Brace for fuselage repairs

Patent metadata

Field	Value
Publication number	US-12522375-B2
Application number	US-202418614412-A
Country	US
Kind code	B2
Filing date	Mar 22, 2024
Priority date	Mar 22, 2024
Publication date	Jan 13, 2026
Grant date	Jan 13, 2026

Abstract

The present disclosure provides a brace having a first leg and a second leg offset from the first leg. The brace also has a pivot assembly having a bar pivotably coupled with the first leg to define a first pivot point and pivotably coupled with the second leg to define a second pivot point. The brace further includes first and second attachment assemblies coupled with the first leg and the second leg, respectively, and each arranged to couple to a portion of a structure. In addition, the brace includes an actuator assembly coupling the first leg with the second leg and having an actuator arranged to pivot, or maintain a position of, the first leg relative to the first pivot point and to pivot, or maintain the position of, the second leg relative to the second pivot point so as to control a load on, and deflection of, the structure.

First claim

What is claimed is:

1 . A brace, comprising:
a first leg; a second leg offset from the first leg; a pivot assembly having a bar pivotably coupled with the first leg to define a first pivot point and pivotably coupled with the second leg to define a second pivot point; first and second attachment assemblies coupled with the first leg and the second leg, respectively, and each arranged to couple to a portion of a structure; and an actuator assembly coupling the first leg with the second leg and having an actuator arranged to pivot the first leg relative to the first pivot point and to pivot the second leg relative to the second pivot point so as to control a load on, and deflection of, the structure, wherein the bar is static and configured to maintain a spacing between the first and second pivot points.

2 . The brace of claim 1 , wherein the first attachment assembly is arranged to couple to a first portion of the structure and the second attachment assembly is arranged to couple to a second portion of the structure, and wherein the first and second portions of the structure are separated by a damaged section or a removed section of the structure.

3 . The brace of claim 1 , wherein:
the first leg has a first end and a second end, and wherein the actuator assembly is pivotably coupled with the first end of the first leg and the first attachment assembly is coupled with a first foot of the first leg at the second end of the first leg, and the second leg has a first end and a second end, and wherein the actuator assembly is coupled with the first end of the second leg and the second attachment assembly is coupled with a second foot of the second leg at the second end of the second leg.

4 . The brace of claim 1 , wherein the first attachment assembly has a first attachment fitting having a coupler, first and second extenders, and first and second fittings, and wherein the coupler is coupled with the first leg, the first and second extenders extend outward from the coupler in opposing directions, and the first fitting is connected to the first extender and the second fitting is connected to the second extender.

5 . The brace of claim 4 , wherein the first attachment assembly has a first bookend fitting and a second bookend fitting, and wherein the first fitting and the first bookend fitting are adapted to receive, and secure, a first frame of the structure therebetween and the second fitting and the second bookend fitting are adapted to receive, and secure, a second frame of the structure therebetween, the first frame and the second frame being spaced from one another.

6 . The brace of claim 4 , wherein the first extender has a first housing and a slider that is slidable relative to the first housing, and wherein the first fitting is connected to the slider.

7 . The brace of claim 1 , wherein the first leg has a backbone, a flange extending from the backbone, and a foot, and wherein the actuator assembly and the pivot assembly are coupled with the flange and the first attachment assembly is coupled with the foot.

8 . The brace of claim 7 , wherein a distance that the flange extends from the backbone varies along a length of the flange, and wherein a notch is defined between an actuator joint where the actuator assembly couples to the first leg and a pivot joint where the pivot assembly couples to the first leg, and wherein the flange tapers from the pivot joint to the foot.

9 . The brace of claim 1 , wherein the pivot assembly has a first clevis coupling the bar with the first leg and a second clevis coupling the bar with the second leg, and wherein the first and second clevises are coupled with the first and second legs at a first pivot joint and a second pivot joint, respectively.

10 . The brace of claim 1 , further comprising:
a load cell placed in-line with the actuator.

11 . The brace of claim 1 , further comprising:
a strain gauge arranged on the bar.

12 . A repair system, comprising:
a brace, comprising:
a first leg;
a second leg offset from the first leg;
a pivot assembly having a bar pivotably coupled with the first leg to define a first pivot point and pivotably coupled with the second leg to define a second pivot point;
first and second attachment assemblies coupled with the first leg and the second leg, respectively, and each arranged to couple to a portion of a structure;
an actuator assembly coupling the first leg and the second leg, the actuator assembly having an actuator;
a sensor; and
a computing system comprising one or more processors and one or more memory devices storing a program, which, when executed by any combination of the one or more processors, causes the one or more processors to perform an operation, the operation comprising:
receiving feedback from the sensor; and
performing at least one of:
i) causing, based at least in part on the feedback, the actuator to pivot, or maintain a position of, the first and second legs relative to the first and second pivot points, respectively, so as to control a load on, and deflection of, the structure; or
ii) presenting the feedback or a target displacement or load associated with the brace determined based at least in part on the feedback.

13 . The repair system of claim 12 , wherein the first attachment assembly is arranged to couple to a first portion of the structure and the second attachment assembly is arranged to couple to a second portion of the structure, and wherein the first and second portions of the structure are separated by a damaged section or a removed section of the structure.

14 . The repair system of claim 12 , wherein:
the first leg has a first end and a second end, and wherein the actuator assembly is pivotably coupled with the first end of the first leg and a first attachment assembly is coupled with a first foot of the first leg at the second end of the first leg, and the second leg has a first end and a second end, and wherein the actuator assembly is coupled with the first end of the second leg and a second attachment assembly is coupled with a second foot of the second leg at the second end of the second leg.

15 . The repair system of claim 14 , wherein the first attachment assembly has a first attachment fitting having a coupler, first and second extenders, and first and second fittings, and wherein the coupler is coupled with the first leg, the first and second extenders extend outward from the coupler in opposing directions, and the first fitting is connected to the first extender and the second fitting is connected to the second extender.

16 . The repair system of claim 15 , wherein the first attachment assembly has a first bookend fitting and a second bookend fitting, and wherein the first fitting and the first bookend fitting are adapted to receive, and secure, a first frame of the structure therebetween and the second fitting and the second bookend fitting are adapted to receive, and secure, a second frame of the structure therebetween, the first frame and the second frame being spaced from one another.

17 . The repair system of claim 15 , wherein the first extender has a first housing and a slider that is slidable relative to the first housing, and wherein the first fitting is connected to the slider.

18 . The repair system of claim 12 , wherein the pivot assembly has a first clevis coupling the bar with the first leg and a second clevis coupling the bar with the second leg, and wherein the first and second clevises are coupled with the first and second legs at a first pivot joint and a second pivot

Assignees

• Boeing Co

Inventors

• Hellman Clifford
• Gruner Bryan J
• Leigh Gregory P

Classifications

• B64F5/40 Primary

  Maintaining or repairing aircraft · CPC title