CPC F42B10/12
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CPC F42B10/12 is a category of patents about Stabilising fins on projectiles which can slide longitudinally[1][2]
Nearby category tree:
- CPC F42B10/00 Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, selecting range, or delaying the fall (Note: "CPC F42B6/00 takes precedence" (? clarify -- that means B6 should be used if possible and if so this one is a minor add-on?))
- CPC F42B10/02 Stabilising arrangements on projectiles
- CPC F42B10/12 Stabilising arrangements using fins longitudinally-slidable with respect to the projectile or missile
- CPC F42B10/14 Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- CPC F42B10/16 Wrap-around fins
- CPC F42B10/02 Stabilising arrangements on projectiles
References
- ↑ CPC F42B10/12 element at Espacenet web site
- ↑ CPC F42B10/12 element listed at USPTO
This wiki has 3 patents in category "CPC F42B10/12".
Patents in category CPC F42B10/12
- Patent US-1857-18824 (English title: Cushion for wings of bomb-lances, Inventors: Nathan Scholfield)
- Patent US-1857-17173 (English title: Improvement in bomb-lances, Inventors: Rufus Sibley)
- Patent US-1912-1049144 (English title: Projectile, Inventors: Rasmus Hagbarth Quisling, Filing date: 1911-08-07)
| Enclosing categories | CPC F42B10/02 |
|---|---|
| Subcategories | |
| Keywords | Projectiles, Stability |
| Start year | |
| End year |
