Isolation coupler for a structural assembly and method for attenuating a load

Patent metadata

Field	Value
Publication number	US-11105459-B2
Application number	US-201816214638-A
Country	US
Kind code	B2
Filing date	Dec 10, 2018
Priority date	Dec 10, 2018
Publication date	Aug 31, 2021
Grant date	Aug 31, 2021

Abstract

An isolation coupler for coupling a functional element to a support structure includes a first bracket. The first bracket includes a number of first-bracket sides. The number of first-bracket sides forms a closed polygonal shape, in plan view. The isolation coupler further includes a number of isolators coupled to each one of the first-bracket sides. The isolation coupler also includes a second bracket. The second bracket includes a number of second-bracket sides. The second bracket sides are coupled to the isolators. The number of second-bracket sides is equal to the number of first-bracket sides and forms the closed polygonal shape, in plan view. The isolators separate each one of the first-bracket sides from a corresponding one of the second-bracket sides to attenuate a load transferred from the first bracket to the second bracket.

First claim

What is claimed is:

1. An isolation coupler for coupling a functional element to a support structure, the isolation coupler comprising:
a first bracket comprising a number of first-bracket sides, wherein the number of first-bracket sides forms a closed polygonal shape, in plan view;
a number of isolators coupled to each one of the first-bracket sides; and
a second bracket comprising a number of second-bracket sides coupled to the isolators, wherein the number of second-bracket sides is equal to the number of first-bracket sides and forms the closed polygonal shape, in plan view, and each one of the second-bracket sides comprises a first sidewall and a second sidewall,
wherein:
a portion of each one of the first-bracket sides is located between the first sidewall and the second sidewall of a corresponding one of the second-bracket sides; and
the isolators separate each one of the first-bracket sides from a corresponding one of the second-bracket sides to attenuate a load transferred from the first bracket to the second bracket.

2. The isolation coupler of claim 1 , wherein:
the first bracket further comprises a number of isolator openings, wherein each one of the isolator openings extends through one of the first-bracket sides; and
each one of the isolators is located in a corresponding one of the isolator openings, between the first sidewall and the second sidewall.

3. The isolation coupler of claim 2 , wherein:
each one of the isolators comprises an isolator body and a peripheral surface; and
the peripheral surface of each one of the isolators engages a perimeter surface of a corresponding one of the isolator openings.

4. The isolation coupler of claim 3 , wherein:
each one of the isolators further comprises a central opening extending through the isolator body; and
the second bracket further comprises:
a number of fastener openings, wherein each one of the fastener openings extends through the first sidewall and the second sidewall; and
a number of fasteners, wherein each one of the fasteners extends through a corresponding one of the fastener openings and the central opening of a corresponding one of the isolators.

5. The isolation coupler of claim 4 , wherein each one of the isolators further comprises:
a first side, wherein a portion of the first side of each one of the isolators is in contact with the first sidewall of one of the second-bracket sides; and
a second side opposite the first side, wherein a portion of the second side of each one of the isolators is in contact with the second sidewall of one of the second-bracket sides.

6. The isolation coupler of claim 5 , wherein each one of the isolators further comprises:
a first flange extending from the first side and surrounding the central opening, wherein the first flange of each one of the isolators is in contact with the first sidewall of one of the second-bracket sides; and
a second flange extending from the second side and surrounding the central opening, wherein the second flange of each one of the isolators is in contact with the second sidewall of one of the second-bracket sides.

7. The isolation coupler of claim 3 , wherein the isolator body of each one of the isolators comprises a plurality of isolator-body sections.

8. The isolation coupler of claim 3 , wherein each one of the isolators is annular.

9. The isolation coupler of claim 3 , wherein the isolator body is made of an elastomeric material.

10. The isolation coupler of claim 9 , wherein the elastomeric material comprises at least one of a silicone material, a rubber material, a fluoroelastomer material, and a polyurethane material.

11. The isolation coupler of claim 9 , wherein the elastomeric material has a Durometer hardness between thirty and ninety, a loss factor between ten percent and sixty percent, and an outgassing of less than six percent total mass.

12. The isolation coupler of claim 9 , wherein the elastomeric material has a Durometer hardness between thirty and fifty, a loss factor between twenty-five percent and sixty percent, and an outgassing of less than one percent total mass.

13. The isolation coupler of claim 1 , wherein each one of the isolators is one of a bearing or a bushing.

14. The isolation coupler of claim 1 , wherein:
the first bracket is configured to be coupled to one of the support structure or the functional element; and
the second bracket is configured to be coupled to the other one of the support structure or the functional element.

15. The isolation coupler of claim 14 , further comprising a number of struts, wherein each one of the struts is coupled to the second bracket and is configured to be coupled to the support structure.

16. The isolation coupler of claim 1 , wherein the number of isolators coupled to at least one of the first-bracket sides is different than the number of isolators coupled to at least another one of the first-bracket sides.

Assignees

• Boeing Co

Inventors

• Aston Richard W
• Langmack Michael John
• Tomzynska Anna M
• Herrmann Matthew
• Woods Emily C

Classifications

• B64G1/413

  Ion or plasma engines · CPC title

• B64G1/40

  Arrangements or adaptations of propulsion systems · CPC title

• B64C1/00

  Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like · CPC title

• B64G1/64

  Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements · CPC title

• F16F2234/02

  cylindrical · CPC title