AT92184B - Device to give projectiles lateral rotations during their flight. - Google Patents
Device to give projectiles lateral rotations during their flight.Info
- Publication number
- AT92184B AT92184B AT92184DA AT92184B AT 92184 B AT92184 B AT 92184B AT 92184D A AT92184D A AT 92184DA AT 92184 B AT92184 B AT 92184B
- Authority
- AT
- Austria
- Prior art keywords
- flight
- projectiles
- give
- rotations during
- lateral rotations
- Prior art date
Links
Landscapes
- Toys (AREA)
Description
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seines Fluges Querdrehung zu erteilen.
PATENT-ANSPRÜCHE :
1. Einrichtung, um Geschossen während ihres Fluges Querdrehungen zu erteilen. dadurch gekennzeichnet, dass der Boden (1, 1') des Geschosses so ausgestaltet ist, dass beim Austritt des Geschosses aus dem Lauf die Treibgase eine Schiefstellung der Geschosslängsachse und dadurch eine Querdrehung um eine senkrecht zur Geschosslängsachse liegende Querachse bewirken.
2. Einrichtung, um Geschossen während ihres Fluges Querdrehungen zu erteilen, dadurch gekennzeichnet, dass die Mündung des Laufes (10) so ausgestaltet ist. dass beim Austritt des Geschosses aus dem Lauf die Treibgase eine Schiefstellung der Geschosslängsachse und dadurch eine Querdrehung um eine senkrecht zur Geschossngsachse liegende Querachse verursachen.
3. Einrichtung, um Geschossen während ihres Fluges Querdrehungen zu erteilen, dadurch gekennzeichnet, dass der Lauf (10) der Waffe vor seiner Mündung mit einer seitlichen Öffnung (14) versehen ist,
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to give lateral rotation to his flight.
PATENT CLAIMS:
1. Device to give projectiles lateral rotations during their flight. characterized in that the bottom (1, 1 ') of the projectile is designed so that when the projectile emerges from the barrel, the propellant gases cause the projectile's longitudinal axis to be inclined and thereby cause it to rotate transversely about a transverse axis perpendicular to the longitudinal axis of the projectile.
2. Device for giving projectiles transverse rotations during their flight, characterized in that the mouth of the barrel (10) is designed. that when the bullet emerges from the barrel, the propellant gases cause the longitudinal axis of the bullet to be inclined and thereby cause a transverse rotation about a transverse axis perpendicular to the bullet axis.
3. Device for giving projectiles transverse rotations during their flight, characterized in that the barrel (10) of the weapon is provided with a lateral opening (14) in front of its muzzle,
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Claims (1)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CS92184X | 1919-06-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
AT92184B true AT92184B (en) | 1923-04-10 |
Family
ID=5443323
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT92184D AT92184B (en) | 1919-06-18 | 1920-09-02 | Device to give projectiles lateral rotations during their flight. |
Country Status (1)
Country | Link |
---|---|
AT (1) | AT92184B (en) |
-
1920
- 1920-09-02 AT AT92184D patent/AT92184B/en active
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