Crushable spacer and bolted joint for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-11066958-B2
Application number	US-202016810186-A
Country	US
Kind code	B2
Filing date	Mar 5, 2020
Priority date	May 25, 2017
Publication date	Jul 20, 2021
Grant date	Jul 20, 2021

Abstract

A bolted joint apparatus includes: a first component including a first row of first bolt holes extending therethrough; a second component including a second row of second bolt holes extending therethrough wherein the second bolt holes are aligned coaxially with the first bolt holes, a plurality of fasteners, each of fasteners disposed through aligned pairs of the first and second bolt holes to couple together the first and second components, each of the fasteners including a shank; and crushable spacers disposed around the shanks of the fasteners, the crushable spacers clamped in compression between the fasteners and one of the components, wherein each of the crushable spacers has a tubular body interconnecting first and second enlarged ends, the tubular body being defined by a peripheral wall which incorporates at least one weakening feature.

First claim

What is claimed is:

1. A bolted joint apparatus, comprising:
a first component including a first row of first bolt holes extending therethrough;
a second component including a second row of second bolt holes extending therethrough, wherein the second bolt holes are aligned coaxially with the first bolt holes, a plurality of fasteners, each of the fasteners disposed through aligned pairs of the first and second bolt holes to couple together the first and second components, each of the fasteners including a shank; and
crushable spacers disposed around respective ones of the shanks of the fasteners, the crushable spacers clamped in compression between the fasteners and one of the components, wherein each of the crushable spacers has a tubular body including a central portion interconnecting first and second enlarged ends, the tubular body being defined by a peripheral wall that incorporates at least one weakening feature, the at least one weakening feature including a plurality of circular holes extending through the peripheral wall and a semicircular annular bulge located near a center of the peripheral wall.

2. The apparatus of claim 1 wherein the fasteners include bolts, each of the bolts including a bolt head, a thread, and a shank therebetween.

3. The apparatus of claim 2 further including a plurality of nuts, each of the nuts engaging the thread of one of the bolts.

4. The apparatus of claim 1 wherein the at least one weakening feature includes an hourglass shape of the peripheral wall.

5. The apparatus of claim 1 wherein the peripheral wall has a first diameter near a center of the peripheral wall and a second diameter near at least one of the first and second enlarged ends, wherein the first diameter is less than the second diameter.

6. The apparatus of claim 1 wherein the at least one weakening feature includes a discrete thin section in the peripheral wall.

7. The apparatus of claim 6 wherein the thin section is configured as an annular band.

8. The apparatus of claim 1 wherein the at least one weakening feature includes a discrete thin section in the peripheral wall having a first thickness which is less than a second thickness of the peripheral wall.

9. A gas turbine engine, comprising: turbomachinery components including a fan, a compressor, a combustor, and a turbine arranged in serial flow relationship and circumscribed about an engine centerline axis; and a supporting static structure circumscribing the turbomachinery components; wherein at least one of the turbomachinery components and the static structure include a bolted flange assembly, including:
a first component having a first flange including a first row of first bolt holes extending therethrough;
a second component having a second flange including a second row of second bolt holes extending therethrough, wherein the second bolt holes are aligned coaxially with the first bolt holes;
a plurality of fasteners, each of the fasteners disposed through aligned pairs of the first and second bolt holes to couple together the first and second flanges, each of the fasteners including a shank; and
crushable spacers disposed around respective ones of the shanks of the fasteners, the crushable spacers clamped in compression between the fasteners and one of the flanges, wherein each of the crushable spacers includes a tubular body extending axially between first and second enlarged ends, the tubular body being defined by a peripheral wall that incorporates at least one weakening feature, the at least one weakening feature including a plurality of circular holes passing through a thickness of the peripheral wall and a semicircular annular bulge located near a center of the peripheral wall.

10. The engine of claim 9 wherein the fasteners include bolts, each of the bolts including a bolt head, a thread, and a shank therebetween.

11. The engine of claim 10 further including a plurality of nuts, each of the nuts engaging the thread of one of the bolts.

12. The engine of claim 9 wherein the at least one weakening feature includes an hourglass shape of the peripheral wall.

13. The apparatus of claim 9 wherein the peripheral wall has a first diameter near a center of the peripheral wall and a second diameter near at least one of the first and second enlarged ends, wherein the first diameter is less than the second diameter.

14. The engine of claim 9 wherein the at least one weakening feature includes a discrete thin section in the peripheral wall.

15. The engine of claim 14 wherein the thin section is configured as an annular band.

16. The apparatus of claim 9 wherein the at least one weakening feature includes a discrete thin section in the peripheral wall having a first thickness which is less than a second thickness of the peripheral wall.

Assignees

• Gen Electric

Inventors

• Karafillis Apostolos Pavlos
• Jain Manoj Kumar
• Waldman Thomas Chadwick
• Prabhakar Nagamohan Govinahalli

Classifications

• F01D25/00

  Component parts, details, or accessories, not provided for in, or of interest apart from, other groups · CPC title

• F01D21/045

  special arrangements in stators or in rotors dealing with breaking-off of part of rotor · CPC title

• F02C7/00

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title

• F01D25/243 Primary

  Flange connections; Bolting arrangements (F01D25/265 takes precedence) · CPC title

• F05D2260/311

  of the frangible or shear type · CPC title