EP 1633688 A4 20111228 - FLEXIBLE INFLATOR WITH CO-EXTRUDED PROPELLANT AND MOISTURE BARRIER AND GAS GENERATING PROPELLANT COMPOSITIONS FOR USE THEREWITH
Title (en)
FLEXIBLE INFLATOR WITH CO-EXTRUDED PROPELLANT AND MOISTURE BARRIER AND GAS GENERATING PROPELLANT COMPOSITIONS FOR USE THEREWITH
Title (de)
FLEXIBLE AUFBLASVORRICHTUNG MIT COEXTRUDIERTEM TREIBMITTEL UND FEUCHTIGKEITSBARRIERE UND GASERZEUGENDE TREIBMITTELZUSAMMENSETZUNGEN ZUR VERWENDUNG DAMIT
Title (fr)
GONFLEUR SOUPLE CONTENANT UN GAZ DE PROPULSION CO-EXTRUDE ET UN BARRIERE A L'HUMIDITE ET COMPOSITIONS DE GAZ DE PROPULSION UTILISEES AVEC LEDIT GONFLEUR
Publication
Application
Priority
- US 2004015756 W 20040520
- US 44469003 A 20030523
- US 44476603 A 20030523
Abstract (en)
[origin: WO2005014507A2] A flexible inflator for an inflation assembly and related gas generating propellant compositions are provided. The flexible inflator includes at least one elongated strand of a propellant co-extruded with a moisture barrier. The propellant compositions are adapted for co-extrusion with a plastic sheath which forms the moisture barrier surrounding the propellant and include a binder fuel component effective to render the composition flexible and to impart sufficient adhesive properties such that the propellant composition and the plastic sheath adhere together, and an oxidizer.
IPC 8 full level
C06B 21/00 (2006.01); B60R 21/264 (2006.01); C06B 45/10 (2006.01); C06C 9/00 (2006.01); C06D 5/06 (2006.01); B60R 21/213 (2011.01)
CPC (source: EP KR)
B60R 21/16 (2013.01 - KR); B60R 21/2646 (2013.01 - EP); C06B 21/0075 (2013.01 - EP KR); C06B 21/0083 (2013.01 - EP KR); C06B 27/00 (2013.01 - KR); C06B 45/10 (2013.01 - EP); C06C 9/00 (2013.01 - EP); C06D 5/06 (2013.01 - EP KR); B60R 21/213 (2013.01 - EP)
Citation (search report)
- [XYI] EP 1205459 A1 20020515 - DAICEL CHEM [JP]
- [Y] WO 0108937 A1 20010208 - AUTOLIV DEV [SE], et al
- [Y] DE 3932576 A1 19910418 - DORNIER GMBH [DE]
- [Y] DE 20207861 U1 20020926 - TRW AIRBAG SYS GMBH & CO KG [DE]
- [Y] EP 0995645 A2 20000426 - OEA INC [US]
- [Y] WO 0032447 A1 20000608 - TAKATA RESTRAINT SYSTEMS INC [US]
- [Y] GB 1582903 A 19810114 - DU PONT
- [Y] US 5540155 A 19960730 - HILL ROBERT O [ZA]
- [Y] WO 02097359 A2 20021205 - UNIVERSAL PROPULSION CO [US]
- [T] WO 2004100177 A2 20041118 - DYNO NOBEL INC [US], et al
- [Y] DE 20207862 U1 20020926 - TRW AIRBAG SYS GMBH & CO KG [DE]
- [Y] US 5212341 A 19930518 - OSBORNE ALFRED M [US], et al
- [Y] WO 0119757 A2 20010322 - AUTOMOTIVE SYSTEMS LAB [US]
- See references of WO 2005014507A2
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IT LI LU MC NL PL PT RO SE SI SK TR
Designated extension state (EPC)
AL MK
DOCDB simple family (publication)
WO 2005014507 A2 20050217; WO 2005014507 A3 20060511; EP 1633688 A2 20060315; EP 1633688 A4 20111228; JP 2007525355 A 20070906; JP 4723485 B2 20110713; KR 101083499 B1 20111116; KR 20060021321 A 20060307
DOCDB simple family (application)
US 2004015756 W 20040520; EP 04776047 A 20040520; JP 2006514900 A 20040520; KR 20057022260 A 20040520