US20170216921A1

US20170216921A1 - Additive manufactured conglomerated powder removal from internal passages

Info

Publication number: US20170216921A1
Application number: US15/011,959
Authority: US
Inventors: Caitlin Oswald; Jesse R. Boyer; Wendell V. Twelves, Jr.; Monica C. Smith; Krzysztof Barnat
Original assignee: United Technologies Corp
Current assignee: RTX Corp
Priority date: 2016-02-01
Filing date: 2016-02-01
Publication date: 2017-08-03
Also published as: US11597014B2; EP3199270B1; EP3199270A1; US20200094326A1

Abstract

A component includes an additively manufactured component with an internal passage; and an additively manufactured elongated member within the internal passage. A method of additively manufacturing a component including additively manufacturing a component with an internal passage; and additively manufacturing an elongated member within the internal passage concurrent with additively manufacturing the component.

Description

BACKGROUND

The present disclosure relates to additive manufacturing and, more particularly, to removing conglomerated powder from within an internal passage.
Precision engineered parts such as gas turbine components may be manufactured by an additive manufacturing operation such that features associated with conventional manufacturing processes, e.g., machining, forging, welding, casting, etc. can be eliminated to facilitate savings in cost, material, and time. Additive manufacturing often results in conglomerated powder building-up around, and within, the completed component as an artifact of the process. When additive manufacturing a component that has internal passages, this conglomerated powder often becomes entrapped in the internal passages and is difficult to remove.
There are currently few methods that directly and rapidly remove the conglomerated powder. One standard practice may include repeated use of an accelerated media blast, combined with mechanically scraping. Oftentimes, such practices are still inefficient at removal of removing conglomerated powder from within the internal passages.

SUMMARY

A component according to one disclosed non-limiting embodiment of the present disclosure can include an additively manufactured component with an internal passage; and an additively manufactured an elongated member within the internal passage.
A further embodiment of the present disclosure may include, wherein the additively manufactured component include a first flange, a second flange, and a conduit with the internal passage therebetween.
A further embodiment of any of the embodiments of the present disclosure may include, wherein the conduit includes multiple bends.
A further embodiment of any of the embodiments of the present disclosure may include, wherein the internal passage is non line of sight.
A further embodiment of any of the embodiments of the present disclosure may include, wherein the additively manufactured elongated member extends along a centerline of the internal passage.
A further embodiment of any of the embodiments of the present disclosure may include, wherein the additively manufactured elongated member extends along a centerline of the internal passage.
A further embodiment of any of the embodiments of the present disclosure may include, wherein the internal passage defines an aspect ratio with a diameter to length of less that 1:4.
A further embodiment of any of the embodiments of the present disclosure may include, wherein a ratio between the internal passage internal diameter and the elongated member outer diameter is between 4.3:1 to 12.5:1.
A further embodiment of any of the embodiments of the present disclosure may include, wherein the elongated member is between about 0.08 and 0.12 inches (˜2-3 mm) in diameter.
A further embodiment of any of the embodiments of the present disclosure may include, wherein the internal passage is between about 0.5 and 1.0 inches (˜13-25 mm) in diameter.
A method of additively manufacturing a component A component according to one disclosed non-limiting embodiment of the present disclosure can include additively manufacturing a component with an internal passage; and additively manufacturing an elongated member within the internal passage concurrent with additively manufacturing the component.
A further embodiment of any of the embodiments of the present disclosure may include cleaning the internal passage of conglomerated powder with the elongated member subsequent to completion of the additively manufacturing.
A further embodiment of any of the embodiments of the present disclosure may include removing the elongated member from within the internal passage subsequent to cleaning the internal passage.
A further embodiment of any of the embodiments of the present disclosure may include destructively removing the elongated member from within the internal passage subsequent to cleaning the internal passage.
A further embodiment of any of the embodiments of the present disclosure may include pulling the elongated member out of the internal passage subsequent to cleaning the internal passage.
A further embodiment of any of the embodiments of the present disclosure may include removing conglomerated powder from the external surfaces of the completed additively manufactured component.
A further embodiment of any of the embodiments of the present disclosure may include agitating the elongated member within the internal passage to remove clean the internal passage of conglomerated powder of the completed additively manufactured component.
The foregoing features and elements may be combined in various combinations without exclusivity, unless expressly indicated otherwise. These features and elements as well as the operation thereof will become more apparent in light of the following description and the accompanying drawings. It should be understood, however, the following description and drawings are intended to be exemplary in nature and non-limiting.

BRIEF DESCRIPTION OF THE DRAWINGS

Various features will become apparent to those skilled in the art from the following detailed description of the disclosed non-limiting embodiment. The components in the drawings are not necessarily to scale. Moreover, in the drawings, like reference numerals designate corresponding parts throughout the several views. The drawings that accompany the detailed description can be briefly described as follows:

FIG. 1 is a perspective view of a representative additively manufactured component.

FIG. 2 is a method of additively manufacturing a component according to one disclosed non-limiting embodiment.

FIG. 3 is a perspective view of the additively manufactured component of FIG. 1 with an elongated member for removing conglomerated powder from within an internal passage.

FIG. 4 is a sectional view of the additively manufactured component with the conglomerated powder according to one embodiment.

FIG. 5 is an sectional view of the additively manufactured component with the conglomerated powder according to another embodiment.

FIG. 6 is an external perspective view of the additively manufactured component within conglomerated powder which is removed from the external portion thereof.

FIG. 7 is an expanded sectional view of the additively manufactured component with the conglomerated powder.

FIG. 8 is an expanded sectional view of the additively manufactured component o FIG. 7 with loosened conglomerated powder.

DETAILED DESCRIPTION

FIG. 1 schematically illustrates a component 20 that includes an internal passage 22. In this example, the component 20 may be a conduit such as that of a manifold, duct, flow passage, or other such component. The component 20 may include a first flange 24, a second flange 26, and a conduit 28 with the internal passage 22 therebetween. The internal passage 22 may be complex and be of a non-line of sight geometry that includes multiple bends. It should be appreciated that various additional or alternative segments and/or fittings may also be provided. It should be further appreciated that although a conduit type example is illustrated herein, other aerospace components, aircraft structures, as well as a wide variety of applications outside the aerospace industry, which include one or more internal passages, will benefit herefrom.
The component 20 may be readily manufactured with an additive manufacturing process that includes but are not limited to, Sterolithography (SLA), Direct Selective Laser Sintering (DSLS), Electron Beam Sintering (EBS), Electron Beam Melting (EBM), Laser Engineered Net Shaping (LENS), Laser Net Shape Manufacturing (LNSM), Direct Metal Deposition (DMD), Laser Powder Bed Fusion (LPBF) and others. Although particular additive manufacturing processes are disclosed, those skilled in the art of manufacturing will recognize that any other suitable rapid manufacturing methods using layer-by-layer construction or additive fabrication can alternatively be used.
The additive manufacturing process sequentially builds-up layers of atomized alloy and/or ceramic powder material that include but are not limited to, 625 Alloy, 718 Alloy, 230 Alloy, stainless steel, tool steel, cobalt chrome, titanium, Ti-6Al-4V, nickel, aluminum and others in atomized powder material form. Alloys such as 625, 718 and 230 may have specific benefit for parts that operate in high temperature environments, such as, for example, environments typically encountered by aerospace and gas turbine engine components.
The additive manufacturing process fabricates or “grows” of components using three-dimensional information, for example a three-dimensional computer model. The three-dimensional information is converted into a plurality of slices, each slice defining a cross section of the component for a predetermined height of the slice. The additive manufactured component 20 is then “grown” slice-by-slice, or layer-by-layer, until finished. Each layer has an example size between about 0.0005-0.001 inches (0.0127-0.0254 mm). The additive manufacturing process facilitates manufacture of the relatively complex internal passage geometry to minimize assembly details, gun-drilling, and multi-component construction.
With reference to FIG. 2, one disclosed non-limiting embodiment of a method 100 to additively manufacture the component 20 initially includes additively manufacturing the component 20 with an elongated member 40 through the internal passage 22 (step 110; FIG. 3). That is, the elongated member 40 is additively manufactured simultaneously with the component 20. The elongated member 40 may be integral to the build geometry and may be an elongated member that generally extends along a centerline A of the internal passage 22 or other member that forms no part of the component 20.
In one embodiment, the internal passage 22 may define an aspect ratio with a diameter to length of less that 1:4. In one non-limiting dimension embodiment, the elongated member 40 diameter 40D dimension is between about 0.08 and 0.12 inches (˜2-3 mm) in diameter and the internal diameter 22D dimension of the internal passage 22 is between about 0.5 and 1.0 inches (˜13-25 mm) in diameter. In the non-limiting dimension embodiment, the ratio between the internal diameter 22D and the elongated member 40 outer diameter 40D and is between 4.3:1 to 12.5:1. It should be appreciated that this is but one example, and various relationship may otherwise benefit herefrom.
Next, conglomerated powder 50 is removed from the external surfaces of the completed additively manufactured component 20 (step 120; FIG. 4). Removal is conventional and may include the use of accelerated media blast, mechanically scraping, vibratory or other methods. The completed component 20 thereby retains the elongated member 40 within the internal passage 22 once the conglomerated powder 50 is removed from the external surfaces. The elongated member 40 may be utilized to facilitate handling and transport of the component 20.
Next, the elongated member 40 is agitated and/or “stirred” around inside the internal passage 22 to mechanically work the conglomerated powder 50 out of the internal passage 22 (step 130). That is, the conglomerated powder 50 may be relatively compacted and the elongated member 40 operates to clean the internal passage 22 of the conglomerated powder 50. As the elongated member 40 generally extends along the centerline A of the internal passage 22, the entirety of the internal passage 22 is readily cleared.
Next, the elongated member 40 is removed from the internal passage 22 (step 140; FIG. 1). In some instances the elongated member 40 is sufficiently flexible and the internal passage geometry is such that the elongated member 40 may be pulled out from the internal passage 22. In other instances, the elongated member 40 may need to be destructively removed such as via abrasive flow, chemical milling, and/or other processes.
The utilization of the elongated member 40 readily facilitates direct and rapid removal of the conglomerated powder from within internal passages.
The use of the terms “a,” “an,” “the,” and similar references in the context of description (especially in the context of the following claims) are to be construed to cover both the singular and the plural, unless otherwise indicated herein or specifically contradicted by context. The modifier “about” used in connection with a quantity is inclusive of the stated value and has the meaning dictated by the context (e.g., it includes the degree of error associated with measurement of the particular quantity). All ranges disclosed herein are inclusive of the endpoints, and the endpoints are independently combinable with each other. It should be appreciated that relative positional terms such as “forward,” “aft,” “upper,” “lower,” “above,” “below,” and the like are with reference to normal operational attitude and should not be considered otherwise limiting.
Although the different non-limiting embodiments have specific illustrated components, the embodiments of this invention are not limited to those particular combinations. It is possible to use some of the components or features from any of the non-limiting embodiments in combination with features or components from any of the other non-limiting embodiments.
It should be appreciated that like reference numerals identify corresponding or similar elements throughout the several drawings. It should also be appreciated that although a particular component arrangement is disclosed in the illustrated embodiment, other arrangements will benefit herefrom.
Although particular step sequences are shown, described, and claimed, it should be understood that steps may be performed in any order, separated or combined unless otherwise indicated and will still benefit from the present disclosure.
The foregoing description is exemplary rather than defined by the limitations within. Various non-limiting embodiments are disclosed herein, however, one of ordinary skill in the art would recognize that various modifications and variations in light of the above teachings will fall within the scope of the appended claims. It is therefore to be understood that within the scope of the appended claims, the disclosure may be practiced other than as specifically described. For that reason the appended claims should be studied to determine true scope and content.

Claims

What is claimed is:

1. A component, comprising:

an additively manufactured component with an internal passage; and

an additively manufactured an elongated member within the internal passage.

2. The component as recited in claim 1, wherein the additively manufactured component include a first flange, a second flange, and a conduit with the internal passage therebetween.

3. The component as recited in claim 2, wherein the conduit includes multiple bends.

4. The component as recited in claim 2, wherein the internal passage is non line of sight.

5. The component as recited in claim 1, wherein the additively manufactured elongated member extends along a centerline of the internal passage.

6. The component as recited in claim 1, wherein the additively manufactured elongated member extends along a centerline of the internal passage.

7. The component as recited in claim 1, wherein the internal passage defines an aspect ratio with a diameter to length of less that 1:4.

8. The component as recited in claim 1, wherein a ratio between the internal passage internal diameter and the elongated member outer diameter is between 4.3:1 to 12.5:1.

9. The component as recited in claim 1, wherein the elongated member is between about 0.08 and 0.12 inches (˜2-3 mm) in diameter.

10. The component as recited in claim 9, wherein the internal passage is between about 0.5 and 1.0 inches (˜13-25 mm) in diameter.

11. A method of additively manufacturing a component, comprising:

additively manufacturing a component with an internal passage; and

additively manufacturing an elongated member within the internal passage concurrent with additively manufacturing the component.

12. The method as recited in claim 11, further comprising cleaning the internal passage of conglomerated powder with the elongated member subsequent to completion of the additively manufacturing.

13. The method as recited in claim 12, further comprising removing the elongated member from within the internal passage subsequent to cleaning the internal passage.

14. The method as recited in claim 13, further comprising destructively removing the elongated member from within the internal passage subsequent to cleaning the internal passage.

15. The method as recited in claim 13, further comprising pulling the elongated member out of the internal passage subsequent to cleaning the internal passage.

16. The method as recited in claim 11, further comprising removing conglomerated powder from the external surfaces of the completed additively manufactured component.

17. The method as recited in claim 16, further comprising agitating the elongated member within the internal passage to remove clean the internal passage of conglomerated powder of the completed additively manufactured component.