Raceway

• US 10,400,918 B2
• Filed: 12/09/2016
• Issued: 09/03/2019
• Est. Priority Date: 12/11/2015
• Status: Active Grant

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: Webb, Michael, Healy, Daren
• Primary Examiner(s): Wujciak, Alfred J
• Application Number:
  US15/373,919
• Publication Number:
  US 20170167637A1
• Time in Patent Office: 998 Days
• Field of Search: 174 40 R, 174 41, 174 44, 248 61, 211162
• CPC Class Codes: B64D 2221/00 Electric power distribution systems onboard aircraft
• CPC Class Codes: F16L 3/223 each support having one transverse base for supporting the pipes F16L3/23, F16L3/237 take precedence
• CPC Class Codes: F16L 3/23 for a bundle of pipes or a plurality of pipes placed side by side in contact with each other F16L3/237 takes precedence
• CPC Class Codes: F16L 3/26 specially adapted for supporting the pipes all along their length, e.g. pipe channels or ducts channels for electric cables formed by wire H02G3/0443
• CPC Class Codes: F16L 59/14 Arrangements for the insulation of pipes or pipe systems F16L59/02 - F16L59/12 take precedence
• CPC Class Codes: H02G 3/04 Protective tubing or conduits, e.g. cable ladders or cable troughs
• CPC Class Codes: H02G 3/0412 Heat or fire protective means for fire in electric circuits A62C3/16
• CPC Class Codes: H02G 3/0437 Channels

Abstract

A raceway and method of forming a raceway is disclosed in which one or more intumescent layers are disposed on the raceway.

Claims

1. An aircraft raceway for securing cables, pipes, or wires in an aircraft, comprising:

a plurality of wall portions adjoining a base portion together defining a plurality of longitudinal U-shaped open channels, the open side of each channel being arranged to provide access for installation of one or more aircraft cables or pipes or wires within the respective channel; and

at least one intumescent layer, wherein each of the at least one intumescent layer is contiguously disposed continuously along on a corresponding inner surface and outer surface, and distal edges of at least one of the wall portions adjacent the open side of the respective channel, the at least one intumescent layer is continuously disposed continuously along on a corresponding inner surface and outer surface of the base portion,

the at least one intumescent layer having a non-activated state in which the open side of the channel is maintained substantially open and a thermally activated state in which the at least one intumescent layer expands so as to close the open side of the respective channel.

2. A raceway according to claim 1 in which the at least one intumescent layer is arranged to expand so as to substantially close the open side of the respective channel.

3. A raceway according to claim 1 in which the at least one intumescent layer is arranged to expand so as to at least partially close the open side of the respective channel.

4. A raceway according to claim 1 in which the at least one intumescent layer is confined to the distal part of the inner surface of the wall portion relative to the base portion.

5. A raceway according to claim 1 in which a third intumescent layer is disposed on substantially all the exterior longitudinal surfaces of the raceway.

6. A raceway according to claim 1 in which at least two of the channels are of substantially different volumes.

7. A raceway according to claim 1 further comprising:

one or more cable clip connector elements formed in the base portion within at least one of the channels; and

a second intumescent layer disposed on the exterior longitudinal surface of the base portion adjacent the cable clip connector elements.

8. A raceway according to claim 1 formed from aluminum or an aluminum alloy.

9. An aircraft structure comprising the raceway according to claim 1.

10. A raceway according to claim 1 in which the at least one intumescent layer exposes a portion of the corresponding inner surface adjacent to the base portion.

11. A method of forming an aircraft raceway for securing cables, pipe, or wires in an aircraft, comprising the steps of:

forming a plurality of wall portions adjoining a base portion together defining a plurality of U-shaped longitudinal open channels, the open side of each channel being arranged to provide access for installation of one or more aircraft cables or pipes or wires within the respective channel; and

disposing at least one intumescent layer continuously and contiguously along on the inner surface, outer surface, and distal edges of at least one of the wall portions adjacent the open side of the respective channel, the at least one intumescent layer is continuously disposed continuously along on a corresponding inner surface and outer surface of the base portion,

the at least one intumescent layer having a non-activated state in which the open side of the channel is maintained substantially open and a thermally activated state in which the at least one intumescent layer expands so as to close the open side of the channel.

12. A method according to claim 11 in which the at least one intumescent layer is confined to the distal part of the inner surface of the wall portion relative to the base portion.

13. A method according to claim 12 in which a third intumescent layer is disposed on substantially all the exterior longitudinal surfaces of the raceway.

14. A method according to claim 12 in which where intumescent layers are disposed on either side of a given wall portion of the plurality of wall portions, the intumescent layers are contiguous so as to extend over the distal edge of the given wall portion.

15. A method according to claim 11 in which the disposing of the at least one intumescent layer comprises exposing a portion of an inner surface adjacent to the base portion.