Turbine engine duct

Patent metadata

Field	Value
Publication number	US-10948108-B2
Application number	US-201715584739-A
Country	US
Kind code	B2
Filing date	May 2, 2017
Priority date	May 2, 2017
Publication date	Mar 16, 2021
Grant date	Mar 16, 2021

Abstract

A duct for a turbine engine, such as a gas turbine engine, can be utilized to carry a fluid from one portion of the engine to another. The duct can include a metallic tubular element having one of a varying wall thickness, a varying cross section, or a tight bend. Such a duct can be formed utilizing additive manufacturing or metal deposition on an additively manufactured mandrel.

First claim

What is claimed is:

1. A duct for carrying a fluid, the duct comprising:
a metal tubular element including both a longitudinally varying wall thickness and a varying cross-section along at least a portion of a length of the metal tubular element; and
wherein the metal tubular element is configured to convey the fluid from a first portion to another portion; and
wherein the metal tubular element has at least one bend with a radius of curvature that is less than twice a diameter of the metal tubular element.

2. The duct of claim 1 wherein the varying cross-section comprises a varying cross-sectional area.

3. The duct of claim 1 wherein the metal tubular element has a non-circular cross-section along a portion of the varying cross-section.

4. The duct of claim 1 , further comprising a bellows wherein the bellows includes at least one of a helical convolution, a set of grooves, a concave outer wall, or a convex outer wall.

5. The duct of claim 1 , further comprising a second metal tubular element provided interiorly of or exteriorly of the metal tubular element.

6. The duct of claim 5 wherein the second metal tubular element includes at least one of a varying wall thickness or a varying cross section along at least a portion of a length of the second metal tubular element.

7. A fluid delivery system for an engine, comprising:
at least one metal tubular element that includes a longitudinally varying wall thickness along at least a portion of its length such that the metal tubular element is configured to have at least one of a mechanical property or a thermal property;
wherein the metal tubular element has at least one curve that includes a radius of curvature less than twice a diameter of the metal tubular element.

8. The fluid delivery system of claim 7 , further comprising a bellows wherein the bellows includes at least one of a helical convolution, a set of grooves, a concave outer wall, or a convex outer wall.

9. The fluid delivery system of claim 7 wherein the metal tubular element has a non-circular cross-section.

10. The fluid delivery system of claim 7 wherein the at least one metal tubular element comprising at least two metal tubular elements, with at least one of the at least two metal tubular elements includes the longitudinally varying wall thickness and a varying cross-section.

Assignees

• Unison Ind Llc

Inventors

• Yang Yanzhe
• Dyer Daniel
• Bringas Armando
• Burdette Jason Levi
• Tajiri Gordon
• Jonnalagadda Dattu Gv
• Kenworthy Michael Thomas

Classifications

• B22F10/66

  by mechanical means · CPC title

• B22F10/28

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

• B22F2998/10

  Processes characterised by the sequence of their steps · CPC title

• B22F2999/00

  Aspects linked to processes or compositions used in powder metallurgy · CPC title

• F05D2250/25

  helical · CPC title