Tortionally Stiff, Thermally Isolating Shaft Coupling with Multiple Degrees of Freedom to Accommodate Misalignment

• US 20090293654A1
• Filed: 05/30/2008
• Published: 12/03/2009
• Est. Priority Date: 05/30/2008
• Status: Active Grant

• Current Assignee: Woodward Incorporated
• Original Assignee: Woodward Governor Company (Woodward Incorporated)
• Inventors: Pintauro, Arthur C.
• Granted Patent: US 8,480,054 B2
• Time in Patent Office: Days
• US Class Current: 74/63
• CPC Class Codes: F01N 2260/20 for heat or sound protection, e.g. using a shield or specially shaped outer surface of exhaust device
• CPC Class Codes: F02B 37/183 Arrangements of bypass valves or actuators therefor
• CPC Class Codes: F02B 39/00 Component parts, details, or accessories relating to, driven charging or scavenging pumps, not provided for in groups F02B33/00 - F02B37/00
• CPC Class Codes: F02D 9/04 concerning exhaust conduits throttle valves, or arrangements thereof in conduits F02D9/08
• CPC Class Codes: F02D 9/1065 Mechanical control linkage between an actuator and the flap, e.g. including levers, gears, springs, clutches, limit stops of the like
• CPC Class Codes: F16D 2300/02 Overheat protection, i.e. means for protection against overheating
• CPC Class Codes: F16D 3/02 adapted to specific functions
• CPC Class Codes: F16D 3/72 with axially-spaced attachments to the coupling parts F16D3/56 takes precedence
• CPC Class Codes: F16K 1/221 specially adapted operating means therefor operating means per se F16K31/00
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies
• CPC Class Codes: Y10T 74/1836 Rotary to rotary

Abstract

A coupling arrangement coupling and thermally isolating a continuously variable electrical actuator rotationally coupled to and from a butterfly valve is provided. The valve may be used to modulate high temperature exhaust gas flow through an engine turbocharger. The actuator provides a continuously variable control of the valve. The coupling arrangement provides a thermal block to reduce heat transfer and vibration insulation between the actuator and the valve. The coupling arrangement generally includes a coupling shaft rotationally coupled at opposite ends to the input and output shafts by torsion spring mechanisms. The torsion spring mechanisms include yokes rotationally locking the coupling shaft to the input and output shafts. The torsion spring mechanisms allow a limited range of axial and pivotal translation between the coupling shaft and the input and output shafts and are preloaded to prevent rotational hysteresis in the valve.

Claims

1. A drive arrangement for translating rotary movement from an actuator apparatus to a valve member, the drive arrangement comprising:

an input shaft having a first end portion;

an output shaft having second end portion;

a first yoke including an axially extending first tang torsionally secured to the first end portion;

a second yoke including an axially extending second tang torsionally secured to the second end portion; and

a coupling shaft including a first slot formed in a first end slidably receiving the first tang torsionally coupling the coupling shaft to the first yoke, the coupling shaft including a second slot formed in a second end slidably receiving the second tang torsionally coupling the coupling shaft to the second yoke.

2. The drive arrangement of claim 1, wherein the coupling shaft has a limited range of axial and angular translation relative to the first and second yokes.

3. The drive arrangement of claim 2, wherein the first yoke and first end portion have a single degree of freedom therebetween providing pivotal movement, and wherein the second yoke and second end portion have a single degree of freedom therebetween providing pivotal movement.

4. The drive arrangement of claim 3, wherein the first and second end portions are rounded and the first end portion includes a first extension portion axially offsetting the rounded first end portion from the rest of the input shaft forming an annular groove between the first end portion and the rest of the of the input shaft providing a relief zone in which the yoke can penetrate when pivoted relative to the first end portion and wherein the rounded second end portion includes a second extension portion axially offsetting the rounded second end portion from the rest of the output shaft forming an annular groove between the second end portion and the rest of the of the output shaft providing a relief zone in which the yoke can penetrate when pivoted relative to the first end portion

5. The drive arrangement of claim 1, wherein the first and second end portions are rounded and the first and second yokes each include a mounting aperture for receiving the first and second end portions, respectively, the inside diameters of the mounting apertures being at least one percent greater than the outside diameters of the first and second end portions providing a first thermal barrier between the input and output shafts and the first and second yokes, respectively.

6. The drive arrangement of claim 5, wherein the width of the first slot is greater than the width of the first tang such that only one side of the first tang contacts one side of the coupling shaft defining the first slot.

7. The drive arrangement of claim 5, further including a torsion mechanism torsionally forcing the first tang into contact with the side of the coupling shaft defining the first slot and substantially preventing all rotational hysteresis between the first yoke and the coupling shaft.

8. The drive arrangement of claim 2, wherein the coupling shaft has a limited range of pivotal movement relative to the input and output shafts via the first and second yokes, respectively.

9. The drive arrangement of claim 1, wherein the output shaft includes a main shaft and an adaptor spud connected to the main shaft in a fixed position, the adaptor spud including the first end portion.

10. The drive arrangement of claim 1, wherein the coupling shaft is generally tubular.

11. The drive arrangement of claim 1, wherein the first and second end portions are rounded, further including a first rigid connecting member extending radially through the first yoke and the rounded first end portion to axially and angularly secure the first yoke to the input shaft and further including a second rigid connecting member extending radially through the second yoke and the rounded second end portion to axially and angularly secure the second yoke to the output shaft

12. The drive arrangement of claim 11, wherein the first rigid connecting member is aligned with a diameter of the first end portion such that the first yoke pivots relative to the first end portion about an axis defined by the first rigid connecting member and wherein the second rigid connecting member is aligned with a diameter of the second end portion such that the second yoke pivots relative to the second end portion about an axis defined by the second rigid connecting member.

13. The drive arrangement of claim 10, further comprising a third tang identical to and angularly spaced from and axially aligned with the first tang, a fourth tang identical to and angularly spaced from and axially aligned with the second tang, a third slot axially aligned and angularly spaced from the first slot, the third slot receiving the third tang, and a fourth slot axially aligned and angularly spaced from the second slot, the fourth slot receiving the fourth tang, the third tang being part of the first yoke, the fourth tang being part of the second yoke, the third and fourth slots being formed in the coupling shaft at opposed ends thereof.

14. A coupling arrangement for coupling an actuator with a flow control valve and providing thermal barriers therebetween, the coupling arrangement comprising:

a yoke including first and second axially extending tangs axially extending from a head portion and angularly coupled to one another by the head portion;

a coupling shaft including first and second axially aligned and angularly spaced slots, the first slot slidably receiving the first tang and the second slot slidably receiving the second tang; and

wherein the coupling shaft has a degree of rotational movement and a degree of axial movement relative to the yoke.

15. The coupling arrangement of claim 14, further comprising a torsion member rotationally coupling the yoke to the coupling shaft while eliminating substantially all rotational hysteresis between the coupling shaft and the yoke.

16. The coupling arrangement of claim 15, wherein the head portion is an annular portion defining a mounting aperture for axially receiving an end of a shaft along a first axis.

17. The coupling arrangement of claim 16, wherein the yoke further includes a second aperture having a transverse orientation to the mounting aperture and intersecting the mounting aperture.

18. The coupling arrangement of claim 17, further including a rigid connector extending through the second aperture and radially penetrating the mounting aperture.

19. The coupling arrangement of claim 18, further including a torsion spring preloading the coupling shaft into engagement with the yoke through the degree of rotational movement to a predetermined amount of torque.