公开(公告)号：US20100320315A1

公开(公告)日：2010-12-23

申请号：US12677380

申请日：2008-09-25

申请人： Masahiro Kashiwagi ,  Yuichiro Kamino ,  Kazuyuki Oguri ,  Takeyasu Tarumi ,  Masahiro Bessho ,  Hideo Yamakoshi ,  Naomoto Ishikawa

发明人： Masahiro Kashiwagi ,  Yuichiro Kamino ,  Kazuyuki Oguri ,  Takeyasu Tarumi ,  Masahiro Bessho ,  Hideo Yamakoshi ,  Naomoto Ishikawa

IPC分类号： B64D45/02

CPC分类号： B64D45/02 ,  F16B33/004 ,  F16B33/06 ,  F16B35/06 ,  F16B37/14

摘要： Provided is a lightning-protection fastener that is capable of reliably preventing peeling off of an insulation layer during the operation of an aircraft and of improving the anti-lightning-strike capability and reliability. There is a lightning-protection fastener that fastens a skin of an aircraft and a structural member positioned inside the skin, in which an insulation layer is melt adhered so as to cover one end surface of a head portion and also to mechanically engage with a fastener-side engagement portion (engagement portion) formed on the end surface.

摘要翻译： 本发明提供一种能够可靠地防止飞机运转时的绝缘层的剥离以及提高防雷击能力和可靠性的防雷紧固件。 存在一个防雷紧固件，其紧固飞机的外观和定位在皮肤内部的结构构件，其中绝缘层被熔化粘附以覆盖头部的一个端面并且还与紧固件机械接合 形成在端面上的侧面接合部（接合部）。

公开(公告)号：US08651413B2

公开(公告)日：2014-02-18

申请号：US12677380

申请日：2008-09-25

申请人： Masahiro Kashiwagi ,  Yuichiro Kamino ,  Kazuyuki Oguri ,  Takeyasu Tarumi ,  Masahiro Bessho ,  Hideo Yamakoshi ,  Naomoto Ishikawa

发明人： Masahiro Kashiwagi ,  Yuichiro Kamino ,  Kazuyuki Oguri ,  Takeyasu Tarumi ,  Masahiro Bessho ,  Hideo Yamakoshi ,  Naomoto Ishikawa

IPC分类号： B64D45/02 ,  B64C1/12

CPC分类号： B64D45/02 ,  F16B33/004 ,  F16B33/06 ,  F16B35/06 ,  F16B37/14

摘要： A lightning-protection fastener is provided that is capable of reliably preventing peeling off of an insulation layer during the operation of an aircraft and improving the anti-lightning-strike capability and reliability. There is a lightning-protection fastener that fastens a skin of an aircraft and a structural member positioned inside the skin, in which an insulation layer is melt adhered so as to cover one end surface of a head portion and also to mechanically engage with a fastener-side engagement portion (engagement portion) formed on the end surface.

摘要翻译： 提供一种防雷紧固件，其能够可靠地防止在飞行器的操作期间剥离绝缘层并提高防雷击能力和可靠性。 存在一个防雷紧固件，其紧固飞机的外观和定位在皮肤内部的结构构件，其中绝缘层被熔化粘附以覆盖头部的一个端面并且还与紧固件机械接合 形成在端面上的侧面接合部（接合部）。