Lightning protection fastener and mounting method thereof
A sealant 34 filled into a cap 30 A is caused to overflow through both an opening in a first end portion 30 a of the cap 30 A and a through-hole 40 of the cap 30 A when the cap 30 A is pressed against a fastener member 25 . With regard to the cap 30 A, a ratio between inside diameter D 1 of the opening on the side of the first end portion 30 a and hole diameter D 2 of the through-hole 40 in the second end portion 30 b is set as follows: 0.10≦D 2 /D 1 ≦0.27.
1. A lightning protection fastener comprising:
a fastener member for fastening a second member to a first member which constitutes an airframe of an aircraft and the fastener member having a shaft which penetrates the first member and the second member and protrudes on a side of at least one of the first member and the second member;
a fastening member mounted on the fastener member shaft which protrudes on the side of at least one of the first member and the second member;
a cap made of an insulating material and the cap being mounted so as to cover the fastener member shaft and the fastening member; and
a sealant made of an insulating material and filled into the cap to fill any space between the cap and the fastener member and the fastening member,
wherein the cap includes an opening adapted to house the fastener member shaft and the fastening member as well as a through-hole formed in a wall surface of the cap, and
inside diameter D 1 of the cap on the side of an end portion of the opening which faces the first member or the second member and hole diameter D 2 of the through-hole are configured to satisfy 0.10≦D 2 /D 1 ≦0.27,
wherein after installation of the cap, the sealant completely fills the space between the cap and the fastener member and the fastening member, and part of the sealant spills out of the cap through the through-hole.
2. The lightning protection fastener according to claim 1 , wherein the through-hole is formed in a top of the cap or in a location closer to the top of the cap than the fastening member.
3. The lightning protection fastener according to claim 1 , wherein a tubular member extending outwardly of the cap is formed around the through-hole.
4. The lightning protection fastener according to claim 3 , wherein:
the tubular member is formed integrally with the cap; and
a groove continuous in a circumferential direction is formed at a root of the tubular member.
5. The lightning protection fastener according to claim 1 , wherein an openable and closable lid adapted to cover the through-hole is formed on the cap.
6. The lightning protection fastener according to claim 5 , wherein outside diameter of the lid is smaller than inside diameter of the through-hole, and part of the lid in a circumferential direction is integrally coupled to the cap.
7. The lightning protection fastener according to claim 2 , wherein the through-hole and a lid are formed on the top of the cap.
8. The lightning protection fastener according to claim 1 , wherein the sealant spilled out of the cap through the through-hole also constitutes the lightning protection fastener.
9. A lightning protection fastener comprising:
a fastener member for fastening a second member to a first member which constitutes an airframe of an aircraft and the fastener member having a shaft which penetrates the first member and the second member and protrudes on a side of at least one of the first member and the second member;
a fastening member mounted on the fastener member shaft which protrudes on the side of at least one of the first member and the second member;
a cap made of an insulating material and the cap being mounted so as to cover the fastener member shaft and the fastening member; and
a sealant made of an insulating material and filled into the cap to fill any space between the cap and the fastener member and the fastening member,
wherein the cap includes an opening adapted to house the fastener member shaft and the fastening member as well as a through-hole formed in a wall surface of the cap, and
wherein after installation of the cap, the sealant completely fills the space between the cap and the fastener member and the fastening member, and part of the sealant spills out of the cap through the through-hole.
10. The lightning protection fastener according to claim 9 wherein the opening and the through-hole are each configured to allow sealant to spill out of the cap during installation of the cap.
11. The lightning protection fastener according to claim 9 , wherein the sealant spilled out of the cap through the through-hole also constitutes the lightning protection fastener.
12. A lightning protection fastener comprising:
a fastener member for fastening a second member to a first member which constitutes an airframe of an aircraft and the fastener member having a shaft which penetrates the first member and the second member and protrudes on a side of at least one of the first member and the second member;
a fastening member mounted on the fastener member shaft which protrudes on the side of at least one of the first member and the second member;
a cap made of an insulating material and the cap being mounted so as to cover the fastener member shaft and the fastening member; and
a sealant made of an insulating material and filled into the cap to fill any space between the cap and the fastener member and the fastening member,
wherein the cap includes an opening adapted to house the fastener member shaft and the fastening member as well as a through-hole formed in a wall surface of the cap, and wherein an openable and closable lid adapted to cover the through-hole is formed on the cap.
13. The lightning protection fastener according to claim 12 , wherein outside diameter of the lid is smaller than inside diameter of the through-hole, and part of the lid in a circumferential direction is integrally coupled to the cap.
14. The lightning protection fastener according to claim 12 , wherein the through-hole and the lid are formed on the top of the cap.