IP Library › Granted Patent US 10,948,108
Granted Patent B2
US 10,948,108 · App. 15/584,739 · Granted Mar 16, 2021

Turbine engine duct

Inventors: Yanzhe Yang (Waynesville, OH); Daniel Dyer (Dayton, OH); Armando Bringas (Querétaro, MX); Jason Levi Burdette (Beavercreek, OH); Gordon Tajiri (Allentown, PA); Dattu GV Jonnalagadda (Ponnur, IN); Michael Thomas Kenworthy (Gilbert, AZ)
Assignee: Unison Industries, LLC
F16L9/006B22F5/106B23P15/00F02C6/08F02C7/14F02C7/185F16L27/111F28D7/106F28F1/06B22F3/1055B22F5/009B22F2005/103B22F2998/10B22F2999/00B64D13/06F05D2220/32F05D2230/22F05D2230/31F05D2230/642F05D2250/12F05D2250/13F05D2250/131F05D2250/25F05D2250/75F05D2260/60F16L9/02F16L51/025F28D7/1615F28F2210/06
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Quick Facts
Patent No.
US 10,948,108
App. No.
15/584,739
Granted
Mar 16, 2021
Kind
B2
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.

Claims (15)

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.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 2, 2017
From: YANG, YANZHE; DYER, DANIEL; BRINGAS, ARMANDO; BURDETTE, JASON LEVI; TAJIRI, GORDON; JONNALAGADDA, DATTU GV; KENTWORTHY, MICHAEL THOMAS
To: UNISON INDUSTRIES, LLC
Reel/Frame 042213/0654 →
Continuity (1)
Related Publication 20180320801A1 · Nov 8, 2018
Cited By (1)
US 12,697,661