Flangeless fuel tank

• US 5,626,776 A
• Filed: 06/05/1995
• Issued: 05/06/1997
• Est. Priority Date: 10/21/1993
• Status: Expired due to Fees

• Current Assignee: Morris Holmes & Co.
• Original Assignee: Morris Holmes & Co.
• Inventors: Morris, H. Edward Jr.
• Primary Examiner(s): Walberg, Teresa J.
• Assistant Examiner(s): Pelham, J.
• Application Number:
  US08/463,918
• Time in Patent Office: 701 Days
• Field of Search: 219/121.6, 219/121.63, 219/121.64, 219/121.85, 219/61.3, 219/64, 220/4.14, 220/4.12, 220/4.21, 220/612, 220/678, 220/680, 220/689
• US Class Current: 219/121.64
• CPC Class Codes: B23K 2101/34 Coated articles , e.g. plated or painted; Surface treated articles
• CPC Class Codes: B23K 2103/08 Non-ferrous metals or alloys
• CPC Class Codes: B23K 2103/50 Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26
• CPC Class Codes: B23K 26/244 Overlap seam welding
• CPC Class Codes: B23K 26/32 taking account of the properties of the material involved
• CPC Class Codes: B60K 15/03 Fuel tanks chassis frame comprising fluid storage compartment B62D21/16 ; Details of the fuel feeding system related to the fuel tank F02M37/0076
• CPC Class Codes: B60K 2015/03453 for fixing or mounting parts of the fuel tank together

Abstract

A flangeless fuel tank formed of two interfitted cup-shaped tank halves welded along the overlapping portion of the tank halves. Locating protrusions stamped into each tank half provide registration of the halves prior to welding. Spacing dimples stamped into at least one of the fuel tank halves provide a vent space for escaping gases from vaporized coatings.

Claims

1. A method for producing a flangeless tank by interfitting and welding together a male and female tank half, wherein at least one of said tank halves is coated with a material having a vaporization temperature lower than the temperature necessary to weld said tank halves, the method comprising the steps of:

stamping at least one of said tank halves with an arrangement of spacing dimples along a weld line;

stamping said tank halves with locating protrusions of substantially greater depth than said spacing dimples and in such a manner that said locating protrusions are disposed adjacent to said arrangement of spacing dimples on the side longitudinally opposite the exterior edge of said tank halves, said locating protrusions on said male tank half extending toward the exterior of said flangeless fuel tank, and said locating protrusions on said female tank half extending toward the interior of said flangeless fuel tank;

interfitting said fuel tank halves such that said male tank half is received within said female tank half up to the extent that said female tank half abuts with said locating protrusions of said male tank half and said male tank half abuts with said locating protrusions of said female tank half, thereby defining an overlap position having the weld line disposed circumferentially thereon, the spacing dimples maintaining a vent space between the two tank halves;

applying an electromagnetic clamping means to forcibly secure said tank halves, said electromagnetic clamping means comprised of two distinct electromagnetic clamping heads disposed in such a manner as to allow access to said weld line; and

laser beam welding said tank halves along the entire length of said weld line.

2. A method for producing a flangeless tank as defined in claim 1 wherein said arrangement of dimples is comprised of four rows of dimples disposed substantially parallel to said weld line and being of substantially lesser depth than said locating protrusions;

said four rows of dimples having a first pair of rows disposed on the same longitudinal side of said weld line and a second pair of rows of dimples disposed on the longitudinal side of said weld line opposite said first two rows.

3. A method for producing a flangeless tank as defined in claim 1 wherein said locating protrusions are further defined as a row of dimples disposed substantially parallel to said weld line.

4. A method for producing a flangeless tank as defined in claim 1 wherein said locating protrusions are further defined as a row of intermittent dashes disposed substantially parallel to said weld line.

5. A method for producing a flangeless tank as defined in claim 1 wherein said locating protrusions are further defined as a continuous trough extending longitudinally around said circumferential walls and substantially parallel to said weld line.

6. A method of fabricating a flangeless fuel tank of coated metal comprising:

forming first and second cup-shaped tank halves each having a peripheral wall terminating in an edge;

forming locator protrusions in at least one of the peripheral walls;

forming spacing dimples in at least one of the peripheral walls, the spacing dimples being of lesser height than the locator protrusions;

interfitting the tank halves until the terminal edge of the other wall engages the locator protrusions in the one wall, the dimples engaging the other wall to provide a vent space between the walls; and

welding the walls together in the area of the dimples, whereby vaporized coatings are vented through the vent space.

7. A method as defined in claim 6 wherein said locator protrusions are formed in both of the walls.

8. A method as defined in claim 6 wherein said locator protrusions are arranged in a line.

9. A method of fabricating a flangeless container comprising:

forming two cup-shaped container halves from coated metal each including a peripheral side wall terminating in an edge;

forming a plurality of locator protrusions arranged in a line in one of the peripheral walls;

forming a plurality of spacing dimples in one of the peripheral walls, the spacing dimples being of lesser height than the locator protrusions;

interfitting said container halves until the edge of the other peripheral wall engages the locator protrusions in the one side wall, the spacing dimples engaging the other container half to define a vent space; and

welding the side walls together with vaporized coatings created during said welding step escaping through the vent space.

10. A method as defined in claim 9 wherein said second forming step comprises forming the protrusions in both of the peripheral walls.