Processes and tooling associated with diffusion bonding the periphery of a cavity-back airfoil

Patent metadata

Field	Value
Publication number	US-11602809-B2
Application number	US-202117169893-A
Country	US
Kind code	B2
Filing date	Feb 8, 2021
Priority date	Jul 2, 2018
Publication date	Mar 14, 2023
Grant date	Mar 14, 2023

Abstract

A fixture assembly includes a first fixture portion, a second fixture portion that interfaces with the first fixture portion, and a sub-fixture movably mounted to the first fixture portion. A multiple of actuators selectively move the sub-fixture toward the second fixture portion. A method of manufacturing a fan blade includes deploying the sub-fixture from the first fixture portion to effectuate a peripheral diffusion bond to join the blade body and the cover of the fan blade.

First claim

What is claimed is:

1. A method of manufacturing a fan blade for a gas turbine engine, comprising:
moving a first fixture portion, shaped to an airfoil contour to receive a blade body, toward a second fixture portion shaped to the airfoil contour to support a cover with respect to the blade body, wherein the cover has an edge that overlaps the body to define a periphery wherein the edge of the cover overlaps the body, wherein the first fixture portion comprises a multiple of sub-fixture elements defining a perimeter corresponding to the periphery;
heating the multiple of sub-fixture elements; and
deploying the multiple of sub-fixture elements from the first fixture portion to effectuate a peripheral diffusion bond at the periphery to join the blade body and the cover of the fan blade at the periphery.

2. The method as recited in claim 1 , wherein moving the first fixture portion toward the second fixture portion comprises movement of 8-12 inches (203-304 mm).

3. The method as recited in claim 1 , wherein deploying the multiple of sub-fixture elements from the first fixture portion comprises movement of 0.040-0.200 inches (1-51 mm).

4. The method as recited in claim 1 , wherein deploying the multiple of sub-fixture elements from the first fixture portion comprises pressurizing a multiple of actuators.

5. The method as recited in claim 4 , wherein each sub-fixture element contains a heating element, and wherein heating the multiple of sub-fixture elements comprises heating the heating element within each sub-fixture element.

6. The method as recited in claim 5 , further comprising measuring a temperature at each sub-fixture element.

7. The method as recited in claim 4 , further comprising measuring a pressure at each of the multiple of actuators.

8. The method as recited in claim 1 , further comprising heating the second fixture portion.

9. The method as recited in claim 1 , wherein the deploying step comprises actuating a bellows located between the first fixture portion and the multiple of sub-fixture elements.

10. The method as recited in claim 1 , wherein the deploying step comprises individually controlling each sub-fixture element to adjust peripheral diffusion bond for the cover in response to a temperature and a pressure at each sub-fixture element, wherein the individually controlling step produces at least one different pressure at different sub-fixture elements.

11. The method as recited in claim 4 , wherein the multiple of actuators are associated with the multiple of sub-fixture elements.

12. The method as recited in claim 1 , wherein the body defines a root, a blade tip and one of a suction or pressure side of the fan blade.

13. The method of claim 1 , wherein the periphery is defined parallel to each of a root, a blade tip and sides defining a suction or pressure side of the fan blade.

14. The method of claim 13 , wherein the deploying step deploys the multiple of sub-fixture elements from the first fixture portion to effectuate a peripheral diffusion bond between the cover and the body along the periphery parallel to each of the root and the blade tip and along the sides defining the suction or pressure side of the fan blade.

Assignees

• Raytheon Tech Corp

Inventors

• Bales Daniel A
• Demichael Thomas

Classifications

• B23K2103/14

  Titanium or alloys thereof · CPC title

• B23K1/19

  taking account of the properties of the materials to be soldered · CPC title

• B23K20/16

  with interposition of special material to facilitate connection of the parts, e.g. material for absorbing or producing gas · CPC title

• B23K3/087

  Soldering or brazing jigs, fixtures or clamping means · CPC title

• B23K2101/001

  Turbines · CPC title