Method for forming article, method for forming turbine bucket, and turbine bucket

Patent metadata

Field	Value
Publication number	US-2019091802-A1
Application number	US-201715713857-A
Country	US
Kind code	A1
Filing date	Sep 25, 2017
Priority date	Sep 25, 2017
Publication date	Mar 28, 2019
Grant date	—

Abstract

A method for forming an article is disclosed, including laser welding a powder of an HTW alloy to a surface of a substrate along a weld path, forming a weld bead of the HTW alloy. The weld path is propagated along a weld direction, forming a cladding layer of the HTW alloy on the surface. The laser welding includes a laser energy density of at least about 11 kJ/cm 2 , and laser welding the powder to the surface includes a welding speed of about 5-20 ipm. The weld path oscillates essentially nonparallel to a reference line, establishing a cladding width wider than the weld bead width. The weld bead contacts itself along each oscillation such that the cladding layer is continuous and essentially free of cracks. A turbine bucket is disclosed including a squealer tip having the cladding layer with a cladding layer thickness of at least about 0.2 inches.

First claim

What is claimed is:

1 . A method for forming an article, comprising:
laser welding a powder of a metal alloy to a surface of a substrate along a weld path, forming a weld bead of the metal alloy having a weld bead width and a weld bead height; and propagating the weld path along a weld direction, forming a cladding layer of the metal alloy disposed on the surface having a cladding layer thickness, wherein:
the metal alloy is a hard-to-weld (HTW) alloy;
the laser welding includes a laser energy density of at least about 11 kJ/cm 2 ;
laser welding the powder of the metal alloy to the surface of the substrate along the weld path includes a welding speed between about 5 ipm to about 20 ipm;
the weld path oscillates essentially nonparallel relative to a reference line, establishing a cladding width wider than the weld bead width;
the weld bead contacts itself along each oscillation such that the cladding layer is continuous; and
the cladding layer is essentially free of cracks.

2 . The method of claim 1 , wherein the article is a turbine bucket including a squealer tip, and the cladding layer forms at least a portion of the squealer tip.

3 . The method of claim 2 , wherein the weld path commences at a trailing edge of the turbine bucket, proceeds across a trailing edge width of the trailing edge, and then proceeds around a periphery of the turbine bucket along one of a suction side and a pressure side, through a leading edge, and back along the other of the suction side and the pressure side until returning to the trailing edge.

4 . The method of claim 1 , wherein the reference line is selected from the group consisting of a weld direction, a center line, a chord line, and combinations thereof.

5 . The method of claim 1 , wherein the metal alloy includes, by weight:
about 15% to about 17% chromium; about 4% to about 5% aluminum; about 2% to about 4% iron; about 0.002% to about 0.04% yttrium; up to about 0.5% manganese; up to about 0.2% silicon; up to about 0.1% zirconium; up to about 0.05% carbon; up to about 0.5% tungsten; up to about 2% cobalt; up to about 0.15% niobium; up to about 0.5% titanium; up to about 0.5% molybdenum; up to about 0.01% boron; and a balance of nickel;

6 . The method of claim 1 , wherein the surface of the substrate includes a surface layer of a surface material selected from the group consisting of:
an alloy composition including, by weight:
about 21% to about 23% chromium;
about 13% to about 15% tungsten;
about 1% to about 3% molybdenum;
about 0.25% to about 0.75% manganese;
about 0.2% to about 0.6% silicon;
about 0.1% to about 0.5% aluminum;
about 0.05% to about 0.15% carbon;
about 0.01% to about 0.03% lanthanum;
up to about 3% iron;
up to about 5% cobalt;
up to about 0.5% niobium;
up to about 0.1% titanium;
up to about 0.015% boron; and
a balance of nickel;
an alloy composition including, by weight:
about 20% to about 23% chromium;
about 8% to about 10% molybdenum;
about 3.15% to about 4.15% niobium and tantalum;
up to about 5% iron;
up to about 0.1% carbon;
up to about 0.5% manganese;
up to about 0.5% silicon;
up to about 0.015% phosphorous;
up to about 0.015% sulfur;
up to about 0.4% aluminum;
up to about 0.4% titanium;
up to about 1% cobalt; and
a balance of nickel;
an alloy composition including, by weight:
about 14% to about 16% nickel;
about 19% to about 21% chromium;
about 8% to about 10% tungsten;
about 4.0% to about 4.8% aluminum;
about 0.1% to about 0.3% titanium;
about 2% to about 4% tantalum;
about 0.25% to about 0.45% carbon;
about 0.5% to about 1.5% hafnium;
about 0.35% to about 0.55% yttrium; and
a balance of cobalt; and
combinations thereof.

7 . The method of claim 1 , wherein the substrate includes a material composition, the surface of the substrate consists essentially of the material composition of the substrate, and the powder of the metal alloy is laser welded directly to the surface of the substrate.

8 . The method of claim 1 , wherein the substrate includes a material composition selected from the group consisting of:
steels; mild steels; superalloys; nickel-based superalloys; cobalt-based superalloys; an alloy composition including, by weight:
about 9% to about 10.5% chromium;
about 7% to about 8% cobalt;
about 3.7% to about 4.7% aluminum;
about 3% to about 4% titanium;
about 1% to about 2% molybdenum;
about 5% to about 7% tungsten;
about 4.3% to about 5.3% tantalum;
about 0.3% to about 0.7% niobium;
about 0.1% to about 0.2% hafnium; and
a balance of nickel;
an alloy composition including, by weight:
about 13.5% to about 14.5% chromium;
about 9% to about 10% cobalt;
about 3.3% to about 4.3% tungsten;
about 4.4% to about 5.4% titanium;
about 2.5% to about 3.5% aluminum;
about 0.05% to about 0.15% iron;
about 2.3% to about 3.3% tantalum;
about 1.1% to about 2.1% molybdenum;
about 0.05% to about 0.15% carbon; and
a balance of nickel;
an alloy composition including, by weight:
about 22.5% to about 24.5% chromium;
about 18% to about 20% cobalt;
about 1.5% to about 2.5% tungsten;
about 0.3% to about 1.3% niobium;
about 1.8% to about 2.8% titanium;
about 0.7% to about 1.7% aluminum;
about 0.5% to about 1.5% tantalum;
about 0.15% to about 0.35% silicon;
about 0.05% to about 0.15% manganese; and
a balance of nickel;
an alloy composition including, by weight:
about 17% to about 21% chromium;
about 50% to about 55% nickel and cobalt;
about 4.75% to about 5.5% niobium and tantalum;
about 2.8% to about 3.3% molybdenum;
about 0.65% to about 1.15% titanium;
about 0.2% to about 0.8% aluminum;
up to about 1% cobalt;
up to about 0.08% carbon;
up to about 0.35% manganese;
up to about 0.35% silicon;
up to about 0.015% phosphorous;
up to about 0.015% sulfur;
up to about 0.006% boron;
up to about 0.3% copper; and
a balance of iron;
an alloy composition including, by weight:
about 5.4% to about 5.7% aluminum;
about 8% to about 8.5% chromium;
about 9% to about 9.5% cobalt;
about 9.3% to about 9.7% tungsten;
about 0.05% to about 0.15% manganese;
about 0.15% to about 0.35% silicon;
about 0.06% to about 0.09% carbon; and
a balance of nickel;
an alloy composition including, by weight:
about 7% to about 8% cobalt;
about 6% to about 8% chromium;
about 5.5% to about 7.5% tantalum;
about 5.2% to about 7.2% aluminum;
about 4% to about 6% tungsten;
about 2.5% to about 3.5% rhenium;
about 1% to about 2% molybdenum;
about 0.1% to about 0.2% hafnium; and
a balance of nickel;
an alloy composition including, by weight:
about 7.9% to about 8.9% chromium;
about 9% to about 10% cobalt;
about 5% to about 6% aluminum;
about 0.5% to about 0.9% titanium;
about 9% to about 10% tungsten;
about 0.3% to about 0.7% molybdenum;
about 2.5% to about 3.5% tantalum;
about 1% to about 2% hafnium; and
a balance of nickel; and
combinations thereof.

9 . The method of claim 1 , wherein the laser energy density is between about 11.5 kJ/cm 2 to about 20.3 kJ/cm 2 .

10 . The method of claim 1 , wherein the powder is applied at a flow rate between about 4 g/min to about 6 g/min.

11 . The method of claim 10 , wherein the flow rate is between about 4.8 g/min to about 5.2 g/min.

12 . The method of claim 1 , wherein forming the cladding layer consists essentially of applying a single layer of the metal alloy, and the cladding layer thickness is about the weld bead height.

13 . The method of claim 1 , wherein forming the cladding layer includes applying a first layer of the me

Assignees

• Gen Electric

Inventors

• Woolridge Jillian Jamison
• Hullender Robert Trent

Classifications

• B23K2201/001

  Operations & Transport · mapped topic

• F05D2300/17

  Alloys · CPC title

• F01D5/147

  Construction, i.e. structural features, e.g. of weight-saving hollow blades (F01D5/148, F01D5/16 and F01D5/20 take precedence; blade shape F01D5/141; blades with cooling or heating channels or cavities F01D5/18; heating, heat-insulating or cooling means on blades F01D5/18) · CPC title

• F01D5/20

  Specially-shaped blade tips to seal space between tips and stator {(F01D5/225 takes precedence)} · CPC title

• F01D5/28

  Selecting particular materials; {Particular measures relating thereto;} Measures against erosion or corrosion · CPC title