IP Library Granted Patent US 7,100,885
Granted Patent B2
US 7,100,885 · App. 11/018,589 · Granted Sep 5, 2006

Seat mounting rail, particularly for a commercial aircraft

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,100,885
App. No.
11/018,589
Granted
Sep 5, 2006
Kind
B2
Abstract

A seat mounting rail for securing seats to a floor of a passenger aircraft is made of a seat securing upper section and a rail mounting lower section. Both sections are made of different metals. The upper section is made of a titanium alloy for corrosion protection. The lower rail section is made of an aluminum alloy for weight reduction. The interconnection between the two sections is made as a thermal joint for example formed as a laser weld, which is preferably a butt weld to save welding material.

Claims (9)

1. A seat mounting rail for securing a seat to a floor of a commercial aircraft, said seat mounting rail comprising a seat securing upper rail section made of a first metal and a rail mounting lower rail section made of a second metal, wherein said first metal is a titanium alloy and wherein said second metal is an aluminum alloy, said seat mounting rail further comprising a thermal interconnection joint between said first and second metals.

2. The seat mounting rail of claim 1 , wherein said thermal interconnection joint is a laser formed weld.

3. The seat mounting rail of claim 2 , wherein said laser formed weld is a butt weld.

4. The seat mounting of claim 1 , wherein said thermal interconnection joint is a butt weld.

5. The seat mounting rail of claim 1 , wherein said seat securing upper rail section has a sectional C-configuration and lateral flanges extending in opposite directions away from said C-configuration, wherein said rail mounting lower rail section comprises an inverted T-configuration with a top edge, and wherein said thermal interconnection joint is a laser formed butt weld between said top edge of said inverted T-configuration and a facing surface of said C-configuration that faces said top edge.

6. The seat mounting rail of claim 5 , wherein said laser formed butt weld extends centrally between edges of said flanges along said C-configuration.

7. The seat mounting rail of claim 5 , wherein said rail mounting lower rail section comprises a plurality of rail portions spaced from each other along said facing surface of said C-configuration.

8. The seat mounting rail of claim 1 , further comprising a corrosion protective coating positioned for protecting said interconnection.

9. The seat mounting rail of claim 1 , wherein said upper rail section comprises a groove (G) opening downwardly, and wherein said lower rail section has a top edge ( 2 ′) welded into said groove.

Assignments (2)
CHANGE OF NAME Recorded May 31, 2011
From: AIRBUS DEUTSCHLAND GMBH
To: AIRBUS OPERATIONS GMBH
Reel/Frame 026360/0849 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 15, 2006
From: ZERNER, INGO
To: AIRBUS DEUTSCHLAND GMBH
Reel/Frame 017802/0104 →