Reusable laser welded hermetic enclosure and method

• US 5,519,184 A
• Filed: 05/20/1994
• Issued: 05/21/1996
• Est. Priority Date: 05/20/1994
• Status: Expired due to Fees

• Current Assignee: James F. Kirk
• Original Assignee: Litton Systems Incorporated
• Inventors: Umlas, Michael P.
• Primary Examiner(s): Lateef, Marvin M.
• Assistant Examiner(s): Pelham, J.
• Application Number:
  US08/246,679
• Time in Patent Office: 732 Days
• Field of Search: 219/121.6, 219/121.63, 219/121.64, 220/612, 228/262.5, 228/262.51, 228/262.9
• US Class Current: 219/121.64
• CPC Class Codes: B23K 26/206 Laser sealing
• CPC Class Codes: B23K 26/24 Seam welding
• CPC Class Codes: B23K 26/244 Overlap seam welding

Abstract

The reusable welded hermetic enclosure and method provides a laser weld between a cover and a chassis to form an enclosure or a laser weld between two parts to form a hermetic seal. In either event, one part has an open mouth with a sloped or tapered external section surrounding the mouth to receive the larger mouth of the other part. The mouth of the other part is sloped or tapered to conform to the sloped or tapered external section of the first part. The parts are pressed together for an interference fit to eliminate gaps and the laser weld connects the sloped or tapered sections. When the materials to be welded are of low silicon content aluminum, it is necessary to include a filler ring of an aluminum-silicon alloy containing a predetermined silicon content between the sloped or tapered sections. The cover and the chassis are reusable after opening. The filler ring is sacrificed during the removal of the cover.

Claims

1. A hermetically sealed reusable enclosure for protecting expensive delicate heat sensitive components comprising in combination:

a chassis having an open mouth, but otherwise being closed;

a tapered external surface integral with the chassis about the mouth;

a weld filler ring tightly about a peripheral portion of said tapered external surface;

a ductile cover having an open internally tapered mouth for receiving the mouth of the chassis and pressing the ring against the peripheral portion of said tapered external surface to establish an interference fit; and

,

a laser weld connecting the cover mouth, ring and the tapered external surface to effect a hermetic seal around the tapered external surface.

2. The enclosure of claim 1, wherein the open mouth of the chassis is circular.

3. The enclosure of claim 2, wherein the weld filler ring is conical shaped to mate with the tapered external surface of the chassis.

4. The enclosure of claim 3, wherein the cover is closed except for its mouth which is tapered to fit the taper of the tapered external surface.

5. The enclosure of claim 4, wherein a small portion of the weld filler ring is alloyed with a small portion of the cover and the chassis in the laser weld.

6. The enclosure of claim 1, wherein at least the tapered external surface of the chassis is A356.0-T65 aluminum alloy, the weld filler ring is 4047 aluminum alloy and at least the cover mouth is 6061 aluminum alloy.

7. The enclosure of claim 5 wherein the cover is a drawn can of 6061 aluminum alloy sheet, the chassis is a casting of A356.0-T6 aluminum alloy, and the weld filler ring is 4047 aluminum alloy sheet.

8. A hermetically sealed reusable light weight enclosure for protecting heat sensitive components comprising, in combination:

a substantially cup-shaped chassis having an open circular mouth, a closed bottom and a continuous wall between the bottom and mouth;

a tapered conical external surface around and integral with the wall adjacent to the mouth sloping inwardly toward the mouth of the chassis;

a conical shaped weld filler ring conforming to a circumferential portion of the tapered external surface and tightly fit thereon;

a closed ductile cover having an open mouth for receiving a portion of the tapered external surface and ring adjacent thereto;

said mouth and adjacent portion of the cover being internally conically flared outwardly in the direction of the chassis to match the slope of the tapered external surface and adjacent weld filler ring whereby the cover, ring and tapered external surface are wedged together in an interference fit with an end of the ring extending beyond the cover mouth, but falling short of the end of the tapered external surface thereby exposing the juxtaposed flared portion of the cover and weld filler ring; and

,

a laser weld connecting the cover mouth, ring and tapered external surface of the chassis to effect a hermetic seal around the tapered surface which is leak proof under 3×

10^-10 cc He/sec. at one atmosphere pressure differential.

9. The enclosure of claim 8 wherein the cover is a drawn can of 6061 aluminum alloy sheet, the chassis is a casting of A356.0-T6 aluminum alloy, and the weld filler ring is from 4047 aluminum alloy sheet, including a percentage of silicon.

10. The method of making a reusable hermetically sealed enclosure for delicate expensive heat sensitive aircraft components comprising the following steps:

forming a closed chassis having an open mouth;

forming a tapered conical external surface on the chassis about the mouth;

placing a conical weld filler ring tightly about the tapered conical external surface;

forming a closed ductile cover having an open mouth to fit about the ring including a tapered internal conical surface;

pressing the cover onto the ring and chassis to establish an interference fit so that the conical cover surface overlies the conical ring which overlies the conical external surface; and

laser welding the cover mouth, ring, and the tapered external surface together to effect a hermetic seal around the tapered external surface.

11. The method of claim 10, comprising the steps of:

drawing the cover in can shape, from 6061 aluminum alloy sheet;

casting the chassis from A356.0-T6 aluminum alloy; and

cutting the weld filler ring from 4047 aluminum alloy sheet including a percentage of silicon.

12. A hermetically sealed enclosure of material other than aluminum capable of protecting heat sensitive components comprising in combination:

a chassis having an open mouth, but otherwise being closed;

an integral conical external surface on the chassis about the mouth;

a ductile cover having an open mouth and an internally flared conical portion for receiving the mouth of the chassis and a portion of the external conical surface and pressing the cover conical surface against said tapered external surface to form an interference fit; and

,

a laser weld connecting the cover portion, and the tapered external surface to effect a hermetic seal around the tapered external surface.