Granted Patent B2

US 12,601,449 · App. 18/742,939 · Granted Apr 14, 2026

Inventors: Matthew Michael Dethlefsen (Normandy Park, WA); Michael Smith Brendel (Snoqualmie, WA); William Thomas Johnson, IV (Kent, WA)

F17C1/14B64G1/4021F17C2201/0128F17C2201/0133F17C2201/0142F17C2203/0643F17C2270/0197

Abstract

Claims (56)

1 . A method for manufacturing a semi-ellipsoidal shell using a multi-conic preform, comprising:

providing a multi-conic preform having:

a preform cap;

a multi-conic preform wall; and

a first latitudinal preform weld joining the preform cap to the preform wall;

wherein the preform cap and the preform wall are sheet metal components;

wherein the preform wall is longitudinally segmented so as to include a plurality of annular preform wall segments; and

wherein each of the plurality of annular preform wall segments is joined to an adjacent preform wall segment by a respective latitudinal preform wall weld;

performing a first fluid pressure forming step, during which an inner surface of the preform is exposed to a strengthening pressure that work hardens at least the preform cap and the preform wall;

performing a second fluid pressure forming step, during which the inner surface of the preform is exposed to a design pressure that causes the preform to plastically deform and bulge so as to form the semi-ellipsoidal shell; and

between the first and second fluid pressure forming steps, at least partially reducing the pressure applied to the inner surface of the preform.

2 . A method for manufacturing a semi-ellipsoidal shell using a multi-conic preform, comprising:

providing a multi-conic preform having:

a preform cap;

a multi-conic preform wall; and

a first latitudinal preform weld joining the preform cap to the preform wall;

wherein the preform cap and the preform wall are sheet metal components;

wherein the preform wall is longitudinally segmented so as to include a plurality of annular preform wall segments; and

wherein each of the plurality of annular preform wall segments is joined to an adjacent preform wall segment by a respective latitudinal preform wall weld;

performing a first fluid pressure forming step, during which an inner surface of the preform is exposed to a strengthening pressure that work hardens at least the preform cap and the preform wall;

performing a second fluid pressure forming step, during which the inner surface of the preform is exposed to a design pressure that causes the preform to plastically deform and bulge so as to form the semi-ellipsoidal shell;

exposing the preform to cold temperatures during at least one of the first fluid pressure forming step and the second fluid pressure forming step.

3 . A method for manufacturing a semi-ellipsoidal shell using a multi-conic preform, comprising:

providing a multi-conic preform having:

a preform cap;

a multi-conic preform wall; and

a first latitudinal preform weld joining the preform cap to the preform wall;

wherein the preform cap and the preform wall are sheet metal components;

wherein the preform wall is longitudinally segmented so as to include a plurality of annular preform wall segments; and

wherein each of the plurality of annular preform wall segments is joined to an adjacent preform wall segment by a respective latitudinal preform wall weld;

performing a first fluid pressure forming step, during which an inner surface of the preform is exposed to a strengthening pressure that work hardens at least the preform cap and the preform wall;

performing a second fluid pressure forming step, during which the inner surface of the preform is exposed to a design pressure that causes the preform to plastically deform and bulge so as to form the semi-ellipsoidal shell;

wherein the plastic deformation and bulging that occurs during the second pressure fluid pressure forming step causes at least one of the preform cap and the preform wall to form a wrinkle; and

wherein the second fluid pressure forming step includes exposing the inner surface of the preform to the design pressure for a predetermined period of time after the wrinkle has formed.

4 . A method for assembling a multi-conic preform, the method comprising:

providing first and second preform wall segments, each in the form of a frustoconical sheet metal component, the first preform wall segment having top edge alignment markings disposed relative to a top edge of the first preform wall segment, and the second preform wall segment having bottom edge alignment markings disposed relative to a bottom edge of the second preform wall segment;

positionally fixing the first preform wall segment relative to the second preform wall segment such that the top edge alignment markings of the first preform wall segment are aligned with the bottom edge alignment markings of the second preform wall segment; and

joining the top edge of the first preform wall segment to the bottom edge of the second preform wall segment via a first latitudinal weld.

5 . The method of claim 4 , wherein the positionally fixing step includes connecting the top edge of the first preform wall segment to the bottom edge of the second preform wall segment via a plurality of tack welds.

6 . The method of claim 4 , wherein the joining step includes joining an entirety of the top edge of the first preform wall segment to the bottom edge of the second preform wall segment via the first latitudinal weld.

7 . The method of claim 6 , wherein the first latitudinal weld is provided by a laser welder.

8 . The method of claim 4 , wherein the joining step includes rotating the first and second preform wall segments on a rotary table while a stationary welder provides the first latitudinal weld.

9 . The method of claim 4 , further comprising: cutting a plurality of preform wall sub-segments from a sheet metal plate; and welding the plurality of preform wall sub-segments together to form the first preform wall segment.

10 . The method of claim 9 , further comprising: providing the top edge alignment markings at predetermined positions on the sheet metal plate before the step of cutting the plurality of preform wall sub-segments from the sheet metal plate.

11 . The method of claim 10 , wherein the step of cutting the plurality of preform wall sub-segments from the sheet metal plate and the step of providing the top edge alignment markings at predetermined positions on the sheet metal plate are performed using a same laser cutter.

12 . The method of claim 4 , wherein each of the top edge alignment markings includes an etching on a radially outer surface of the first preform wall segment and each of the bottom edge alignment markings includes an etching on a radially outer surface of the second preform wall segment.

13 . The method of claim 4 , wherein each of the top edge alignment markings includes an etching on a radially inner surface of the first preform wall segment and each of the bottom edge alignment markings includes an etching on a radially inner surface of the second preform wall segment.

14 . The method of claim 4 , wherein the top edge alignment markings and the bottom edge alignment markings extend beyond a heat-affected zone of the first latitudinal weld.

15 . The method of claim 4 , wherein the step of providing the top edge alignment markings includes depositing the top edge alignment markings at the predetermined positions on the sheet metal plate.

16 . The method of claim 15 , further comprising grinding the top edge alignment markings after the joining step.

17 . The method of claim 4 , wherein the first and second preform wall segments are each formed of stainless steel sheet metal.

18 . The method of claim 4 , wherein the first preform wall segment is formed of stainless steel sheet metal having a first predetermined hardness, the second preform wall segment is formed of stainless steel sheet metal having a second predetermined hardness that is different than the first predetermined hardness.

19 . The method of claim 4 , wherein the plurality of preform wall sub-segments are identical to one another, including respective positions of the top edge alignment markings thereon.

20 . The method of claim 4 , wherein the positionally fixing step includes simultaneously applying tack welds at circumferentially spaced locations corresponding to aligned top edge alignment markings and bottom edge alignment markings.

21 . The method of claim 4 , wherein the top edge alignment markings are provided by a laser etching step performed using a laser cutter at a first laser power setting and the cutting step is performed using the laser cutter at a second laser power setting greater than the first laser power setting.

22 . The method of claim 4 , wherein the top edge alignment markings define predetermined circumferential spacing such that alignment positions lie in a plane perpendicular to a semi-axis of the multi-conic preform.

Assignments (2)

Continuity (5)

References Cited (27)