Horizontal integration tooling for launch vehicles, and associated systems and methods

Patent metadata

Field	Value
Publication number	US-12097976-B2
Application number	US-202318364069-A
Country	US
Kind code	B2
Filing date	Aug 2, 2023
Priority date	May 14, 2021
Publication date	Sep 24, 2024
Grant date	Sep 24, 2024

Abstract

A representative system includes an alignment tool for aligning attachment interfaces of horizontally-oriented launch vehicle portions. The tool can include a receiver assembly for connecting to a first launch vehicle portion and an actuation assembly for connecting to a second launch vehicle portion. When a first connecting element of the receiver assembly is engaged with a second connecting element of the actuation assembly, the second connecting element can apply force to the receiver assembly, and the actuator assembly applies an opposite force to the second launch vehicle portion, to align fastening features in the launch vehicle portions and/or to reshape the launch vehicle portions. A representative method includes connecting the alignment tool to the launch vehicle portions and operating the tool to apply oppositely-directed forces to align the launch vehicle portions for installing fasteners to connect the launch vehicle portions. One or more bracing beams can connect two tools together.

First claim

I claim:

1. A method of aligning and fastening a first launch vehicle portion to a second launch vehicle portion, the method comprising:
coupling a receiver assembly to the first launch vehicle portion;
coupling an actuation assembly to the second launch vehicle portion;
establishing a load path between the receiver assembly and the actuation assembly;
operating the actuation assembly to apply oppositely-directed forces to the receiver assembly and to the second launch vehicle portion until a first fastener hole in the first launch vehicle portion aligns with a second fastener hole in the second launch vehicle portion, wherein the actuation assembly comprises an actuation nub in engagement with a socket of the receiver assembly;
and installing one or more fasteners in the first launch vehicle portion and in the second launch vehicle portion to fasten the first launch vehicle portion to the second launch vehicle portion.

2. The method of claim 1 , wherein coupling the receiver assembly to the first launch vehicle portion comprises positioning a first peg in the first fastener hole in the first launch vehicle portion, and wherein coupling the actuation assembly to the second launch vehicle portion comprises positioning a second peg in the second fastener hole in the second launch vehicle portion.

3. The method of claim 2 , further comprising positioning a bushing in the first fastener hole or the second fastener hole.

4. The method of claim 1 , wherein coupling the receiver assembly to the first launch vehicle portion comprises engaging a first locking mechanism comprising a first movable shoe positioned to press against the first launch vehicle portion, and wherein coupling the actuation assembly to the second launch vehicle portion comprises engaging a second locking mechanism comprising a second movable shoe positioned to press against the second launch vehicle portion.

5. The method of claim 1 , wherein establishing the load path between the receiver assembly and the actuation assembly comprises positioning the actuation nub carried by the actuation assembly in the socket carried by the receiver assembly or positioning the actuation nub carried by the receiver assembly in the socket carried by the actuation assembly.

6. The method of claim 1 , wherein the receiver assembly is a first receiver assembly and the actuation assembly is a first actuation assembly, the method further comprising:
coupling a second receiver assembly to the first launch vehicle portion;
coupling a second actuation assembly to the second launch vehicle portion; and
establishing a load path between the second receiver assembly and the second actuation assembly.

7. The method of claim 6 , further comprising:
via a bracing beam, connecting the first receiver assembly to the second receiver assembly or connecting the first actuation assembly to the second actuation assembly.

8. A method of aligning a first component with a second component, the method comprising:
coupling a receiver assembly to the first component, wherein the receiver assembly includes a first connecting element;
coupling an actuation assembly to the second component, wherein the actuation assembly carries a second, movable, connecting element;
establishing a load path by engaging the first connecting element and the second connecting element, wherein the first connecting element comprises an actuation nub and the second connecting element comprises a socket; and
operating the actuation assembly to move the second connecting element, wherein the actuation assembly applies one or more forces to the receiver assembly and to the second component, to move the second component relative to the first component and/or to move the first component relative to the second component.

9. The method of claim 8 , wherein the first connecting element is fixed in place relative to a chassis of the receiver assembly.

10. The method of claim 8 , wherein coupling the receiver assembly to the first component comprises positioning a first peg in a first fastener hole in the first component, and wherein coupling the actuation assembly to the second component comprises positioning a second peg in a second fastener hole in the second component.

11. The method of claim 8 , wherein coupling the receiver assembly to the first component comprises engaging a first locking mechanism comprising a first movable shoe positioned to press against the first component, and wherein coupling the actuation assembly to the second component comprises engaging a second locking mechanism comprising a second movable shoe positioned to press against the second component.

12. The method of claim 8 , further comprising: establishing the load path between the first connecting element and the second connecting element comprises positioning the actuation nub in the socket.

13. The method of claim 8 , wherein the receiver assembly is a first receiver assembly and the actuation assembly is a first actuation assembly, the method further comprising:
coupling a second receiver assembly to the first component;
coupling a second actuation assembly to the second component; and
establishing a load path between the second receiver assembly and the second actuation assembly.

14. The method of claim 13 , further comprising:
via a bracing beam, connecting the first receiver assembly to the second receiver assembly and/or connecting the first actuation assembly to the second actuation assembly.

15. The method of claim 8 , wherein the first component is a first launch vehicle portion, the second component is a second launch vehicle portion, and the method further comprises aligning a first fastener hole in the first launch vehicle portion with a second fastener hole in the second launch vehicle portion.

16. A method of aligning a first fastener hole in a first component with a second fastener hole in a second component, the method comprising:
engaging a portion of a receiver assembly with the first fastener hole;
engaging a portion of an actuation assembly with the second fastener hole;
establishing a load path between a first connecting element carried by the receiver assembly and a second connecting element carried by the actuation assembly, wherein the second connecting element is movable, wherein the first connecting element comprises an actuation nub and the second connecting element comprises a socket, the load path is established when the actuation nub engages the socket; and
operating the actuation assembly to move the second connecting element, wherein movement of the second connecting element applies force to the first connecting element to move the receiver assembly and the first fastener hole relative to the second fastener hole and/or to move the second fastener hole relative to the first fastener hole.

17. The method of claim 16 , wherein the first component is a first launch vehicle portion, the second component is a second launch vehicle portion, the receiver assembly is a first receiver assembly, and the actuation assembly is a first actuation assembly, and the method further comprises:
coupling a second receiver assembly to the first launch vehicle portion;
coupling a second actuation assembly to the second launch vehicle portion;
establishing a load path between the second receiver assembly and the second actuation assembly; and
via a bracing beam, connecting the first receiver assembly to the second receiver assembly and/or connecting the first actuation assembly to the second actuation assembly.

18. The method of claim 16 , wherein engag

Assignees

• Blue Origin Llc

Inventors

• Johnson Derek

Classifications

• B64G1/002

  Launch systems · CPC title

• B23P19/10

  Aligning parts to be fitted together · CPC title

• B23Q3/186

  Aligning devices · CPC title

• B64F5/10 Primary

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title