EP 0229086 B1 19891220 - FUSE FOR PROJECTILE
Title (en)
FUSE FOR PROJECTILE
Publication
Application
Priority
CH 302485 A 19850712
Abstract (en)
[origin: WO8700616A1] The rocket comprises a detonator-carrier rotor pivotingly mounted on a body (1) by means of a shaft (15) and susceptible of pivoting from an inactive position to an active position. An exhaust time delay device (26) enables to brake the rotation of the rotor and comprises a multiplier gear train (27) carried by two platens (36) and co-operating with a rock lever (28). The rotor is integral with a toothed sector (29) in mesh with the time delay device (26). The platens (36) are pivotingly mounted on bearings (14) of the shaft (13), thereby enabling an angular displacement of the time delay device (26) about said shaft to enable an adjustment of the angular meshing distance of the toothed sector (29) with the time delay device (26) and, therefore, an adjustment of the time duration of the passage from the safety position of the rotor to the cocked position. The safety distance of the mouth may thus be adjusted by a low cost and safe device.
IPC 1-7
IPC 8 full level
F42C 15/192 (2006.01)
CPC (source: EP US)
F42C 15/192 (2013.01 - EP US)
Citation (examination)
FR 2474687 A1 19810731 - MEFINA SA [CH]
Designated contracting state (EPC)
AT DE FR GB IT NL SE
DOCDB simple family (publication)
WO 8700616 A1 19870129; CA 1267566 A 19900410; CH 663875G A3 19880129; DE 3667729 D1 19900125; EP 0229086 A1 19870722; EP 0229086 B1 19891220; ES 555935 A0 19871016; ES 8800423 A1 19871016; FI 871055 A0 19870311; FI 871055 A 19870311; FI 89981 B 19930831; FI 89981 C 19931210; US 4739706 A 19880426
DOCDB simple family (application)
CH 8600085 W 19860612; CA 510851 A 19860604; CH 302485 A 19850712; DE 3667729 T 19860612; EP 86903192 A 19860612; ES 555935 A 19860611; FI 871055 A 19870311; US 4107587 A 19870312