Barrel nut with stress reduction features

Patent metadata

Field	Value
Publication number	US-10520002-B2
Application number	US-201715671513-A
Country	US
Kind code	B2
Filing date	Aug 8, 2017
Priority date	Aug 27, 2014
Publication date	Dec 31, 2019
Grant date	Dec 31, 2019

Abstract

A barrel nut with features for reducing tensile stresses under heavy load within the barrel nut has a partial-cylindrical body having a first planar end surface and a second planar end surface. A threaded bore extends through the partial-cylindrical body with a central axis substantially parallel to the first planar end surface and the second planar end surface. At least one groove is formed in each of the first planar end surface and the second planar end surface, the groove having a rounded surface extending at least a part of a distance between a curved upper surface of the partial-cylindrical body to a bottom surface thereof in a direction substantially parallel to the central axis of the threaded bore.

First claim

The invention claimed is:

1. A method of reducing stress in a barrel nut comprising:
forming a one-piece partial-cylindrical body having a first planar end surface and a second planar end surface;
forming a threaded bore through the partial-cylindrical body with a central axis substantially parallel to the first planar end surface and the second planar end surface; and
forming at least one groove recessed into each of the first planar end surface and the second planar end surface extending at least a part of a length of the partial-cylindrical body in a direction substantially parallel to the central axis of the threaded bore.

2. The method of claim 1 , further comprising forming the at least one recessed groove to have a rounded surface.

3. The method of claim 2 , wherein the rounded surface has a radius in the range of about 0.015 to 0.15 times a diameter of the barrel nut.

4. The method of claim 1 , further comprising aligning the at least one recessed groove in each of the first planar end surface and the second planar end surface with the central axis of the threaded bore such that the at least one recessed groove is positioned on a center line in each of the first planar end surface and the second planar end surface.

5. The method of claim 1 , further comprising forming two grooves in each of the first planar end surface and the second planar end surface to extend in a direction substantially parallel to the central axis from a curved upper surface to a bottom surface of the partial-cylindrical body.

6. The method of claim 5 , further comprising positioning the two grooves equidistant from a center line of each of the first planar end surface and the second planar end surface, the center line being aligned with the central axis.

7. The method of claim 6 , wherein a distance between a center line of each of the two grooves is in a range of about 0.25 to 0.5 times a diameter of the barrel nut.

8. The method of claim 1 , further comprising forming in a bottom surface of the partial-cylindrical body a flange surrounding the threaded bore, the flange being raised above the bottom surface and extending from a circumferential edge of the threaded bore to a side edge of the bottom surface.

9. The method of claim 8 , wherein the flange at the side edge extends a curved upper surface of the partial-cylindrical body below the bottom surface in a central area, the central area having a length substantially equal to a diameter of the threaded bore.

10. A method of mounting an aircraft engine to an aircraft, comprising the steps of:
inserting a barrel nut into a cylindrical bore extending through an aircraft engine mount, the barrel nut comprising a one-piece partial-cylindrical body having a first planar end surface and a second planar end surface, a threaded bore extending through the partial-cylindrical body and at least one groove recessed into each of the first planar end surface and the second planar end surface extending at least a part of a distance between a curved upper surface of the partial-cylindrical body and a bottom surface of the partial-cylindrical body in a direction substantially parallel to a central axis of the threaded bore;
aligning the barrel nut within the cylindrical bore with bolt holes positioned through a top surface of the aircraft engine mount;
inserting bolts through the bolt holes and into the threaded bore in the barrel nut; and
tightening the bolts.

11. A method of reducing stress in a barrel nut comprising:
forming a partial-cylindrical body having a first planar end surface and a second planar end surface;
forming a threaded bore through the partial-cylindrical body with a central axis substantially parallel to the first planar end surface and the second planar end surface;
forming at least one groove recessed into each of the first planar end surface and the second planar end surface extending at least a part of a length of the partial-cylindrical body in a direction substantially parallel to the central axis of the threaded bore; and
forming in a bottom surface of the partial-cylindrical body a flange surrounding the threaded bore, the flange being raised above the bottom surface and extending from a circumferential edge of the threaded bore to a side edge of the bottom surface.

12. The method of claim 11 , wherein the flange at the side edge extends a curved upper surface of the partial-cylindrical body below the bottom surface in a central area, the central area having a length substantially equal to a diameter of the threaded bore.

13. The method of claim 11 , further comprising forming the at least one groove to have a rounded surface recessed into each of the first planar end surface and the second planar end surface.

14. The method of claim 13 , wherein the rounded surface has a radius in a range of about 0.015 to 0.15 times a diameter of the barrel nut.

15. The method of claim 11 , further comprising aligning the at least one groove in each of the first planar end surface and the second planar end surface with the central axis of the threaded bore such that the at least one groove is positioned on a center line in each of the first planar end surface and the second planar end surface.

16. The method of claim 11 , further comprising forming two grooves in each of the first planar end surface and the second planar end surface to extend in a direction substantially parallel to the central axis from a curved upper surface to the bottom surface of the partial-cylindrical body.

17. The method of claim 16 , further comprising positioning the two grooves equidistant from a center line of each of the first planar end surface and the second planar end surface, the center line being aligned with the central axis.

18. The method of claim 16 , wherein a distance between a center line of each of the two grooves is in a range of about 0.25 to 0.5 times a diameter of the barrel nut.

19. The method of claim 11 , further comprising forming the flange with a thickness between about 0.05 to about 0.10 times a diameter of the barrel nut.

20. The method of claim 11 , further comprising forming the threaded bore with a plurality of threads having a total length extending from the bottom surface to a point below a curved upper surface of the partial-cylindrical body.

Assignees

• Boeing Co

Inventors

• Stanescu Adrian
• Kostakis Constantine
• Butcher Michael Ronald

Classifications

• F16B31/06 Primary

  having regard to possibility of fatigue rupture · CPC title

• B23G9/006 Primary

  Slotting nuts · CPC title

• F16B37/047

  Barrel nuts · CPC title

• F16B37/04

  Devices for fastening nuts to surfaces, e.g. sheets, plates {(nuts fastened behind a wall by a toggle-mechanism F16B13/0808; threaded inserts F16B37/122; measures against loss of bolts, nuts or pins F16B41/002)} · CPC title