Method for making an integrally bladed rotor with hollow blades

Patent metadata

Field	Value
Publication number	US-9914170-B2
Application number	US-201414303673-A
Country	US
Kind code	B2
Filing date	Jun 13, 2014
Priority date	Jun 13, 2014
Publication date	Mar 13, 2018
Grant date	Mar 13, 2018

Abstract

A method of making an integrally bladed rotor with hollow blades. A plurality of segmented layers are sequentially placed to form each one of a plurality of blades on a radially outward surface of a hub. This is done using an additive manufacturing process. The placement of the segmented layers also comprises omitting portions of one or more of the plurality of segmented layers to form one or more cavities and intermittently removing a quantity of particles from the one or more cavities using an evacuation tool.

First claim

The invention claimed is:

1. A method of making an integrally bladed rotor comprising a hub and a plurality of hollow blades, the method comprising:
forming each of a plurality of hollow blades by using an additive manufacturing process to integrally form a plurality of segmented layers successively outward from a radially outward surface of a hub;
while forming the plurality of hollow blades, forming one or more cavities in one or more of the plurality of hollow blades by omitting a portion of one or more of the plurality of segmented layers and periodically evacuating a quantity of excess material from the one or more cavities;
forming a relief hole for each of the one or more cavities at a tip of each of the plurality of hollow blades;
evacuating each of the one of the one or more cavities via the relief hole; and
plugging the relief hole.

2. The method of claim 1 , wherein plugging the relief hole comprises:
arranging a plug in the relief hole;
disposing a filler material along a periphery of the plug; and
solidifying the filler material to secure the plug in the relief hole, the plug and the filler material forming an outer surface that conforms to a selected profile.

3. The method of claim 1 , further comprising using a subtractive manufacturing process to shape one or more of the segmented layers.

4. The method of claim 1 , wherein integrally forming the plurality of segmented layers comprises supplying a quantity of a raw material irradiating the raw material to form the segmented layer.

5. The method of claim 4 , wherein the raw material is controlled to have a particle size of less than about 50 microns.

6. The method of claim 4 , wherein the raw material is about 99% pure.

7. The method of claim 1 , wherein removing the quantity of excess material is performed using a wind curtain or other evacuation tool.

8. A method of making an integrally bladed rotor with hollow blades, the method comprising:
sequentially forming a plurality of segmented layers to form each one of a plurality of blades on a radially outward surface of a hub using an additive manufacturing process, forming the plurality of segmented layers further comprising:
omitting portions of one or more of the plurality of segmented layers to form one or more cavities;
intermittently removing a quantity of particles from the one or more cavities using an evacuation tool;
forming a relief hole at a tip of each one of a plurality of blades for at least one of the one or more cavities;
evacuating the at least one of the one or more cavities via the relief hole; and
filling the relief hole.

9. The method of claim 8 , wherein sequentially forming one of the plurality of segmented layers comprises supplying a quantity of a raw material irradiating the raw material to form the segmented layer.

10. The method of claim 8 , wherein sequentially forming the plurality of segmented layers further comprises periodically machining the segmented layers.

11. The method of claim 8 , wherein filling the relief hole comprises:
arranging a plug in the relief hole; and
disposing a filler material along a periphery of the plug.

12. The method of claim 11 , wherein filling the relief hole further comprises solidifying the filler material to secure the plug in the relief hole, the plug and the filler material forming an outer surface that conforms to a selected profile.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Kountanya Raja
• Klecka Michael A

Classifications

• B22F10/68

  Cleaning or washing · CPC title

• B22F10/50

  Treatment of workpieces or articles during build-up, e.g. treatments applied to fused layers during build-up · CPC title

• B22F10/38

  to achieve specific product aspects, e.g. surface smoothness, density, porosity or hollow structures · CPC title

• B22F10/25

  Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS] · CPC title

• B23K26/211

  with interposition of special material to facilitate connection of the parts · CPC title