Pre-cured EME edge seal

Patent metadata

Field	Value
Publication number	US-9789971-B2
Application number	US-201514722117-A
Country	US
Kind code	B2
Filing date	May 26, 2015
Priority date	Mar 20, 2015
Publication date	Oct 17, 2017
Grant date	Oct 17, 2017

Abstract

An aircraft fuel cell seal and methods of its use. The disclosed seal takes the form of a pre-cured, partially hollow elongate member that does not subtend a complete circle, but rather leaves an elongate gap in the member that can be placed over an edge or fillet of a fuel cell. In some cases, chambers within the member may be filled with wet sealant to provide redundant protection against EME effects.

First claim

We claim:

1. An aircraft fuel cell seal, comprising:
a pre-cured elongate member with a curved outer shell having a radial thickness at least equal to a predefined minimum radial thickness, the curved outer shell extending circumferentially about a longitudinal axis of the elongate member in an angularly incomplete manner such that is subtends an angle of at least 180 degrees and less than 360 degrees to define an elongated gap in the outer shell, the gap for receiving an edge or a fillet of an aircraft fuel cell;
a plurality of partially cylindrical open chambers disposed within the outer shell, each having a radius at least equal to a predefined minimum radius; and
a plurality of support members disposed within the outer shell and separating the open chambers.

2. The fuel cell seal of claim 1 , wherein the angle is approximately 270 degrees.

3. The fuel cell seal of claim 1 , wherein the predefined minimum radial thickness is 0.13 inches.

4. The fuel cell seal of claim 3 , wherein the predefined minimum radius is 0.13 inches.

5. The fuel cell seal of claim 1 , wherein the ribs are spaced between 0.25-0.75 inches apart.

6. The fuel cell seal of claim 5 , wherein the ribs are spaced approximately 0.5 inches apart.

7. The fuel cell seal of claim 1 , wherein the curved outer shell forms a partial cylinder.

8. The fuel cell seal of claim 1 , wherein the predefined minimum radial thickness and the predefined minimum radius are each sufficient to meet aircraft electromagnetic environment safety requirements for a fuel cell seal.

9. The fuel cell seal of claim 8 , wherein the predefined minimum radial thickness and the predefined minimum radius are equal.

10. An aircraft fuel cell seal, comprising:
a pre-cured elongate sealing member with an outer shell having a thickness at least equal to a predefined minimum thickness, the curved outer shell extending circumferentially about a longitudinal axis of the elongate member in an angularly incomplete manner such that is subtends an angle of at least 180 degrees and less than 360 degrees to define an elongated gap in the outer shell, the gap for receiving an edge or a fillet of an aircraft fuel cell;
a plurality of support ribs disposed within the outer shell and oriented perpendicular to the shell; and
a plurality of open chambers each bounded by the outer shell and two of the support ribs, and each having an open side defined by the gap in the outer shell.

11. The fuel cell seal of claim 10 , wherein each open chamber defines a volume having a radial thickness at least equal to the predefined minimum thickness of the outer shell.

12. The fuel cell seal of claim 11 , wherein the predefined minimum thickness is 0.13 inches.

13. The fuel cell seal of claim 10 , wherein the angle is at least 270 degrees.

14. The fuel cell seal of claim 10 , wherein the outer shell and the open chambers are each partially cylindrical.

15. A method of sealing a fuel cell edge in an aircraft fuel cell, comprising:
providing an aircraft fuel cell seal, including:
a pre-cured elongate member with a curved outer shell having a thickness at least equal to a predefined minimum thickness, the curved outer shell extending circumferentially about a longitudinal axis of the elongate member in an angularly incomplete manner such that is subtends an angle of at least 180 degrees and less than 360 degrees to define an elongated gap in the outer shell, the gap for receiving an edge or a fillet of an aircraft fuel cell;
a plurality of open chambers disposed within the outer shell, each defining a volume having a thickness at least equal to the predefined minimum thickness; and
a plurality of support members disposed within the outer shell and separating the open chambers;
filling the open chambers with a wet sealant; and
positioning the fuel cell seal around a fuel cell edge.

16. The method of claim 15 , further comprising applying additional wet sealant at edge portions of the fuel cell seal, after positioning the fuel cell seal around the fuel cell edge.

17. The method of claim 16 , further comprising fairing the wet sealant at the edge portions of the fuel cell seal, after applying additional wet sealant.

18. The method of claim 15 , further comprising trimming the fuel cell seal to a desired length.

19. The method of claim 15 , wherein the minimum thickness is 0.13 inches.

20. The method of claim 15 , wherein the fuel cell edge is a free edge, and wherein after positioning the fuel cell seal around the edge, each portion of free edge is covered by at least 0.13 inches in thickness of the fuel cell seal.

Assignees

• Boeing Co

Inventors

• Wiseman Jesse Randal
• Pate Kevin Darrell
• Chaney Matthew G

Classifications

• F16J15/14

  by means of granular or plastic material, or fluid · CPC title

• B60K2015/03447

  for improving the sealing · CPC title

• B64D37/02

  Tanks (tanks constructed integrally with aircraft wings B64C3/34) · CPC title

• H01M2250/20

  Fuel cells in motive systems, e.g. vehicle, ship, plane · CPC title

• F16J15/022

  characterised by structure or material · CPC title