Processes and tooling associated with diffusion bonding

Patent metadata

Field	Value
Publication number	US-11346362-B2
Application number	US-201715658786-A
Country	US
Kind code	B2
Filing date	Jul 25, 2017
Priority date	Jul 25, 2017
Publication date	May 31, 2022
Grant date	May 31, 2022

Abstract

A fixture assembly including a first fixture portion; a second fixture portion that interfaces with the first fixture portion; and a bladder assembly mounted to the second fixture portion to face the first fixture portion. A method of manufacturing a fan blade includes inserting a blade body and a cover into a fixture; and deploying a bladder assembly within the fixture to press the cover into the blade body.

First claim

What is claimed is:

1. A fixture assembly, comprising:
a first fixture portion shaped to an exterior airfoil contour to receive a blade body that comprises a blade leading edge and a blade trailing edge;
a second fixture portion that interfaces with the first fixture portion; and
a bladder assembly mounted to the second fixture portion and directed toward the first fixture portion, wherein the bladder assembly includes a face sheet with a bellows around a periphery of the face sheet, the face sheet shaped to the exterior airfoil contour of a cover for the blade body, deployment of the bladder assembly serves to move the face sheet toward the first fixture portion and press the cover toward the blade body.

2. The assembly as recited in claim 1 , wherein the blade body is manufactured of titanium.

3. The assembly as recited in claim 1 , wherein the cover is manufactured of titanium.

4. The assembly as recited in claim 1 , wherein the bellows comprises an “S” shape in cross-section.

5. The assembly as recited in claim 4 , wherein the bellows is machined about the periphery of the face sheet.

6. The assembly as recited in claim 1 , wherein the bellows is integral with the periphery of the face sheet, the bellows forming a convolute.

7. The assembly as recited in claim 1 , further comprising a retainer to retain the bellows.

8. The assembly as recited in claim 7 , further comprising a seal that interfaces with an extension from the bellows.

9. The assembly as recited in claim 4 , further comprising a retainer to retain the bellows.

10. The assembly as recited in claim 1 , wherein the face sheet is pillowed.

11. The assembly as recited in claim 1 , wherein the face sheet includes a multiple of flats and spans therebetween, each of the multiple of flats correspond with a location of a rib in the blade body to press the cover against the rib, the spans are of an arcuate shape displaced from the cover.

12. The assembly as recited in claim 1 , wherein the second fixture portion includes a surface that follows a contour of the face sheet.

13. A method of manufacturing a fan blade, comprising:
inserting a blade body and a cover into a first fixture portion and a second fixture portion; and
deploying a bladder assembly within the second fixture portion directed toward the first fixture portion to press the cover into the blade body, where the bladder assembly includes a face sheet with a bellows around a periphery of the face sheet, the face sheet shaped to an exterior contour of the cover of the blade body, wherein deploying the bladder assembly includes pressing the face sheet into the cover only in areas adjacent to ribs in the blade body.

14. The method as recited in claim 13 , further comprising manufacturing the blade body and the cover from titanium.

15. The method as recited in claim 13 , wherein deploying the bladder assembly includes pressurizing the bellows assembly.

16. The assembly as recited in claim 1 , wherein a tolerance of the face sheet is in tens of thousandths of an inch to the exterior airfoil contour of a cover for the blade body.

17. The assembly as recited in claim 1 , wherein the bellows provides 100 thousandths of an inch (2.5 mm) of movement nominally to provide a uniform pressure to the cover.

18. The assembly as recited in claim 1 , wherein the bellows are retained by a retainer that is received within a respective recess in the second fixture portion.

19. The assembly as recited in claim 18 , wherein the retainer sandwiches an extension from the bellows.

20. The assembly as recited in claim 18 , wherein the retainer is integral with the bellows.

21. The assembly as recited in claim 1 , wherein the cover at least partially forms a concave pressure side of a fan blade.

22. The assembly as recited in claim 21 , wherein the face sheet is shaped with an approximate twist of from about +30 degrees to about −30 degrees.

23. A fixture assembly for a fan blade of a gas turbine engine, comprising:
a first fixture portion shaped to an exterior airfoil contour of a fan blade body, the fan blade body forms a convex suction side of a fan blade and a fan blade leading edge and a fan blade trailing edge;
a second fixture portion that interfaces with the first fixture portion; and
a bladder assembly mounted to the second fixture portion and directed toward the first fixture portion, wherein the bladder assembly includes a face sheet with a bellows around a periphery of the face sheet, the face sheet shaped to an exterior airfoil contour of a cover for the fan blade body, deployment of the bladder assembly serves to move the face sheet toward the first fixture portion and press the cover at least partially into the fan blade body.

24. The assembly as recited in claim 23 , wherein the cover partially forms a concave pressure side of the fan blade.

25. The assembly as recited in claim 23 , wherein the bellows is integral with a periphery of the face sheet, the bellows forming a convolute, a seal seals the bellows to the second fixture portion to form a pressurized space, pressurization of the pressurized space operable to move the face sheet.

26. The assembly as recited in claim 25 , further comprising a source of inert gas to selectively communicate inert gas to the pressurized space through a passage network within the second fixture portion.

27. The assembly as recited in claim 23 , wherein the face sheet and the bellows are nominally 60 thousandths of an inch (1.5 mm) in thickness.

28. The assembly as recited in claim 25 , wherein the face sheet is shaped with an approximate twist of from about +30 degrees to about −30 degrees.

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Bales Daniel A
• Demichael Thomas

Classifications

• F04D29/324

  Blades · CPC title

• F05D2230/23

  by permanently joining parts together · CPC title

• F05D2300/133

  Titanium · CPC title

• F05D2230/68

  using auxiliary equipment for lifting or holding · CPC title

• F01D25/285

  Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures · CPC title