LIGHTNING-RESISTANT FASTENER AND MOUNTING STRUCTURE OF LIGHTNING-RESISTANT FASTENER
First Claim
Patent Images
1. A lightning-resistant fastener comprising:
- a fastener member used for fastening a second member to a first member constituting an airframe of an aircraft, the fastener member being made of a conductive material; and
a cap installed so as to cover the fastener member projecting to the interior side of the airframe, the cap being made of an insulating material, whereinthe fastener member has an engaging part in a portion projecting to the interior side of the airframe,the cap has an engaged part to be engaged with the engaging part of the fastener member in a central portion of the inner peripheral surface of the cap, the cap being installed to the fastener member with the engaged part being engaged with the engaging part of the fastener member, a tip end part of the cap opposite to the engaged part abutting against the second member, and a gap being provided between the fastener member and a portion of the cap other than the engaged part, andan elastically deformable part is provided to allow the cap to be elastically deformed in the direction to compress the cap between the engaged part and the tip end part abutting against the second member while the engaged part is engaged with the engaging part.
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Accused Products
Abstract
To provide a lightning-resistant fastener capable of assuring a sufficient lightning-resistant performance. A cap 30A has an elastically deformable part 50 continuous in the circumferential direction thereof. The elastically deformable part 50 has a smaller thickness than the other parts of the cap 30A in a circumferentially continuous area thereof. Since the cap 30A has the elastically deformable part 50, even if a surface 22b of a member 22 is inclined with respect to a plane perpendicular to the axis of a fastener main body 25, the cap 30A can be installed without forming a gap.
27 Citations
9 Claims
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1. A lightning-resistant fastener comprising:
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a fastener member used for fastening a second member to a first member constituting an airframe of an aircraft, the fastener member being made of a conductive material; and a cap installed so as to cover the fastener member projecting to the interior side of the airframe, the cap being made of an insulating material, wherein the fastener member has an engaging part in a portion projecting to the interior side of the airframe, the cap has an engaged part to be engaged with the engaging part of the fastener member in a central portion of the inner peripheral surface of the cap, the cap being installed to the fastener member with the engaged part being engaged with the engaging part of the fastener member, a tip end part of the cap opposite to the engaged part abutting against the second member, and a gap being provided between the fastener member and a portion of the cap other than the engaged part, and an elastically deformable part is provided to allow the cap to be elastically deformed in the direction to compress the cap between the engaged part and the tip end part abutting against the second member while the engaged part is engaged with the engaging part. - View Dependent Claims (2, 3)
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4. A structure for mounting a lightning-resistant fastener comprising:
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a fastener member used for fastening a second member to a first member constituting an airframe of an aircraft, the fastener member being made of a conductive material; and a cap having one open end opening at one end and installed so as to cover the fastener member projecting to the interior side of the airframe, the cap being made of an insulating material, wherein a recess is formed in a surface of the second member, and the cap is installed with the open end being housed in the recess formed in the second member. - View Dependent Claims (5, 6, 7, 8, 9)
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Specification