Vibration-damping components, gas turbine engine and method of forming such components

Patent metadata

Field	Value
Publication number	US-10801329-B2
Application number	US-201715816698-A
Country	US
Kind code	B2
Filing date	Nov 17, 2017
Priority date	Nov 17, 2017
Publication date	Oct 13, 2020
Grant date	Oct 13, 2020

Abstract

A vibration-damping component, a gas turbine engine having the vibration-damping component and a method for forming such component are disclosed. The vibration-damping component comprises a body formed from an additive manufacturing material by an additive manufacturing process and defining a cavity within the body, and a vibration damper disposed within the cavity. The vibration damper comprises a damping element and a damping medium containing a viscoelastic material surrounding the damping element. The damping element has a relative motion when the component vibrates.

First claim

What is claimed is:

1. A vibration-damping component, comprising:
a body formed from an additive manufacturing material by an additive manufacturing process and defining a cavity within the body; and
a vibration damper disposed within the cavity and comprising:
a damping-material having a relative motion when the component vibrates; and
a damping medium containing a viscoelastic material surrounding the damping material,

wherein the body is formed of solidified portions of the additive manufacturing material, and
wherein the damping material is formed of unsolidified portions of the additive manufacturing material.

2. The vibration-damping component of claim 1 , wherein the additive manufacturing material comprises at least one of a metal powder, a thermoplastic powder, a photopolymer resin, a thermoset resin, and a thermoplastic resin.

3. The vibration-damping component of claim 1 , wherein the damping material comprises powders or particles suspended in the viscoelastic material.

4. The vibration-damping component of claim 3 , wherein the powders or particles have particle size in a range of 5-1000 microns.

5. The vibration-damping component of claim 1 , wherein the damping material is formed of unsolidified portions of the additive manufacturing material used to form the body of the component left inside the cavity during the additive manufacturing process.

6. The vibration-damping component of claim 3 , wherein the powders or particles are introduced into the cavity during the additive manufacturing process.

7. The vibration-damping component of claim 1 , wherein the viscoelastic material comprises epoxy resin or polyurethane.

8. A gas turbine engine comprising:
a combustor assembly including a plurality of fuel mixers;
a turbine assembly including a plurality of turbine blades; and
a compressor assembly including a plurality of fan blades,
wherein at least one of the fuel mixers, the turbine blades, and the fan blades comprises the component according to claim 1 .

9. A method of forming a vibration-damping component, comprising:
forming a body of the component from an additive manufacturing material by an additive manufacturing process;
forming a cavity within the body during the additive manufacturing process, the cavity having at least one through hole;
forming a damping material within the cavity during the additive manufacturing process, the damping material having a relative motion when the component vibrates;
injecting a damping medium containing a viscoelastic material into the cavity through the at least one through hole; and
closing the at least one through hole,
wherein the body is formed of solidified portions of the additive manufacturing material, and
wherein the damping material is formed of unsolidified portions of the additive manufacturing material.

10. The method of claim 9 , wherein the at least one through hole is closed by welding or brazing.

11. The method of claim 9 , wherein the at least one through hole is closed using epoxy.

12. The method of claim 9 , wherein forming the damping material comprises introducing powders or particles into the cavity.

13. The method of claim 9 , wherein forming the damping material comprises leaving the unsolidified portions of the additive manufacturing material used to form the body of the component in the cavity.

Assignees

• Gen Electric

Inventors

• Garay Gregory Terrence
• Capps Drew Michael
• Choi Yoon

Classifications

• F04D29/324 Primary

  Blades · CPC title

• F01D5/16 Primary

  for counteracting blade vibration · CPC title

• B22F10/12

  by photopolymerisation, e.g. stereolithography [SLA] or digital light processing [DLP] · CPC title

• B22F10/28

  Powder bed fusion, e.g. selective laser melting [SLM] or electron beam melting [EBM] · CPC title

• B33Y40/00

  Auxiliary operations or equipment, e.g. for material handling · CPC title