Methods and apparatus to provide damping of an airfoil

Patent metadata

Field	Value
Publication number	US-11814973-B2
Application number	US-202217568555-A
Country	US
Kind code	B2
Filing date	Jan 4, 2022
Priority date	Jan 4, 2022
Publication date	Nov 14, 2023
Grant date	Nov 14, 2023

Abstract

Methods, apparatus, systems, and articles of manufacture to provide damping of an airfoil are disclosed. An example airfoil is disposed in a flow path, the airfoil including a shell defining an exterior surface of the airfoil and forming a cavity in an interior surface of the airfoil, and a lattice damper disposed in the cavity, the lattice damper to reduce vibrational loads exerted on the airfoil.

First claim

What is claimed is:

1. An airfoil comprising:
a shell defining an exterior surface of the airfoil and forming a cavity in an interior surface of the airfoil;
a lattice damper disposed in the cavity, the lattice damper to reduce vibrational loads exerted on the airfoil, the lattice damper including a plurality of unit cells, the plurality of unit cells being cross-cube shaped and hollow with a single continuous surface;
an inlet opening extending through a wall of the shell proximate a leading edge of the airfoil;
an outlet opening extending through the wall of the shell proximate a trailing edge of the airfoil; and
a plurality of channels defined in the lattice damper to fluidly couple the inlet opening to the outlet opening, the inlet opening to receive heated fluid to flow from the leading edge to the trailing edge via the plurality of channels.

2. The airfoil of claim 1 , wherein the lattice damper includes a foam material.

3. The airfoil of claim 1 , wherein the inlet opening is fluidly coupled to a high-temperature region, the inlet opening to receive the heated fluid from the high-temperature region.

4. The airfoil of claim 1 , wherein the inlet opening and the outlet opening are positioned at a same cross-section of the airfoil.

5. The airfoil of claim 1 , wherein the inlet opening and the outlet opening are positioned at a same radial distance from a core engine.

6. The airfoil of claim 1 , wherein the lattice damper includes polyether ether ketone.

7. A gas turbine comprising:
a core cowl;
a fan cowl circumscribing the core cowl; and
a shell defining an exterior surface of the outlet guide vane and forming a cavity in an interior surface of the outlet guide vane;
a lattice damper disposed in the cavity, the lattice damper to reduce vibrational loads exerted on the outlet guide vane, the lattice damper including a plurality of unit cells, the plurality of unit cells being cross-cube shaped and hollow with a single continuous surface;
an inlet opening extending through a wall of the shell proximate a leading edge of the outlet guide vane;
an outlet opening extending through the wall of the shell proximate a trailing edge of the outlet guide vane; and
a plurality of channels defined in the lattice damper to fluidly couple the inlet opening to the outlet opening, the inlet opening to receive heated fluid to flow from the leading edge to the trailing edge via the plurality of channels.

8. The gas turbine of claim 7 , wherein the lattice damper includes a foam material.

9. The gas turbine of claim 7 , further including a high-temperature region fluidly coupled to the inlet opening, the inlet opening to receive the heated fluid from the high-temperature region, the heated fluid to flow from the inlet opening to the outlet opening via the plurality of channels.

10. The gas turbine of claim 7 , wherein the outlet guide vane is a first outlet guide vane, further including a second outlet guide vane coupled between the core cowl and the fan cowl, the first outlet guide vane positioned at a top of the core cowl, the second outlet guide vane spaced apart from the first outlet guide vane in a circumferential direction of the core cowl.

11. The gas turbine of claim 10 , wherein the first outlet guide vane includes titanium and the second outlet guide vane includes aluminum.

12. An apparatus comprising:
a shell means defining an exterior surface of an outlet guide vane and forming a cavity in an interior surface of the outlet guide vane;
a damping means disposed in the cavity, the damping means to reduce vibrational loads exerted on the outlet guide vane,
a fluid inlet means extending through a wall of the shell means proximate a leading edge of the outlet guide vane;
a fluid outlet means extending through the wall of the shell means proximate a trailing edge of the outlet guide vane; and
a fluid flow means defined in the damping means to fluidly couple the fluid inlet means to the fluid outlet means, the fluid inlet means to receive heated fluid to flow from the leading edge to the trailing edge via the fluid flow means.

13. The apparatus of claim 12 , wherein a unit cell of the damping means is cross-cube shaped.

Assignees

• Gen Electric

Inventors

• Zheng Li
• Sun Changjie
• Kray Nicholas J

Classifications

• F01D25/06 Primary

  for preventing blade vibration (means on blade-carrying members or blades F01D5/00) · CPC title

• F01D5/18

  Hollow blades, {i.e. blades with cooling or heating channels or cavities (structure of hollow blades in general F01D5/147)}; Heating, heat-insulating or cooling means on blades · CPC title

• F01D9/041

  using blades (F01D5/148 takes precedence) · CPC title

• F01D25/02

  De-icing means for engines having icing phenomena · CPC title

• F01D5/046

  Heating, heat insulation or cooling means · CPC title