Generally wye shaped elbow for cabin air flow system

Patent metadata

Field	Value
Publication number	US-9381787-B2
Application number	US-201213661069-A
Country	US
Kind code	B2
Filing date	Oct 26, 2012
Priority date	Oct 26, 2012
Publication date	Jul 5, 2016
Grant date	Jul 5, 2016

Abstract

An elbow for use in a cabin air supply system for an aircraft has an inlet duct. The inlet duct diverges into two outlet ducts with an interface area between the outlet ducts. Each of the outlet ducts has a nominal wall thickness, with a central portion of the interface having a first thickness at a point of maximum thickness, and the nominal wall thickness being of a second thickness. The central portion of the interface curves to the central portion of the interface area. A ratio of the first thickness to the second thickness is between 3 and 8. A cabin air supply system is also disclosed.

First claim

The invention claimed is:

1. An elbow for use in a cabin air supply system for an aircraft comprising:
an inlet duct diverging into two outlet ducts with an interface area between said outlet ducts; said inlet duct having a first diameter, and said two outlet ducts each having a second diameter;
a nominal wall thickness between said interface area and said outlet ducts, with a central portion of said interface area having a first thickness at a point of maximum thickness, and said nominal wall thickness being of a second thickness, and wherein said interface area curving to said central portion of said interface area, and a ratio of said first thickness to said second thickness being between 3 and 8;
wherein said outlet duct having a second diameter, and a ratio of said second diameter to said first thickness being between 4 and 7;
wherein an outer face of said central portion of said interface area is formed at a first radius of curvature, and a ratio of said first thickness to said first radius of curvature is between 0.5 and 0.9 ; and
wherein a ratio of said first radius of curvature to radius of curvature on an inner face of said inner face area face is between 2.4 and 3.4.

2. A cabin air supply system comprising:
a cabin air compressor delivering air into an inlet duct of an elbow, and said elbow having two outlet ducts, with each of said outlet ducts communicating to trim valves, with said trim valves selectively supplying air to ducts to be positioned in an aircraft cabin;
said inlet duct diverging into said two outlet ducts with an interface area section between said outlet ducts; said inlet duct having a first diameter, and said two outlet ducts each having a second diameter;
a nominal wall thickness between said interface area and said outlet ducts, with a central portion of said interface area having a first thickness at a point of maximum thickness, and said nominal wall thickness being of a second thickness, and wherein said interface area curving to said central portion of said interface area, and a ratio of said first thickness to said second thickness being between 3 and 8;
wherein said outlet ducts having a second diameter, and a ratio of said second diameter to said first thickness being between 4 and 7;
wherein an outer face of said central portion of said interface area is formed at a first radius of curvature and a ratio of said first thickness to said first radius of curvature is between 0.5 and 0.9; and
wherein a ratio of said first radius of curvature to a radius of curvature on an inner face of said inner area is between 2.4 and 3.4.

3. The cabin air supply system as set forth in claim 2 , wherein said elbow is formed of aluminum.

4. An elbow for use in a cabin air supply system for an aircraft comprising:
an inlet duct diverging into two outlet ducts with an interface area between said outlet ducts; said inlet duct having a first diameter, and said two outlet ducts each having a second diameter;
a nominal wall thickness between said interface area and said outlet ducts, with a central portion of said interface area having a first thickness at a point of maximum thickness, and said nominal wall thickness being of a second thickness, and wherein said interface area curving to said central portion of said interface area, and a ratio of said first thickness to said second thickness being between 3 and 8;
said outlet ducts having a second diameter, and a ratio of said second diameter to said first thickness being between 4 and 7;
an outer face of said central portion of said interface area is formed at a first radius of curvature, and a ratio of said first thickness to said first radius of curvature is between 0.5 and 0.9; and
said elbow formed of aluminum.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Vignali Mark
• Rupp Caroline

Classifications

• B60H1/00564 Primary

  of air ducts · CPC title

• B64D13/02

  the air being pressurised · CPC title

• F16L41/023

  Y- pieces (F16L41/025, F16L41/026, F16L41/028 take precedence) · CPC title