Compensating for thermal expansion via controlled tube buckling

Patent metadata

Field	Value
Publication number	US-10001280-B2
Application number	US-201715452345-A
Country	US
Kind code	B2
Filing date	Mar 7, 2017
Priority date	Jan 3, 2014
Publication date	Jun 19, 2018
Grant date	Jun 19, 2018

Abstract

One embodiment includes a fuel injector for a gas turbine engine. The fuel injector has an inlet fitting for receiving fuel. The fuel injector also has an outlet fitting for delivering fuel through a nozzle to a combustor of the gas turbine engine. An injector support extends between the inlet fitting and the outlet fitting and has an internal bore therethrough. A fuel tube extends from the inlet fitting through the internal bore of the injector support to the outlet fitting. The injector support has a greater coefficient of thermal expansion than the fuel tube. At room temperature the fuel tube is under compressive stress such that the fuel tube is buckled. As a result of differential thermal expansion of the fuel tube and the injector support during engine operation the fuel tube is relieved of compressive stress.

First claim

The invention claimed is:

1. A method to allow for thermal expansion of a fuel injector during engine operation without causing a failure in a fuel circuit, the method comprising:
fixing a first end of a first fuel tube which extends from an inlet fitting through an internal bore of an injector support to an outlet fitting at one of the inlet fitting or the outlet fitting, such that the first fuel tube is constrained at the first end and free to slide in a joint at a second end, and wherein the injector support has a greater coefficient of thermal expansion than the first fuel tube;
heating the fuel injector to an elevated temperature to cause differential thermal expansion such that the injector support expands more than the first fuel tube;
fixing the second end of the first fuel tube at the other of the inlet fitting and the outlet fitting while the fuel injector is at the elevated temperature; and
cooling the fuel injector to room temperature such that the injector support contracts more than the first fuel tube putting compressive stress on the first fuel tube and causing the first fuel tube to be buckled at room temperature.

2. The method of claim 1 , wherein the heating and fixing are performed during a braze cycle.

3. The method of claim 1 , wherein the first fuel tube has a slenderness ratio of 90 or greater.

4. The method of claim 1 , wherein the injector support is made of 300 series stainless steel.

5. The method of claim 4 , wherein the first fuel tube is made of 400 series stainless steel.

6. The method of claim 4 , wherein the first fuel tube is made of Inconel 625 or Hastelloy X.

7. The method of claim 1 and further comprising:
fixing a first end of a second fuel tube which extends from the inlet fitting through an internal bore of an injector support to the outlet fitting at one of the inlet fitting or the outlet fitting, such that the second fuel tube is constrained at the first end and free to slide in a joint at a second end, and wherein the injector support has a greater coefficient of thermal expansion than the second fuel tube;
heating the fuel injector to an elevated temperature to cause differential thermal expansion such that the injector support expands more than the second fuel tube;
fixing the second end of the second fuel tube at the other of the inlet fitting and the outlet fitting while the fuel injector is at the elevated temperature; and
cooling the fuel injector to room temperature such that the injector support contracts more than the second fuel tube putting compressive stress on the second fuel tube and causing the second fuel tube to be buckled at room temperature.

8. The method of claim 7 , wherein the second fuel tube extends parallel to the first fuel tube and is positioned adjacent to the first fuel tube.

9. The method of claim 7 , wherein the second fuel tube has a slenderness ratio of 90 or greater.

10. The method of claim 7 , wherein the injector support is made of 300 series stainless steel.

11. The method of claim 10 , wherein the second fuel tube is made of 400 series stainless steel.

12. The method of claim 10 , wherein the second fuel tube is made of Inconel 625 or Hastelloy X.

Assignees

• Delavan Inc

Inventors

• Caples Mark

Classifications

• F23R2900/00005

  Preventing fatigue failures or reducing mechanical stress in gas turbine components · CPC title

• Y10T29/49865

  by temperature differential [e.g., shrink fit] · CPC title

• Y10T29/49945

  by driven force fit · CPC title

• F23R3/283 Primary

  Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances · CPC title