High efficiency torque converter
View Patent ↗A torque converter assembly is provided, which includes an impeller, a turbine, and a stator. The impeller and the turbine each have a plurality of passages for directing fluid. The inlet and outlet of each passage are larger in cross-sectional area than the middle portion of the passage, located between the inlet and outlet. This structure reduces energy losses, which typically occur near the midpoint of the passage due to flow separation. Additionally, reducing the flow area of the torus of the impeller and turbine permits an overall thinner torque converter, which is preferred for engine packaging purposes. The stator includes a core, a shell, and a plurality of stator blades. One end of each stator blade is fixed to the core, while the opposite end is fixed to the shell. Each stator blade has a mean camber line and an associated mean camber line length. The maximum thickness of each stator blade is approximately 20% of the mean camber line length. Each stator blade has a midsection located between the ends affixed to the core and the shell. The midsection of each stator blade has a larger cross-sectional area than either end of the blade. This stator blade structure creates a larger stator blade surface, which is more effective at re-directing fluid within the torque converter.
1. A torque converter assembly including an impeller, a turbine, and a stator, comprising:
at least one of the impeller and the turbine having a passage for directing fluid wherein each said passage has an inlet having an inlet cross-sectional area, an outlet having an outlet cross-sectional area, and a middle portion having a middle portion cross-sectional area, wherein said middle portion cross-sectional area is smaller than each of said inlet cross-sectional area and said outlet cross-sectional area;
the stator including a core, a shell, and a plurality of stator blades; and
each said stator blade having a midsection defined by a mid-cross-sectional area, a first end defined by a first end cross-sectional area attached to said core, and a second end defined by a second end cross-sectional area attached to said shell, wherein said mid-cross-sectional area is larger than each of said first end cross-sectional area and said second end cross-sectional area.
2. The torque converter defined in claim 1 wherein a ratio of said inlet cross-sectional area, said middle portion cross-sectional area, and said outlet cross-sectional area is approximately 1:0.8:1.
3. The torque converter defined in claim 1 wherein an angle difference between an inlet and an outlet of each said stator blade is between approximately 37° and 43°.
4. The torque converter defined in claim 1 wherein each said stator blade has a mean camber line, a mean camber line length and a maximum thickness which is less than 20% of said mean camber line length.
5. The torque converter defined in claim 4 wherein each said stator blade is nonsymmetrical with respect to said mean camber line.
6. The torque converter defined in claim 1 wherein each said stator blade becomes smaller in cross-sectional area in a direction from said mid-cross-sectional area to said first end cross-sectional area.
7. The torque converter defined in claim 6 wherein each said stator blade is linearly tapered between said mid-cross-sectional area and said first end cross-sectional area.
8. The torque converter defined in claim 1 wherein each said stator blade becomes smaller in cross-sectional area in a direction from said mid-cross-sectional area to said second end cross-sectional area.
9. The torque converter defined in claim 8 wherein each said stator blade is linearly tapered between said mid-cross-sectional area and said second end cross sectional area.
10. A torque converter assembly including an impeller, a turbine, and a stator, comprising:
at least one of the impeller and the turbine having a passage for directing fluid wherein each said passage has an inlet having an inlet cross-sectional area, an outlet having an outlet cross-sectional area, and a middle portion having a middle portion cross-sectional area, wherein said middle portion cross-sectional area is smaller than each of said inlet cross-sectional area and said outlet cross-sectional area; and
the stator including a plurality of stator blades, each said stator blade having a mean camber line length and having a maximum thickness which is less than approximately 20% of said mean camber line length.
11. The torque converter defined in claim 10 wherein each said stator blade is nonsymmetrical with respect to said mean camber line.
12. The torque converter defined in claim 10 wherein each said stator blade may be characterized by an airfoil wherein a maximum thickness of said airfoil is between approximately 15% and 18% of said mean camber line length.
13. The torque converter defined in claim 10 wherein a suction surface of each said stator blade is located at a maximum distance from said mean camber line of 8% of said mean camber line length.
14. The torque converter defined in claim 10 wherein a pressure surface of each said stator blade is located at a maximum distance from said mean camber line of 10% of said mean camber line length.
15. The torque converter defined in claim 10 wherein a ratio of said inlet cross-sectional area, said middle portion cross-sectional area, and said outlet cross-sectional area is approximately 1:0.8:1.
16. A torque converter assembly including an impeller, a turbine, and a stator, comprising:
the stator including a plurality of stator blades, each said stator blade having a mean camber line length and having a maximum thickness which is less than approximately 20% of said mean camber line length; and
each said stator blade having a midsection defined by a mid-cross-sectional area, a first end defined by a first end cross-sectional area attached to said core, and a second end defined by a second end cross-sectional area attached to said shell, wherein said mid-cross-sectional area is larger than each of said first end cross-sectional area and said second end cross-sectional area.
17. The torque converter defined in claim 16 wherein each said stator blade is nonsymmetrical with respect to said mean camber line.
18. The torque converter defined in claim 16 wherein an angle difference between an inlet and an outlet of each said stator blade is between approximately 37° and 43°.
19. The torque converter defined in claim 16 wherein each said stator blade may be characterized by an airfoil wherein a maximum thickness of said airfoil is between approximately 15% and 18% of said mean camber line length.
20. The torque converter defined in claim 16 wherein a suction surface of each said stator blade is located at a maximum distance from said mean camber line of 8% of said mean camber line length.
21. The torque converter defined in claim 16 wherein a pressure surface of each said stator blade is located at a maximum distance from said mean camber line of 10% of said mean camber line length.
22. The torque converter defined in claim 16 wherein each said stator blade becomes smaller in cross-sectional area in a direction from said mid-cross-sectional area to said first end cross-sectional area.
23. The torque converter defined in claim 22 wherein each said stator blade is linearly tapered between said mid-cross-sectional area and said first end cross-sectional area.
24. The torque converter defined in claim 16 wherein each said stator blade becomes smaller in cross-sectional area in a direction from said mid-cross-sectional area to said second end cross-sectional area.
25. The torque converter defined in claim 24 wherein each said stator blade is linearly tapered between said mid-cross-sectional area and said second end cross sectional area.