Injectable nut cap

• US 9,400,007 B2
• Filed: 05/17/2013
• Issued: 07/26/2016
• Est. Priority Date: 05/31/2012
• Status: Active Grant

• Current Assignee: Airbus Operations Limited (Airbus SE)
• Original Assignee: Airbus Operations Limited (Airbus SE)
• Inventors: Dobbin, Richard, Tothill, Guy, Liversage, David, Crew, Darren
• Primary Examiner(s): DELISLE, ROBERTA S
• Application Number:
  US14/404,263
• Publication Number:
  US 20150184688A1
• Time in Patent Office: 1,166 Days
• Field of Search: 411/82, 411/82.3, 411/103, 411/172, 4113725-3726, 411/373, 411/377
• US Class Current: 1/1
• CPC Class Codes: B64D 45/02 Lightning protectors; Static dischargers in general H01T
• CPC Class Codes: F16B 11/006 by gluing gluing of plastics material B29C65/48
• CPC Class Codes: F16B 33/004 Sealing; Insulation by means of washers F16B43/001
• CPC Class Codes: F16B 37/14 Cap nuts; Nut caps or bolt caps
• CPC Class Codes: F16B 39/021 by injecting a settable material after the screwing down
• CPC Class Codes: Y10T 29/49993 Filling of opening

Abstract

The present invention proposes a cap for forming a sealed cavity around one end of a fastener to thereby contain out-gassing and sparking events in the event of a lightning strike to the fastener. The invention also proposes a joint comprising such a cap, and a kit of parts and method for installing such a cap. A cap according to the invention comprises: an inner cap member having an annular base terminating at an edge which surrounds an opening into an air cavity for enclosing the one end of a fastener; and an outer cap member having an annular skirt or flange which extends radially outwardly away from the annular base, the annular skirt or flange and annular base between them defining an annular sealing cavity. The cap also comprises a sealing material inlet comprising an opening in the outer cap member that is in fluid communication with the annular sealing cavity, the opening being arranged to interconnect with a sealing material injection device to provide a flow of curable sealing material from the sealing material inlet into the annular sealing cavity.

Claims

1. A cap for forming a sealed cavity around one end of a fastener, the cap comprising:

an inner cap member having an annular base terminating at an edge which surrounds an opening into an air cavity for enclosing the one end of a fastener;

an outer cap member having an annular skirt or flange, the annular skirt or flange and annular base between them defining an annular sealing cavity; and

a sealing material inlet comprising an opening in the outer cap member that is in fluid communication with the annular sealing cavity, the opening being arranged to interconnect with a sealing material injection device to provide a flow of curable sealing material from the sealing material inlet into the annular sealing cavity.

2. A cap according to claim 1, comprising an interfay cavity in fluid communication with the opening of the sealing material inlet and the annular sealing cavity.

3. A cap according to claim 2, wherein the interfay cavity comprises a flow restriction feature arranged to restrict flow of curable sealing material from the opening to the annular sealing cavity.

4. A cap according to claim 2, wherein the interfay cavity includes a sealant reservoir arranged to receive curable sealing material from the opening and distribute it to the annular sealing cavity.

5. A cap according to claim 2, wherein the interfay cavity has an annular cross-sectional shape.

6. A cap according to claim 1, wherein the opening of the sealing material inlet is centred on a central axis of the outer cap member.

7. A cap according to claim 1, further comprising a plurality of channels formed in either an outer surface of the inner cap member or an inner surface of the outer cap member, each channel being in fluid communication with the opening of the sealing material inlet and the annular sealing cavity.

8. A cap according to claim 7 wherein either:

the channels are formed in the outer surface of the inner cap member and are separated by channels which abut the inner surface of the outer cap member;

or the channels are formed in the inner surface of the outer cap member and separated by ridges which abut the outer surface of the outer cap member.

9. A cap according to claim 7 wherein each channel has an inlet arranged to receive the flow of curable sealing material from the sealing material inlet and an outlet arranged to feed the flow of curable sealing material into the annular sealing cavity, wherein the outlets of the channels are set back in an axial direction from the edge of the annular base of the inner cap member.

10. A cap according to claim 7, wherein each channel has a width which increases as it extends towards the annular sealing cavity.

11. A cap according to claim 7, wherein each channel has a depth which decreases as it extends towards the annular sealing cavity.

12. A cap according to claim 7, wherein either:

the channels are formed in an outer surface of the inner cap member and a plurality of corresponding channels are formed in an inner surface of the inner cap member;

or the channels are formed in an inner surface of the outer cap member and a corresponding plurality of channels are formed in an outer surface of the outer cap member.

13. A cap according to claim 12, wherein either:

the inner cap member has side walls with a substantially uniform wall thickness, the channels are formed in an outer surface of the inner cap member and a plurality of corresponding channels are formed in an inner surface of the inner cap member;

or the outer cap member has side walls with a substantially uniform wall thickness, the channels are formed in an inner surface of the outer cap member and a corresponding plurality of channels are formed in an outer surface of the outer cap member.

14. A cap according to claim 1, wherein the inner cap member comprises a substantially dome-shaped portion extending from the annular base, and the outer cap member comprises a corresponding substantially dome-shaped portion extending from the annular skirt or flange.

15. A cap according to claim 1, wherein the annular skirt or flange of the outer cap member terminates at an edge, the edge of the annular skirt or flange being offset in an axial direction from the edge of the annular base of the inner cap member.

16. A cap according to claim 1, wherein the inner cap member and outer cap member are formed as separate parts.

17. A cap according to claim 1, wherein the sealing material inlet comprises a projection in the outer cap member, the projection containing the opening and being arranged to interconnect with the sealing material injection device.

18. A cap according to claim 1, further comprising a plurality of vanes between the inner face of the outer cap member and the outer face of the inner cap member.

19. A joint comprising:

a structure;

a fastener passing through the structure;

a cap according to claim 1, wherein the air cavity of the inner cap member encloses an end of the fastener and the edge of the inner cap member abuts the structure; and

sealing material filling the annular sealing cavity of the cap and contacting the structure to seal the air cavity.

20. A joint according to claim 19, wherein the structure is a structural component of an aircraft.

21. A joint according to claim 19, wherein the sealing material comprises an epoxy based adhesive.

22. A kit of parts for forming a sealed cavity around one end of a fastener, the kit including:

a cap comprising;

an inner cap member having an annular base terminating at an edge which surrounds an opening into an air cavity for enclosing the one end of a fastener;

an outer cap member having an annular skirt or flange which extends radially outwardly away from the annular base, the annular skirt or flange and annular base between them defining an annular sealing cavity; and

a sealing material inlet in fluid communication with the annular sealing cavity; and

a sealing material injection device having a nozzle arranged to interconnect with the sealing material inlet of the cap to direct a flow of curable sealing material into the annular sealing cavity.

23. A kit of parts according to claim 22, wherein the curable sealing material comprises an epoxy based adhesive.

24. A method of installing a cap to form a sealed cavity around one end of a fastener passing through a structure, the cap comprising:

an inner cap member having an annular base terminating at an edge which surrounds an opening into an air cavity for enclosing the one end of a fastener;

an outer cap member having an annular skirt or flange which extends radially outwardly away from the annular base, the annular skirt or flange and annular base between them defining an annular sealing cavity; and

a sealing material inlet comprising an opening in the outer cap member that is in fluid communication with the annular sealing cavity, the method including;

installing the cap over the one end of the fastener so that it is enclosed within the air cavity of the inner cap member and the edge of the annular base abuts the structure;

injecting curable sealing material into the annular sealing cavity via the sealing material inlet so that the curable sealing material contacts the structure; and

curing the curable sealing material to seal the air cavity.

25. A method according to claim 24, wherein the structure comprises a structural component of an aircraft.

26. A method according to claim 24, wherein the curable sealing material comprises an epoxy based adhesive.