Global Patent Index - EP 0013096 B1

EP 0013096 B1 19830413 - DEPLOYABLE WING MECHANISM

Title (en)

DEPLOYABLE WING MECHANISM

Publication

EP 0013096 B1 19830413 (EN)

Application

EP 79302854 A 19791211

Priority

AU PD723878 A 19781229

Abstract (en)

[origin: EP0013096A1] A deployable wing assembly using an inner wing segment (5) and an outer wing segment (7) with the inner wing segment hinged longitudinally to the body of a missile, or the like, and with the outer wing segment hinged by a pin (8) perpendicular to the surface of the wing segment at the junction, and including deploying means and locking means for both sections.

IPC 1-7

F42B 13/32; B64C 3/56

IPC 8 full level

B64C 3/56 (2006.01); F42B 10/14 (2006.01)

CPC (source: EP)

F42B 10/14 (2013.01)

Citation (examination)

Designated contracting state (EPC)

CH DE FR GB IT NL SE

DOCDB simple family (publication)

EP 0013096 A1 19800709; EP 0013096 B1 19830413; AU 524255 B2 19820909; AU 5387979 A 19800703; CA 1113070 A 19811124; DE 2965231 D1 19830519; JP S5592900 A 19800714

DOCDB simple family (application)

EP 79302854 A 19791211; AU 5387979 A 19781229; CA 341765 A 19791212; DE 2965231 T 19791211; JP 17390579 A 19791228