Variable stator vane and method of fabricating variable stator vane

Patent metadata

Field	Value
Publication number	US-11448086-B2
Application number	US-202117169871-A
Country	US
Kind code	B2
Filing date	Feb 8, 2021
Priority date	Feb 14, 2020
Publication date	Sep 20, 2022
Grant date	Sep 20, 2022

Abstract

The present disclosure relates to a variable stator vane and a method of fabricating the variable stator vane of a gas turbine engine. The method includes providing at least one fibre sheet. The method further includes rolling the at least one fibre sheet around a mandrel to form a spindle section of the variable stator vane. An excess of material of the at least one fibre sheet remains after forming the spindle section. The method further includes using the excess of material of the at least one fibre sheet to form the at least one aerofoil section of the variable stator vane.

First claim

The invention claimed is:

1. A method of fabricating a variable stator vane, the method comprising:
providing at least one fibre sheet;
rolling the at least one fibre sheet around a mandrel to form a spindle section of the variable stator vane, the spindle section having a spindle axis, wherein an excess of material of the at least one fibre sheet remains after forming the spindle section and a first portion of the at least one fibre sheet extends further in a direction along the spindle axis than a second portion of the at least one fibre sheet to form a projection in the spindle section; and
using the excess of material of the at least one fibre sheet to form at least one aerofoil section of the variable stator vane.

2. The method of claim 1 , wherein rolling the at least one fibre sheet around the mandrel comprises rolling a plurality of turns of the at least one fibre sheet around the mandrel.

3. The method of claim 1 , further comprising wrapping the excess of material of the at least one fibre sheet around one or more inserts.

4. The method of claim 1 , wherein rolling the at least one fibre sheet around the mandrel comprises rolling a turn of the at least one fibre sheet around an insert so that the insert is disposed between two adjacent turns of the spindle section.

5. The method of claim 1 , further comprising providing a further fibre sheet over the spindle section and the at least one aerofoil section to provide an outer layer of the variable stator vane.

6. The method of claim 1 , wherein using the excess of material further comprises pressing the excess of material of the at least one fibre sheet between a female aerofoil tool and a male aerofoil tool.

7. The method of claim 1 , wherein the at least one fibre sheet comprises a first fibre sheet and a second fibre sheet, wherein rolling the at least one fibre sheet further comprises rolling the first fibre sheet and the second fibre sheet around the mandrel to form the spindle section, and wherein a first excess of material from the first fibre sheet remains after forming the spindle section and a second excess of material from the second fibre sheet remains after forming the spindle section.

8. The method of claim 7 , wherein the at least one aerofoil section comprises a first aerofoil section and a second aerofoil section, and wherein using the excess of material comprises using the first excess of material to form the first aerofoil section and using the second excess of material to form the second aerofoil section.

9. A variable stator vane configured for rotation about a rotation axis, the variable stator vane comprising:
a spindle section formed from a first portion of an at least one continuous fibre sheet wrapped around a spindle axis of the variable stator vane; and
at least one aerofoil section at least partially formed from an excess of material from a second portion of the at least one continuous fibre sheet,
wherein the first portion of the at least one continuous fibre sheet extends further in a direction along the spindle axis then the second portion of the at least one continuous fibre sheet to form a projection in the spindle section.

10. The variable stator vane of claim 9 , wherein the spindle section comprises a plurality of turns of the at least one continuous fibre sheet wrapped around the spindle axis.

11. The variable stator vane of claim 9 , further comprising at least one insert.

12. The variable stator vane of claim 9 , further comprising an outer layer of fibre sheet disposed over the spindle section and the at least one aerofoil section.

13. The variable stator vane of claim 9 , wherein the spindle section further comprises a mandrel, and wherein the at least one continuous fibre sheet is disposed around the mandrel.

14. The variable stator vane of claim 9 , wherein the at least one continuous fibre sheet comprises a first continuous fibre sheet and a second continuous fibre sheet, and wherein the spindle section is formed from the first continuous fibre sheet and the second continuous fibre sheet rolled around the spindle axis.

15. The variable stator vane of claim 14 , wherein the at least one aerofoil section comprises a first aerofoil section and a second aerofoil section, wherein the first aerofoil section is at least partially formed from an excess of material from the first continuous fibre sheet, and wherein second aerofoil section is at least partially formed from an excess of material from the second continuous fibre sheet.

16. The variable stator vane of claim 9 , further comprising at least one insert disposed within the aerofoil section, wherein the at least one insert has a triangular cross section.

17. The variable stator vane of claim 9 , wherein the second portion of the at least one continuous fibre sheet is trapezoidal in shape.

18. The variable stator vane of claim 9 , further comprising a plurality of inserts disposed within the aerofoil section.

19. The variable stator vane of claim 9 , wherein the at least one continuous fibre sheet is impregnated with a polymeric material.

20. The variable stator vane of claim 9 , wherein the spindle axis and the rotation axis are colinear.

Assignees

• Rolls Royce Plc

Inventors

• Jones Christopher D
• Backhouse Robert C
• Bishop Adam J

Classifications

• B29C70/86

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• F01D11/005

  Sealing means between non relatively rotating elements · CPC title

• B29L2031/08

  Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers · CPC title

• F05D2300/601

  Fabrics · CPC title

• F01D5/282

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title