Methods and tooling assemblies for the manufacture of metallurgically-consolidated turbine engine components

• US 8,408,446 B1
• Filed: 02/13/2012
• Issued: 04/02/2013
• Est. Priority Date: 02/13/2012
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Smoke, Jason, Jan, David K., Mittendorf, Don
• Primary Examiner(s): STONER, KILEY SHAWN
• Application Number:
  US13/371,922
• Time in Patent Office: 414 Days
• Field of Search: None
• US Class Current: 228/193
• CPC Class Codes: B23K 1/0018 Brazing of turbine parts
• CPC Class Codes: B23K 20/021 Isostatic pressure welding
• CPC Class Codes: B23K 2101/001 Turbines
• CPC Class Codes: B23P 15/006 turbine wheels
• CPC Class Codes: F01D 5/3061 by welding, brazing
• CPC Class Codes: F05D 2230/236 Diffusion bonding
• CPC Class Codes: F05D 2230/237 Brazing
• CPC Class Codes: F05D 2300/175 Superalloys
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10T 29/4932 Turbomachine making

Abstract

Embodiments of a method for manufacturing a turbine engine component are provided, as are embodiments of a thermal growth constraint tool for the manufacture of turbine engine components. In one embodiment, the method includes the steps of obtaining a plurality of arched pieces, arranging the plurality of arched pieces in a ring formation, and bonding the plurality of arched pieces together to produce a monolithic ring by heating the ring formation to a predetermined bonding temperature while constraining the outward radial growth thereof.

Claims

1. A method for producing a turbine engine component, comprising:

obtaining a plurality of arched pieces;

arranging the plurality of arched pieces in a ring formation; and

bonding the plurality of arched pieces together to produce a monolithic ring by heating the ring formation to a predetermined bonding temperature while constraining the outward radial growth thereof, the step of bonding comprising;

positioning a thermal growth constraint ring around the ring formation; and

heating the ring formation to a predetermined bonding temperature at which the ring formation grows into the thermal growth constraint ring.

2. A method according to claim 1 wherein the thermal growth constraint ring has a coefficient of thermal expansion less than that of the ring formation.

3. A method according to claim 2 further comprising positioning a sacrificial crush ring between the ring formation and the thermal growth constraint ring prior to the step of heating.

4. A method according to claim 2 further comprising the step of disposing braze material between the plurality of arched pieces prior to the step of heating, and wherein the step of heating comprises heating the ring formation to a predetermined bonding temperature exceeding the melt point of the braze material.

5. A method according to claim 4 wherein the step of disposing comprises disposing at least one strip of braze foil between each pair of neighboring arched pieces prior to the step of heating.

6. A method according to claim 1 wherein the step of obtaining comprises obtaining a plurality of arched pieces, each comprising:

a shank; and

an airfoil extending radially from the shank.

7. A method according to claim 6 wherein the step of arranging comprises arranging the plurality of arched pieces in a ring formation such that each shank is positioned between two neighboring shanks and the airfoils are circumferentially-spaced about the ring formation.

8. A method according to claim 7 wherein the step of bonding comprising:

assembling a thermal growth constraint tool around the ring formation; and

bonding the plurality of arched pieces together to produce a monolithic airfoil ring by heating the ring formation to a predetermined bonding temperature at which the ring formation grows into the thermal growth constraint tool.

9. A method according to claim 8 wherein the thermal growth constraint tool comprises an annual void, and wherein the step of assembling comprises assembling the thermal growth constraint tool around the ring formation such that the airfoils extend into the annular void.

10. A method according to claim 5 wherein the step of bonding comprises:

inserting strips of braze foil between neighboring shanks prior to the step of bonding; and

bonding the plurality of airfoils together to produce a monolithic ring by heating the ring formation to a temperature exceeding the melt point of the strips of braze foil while constraining the outward radial growth thereof.

11. A method according to claim 10 wherein the step of obtaining comprises fabricating the plurality of arched pieces to each include a braze foil pocket formed in its shank, and wherein the step of inserting comprises inserting strips of braze foil between neighboring shanks and into the braze foil pockets prior to the step of bonding.

12. A method according to claim 11 wherein the step of fabricating comprises fabricating each braze foil pockets to have a depth less than the thickness of the sheets of braze foil.

13. A method according to claim 1 further comprising the steps of:

fitting a disk member within the monolithic ring;

sealing the interface between the disk member and the monolithic ring; and

subjecting the disk member and the monolithic ring to a hot isostatic press process after sealing to bond the disk member to the monolithic ring.

14. A method for manufacturing a turbine engine component, comprising:

producing a plurality of arched pieces, each comprising;

a shank; and

an airfoil extending radially from the shank; and

after producing the plurality of arched pieces to each include a shank and an airfoil extending radially therefrom, bonding the plurality of arched pieces together to form a monolithic airfoil ring, the step of bonding comprising;

arranging the plurality of arched pieces in a ring formation such that each shank is positioned between two neighboring shanks;

disposing a thermal growth constraint tool around the ring formation; and

heating the plurality of arched pieces to a predetermined temperature at which outward radial growth of the ring formation is impeded by the thermal growth constraint tool to urge the neighboring shanks together and promote the bonding thereof.

19. A method according to claim 14 further comprising the step of disposing braze material between neighboring shanks of the plurality of arched pieces prior to the step of heating, and wherein the step of heating comprises heating the ring formation to a predetermined bonding temperature exceeding the melt point of the braze material.

20. A method according to claim 19 further comprising forming a braze pocket in at least one of the shanks of the plurality of arched pieces, and wherein the step of disposing comprises positioning at least one strip of braze foil in the braze foil pocket prior to the step of heating.

15. A method for manufacturing a turbine engine component, comprising:

producing a plurality of arched pieces, each comprising;

a shank; and

an airfoil extending radially from the shank; and

bonding the plurality of arched pieces together to form a monolithic airfoil ring, the step of bonding comprising;

arranging the plurality of arched pieces in a ring formation such that each shank is positioned between two neighboring shanks;

disposing a thermal growth constraint tool around the ring formation; and

heating the plurality of arched pieces to a predetermined temperature at which outward radial growth of the ring formation is impeded by the thermal growth constraint tool to urge the neighboring shanks together and promote the bonding thereof;

wherein the thermal growth constraint tool comprises first and second thermal growth constraint rings each having a coefficient of thermal expansion less than that of the ring formation, and wherein the step of disposing comprises positioning the first and second thermal growth constraint rings around the ring formation.

16. A method according to claim 15 wherein the step of positioning comprises assembling the thermal growth constraint tool around the ring formation such that the first and second thermal growth constraint rings are axially spaced by at least one spacer member having a coefficient of thermal expansion less than that of the first and second thermal growth constraint rings.

17. A method according to claim 16 wherein each of the plurality of arced pieces comprises opposing axial shoulders, and wherein the step of arranging comprises arranging the plurality of arched pieces in a ring formation having first and second annular tooling contact surfaces generally defined by the opposing axial shoulders of the plurality of arched pieces.

18. A method according to claim 17 wherein the step of disposing a thermal comprises assembling the thermal growth constraint tool around the ring formation such that the first and second thermal growth constraint rings extend around the first and second annular tooling contact surfaces, respectively.