CPC F42B10/26
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CPC F42B10/26 is a patent category for arrangements to stabilize a projectile in flight by spinning it.[1][2]
Category tree enclosing it:[1]
- CPC F42B10/00 Means for influencing aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding (CPC F42B6/00 takes precedence)
- CPC F42B10/02 Stabilising arrangements
- CPC F42B10/26 using spin (CPC F42B10/04, CPC F42B10/12, CPC F42B10/14, CPC F42B10/24, CPC F42B14/02 take precedence)
- CPC F42B10/28 induced by gas action
- CPC F42B10/30 using rocket motor nozzles
- CPC F42B10/28 induced by gas action
- CPC F42B10/26 using spin (CPC F42B10/04, CPC F42B10/12, CPC F42B10/14, CPC F42B10/24, CPC F42B14/02 take precedence)
- CPC F42B10/02 Stabilising arrangements
References
- ↑ 1.0 1.1 CPC F42B10/26 element at Espacenet web site
- ↑ CPC F42B10/26 element listed at USPTO
This wiki has 2 patents in category "CPC F42B10/26". Other techtypes related to CPC F42B10/26: USPC 244/3.23
Patents in category CPC F42B10/26
- Patent US-1890-463922 (English title: Projectile, Inventors: Philip G. Russell, Filing date: 1890-12-27)
- Patent FR-1909-406375 (English title: Advanced shell projectile, Inventors: Heinrich Brust, Filing date: 1909-08-21)
| Enclosing categories | CPC F42B10/02 |
|---|---|
| Subcategories | |
| Keywords | Projectiles, Stability |
| Start year | |
| End year |
