Mounting arrangement for the pivotally openable rudder blades of a guided missile
US6202958A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Jun 15, 1999 |
| Grant date | Mar 20, 2001 |
| Priority date | — |
| Expiry date | Jun 15, 2019 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF42B10/64
- WIPO fieldOther special machines
- WIPO sectorMechanical engineering
Abstract
To maintain control accuracy for the pivotable rudder blades (14), which lie in a combustion chamber, of a guided projectile (12) which can be fired by means of propellent charge, there is provide a mounting arrangement in which the trunnions (20) of the rudder blade holders (16) of the diametrally mutually opposite rudder blades (14) are torsionally stiffly rigidly connected through an associated coupling element (32) which is limitedly resilient in the radial direction of the guided projectile (12).
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.