Thermally free hanger with length adjustment feature

Patent metadata

Field	Value
Publication number	US-9447700-B2
Application number	US-201414179739-A
Country	US
Kind code	B2
Filing date	Feb 13, 2014
Priority date	Feb 19, 2013
Publication date	Sep 20, 2016
Grant date	Sep 20, 2016

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 system for fastening first and second spaced components in a gas turbine engine, with the second spaced component arranged a desired distance from the first spaced component the system comprising:
a T-bar having a shaft portion and a crossbar portion, wherein the shaft portion of the T-bar passes through a first aperture in the first spaced component and the crossbar portion of the T-bar is arranged adjacent to the second spaced component;
a hanger nut configured to capture the shaft portion of the T-bar, wherein the hanger nut extends through the first spaced component;
a cap nut configured to attach the hanger nut and the shaft portion of the T-bar to the first spaced component; and
a bracket, wherein the bracket is coupled to the second spaced component and captures the crossbar portion of the T-bar 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.

2. The system of claim 1 , wherein the first spaced component and the second spaced component are separated by a distance determined by the dimensions of the T-bar.

3. The system of claim 1 , wherein the bracket is coupled with the second spaced component using a plurality of bolts.

4. The system of claim 1 , wherein the shaft of the T-bar is threaded.

5. The system of claim 4 , wherein the cap nut is configured to screw on to the threading.

6. The system of claim 1 , wherein the hanger nut includes at least one tab including a bolt passage.

7. The system of claim 6 , and further comprising a bolt passing through the bolt passage.

8. The system of claim 7 , and further comprising a duct insert arranged within the first spaced component for each bolt, each duct insert configured to capture the bolt.

9. The system of claim 1 , wherein the first spaced component is a structural component of a gas turbine engine, and the second spaced component is a liner of a gas turbine engine.

Assignees

• United Technologies Corp

Inventors

• Mcmahon Shawn M
• Lavin Jeffrey R

Classifications

• F16B5/0233

  allowing for adjustment perpendicular to the plane of the plates · CPC title

• Y10T29/4932

  Turbomachine making · CPC title

• F02K1/80

  Couplings or connections · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• F16B37/041

  Releasable devices (F16B37/044, F16B37/045 take precedence) · CPC title