Thermally free hanger with length adjustment feature

Patent metadata

Field	Value
Publication number	US-9719376-B2
Application number	US-201615240459-A
Country	US
Kind code	B2
Filing date	Aug 18, 2016
Priority date	Feb 19, 2013
Publication date	Aug 1, 2017
Grant date	Aug 1, 2017

Abstract

A system for connecting spaced components of a gas turbine engine includes connecting one end of a T-bar to each of the spaced components. One component is attached to the crossbar portion of the T-bar by trapping the crossbar between the component and a bracket. The second component is attached to the shaft portion using a hanger nut connected to the shaft portion of the T-bar and bolted to the second component. The system may be installed by attaching the crossbar portion, then advancing the first component towards the second component until the shaft portion passes through an aperture in the second component. The hanger nut is attached to the shaft portion and the second component.

First claim

The invention claimed is:

1. A method for connecting components in a gas turbine engine, the method comprising:
arranging a T-bar having a shaft and a crossbar portion such that:
the shaft portion protrudes through an aperture in a first spaced component; and
the crossbar portion is adjacent to a second spaced component;

attaching a bracket to the second spaced component to capture the crossbar portion between the second spaced component and the bracket;
arranging a hanger nut adjacent to the T-bar and the first spaced component, the hanger nut having an aperture, such that the aperture is adjacent to a bolt hole in the first spaced component;
attaching the hanger nut to the first spaced component by inserting a bolt through the aperture and the bolt hole; and
attaching a cap nut to a threaded portion of the shaft portion of the T-bar.

2. The method of claim 1 , wherein attaching the bracket to the second spaced component includes welding the bracket to the second spaced component with sufficient head space to permit limited movement of the crossbar portion.

3. The method of claim 1 , wherein attaching the bracket to the second spaced component includes riveting the bracket to the second spaced component with sufficient head space to permit limited movement of the crossbar portion.

4. The method of claim 1 , wherein:
the hanger nut has a quantity of apertures;
the first spaced component has the quantity of bolt holes; and
each aperture is arranged adjacent to a bolt hole.

5. The method of claim 1 , wherein arranging the hanger nut adjacent to the T-bar and the first space component further comprises:
arranging the hanger nut such that the hanger nut extends through the first spaced component.

6. The method of claim 5 , wherein attaching the bracket to the second spaced component includes welding the bracket to the second spaced component with space between the bracket and the T-bar to permit movement of the crossbar portion with respect to the bracket and the second spaced component.

7. The method of claim 5 , wherein attaching the bracket to the second spaced component includes riveting the bracket to the second spaced component with space between the bracket and the T-bar to permit movement of the crossbar portion with respect to the bracket and the second spaced component.

8. The method of claim 5 , wherein:
the hanger nut has a quantity of apertures;
the first spaced component has a quantity of bolt holes; and
each aperture is arranged adjacent to a bolt hole.

9. A method of installing a liner in a gas turbine engine, the method comprising:
inserting a crossbar portion of a T-bar between a liner and a bracket to substantially encapsulate the crossbar portion between the liner and the bracket, the T-bar including the crossbar portion and an integrally formed shaft portion transecting the crossbar portion at a midsection;
affixing the bracket to the liner;
advancing the liner towards a structural component, the structural component having an aperture, such that a shaft portion of the T-bar passes through the aperture;
inserting a hanger nut into the aperture, such that the hanger nut circumscribes the shaft portion of the T-bar and is connected to the T-bar by a threaded connection; and
bolting the hanger nut to the structural component.

10. The method of claim 9 , and further comprising inserting a duct insert in a bolt hole in the structural component.

11. The method of claim 10 , and further comprising passing a bolt through the duct insert and the hanger nut to connect the structural component to the hanger nut.

12. The method of claim 11 , wherein a plurality of bolts connect the structural component to the hanger nut.

13. The method of claim 9 , and further comprising attaching a cap nut to a threaded portion of the shaft portion of the T-bar, such threaded portion extending through the aperture in the structural component.

14. The method of claim 9 , wherein affixing the bracket to the liner includes capturing the crossbar portion of the T-bar between the bracket and the liner, with sufficient head space to permit limited movement of the crossbar portion.

15. The method of claim 9 , wherein inserting the hanger nut into the aperture further comprises inserting the hanger nut so that the hanger nut extends through the structural component.

16. The method of claim 15 , and further comprising inserting a duct insert in a bolt hole in the structural component.

17. The method of claim 16 , and further comprising passing a bolt through the duct insert and the hanger nut to connect the structural component to the hanger nut.

18. The method of claim 17 , wherein a plurality of bolts connect the structural component to the hanger nut.

19. The method of claim 15 , and further comprising attaching a cap nut to a threaded portion of the shaft portion of the T-bar, such threaded portion extending through the first aperture in the structural component.

20. The method of claim 15 , wherein affixing the bracket to the liner includes capturing the crossbar portion of the T-bar between the bracket and the liner, with space between the bracket and the T-bar to permit movement of the crossbar portion with respect to the bracket and the second spaced component.

Assignees

• United Technologies Corp

Inventors

• Mcmahon Shawn M
• Lavin Jeffrey R

Classifications

• F05D2230/60

  Assembly methods · CPC title

• F23R3/002

  Wall structures (F23R3/02 and F23R3/007 take precedence) · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F01D25/28 Primary

  Supporting or mounting arrangements, e.g. for turbine casing · CPC title

• F05D2240/35

  Combustors or associated equipment · CPC title