EP 1628112 A1 20060222 - Wing arrangement
Title (en)
Wing arrangement
Title (de)
Flügelanordnung
Title (fr)
Disposition d'ailettes
Publication
Application
Priority
DE 102004039770 A 20040816
Abstract (en)
The wing arrangement (10) for a missile comprises two wing elements, the first (12) of which is fastened on the missile by a hinge connection (24) to swing out along the missile's longitudinal axis, and the second (14) connected to the first wing element in such a way that it is pivotable around an axis which is perpendicular to the longitudinal axis of the first wing element. The second wing element is pivotable at least partially in an inner cavity of the first wing element.
IPC 8 full level
F42B 10/16 (2006.01); B64C 3/42 (2006.01)
IPC 8 main group level
B64C (2006.01)
CPC (source: EP)
F42B 10/16 (2013.01)
Citation (applicant)
US 4667899 A 19870526 - WEDERTZ LARRY D [US]
Citation (search report)
- [XY] DE 1199664 B 19650826 - DYNAMIT NOBEL AG
- [DY] US 4667899 A 19870526 - WEDERTZ LARRY D [US]
- [A] US 4778127 A 19881018 - DUCHESNEAU JEROME G [US]
- [A] US 4635881 A 19870113 - BRIESECK BERND [DE], et al
- [A] US 3633846 A 19720111 - BIGGS LAWRENCE M JR
Designated contracting state (EPC)
DE FR GB IT
DOCDB simple family (publication)
EP 1628112 A1 20060222; DE 102004039770 A1 20060302; NO 20053824 D0 20050815; NO 20053824 L 20060217
DOCDB simple family (application)
EP 05016830 A 20050803; DE 102004039770 A 20040816; NO 20053824 A 20050815