F - Mech Eng,Light,Heat,Weapons – 42 – B
Patent
F - Mech Eng,Light,Heat,Weapons
42
B
F42B 10/38 (2006.01) F42B 10/14 (2006.01) F42B 10/40 (2006.01) F42B 15/10 (2006.01)
Patent
CA 2419747
The present invention relates to an artillery missile (1) intended for firing on a ballistic trajectory, with gliding characteristics which can be put into effect, after it has reached the summit of this trajectory, to increase the maximum range of the missile. In order to obtain these gliding characteristics, the missile is provided with extendable aerodynamic bearing surfaces divided into firstly canard fins (5-8), which are retracted in the front part of the missile body and can be extended after the summit of trajectory, secondly main bearing surfaces (9, 10) made of resilient material, which, likewise during launching, are curved in against and around the central part (3) of the missile body in shallow recesses adapted thereto in the outer casing of the missile and which, after the summit of trajectory and being extended, form the wings (9, 10) of the missile, and thirdly stern fins, which, durign at least launching, are covered i the retracted position by a protective cover (14) in the rear part (4) of the missile.
La présente invention concerne un missile d'artillerie (1) devant être lancé sur une trajectoire balistique, avec des caractéristiques de vol plané qui agissent lorsque l'engin atteint le point culminant de sa trajectoire, de manière à augmenter la portée maximale du missile. Les caractéristiques de vol plané du missile sont dues aux surfaces portantes aérodynamiques déployables comprenant des ailerons canard (5-8) qui sont repliés dans la partie avant du corps du missile et qui se déploient lorsque celui-ci atteint le point culminant de sa trajectoire; des surfaces portantes principales courbes (9, 10) faites en matériau souple, qui, de même, pendant le lancement, sont rabattues contre la partie centrale du corps du missile (3) dans des évidements, et qui, une fois le point culminant de la trajectoire atteint, se déploient et forment les ailes (9, 10) du missile; et enfin, des ailerons arrière, qui au moins pendant le lancement, sont recouverts en position repliée par un couvercle (14) dans la partie arrière (4) du missile.
Bofors Defence Ab
Fetherstonhaugh & Co.
LandOfFree
Guided artillery missile with extremely long range does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Guided artillery missile with extremely long range, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Guided artillery missile with extremely long range will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1534956