Pin member for turbine

Patent metadata

Field	Value
Publication number	US-11788435-B2
Application number	US-202017776134-A
Country	US
Kind code	B2
Filing date	Nov 11, 2020
Priority date	Nov 14, 2019
Publication date	Oct 17, 2023
Grant date	Oct 17, 2023

Abstract

A pin member is proposed for a turbo-machine having a shroud arranged to rotate within a turbine housing. The pin member is configured to limit this rotation. It is a one-piece element comprising a cylindrical body and a limit surface for opposing motion of the shroud.

First claim

The invention claimed is:

1. A pin member suitable for limiting rotational movement of a shroud relative to a turbine housing, the pin member comprising a generally cylindrical body defining a pin axis, and a head portion at one end of the cylindrical body, the head portion being integrally formed with the cylindrical body so that the head portion and the cylindrical body together form a one-piece unit,
the head portion having a limit surface for in use bearing against a surface of the shroud and limiting its rotational motion, and an opposed positioning surface for positioning the pin member, the limit surface and positioning surfaces being spaced from each other in a first direction;
the head portion of the pin member having a head surface which is transverse to the pin axis, and bounded on one side by the limit surface and on the other side by the positioning surface,
the extent H 1 of the limit surface in a second direction transverse to the first direction and to the pin direction being less than the extent H 2 of the positioning surface in the second direction;
and the limit surface being convex.

2. The pin member of claim 1 in which the head surface is substantially composed of two generally rectangular portions, with a first of the rectangular portions being further in the second direction than second of the rectangular portions, the first of the rectangular portions having a greater area than the second of the rectangular portions, the first and second rectangular portions both being bordered by the positioning surface.

3. The pin member of claim 2 in which the head portion of the pin member has a greater extent W 1 in the first direction, than the extent W 2 in the first direction of the second rectangular portion.

4. The pin member of claim 1 in which the limit surface has translational symmetry parallel to the pin axis, the limit surface having a radius of curvature R.

5. The pin member of claim 4 in which the radius of curvature of the limit surface, R, is greater than the extent W 1 of the head portion of the pin member in the first direction.

6. The pin member of claim 3 in which the limit surface has translational symmetry parallel to the pin axis, the limit surface having a radius of curvature R, and W 1 , W 2 , H 1 , H 2 and R satisfy the equation:

(

W
1

-

W
2

)

2

+

(

H
2

-

1
2

⁢

H
1

)

2

2
⁢

(

W
1

-

W
2

)

≤
R
≤

2
⁢
0
⁢

H
1

.

7. The pin member of claim 1 which is without an internal transition.

8. The pin member of claim 1 which is composed of an alloy comprising Cobalt.

9. The pin member of claim 1 in which the cylindrical body has a diameter of substantially 4 mm.

10. A turbine housing for a turbine, the turbine housing defining a central axis which in use is the rotational axis of the turbine, and at least one pin member suitable in use for limiting rotational movement relative to the turbine housing of a shroud mounted in the turbine housing encircling the central axis of the turbine housing,
the pin member comprising a generally cylindrical body defining a pin axis, and a head portion at one end of the cylindrical body, the head portion being integrally formed with the cylindrical body so that the head portion and the cylindrical body together form a one-piece unit,
the head portion having a limit surface for in use bearing against a surface of the shroud and limiting its rotational motion, and an opposed positioning surface for positioning the pin member, the limit surface and positioning surfaces being spaced from each other in a first direction;
the head portion of the pin member having a head surface which is transverse to the pin axis, and bounded on one side by the limit surface and on the other side by the positioning surface,
the extent H1 of the limit surface in a second direction transverse to the first direction and to the pin direction being less than the extent H2 of the positioning surface in the second direction;
and the limit surface being convex.

11. The turbine housing of claim 10 in which each pin member is located in a corresponding aperture of the turbine housing.

12. The turbine housing of claim 10 in which the pin member has a circular cross-section having a diameter d which is given by d=A×PCD to within an accuracy of 10%, where A=0.035 and PCD is a value which is twice a distance from the pin axis to the central axis.

13. The turbine housing of claim 11 in which the pin member does not fill a chamber of the aperture, whereby in use the pressure is reduced of any gas which was trapped within the aperture when the cylindrical body of the pin member was located in the aperture.

14. A turbocharger comprising a turbine and a compressor driven by the turbine, the turbine comprising:
a turbine housing defining a central axis which is a rotational axis of the turbine;
a turbine wheel within the turbine housing;
a shroud within the turbine housing encircling the rotational axis of the turbine; and
at least pin member configured to limit rotational movement of the shroud relative to a turbine housing,
the pin member comprising a generally cylindrical body defining a pin axis, and a head portion at one end of the cylindrical body, the head portion being integrally formed with the cylindrical body so that the head portion and the cylindrical body together form a one-piece unit,
the head portion having a limit surface for in use bearing against a surface of the shroud and limiting its rotational motion, and an opposed positioning surface for positioning the pin member, the limit surface and positioning surfaces being spaced from each other in a first direction;
the head portion of the pin member having a head surface which is transverse

Assignees

• Cummins Ltd

Inventors

• Moore Simon David
• Conlon Karl
• Edwards Matthew William

Classifications

• F01D25/24 Primary

  Casings (modified for heating or cooling F01D25/14); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general F16M {; special arrangements in stators dealing with breaking-off of part of rotor F01D21/045}) · CPC title

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title

• F01D25/28

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F05D2220/40

  in turbochargers · CPC title

• F05D2230/64

  using positioning or alignment devices for aligning or centring, e.g. pins · CPC title