Piston assembly

• US 9,856,820 B2
• Filed: 10/05/2010
• Issued: 01/02/2018
• Est. Priority Date: 10/05/2010
• Status: Active Grant

• Current Assignee: Mahle International GmbH (MAHLE-STIFTUNG GmbH)
• Original Assignee: Mahle International GmbH (MAHLE-STIFTUNG GmbH)
• Inventors: Menezes, Leandro, Gabriel, Dieter, Lapp, Michael T., Rein, Wolfgang
• Primary Examiner(s): Low, Lindsay
• Assistant Examiner(s): Morales, Omar
• Application Number:
  US12/898,251
• Publication Number:
  US 20120080004A1
• Time in Patent Office: 2,646 Days
• Field of Search: 1231936, 92186, 92231, 92220, 2988804, 29888043
• CPC Class Codes: F02F 2003/0061 by welding
• 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

Exemplary piston assemblies and methods of making the same are disclosed. An exemplary piston assembly may include a piston crown and a piston skirt that is received in a central opening of the crown. The piston crown may include a ring belt portion defining, at least in part, a cooling gallery. The crown and skirt may each further include corresponding mating surfaces that extend about a periphery of the crown and skirt. The skirt mating surface and crown mating surface may generally be secured to each other that the crown and the skirt cooperate to form a continuous upper combustion bowl surface. The skirt and crown may cooperate to define a radially outer gap about a periphery of the piston crown.

Claims

1. A method, comprising:

providing a piston crown blank defining a doughnut shape having a preformed central aperture;

forming from the piston crown blank a piston crown including a ring belt portion defining at least in part a cooling gallery;

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;

securing the skirt to the crown along a single circumferential interface region between the crown and skirt, the interface region including corresponding mating surfaces of the skirt and crown, the mating surfaces being oriented at an acute angle with respect to an axis of the skirt and the crown, the skirt and crown cooperating to define a radially outer gap between the skirt and the crown about a periphery of the piston crown; and

installing a cover plate to enclose the cooling gallery, the cover plate forming a lower boundary of the cooling gallery;

wherein the corresponding mating surfaces meet near a base of the combustion bowl such that 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;

wherein securing the skirt to the crown is achieved by welding from inside the combustion bowl radially outward toward the radially outer gap such that weld splatter is reduced in the cooling gallery.

2. The method of claim 1, wherein the corresponding mating surfaces define the sole connection between the crown and skirt.

3. The method of claim 1, further comprising establishing welding the skirt to the crown as laser welding the skirt to the crown.

4. The method of claim 3, wherein laser welding the skirt to the crown includes directing a laser beam radially outward toward the corresponding mating surfaces.

5. The method of claim 4, wherein the corresponding mating surfaces cooperate to define a joint depth, the laser beam penetrating the crown and skirt along the corresponding mating surfaces to a beam depth less than the joint depth.

6. The method of claim 5, wherein the beam depth is approximately 1 millimeter less than the joint depth.

7. The method of claim 3, wherein directing the laser beam radially inward toward the corresponding mating surfaces includes directing the laser beam through the radially outer gap defined between the crown and the skirt.

8. The method of claim 1, wherein providing the piston crown blank includes one of casting and machining the piston crown blank.

9. A method, comprising:

providing a piston crown blank defining a doughnut shape having a preformed central aperture;

forming from the piston crown blank a piston crown including a ring belt portion defining at least in part a cooling gallery;

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;

directing a laser toward a single circumferential interface region between the crown and skirt, the interface region including corresponding mating surfaces of the skirt and crown, the mating surfaces being oriented at an acute angle with respect to an axis of the skirt and the crown, thereby welding the skirt to the crown along the corresponding mating surfaces, the skirt and crown cooperating to define a radially outer gap between the skirt and the crown about a periphery of the piston crown; and

installing a cover plate to enclose the cooling gallery, the cover plate forming a lower boundary of the cooling gallery;

wherein the corresponding mating surfaces meet near a base of the combustion bowl such that 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;

wherein the laser is directed from inside the combustion bowl radially outward toward the radially outer gap such that weld splatter is reduced in the cooling gallery.

10. The method of claim 9, wherein the corresponding mating surfaces define the sole connection between the crown and skirt.

11. The method of claim 9, wherein welding the skirt to the crown includes directing the laser radially outward toward the corresponding mating surfaces.

12. A piston assembly, comprising:

a piston crown, including a ring belt portion defining at least in part a cooling gallery, the crown including a crown mating surface extending about a periphery of the crown;

a piston skirt received in a central opening of the crown, the skirt including a skirt mating surface extending about a periphery of the skirt, the crown and skirt mating surfaces included in a single circumferential interface region between the crown and skirt and oriented at an acute angle with respect to an axis of the skirt and the crown, the skirt secured to the crown by the interface region such that the crown and skirt cooperate to form a continuous upper combustion bowl surface, the skirt and crown cooperating to define a radially outer gap between the skirt and the crown about a periphery of the piston crown;

wherein the corresponding mating surfaces meet near a base of the combustion bowl such that 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, and such that the mating surfaces are able to be welded from inside the combustion bowl radially outward toward the radially outer gap to reduce weld splatter in the cooling gallery; and

wherein the corresponding mating surfaces have a single slope to define the sole connection between the crown and skirt.

13. The piston assembly of claim 12, further comprising a cooling gallery cover plate forming a lower boundary of the cooling gallery, wherein the cooling gallery is generally enclosed by the crown and the cover plate.

14. The piston assembly of claim 12, wherein the combustion bowl surface is substantially smooth across the interface region.

15. The piston assembly of claim 12, wherein the ring belt portion is spaced apart from the skirt by the radially outer gap.