ATE467807T1
Deployment mechanism for stowable fins in missiles
Abstract
A deployment mechanism ( 414 ) in combination with a missile ( 10 ), guided projectile ( 410 ) or other ordnance that automatically pivots and rotates a fin ( 412 ) from a stowed orientation to a deployed orientation. The deployment mechanism ( 414 ) includes a tubular cam ( 434 ) having a retention mechanism ( 455 ) that retains the fin ( 412 ) simply and reliably in the stowed orientation. The tubular cam also guides the fin ( 412 ) quickly to the deployed orientation.
Term
Term ended
Projected expiry passed 14 March 2023, 3.5 years ago.
- Priority
- Filed
- Published
- Projected expiry
- Today
13 members in 7 offices
Priority claims2
| Document | Office | Kind | Date |
|---|---|---|---|
| 10203202 | United States of America | A | |
| 0307931 | United States of America | W |
Members13
| Document | Office | Kind | |
|---|---|---|---|
| US2003178527A1 | United States of America | A1 | |
| WO03081165A1 | World Intellectual Property Organization (WIPO) | A1 | |
| AU2003220289A1 | Australia | A1 | |
| US6761331B2 | United States of America | B2 | |
| US2004144888A1 | United States of America | A1 | |
| EP1485668A1 | European Patent Office (EPO) | A1 | |
| US6905093B2 | United States of America | B2 | |
| RU2004130842A | Russian Federation | A | |
| RU2320952C2 | Russian Federation | C2 | |
| EP1485668B1 | European Patent Office (EPO) | B1 | |
| AT467807T | Austria | T | |
| ATE467807T1This record | Austria | T1 | |
| DE60332526D1 | Germany | D1 |
1 legal event, as the office reported them to INPADOC
Events
| Event | Code | |
|---|---|---|
| Publication of translation of european patent specificationUEP | UEP |
Numbers
- Application
- 3716587
Titles2
- German
- MECHANISMUS ZUM AUSKLAPPEN VON VERSTAUBAREN FLOSSEN AN FLUGKÖRPERN
- English
- MECHANISM FOR FOLDING OUT STOWABLE FINS ON MISSILES
Classification
- CPC, 1
- F42B10/14
- IPC, 2
- F42B10 14
- F42B10 60