A projectile that is free of yaw angle
CA 1339565 C · Owner: Wiemer, Peter · Inventors: Grosswendt, Werner; Wiemer, Peter
Overview
Its claims, description and drawings are in the Canadian Patents Database.
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Abstract From the Canadian patent
In a fin-stabilized projectile (I) of a weapon used to, engage a tank (2) from above, the target end phase of the flight is initiated by a force on the nose of the missile body in, particular on the control unit that is located therein. Because of the fact that the control unit (4) is rotating because of a target-detection sensor, during this rotary movement the projectile oscillates because of the gyroscopic effect and thus there are target deviations at different combat ranges. In order to avoid the yaw angle and lateral deflections of the projectile that occur in the rotational-descent phase, within the projectile (I) between the control unit (4) and a warhead (3) there are means that …
Read the whole patent
Listed from its CIPO record in Patent Yard's archive of Canadian patents past their term. Its claims, description and drawings are in the CIPO record and on Google Patents.
Why it's free to use
- Granted December 2, 1997. A Canadian patent filed before October 1, 1989 lasted 17 years from grant, so its term ended December 2, 2014.
- We check Canadian rights only. A patent in its family in another country could still be in force: check its family on Google Patents.
Timeline
Timeline From CIPO dates
Sources & verification
Official CIPO records
Everything on this page comes from the CIPO record linked above. Contains information licensed under the Open Government Licence – Canada.