IP Library Granted Patent US 7,104,307
Granted Patent B2
US 7,104,307 · App. 10/783,405 · Granted Sep 12, 2006

Casting mold for engine block

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Quick Facts
Patent No.
US 7,104,307
App. No.
10/783,405
Granted
Sep 12, 2006
Kind
B2
Abstract

A casting mold for an engine block and method for manufacturing the casting mold. In one embodiment, the casting mold includes a mold seat with a double-curved surface, and a cast-in cylinder liner. The cylinder liner has an axis and an end surface. The end surface is in tangential contact with the double-curved surface in a seated position prior to any thermal expansion of the cylinder liner. In various embodiments, the cylinder liner becomes slightly unseated upon thermal expansion.

Claims (37)

1. A casting mold for an engine block, the casting mold comprising:

a mold seat comprising a double-curved surface; and

a cast-in cylinder liner comprising an axis and a conical chamfer, wherein the conical chamfer is in a tangential contact with the double-curved surface in a seated position absent thermal expansion of the cylinder liner, wherein a first curved region of the double-curved surface is located on a first side of the tangential contact and a second curved region of the double-curved surface is on a second side of the tangential contact, wherein the double-curved surface forms a portion of one of a spherical surface or a toroidal surface about an axis.

2. The casting mold of claim 1 , wherein the conical chamfer forms an angle a with a plane perpendicular to the axis, such that the cylinder liner is unseated from the seated position upon thermal expansion.

3. The casting mold of claim 1 , wherein the double-curved surface is a spherical segment.

4. The casting mold of claim 1 , wherein the double-curved surface is a toroidal segment.

5. A casting mold for an engine block, the casting mold comprising:

a first mold seat comprising a double-curved first surface;

a second mold seat comprising a conical second surface; and

a cast-in cylinder liner comprising an axis and conical first and second chamfers, wherein the first and second chamfers are respectively in contact with the first and second surfaces at first and second contact circles in a seated position, such that upon thermal expansion the cylinder liner becomes unseated from the seated position, wherein a first curved region of the double-curved surface is located on a first side of the tangential contact and a second curved region of the double-curved surface is on a second side of the tangential contact, further wherein the double-curved surface forms a portion of one of a spherical surface or a toroidal surface about an axis of the cast-in cylinder liner.

6. The casting mold of claim 5 , wherein the first and second chamfers form angles α 1 and α 2 respectively relative to a plane perpendicular to the axis, and wherein α 1 is greater than the angle defined by tan −1 (L/2R), and α 2 is equal to tan −1 (L/2R), wherein L is the length of the cylinder liner between the contact circles and R is the inner radius of the cylinder liner at the contact circles.

7. The casting mold of claim 5 , wherein the first and second chamfers form angles α 1 and α 2 respectively relative to a plane perpendicular to the axis, and wherein α 1 is greater than the angle defined by tan −1 (L/2R), and α 2 is greater than tan −1 (L/2R), wherein L is the length of the cylinder liner between the contact circles and R is the inner radius of the cylinder liner at the contact circles.

8. A casting mold for an engine block, the casting mold comprising:

a double-curved mold seat comprising a conical surface, wherein said double-curved mold seat forms a portion of one of a spherical surface or a toroidal surface about an axis of a cast-in cylinder liner;

a cast-in cylinder liner comprising an axis and contacting the conical surface in a seated position absent thermal expansion, wherein the conical surface is inclined at an angle a with a plane perpendicular to the axis, such that upon thermal expansion the cylinder liner becomes unseated from the seated position.

9. A casting mold for an engine block, the casting mold comprising:

a first mold seat comprising a double-curved first surface;

a second mold seat comprising a double-curved second surface; and

a cast-in cylinder liner comprising an axis and first and second chamfers, wherein the first and second chamfers are respectively in a first and a second tangential contact with the first and second surfaces at first and second contact circles in a seated position, wherein the first tangential contact forms a first region of the double-curved first surface on a first side of the first tangential contact and forms a second region of the double-curved first surface on a second side of the tangential contact, and wherein the second tangential contact forms a first region of the double-curved second surface on a first side of the tangential contact and forms a second region of the double-curved second surface on the second side of the tangential contact, further wherein the double-curved surface of the first mold seat and of the second mold seat form a portion of one of a spherical surface or a toroidal surface about an axis of the cast-in cylinder liner, such that upon thermal expansion the cylinder liner becomes unseated from the seated position.

10. The casting mold of claim 9 , wherein the first and second chamfers are inclined at angles α 1 and α 2 respectively relative to a plane perpendicular to the axis, and wherein α 1 is greater than the angle defined by tan −1 (L/2R), and α 2 is equal to tan −1 (L/2R), wherein L is the length of the cylinder liner between the contact circles and R is the inner radius of the cylinder liner at the contact circles.

11. The casting mold of claim 9 , wherein the first and second chamfers form angles α 1 and α 2 respectively relative to a plane perpendicular to the axis, and wherein α 1 is greater than the angle defined by tan −1 (L/2R), and α 2 is greater than tan −1 (L/2R), wherein L is the length of the cylinder liner between the contact circles and R is the inner radius of the cylinder liner at the contact circles.

12. The casting mold of claim 11 , wherein α 1 =α 2 .

13. The casting mold of claim 9 , wherein each double-curved surface comprises a spherical portion.

14. The casting mold of claim 9 , wherein each double-curved surface comprises a toroidal portion.

15. A casting mold for an engine block, the casting mold comprising:

a first mold seat comprising a first double-curved surface;

a second mold seat comprising a second surface; and

a cast-in cylinder liner comprising an axis and first and second end surfaces, wherein the first and second end surfaces are respectively in tangential contact with the first and second surfaces in a seated position, such that upon thermal expansion the cylinder liner becomes unseated from the seated position, wherein a first curved region of the double-curved surface is located on a first side of the tangential contact and a second curved region of the double-curved surface is on a second side of the tangential contact, further wherein the double-curved surface forms a portion of one of a spherical surface or a toroidal surface about an axis of the cast-in cylinder liner.

16. The casting mold of claim 15 , wherein the first surface is conical.

17. A method of manufacturing a casting mold for an engine block, the method comprising:

providing a first mold seat comprising a first double-curved surface, wherein the double-curved surface forms a portion of one of a spherical surface or a toroidal surface about an axis of the cast-in cylinder liner;

providing a second mold seat comprising a second surface; and

placing the cast-in cylinder liner in a seated position in contact with the first and second surfaces respectively at first and second end surfaces of the cylinder liner absent thermal expansion, wherein the first surface is shaped such that upon thermal expansion the cylinder liner becomes unseated.

18. The method of claim 17 , wherein the first surface comprises a double-curved portion in contact with the first end surface of the cylinder.

19. The method of claim 17 , wherein the first surface comprises a conical portion in contact with the first end surface of the cylinder liner.

20. The method of claim 17 , wherein the second surface is shaped such that upon thermal expansion the cylinder liner is unseated from the seated position.

21. The method of claim 20 , wherein the second surface comprises a conical portion in contact with the second end surface of the cylinder liner.

Assignments (13)
RELEASE OF SECURITY INTEREST Recorded Nov 7, 2014
From: WILMINGTON TRUST COMPANY
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 034371/0676 →
CHANGE OF NAME Recorded Feb 10, 2011
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: GM GLOBAL TECHNOLOGY OPERATIONS LLC
Reel/Frame 025780/0902 →
SECURITY AGREEMENT Recorded Nov 8, 2010
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: WILMINGTON TRUST COMPANY
Reel/Frame 025327/0262 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025245/0442 →
RELEASE OF SECURITY INTEREST Recorded Nov 4, 2010
From: UAW RETIREE MEDICAL BENEFITS TRUST
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 025311/0770 →
SECURITY AGREEMENT Recorded Aug 28, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UAW RETIREE MEDICAL BENEFITS TRUST
Reel/Frame 023162/0001 →
SECURITY AGREEMENT Recorded Aug 27, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 023156/0052 →
RELEASE OF SECURITY INTEREST Recorded Aug 21, 2009
From: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023127/0468 →
RELEASE OF SECURITY INTEREST Recorded Aug 20, 2009
From: UNITED STATES DEPARTMENT OF THE TREASURY
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 023124/0429 →
SECURITY AGREEMENT Recorded Apr 16, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: CITICORP USA, INC. AS AGENT FOR BANK PRIORITY SECURED PARTIES; CITICORP USA, INC. AS AGENT FOR HEDGE PRIORITY SECURED PARTIES
Reel/Frame 022553/0446 →
SECURITY AGREEMENT Recorded Feb 4, 2009
From: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
To: UNITED STATES DEPARTMENT OF THE TREASURY
Reel/Frame 022201/0610 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 14, 2009
From: GENERAL MOTORS CORPORATION
To: GM GLOBAL TECHNOLOGY OPERATIONS, INC.
Reel/Frame 022117/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 20, 2004
From: NEWCOMB, THOMAS P.; MEYER, MAURICE G.
To: GENERAL MOTORS CORPORATIN
Reel/Frame 015013/0963 →