Granted Patent B2

US 12,486,048 · App. 18/887,817 · Granted Dec 2, 2025

Inventor: Derek Johnson (Seattle, WA)

Assignee: Blue Origin Manufacturing, LLC

B64F5/10B23P19/10B23Q3/186B64G1/002

Abstract

Claims (52)

1 . A method of aligning annular sections of a launch vehicle, the method comprising:

coupling a receiver assembly to a first one of the annular sections;

coupling an actuation assembly to a second one of the annular sections;

establishing a load path between the receiver assembly and the actuation assembly; and

operating a threaded shaft of the receiver assembly or the actuation assembly to cause opposite movements to occur at the same time, in part through the load path, for a first feature of the receiver assembly and for a second feature of the actuation assembly, wherein the opposite movements allow the first feature and the second feature to cause the annular sections to align while maintaining a circular shape in each of the annular sections.

2 . The method of claim 1 , further comprising:

providing an actuation block comprising an actuation nub to be movable along the threaded shaft; and

associating the actuation nub within a socket of the receiver assembly to provide the load path.

3 . The method of claim 1 , further comprising:

providing at least one locking mechanism which is associated with one or more of the receiver assembly or the actuation assembly, the at least one locking mechanism to lock one or more of the receiver assembly or the actuation assembly; and

activating the at least one locking mechanism prior to operating the threaded shaft.

4 . The method of claim 1 , further comprising:

providing the first feature of the receiver assembly and the second feature of the actuation assembly through a plurality of bolt holes in the annular sections, wherein the first feature and the second feature support the opposite movements through the plurality of bolt holes to cause the annular sections to align while maintaining the circular shape in each of the annular sections.

5 . The method of claim 4 , wherein the plurality of bolt holes comprise bushings of a softer material relative to an annular section material having the plurality of bolt holes, the bushings to protect the annular section material during the opposite movements imparted through the first feature and the second feature.

6 . The method of claim 4 , wherein the plurality of bolt holes are within a plurality of flanges in individual edges of individual ones of the annular sections, the plurality of flanges to be aligned as part of the annular sections being aligned while maintaining the circular shape in each of the annular sections.

7 . The method of claim 4 , wherein the plurality of bolt holes are within a plurality of tool regions in individual edges of individual ones of the annular sections, the plurality of tool regions to comprise at least part of the receiver assembly or part of the actuation assembly to allow positioning of one or more of the receiver assembly or the actuation assembly to perform the aligning of the annular sections.

8 . A method of using an alignment tool with annular sections of a launch vehicle, the method comprising:

providing, as part of the alignment tool, a receiver assembly which is adapted to couple with a first one of the annular sections using a first feature and which comprises a first load feature of a load path;

providing, as part of the alignment tool, an actuation assembly which is adapted to couple with a second one of the annular sections using a second feature and which comprises a second load feature of the load path; and

associating a threaded shaft with at least one of the receiver assembly or the actuation assembly to enable opposite movements to occur at the same time and through the load path, through the first feature, and through second feature, wherein the opposite movements are to cause the annular sections to align while maintaining a circular shape in each of the annular sections.

9 . The method of claim 8 , further comprising:

associating the threaded shaft with the actuation assembly by threading the treaded threaded shaft through an actuation block which comprises an actuation nub, the actuation nub forming the second load feature and to be movable along the threaded shaft.

10 . The method of claim 9 , further comprising:

providing a socket in the receiver assembly, the socket forming the first load feature and to be movable along with the actuation nub.

11 . The method of claim 8 , further comprising:

providing at least one locking mechanism which is associated with one or more of the receiver assembly or the actuation assembly, the at least one locking mechanism to lock one or more of the receiver assembly or the actuation assembly.

12 . A method of aligning annular sections of a launch vehicle, the method comprising:

providing a plurality of flanges in a first one of the annular sections and in a second one of the annular sections;

providing a plurality of bolt holes in the plurality of flanges, wherein the plurality of bolt holes are to receive features of at least one receiver assembly and at least one actuation assembly of an alignment tool, and wherein the at least one receiver assembly and the at least one actuation assembly are associated with at least one load path therebetween; and

enabling the plurality of flanges to receive opposite movements through the at least one load path, wherein the opposite movements are caused at the same time, in part, by the at least one receiver assembly or the at least one actuation assembly and caused through the features of the at least one receiver assembly and the at least one actuation assembly, and wherein the opposite movements cause the aligning of the annular sections while maintaining a circular shape in each of the annular sections.

13 . The method of claim 12 , further comprising:

providing bushings within the plurality of bolt holes, the bushings comprising a softer material relative to an annular section material having the plurality of bolt holes, the bushings to protect the annular section material during the opposite movements imparted through a first feature of the at least one receiver assembly and a second feature of the at least one actuation assembly.

14 . The method of claim 12 , further comprising:

providing a plurality of tool regions adjacent to the plurality of flanges, the plurality of tool regions to comprise at least part of the receiver assembly or part of the actuation assembly to allow positioning of one or more of the receiver assembly or the actuation assembly to perform the aligning of the annular sections.

15 . The method of claim 12 , further comprising:

determining different parts of respective perimeters of the annular sections to be used for the aligning of the annular sections;

associating, at the different parts of the respective perimeters, a plurality of receiver assemblies as part of the at least one receiver assembly and a plurality of actuation assemblies as part of the at least one actuation assembly; and

causing the opposite movements through the different parts of the respective perimeters of the annular sections by the plurality of receiver assemblies and the plurality of actuation assemblies.

16 . An alignment tool to align annular sections of a launch vehicle, the alignment tool comprising:

a receiver assembly to couple with a first one of the annular sections and comprising a first load feature of a load path;

an actuation assembly to couple with a second one of the annular sections and comprising a second load feature of the load path; and

a threaded shaft of the receiver assembly or the actuation assembly to cause opposite movements to occur at the same time, in part through the load path of the first load feature and the second load feature, wherein the opposite movements allow are to cause the annular sections to align while maintaining a circular shape in each of the annular sections.

17 . The alignment tool of claim 16 , further comprising:

a first feature of the receiver assembly to be within a first bolt hole of the first one of the annular sections; and

a second feature of the actuation assembly to be within a second bolt hole of the second one of the annular sections, wherein the first feature and the second feature are to be moved by the opposite movements to cause the annular sections to align while maintaining the circular shape in each of the annular sections.

18 . The alignment tool of claim 16 , further comprising:

an actuation block comprising an actuation nub as the first load feature and to be movable along the threaded shaft; and

a socket of the receiver assembly as the second load feature and to receive the actuation nub.

19 . The alignment tool of claim 16 , further comprising:

at least one locking mechanism which is associated with one or more of the receiver assembly or the actuation assembly, the at least one locking mechanism to lock one or more of the receiver assembly or the actuation assembly prior to operating the threaded shaft.

20 . The alignment tool of claim 16 , further comprising:

a bracing beam to associate the alignment tool with a further alignment tool, the alignment tool and the further alignment tool located in different parts of respective perimeters of the annular sections and to be used for the aligning of the annular sections.

Assignments (1)

Continuity (3)

References Cited (38)