invention of claim 1 wherein the stator assembly further comprises a generally cylindrical inner section, and staggered outwardly extending stator arms connected to and extending around a circumference of an outer-surface of the generally cylindrical inner section.

3. The invention of claim 2 wherein the winding is disposed within inner compartments, defined by the outer surface and the staggered outwardly extending stator arms, the inner compartments staggered around the circumference of the outer-surface of the generally cylindrical inner section.

4. The invention of claim 1 wherein the winding comprises one of a round wire and a rectangular wire.

5. The invention of claim 1 wherein the rotor is operable to generate an armature magnetomotive force.

6. The invention of claim 1 wherein the rotor comprises a shaft.

7. The invention of claim 1 wherein the conductive layer is one of copper and nickel.

8. The invention of claim 1 wherein the conductive layer is attached to a generally cylindrical inner surface of the rotor.

9. The invention of claim 8 wherein the conductive layer is brazed to the generally cylindrical inner surface of the rotor.

10. The invention of claim 1 wherein the conductive layer acts to increase torque on the rotor at rotational frequencies in the range of about 200 revolutions per minute to approximately 2000 revolutions per minute by approximately 30 percent.

11. The invention of claim 1 wherein the thickness of the conductive layer is determined using finite element analysis to obtain the torque at the rotational frequency.

12. A method of obtaining a certain desired torque at a certain desired low rotational frequency in an eddy current braking system in a vehicle, the method comprising:

providing an eddy current braking system comprising a rotor defining a generally cylindrical inner pocket extending axially along the rotor, a stator assembly at least partially disposed within the generally cylindrical inner pocket of the rotor, the stator assembly comprising a winding, the winding capable of inducing a magnetomotive force capable of slowing rotation of the rotor, and a conductive layer having a specified thickness disposed between an inner surface of the rotor and the winding;

determining a certain desired torque at a certain desired low rotational frequency, wherein the certain desired torque is larger than about 200 Nm and the certain desired low rotational frequency is in the range of about 200 revolutions per minute to approximately 2000 revolutions per minute;

determining the specified thickness of the conductive layer to obtain the certain desired torque at the certain desired low rotational frequency, wherein the specified thickness is in the range of about 0.125 mm to 2 mm; and

applying the conductive layer, with the determined specified thickness, to obtain the certain desired torque at the certain desired low rotational frequency.

13. The method of claim 12 wherein the conductive layer is one of copper and nickel.

14. The invention of claim 12 wherein the conductive layer is attached to a generally cylindrical inner surface of the rotor.

15. The invention of claim 14 wherein the conductive layer is brazed to the generally cylindrical inner surface of the rotor.

16. The invention of claim 12 wherein the conductive layer acts to increase torque on the rotor at rotational frequencies in the range of about 200 revolutions per minute to approximately 2000 revolutions per minute by approximately 30 percent.

17. The invention of claim 12 wherein the specified thickness of the conductive layer is determined using finite element analysis to obtain the certain desired torque at the certain desired low rotational frequency.

Assignments (4)
RELEASE OF SECURITY INTEREST IN INTELLECTUAL PROPERTY Recorded Jun 9, 2014
From: MORGAN STANLEY SENIOR FUNDING, INC.
To: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDINGS, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
Reel/Frame 033107/0717 →
RELEASE BY SECURED PARTY AGAINST SECURITY INTEREST IN PATENTS ON REEL 025241 FRAME 0317 Recorded Apr 26, 2011
From: MORGAN STANLEY SENIOR FUNDING, INC.
To: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDING, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
Reel/Frame 026178/0412 →
SECURITY AGREEMENT (REVOLVER) Recorded Oct 19, 2010
From: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDINGS, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC., AS AGENT
Reel/Frame 025238/0298 →
SECURITY AGREEMENT Recorded Oct 19, 2010
From: VISTEON CORPORATION; VC AVIATION SERVICES, LLC; VISTEON ELECTRONICS CORPORATION; VISTEON GLOBAL TECHNOLOGIES, INC.; VISTEON INTERNATIONAL HOLDINGS, INC.; VISTEON GLOBAL TREASURY, INC.; VISTEON EUROPEAN HOLDING, INC.; VISTEON SYSTEMS, LLC; VISTEON INTERNATIONAL BUSINESS DEVELOPMENT, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC., AS AGENT
Reel/Frame 025241/0317 →