GB9807198D0
(en)
|
1998-04-04 |
1998-06-03 |
British Aerospace |
Adhesively bonded joints in carbon fibre composite structures
|
ES2163951B1
(es)
*
|
1998-07-29 |
2003-05-16 |
Airbus Espana Sl |
Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones.
|
ES2162718A1
(es)
*
|
1998-07-29 |
2002-01-01 |
Const Aeronauticas Sa |
Un sistema de proteccion contra descargas electricas, especialmente rayos, de componentes estructurales de aviones.
|
US7223312B2
(en)
*
|
2000-09-21 |
2007-05-29 |
Integument Technologies, Inc. |
Methods and materials for reducing damage from environmental electromagnetic effects
|
US20020081921A1
(en)
*
|
2000-09-21 |
2002-06-27 |
Vargo Terrence G. |
Methods and materials for reducing damage from environmental electromagnetic effects
|
US6679667B2
(en)
*
|
2001-02-28 |
2004-01-20 |
Northrop Grumman Corporation |
Hot melt fastener filler
|
GB0117805D0
(en)
*
|
2001-07-21 |
2001-09-12 |
Bae Systems Plc |
A method of securing composite elements together
|
FR2830236B1
(fr)
*
|
2001-10-02 |
2004-02-27 |
Airbus France |
Dispositif de fixation d'un pare-brise d'aeronef
|
DE10200564B4
(de)
*
|
2002-01-09 |
2007-08-09 |
Eads Deutschland Gmbh |
Blitzschutzeinrichtung an faserverstärkten Bauteilen für mittels lösbaren Bolzenverbindungen entfernbare Verschluss-Deckel
|
DE602004002482T2
(de)
|
2003-05-30 |
2007-02-01 |
Bae Systems Plc |
Verbundstruktur-blitzschlagschutz
|
ES2264299B1
(es)
*
|
2003-06-06 |
2007-11-16 |
Airbus España S.L. |
Sistema de proteccion contra rayos para depositos de combustible fabricados en materiales compuestos de pobre conductividad electrica.
|
EP1544099B1
(de)
*
|
2003-12-18 |
2009-01-07 |
Airbus UK Limited |
Verfahren zum Verbinden von Flugzeugstrukturbauteilen
|
GB0329373D0
(en)
|
2003-12-18 |
2004-01-21 |
Airbus Uk Ltd |
Method of joining structural elements in an aircraft
|
FR2873347B1
(fr)
*
|
2004-07-22 |
2006-11-17 |
Airbus France Sas |
Dispositif d'eclissage d'elements de structure composite avec des elements de structure metallique
|
GB0417472D0
(en)
*
|
2004-08-05 |
2004-09-08 |
Airbus Uk Ltd |
Fuel tank system
|
US8231751B2
(en)
*
|
2005-09-06 |
2012-07-31 |
The Boeing Company |
Repair technique for lightning strike protection
|
US7686905B2
(en)
|
2005-09-06 |
2010-03-30 |
The Boeing Company |
Copper grid repair technique for lightning strike protection
|
US8246770B2
(en)
|
2005-09-06 |
2012-08-21 |
The Boeing Company |
Copper grid repair technique for lightning strike protection
|
JP4786426B2
(ja)
*
|
2005-10-06 |
2011-10-05 |
三菱重工業株式会社 |
ファスナ
|
US20070137032A1
(en)
*
|
2005-12-15 |
2007-06-21 |
Braden Stephen M |
Ground stud installation on composite structure for electrostatic charges
|
US7886439B2
(en)
|
2005-12-15 |
2011-02-15 |
The Boeing Company |
Ground stud installation on composite structures for electrostatic charges
|
US7277266B1
(en)
|
2006-03-29 |
2007-10-02 |
The Boeing Company |
Lightning protection system for composite structure
|
US20080003078A1
(en)
*
|
2006-05-02 |
2008-01-03 |
United Technologies Corporation |
Fastener
|
GB0609166D0
(en)
*
|
2006-05-09 |
2006-06-21 |
Airbus Uk Ltd |
Apparatus for and method of inhibiting delamination
|
EP2028100B1
(de)
*
|
2006-06-09 |
2013-05-15 |
Mitsubishi Heavy Industries, Ltd. |
Befestigungselement
|
JP4657194B2
(ja)
*
|
2006-11-20 |
2011-03-23 |
本田技研工業株式会社 |
前縁スキンの段差調整構造および前縁スキンの組付方法
|
US7898785B2
(en)
*
|
2006-12-07 |
2011-03-01 |
The Boeing Company |
Lightning protection system for an aircraft composite structure
|
US7599164B2
(en)
*
|
2006-12-07 |
2009-10-06 |
The Boeing Company |
Lightning protection system for aircraft composite structure
|
US7738236B2
(en)
*
|
2007-01-12 |
2010-06-15 |
The Boeing Company |
Light weight system for lightning protection of nonconductive aircraft panels
|
DE102007003276B4
(de)
|
2007-01-23 |
2013-11-28 |
Airbus Operations Gmbh |
Luft- und Raumfahrzeug mit einem CFK-Bauteil und einem Metallbauteil, wobei das CFK-Bauteil und das Metallbauteil über wenigstens ein Verbindungselement mit einem Verbindungsabschnitt miteinander verbunden sind
|
JP2008285115A
(ja)
*
|
2007-05-21 |
2008-11-27 |
Mitsubishi Heavy Ind Ltd |
航空機組立品およびその製造方法
|
US7934676B2
(en)
*
|
2007-06-28 |
2011-05-03 |
The Boeing Company |
Pre-fabricated article for EME protection of an aircraft
|
US7883050B2
(en)
*
|
2007-06-28 |
2011-02-08 |
The Boeing Company |
Composites with integrated multi-functional circuits
|
US8398027B2
(en)
*
|
2007-09-17 |
2013-03-19 |
The Boeing Company |
Method and apparatus for reinforcing composite structures
|
JP4719203B2
(ja)
*
|
2007-09-28 |
2011-07-06 |
三菱重工業株式会社 |
耐雷ファスナ
|
US7835130B2
(en)
|
2007-10-05 |
2010-11-16 |
The Boeing Company |
Method and apparatus for lightning protection of a composite structure
|
US20090092764A1
(en)
*
|
2007-10-05 |
2009-04-09 |
Hoeckelman Leslie A |
Method and apparatus for simultaneous spray and cure initiation of curable polymer coating compositions
|
US7721996B2
(en)
*
|
2007-11-13 |
2010-05-25 |
The Boeing Company |
Fabrication and installation of preformed dielectric inserts for lightning strike protection
|
FR2924685B1
(fr)
*
|
2007-12-11 |
2010-03-19 |
Airbus France |
Systeme parafoudre et aeronef comportant un tel systeme.
|
FR2924686B1
(fr)
*
|
2007-12-11 |
2010-05-14 |
Airbus France |
Systeme parafoudre et aeronef comportant un tel systeme.
|
JP5055178B2
(ja)
|
2008-03-24 |
2012-10-24 |
三菱重工業株式会社 |
航空機組立品
|
FR2932456B1
(fr)
*
|
2008-06-17 |
2010-05-28 |
Airbus France |
Systeme de drainage d'un courant de foudre genere par une decharge orageuse sur un aeronef
|
GB0819159D0
(en)
*
|
2008-10-20 |
2008-11-26 |
Airbus Uk Ltd |
Joint between aircraft components
|
ES2376323B1
(es)
*
|
2009-02-27 |
2013-01-24 |
Airbus Operations, S.L. |
Mejora de la protección contra impacto directo de rayos en zonas remachadas de paneles en cfrp.
|
JP5237170B2
(ja)
*
|
2009-03-30 |
2013-07-17 |
三菱重工業株式会社 |
複合材タンク、翼、および、複合材タンクの製造方法
|
KR20120046164A
(ko)
*
|
2009-06-12 |
2012-05-09 |
로오드 코포레이션 |
벼락으로부터 기판을 보호하는 방법
|
US9821538B1
(en)
|
2009-06-22 |
2017-11-21 |
The Boeing Company |
Ribbed caul plate for attaching a strip to a panel structure and method for use
|
US8282042B2
(en)
|
2009-06-22 |
2012-10-09 |
The Boeing Company |
Skin panel joint for improved airflow
|
EP2455286B1
(de)
|
2010-11-22 |
2016-09-28 |
Airbus Defence and Space SA |
Blitzschutz für Flugzeugverbundstrukturen
|
US20120201999A1
(en)
*
|
2011-02-08 |
2012-08-09 |
Woods Mark A |
Methods and apparatus for mechanically joining metal components and composite components
|
JP5535956B2
(ja)
*
|
2011-02-14 |
2014-07-02 |
三菱重工業株式会社 |
耐雷ファスナ
|
WO2013084308A1
(ja)
*
|
2011-12-07 |
2013-06-13 |
株式会社Ihi |
取付用ボスおよびファンケース
|
US9481012B2
(en)
*
|
2012-05-23 |
2016-11-01 |
The Boeing Company |
Method of filling voids around countersunk fastener heads
|
US9739402B2
(en)
|
2013-03-04 |
2017-08-22 |
Eaton Corporation |
Electrically conductive seals for fluid conveyance systems
|
EP2799220B1
(de)
*
|
2013-04-30 |
2020-06-17 |
Airbus Operations S.L. |
Verbundstruktur für ein Flugzeug und Herstellungsverfahren dafür
|
US20140331477A1
(en)
*
|
2013-05-07 |
2014-11-13 |
The Boeing Company |
Flush fastener design and installation
|
US9908637B2
(en)
|
2014-05-23 |
2018-03-06 |
The Boeing Company |
Modified shank fasteners for electromagnetic effect (EME) technology
|
US20160229552A1
(en)
*
|
2015-02-05 |
2016-08-11 |
The Boeing Company |
Intermetallic and composite metallic gap filler
|
US10457411B2
(en)
*
|
2016-06-17 |
2019-10-29 |
Goodrich Corporation |
Lightning strike dispersion for composite aircraft structures
|
US11572195B2
(en)
|
2018-07-26 |
2023-02-07 |
Honeywell International Inc. |
Lightning-dissipative aircraft assemblies and valve frames utilized in the same
|
JP2020034144A
(ja)
*
|
2018-08-31 |
2020-03-05 |
川崎重工業株式会社 |
シール構造
|
US11137014B2
(en)
|
2019-01-08 |
2021-10-05 |
The Boeing Company |
Conductive fastening system and method for improved EME performance
|
CN114180083B
(zh)
*
|
2021-11-19 |
2023-09-01 |
中国直升机设计研究所 |
一种利用铜杯实现的复合材料结构件之间导电处理方法
|