PISTON ASSEMBLY

• US 20110197845A1
• Filed: 10/05/2010
• Published: 08/18/2011
• Est. Priority Date: 02/17/2010
• Status: Abandoned Application

• Current Assignee: Mahle International GmbH (MAHLE-STIFTUNG GmbH)
• Original Assignee: Mahle International GmbH (MAHLE-STIFTUNG GmbH)
• Inventors: Klein, Ralph, Flowers, William, Gabriel, Dieter, Zhao, Grace
• Application Number:
  US12/898,300
• Publication Number:
  US 20110197845A1
• Time in Patent Office: Days
• US Class Current: 123/193.6
• CPC Class Codes: F02F 3/003 the parts being connected by casting, brazing, welding or clamping
• CPC Class Codes: F02F 3/22 the fluid being liquid
• CPC Class Codes: Y10T 29/49254 Utilizing a high energy beam, e.g., laser, electron beam

Abstract

An exemplary piston assembly and method of making the same are disclosed. A piston assembly may include a piston crown and piston skirt. The crown may include a ring belt portion defining at least in part a cooling gallery, as well as radially inner and outer crown mating surfaces. The skirt may be received in a central opening of the crown such that the crown and skirt cooperate to form an upper combustion bowl surface. The skirt also may include radially inner and outer skirt mating surfaces that are abutted with the inner and outer crown mating surfaces, respectively, such that the cooling gallery is generally enclosed by the skirt.

Claims

1. A piston assembly, comprising:

a piston crown, including a ring belt portion defining at least in part a cooling gallery, the crown including radially inner and outer crown mating surfaces; and

a piston skirt received in a central opening of the crown such that the crown and skirt cooperate to form an upper combustion bowl surface, the skirt including a radially inner skirt mating surface abutted along a radially inner interface region with the radially inner crown mating surface, the skirt including a radially outer skirt mating surface abutted along a radially outer interface region with the radially outer crown mating surface such that the cooling gallery is substantially enclosed.

2. The piston assembly of claim 1, wherein each of the inner and outer crown mating surfaces and the inner and outer skirt mating surfaces extend about substantially an entire circumference of the crown and skirt.

3. The piston assembly of claim 1, wherein the crown includes a securement flange extending around the central opening adjacent the radially inner mating surfaces of the crown and skirt, wherein a longitudinal height of the securement flange is smaller than a radial extent of the securement flange, the radial extent of the securement flange contacting the skirt.

4. The piston assembly of claim 1, wherein the crown and skirt are fixedly secured together by the radially inner interface region, including the radially inner mating surfaces of the crown and skirt.

5. The piston assembly of claim 4, wherein the crown and skirt are welded together along the radially inner mating surfaces of the crown and skirt.

6. The piston assembly of claim 4, wherein the crown and skirt are fixedly secured together along the radially outer mating surfaces of the crown and skirt.

7. The piston assembly of claim 1, wherein the piston skirt defines at least one passageway extending from a cooling gallery surface to an outer surface of the piston assembly, the cooling gallery surface defining at least in part the cooling gallery.

8. The piston assembly of claim 7, wherein the outer surface is configured to slide along a cylinder bore surface during engine operation.

9. The piston assembly of claim 7, wherein the outer surface of the piston assembly is spaced away from a radially outer surface of the piston skirt such that the skirt defines a pocket.

10. The piston assembly of claim 1, wherein the crown defines a radially outer portion of the combustion bowl surface and the skirt defines a radially inner portion of the combustion bowl surface.

11. A method, comprising:

providing a piston crown including a ring belt portion defining at least in part a cooling gallery, the piston crown including radially inner and outer crown mating surfaces;

receiving a piston skirt in a central opening of the crown such that the crown and skirt cooperate to form a continuous upper combustion bowl surface having a radially inner portion defined by the skirt and a radially outer portion defined by the crown, the piston skirt including radially inner and outer skirt mating surfaces; and

abutting the skirt to the crown along the corresponding radially inner and outer mating surfaces of the skirt and crown such that the skirt and crown are abutted along a radially inner interface region including the radially inner mating surfaces of the crown and skirt and the skirt and crown are abutted along a radially outer interface region including the radially outer mating surfaces of the crown and skirt, the skirt thereby generally enclosing the cooling gallery.

12. The method of claim 11, further comprising establishing each of the radially inner and outer crown mating surfaces and each of the inner and outer skirt mating surfaces as extending about substantially an entire circumference of the crown and skirt, respectively.

13. The method of claim 11, further comprising establishing the crown as including a securement flange extending around the central opening adjacent the radially inner mating surfaces of the crown and skirt, a longitudinal height of the securement flange being smaller than a radial extent of the securement flange, the radial extent of the securement flange contacting the skirt.

14. The method of claim 11, further comprising fixedly securing the crown and skirt together by the radially inner interface region, including the radially inner mating surfaces of the crown and skirt.

15. The method of claim 14, wherein fixedly securing the crown and skirt together includes welding the crown and skirt together along the radially inner mating surfaces of the crown and skirt.

16. The method of claim 15, further comprising establishing welding the skirt to the crown as laser welding the skirt to the crown.

17. The method of claim 16, wherein laser welding the skirt to the crown includes directing a weld laser generally longitudinally with respect to the piston toward the radially inner mating surfaces of the crown and skirt.

18. The method of claim 14, further comprising fixedly securing the crown and skirt together along the radially outer mating surfaces of the crown and skirt.

19. The method of claim 11, further comprising forming at least one passageway in the skirt, the passageway extending from a cooling gallery surface to an outer surface of the piston assembly, the cooling gallery surface defining at least in part the cooling gallery.

20. The method of claim 11, further comprising:

forming a weld spatter trap adjacent at least one of the radially inner and outer mating surfaces of the crown and skirt;

welding the at least one of the radially inner and outer mating surfaces together, thereby directing heated material into the weld spatter trap on an opposite side of a weld joint associated with the at least one of the radially inner and outer mating surfaces.