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AERODYNAMIC FIN OF JET PROJECTILE

机译:射流弹的气动鳍

摘要

FIELD: rocketry, in particular, aerodynamic fins of jet projectiles.;SUBSTANCE: the aerodynamic fin has a fairing with grooves. Foldable bent blades are placed in the fairing. The blades are made in the form of plates with a trapezoid cross-section. The blades are bent in radius making up 0.4-0.5 of the projectile caliber on a section equal to 0.6-0.8 of the blade height. The blade base thickness-to-its end thickness ratio makes up 1.8-2.0. The number of the supporting surfaces and engageable springs makes up at least two per blades.;EFFECT: completely eliminated instability of projectile flight and enhanced range and close grouping of fire.;3 dwg
机译:领域:火箭技术,尤其是喷气射弹的气动鳍。;实质:气动鳍具有带有凹槽的整流罩。可折叠的弯曲刀片放置在整流罩中。叶片以具有梯形横截面的板的形式制成。叶片在等于叶片高度0.6-0.8的截面上弯曲半径,构成弹丸口径的0.4-0.5。叶片基部厚度与端部厚度之比为1.8-2.0。每个叶片至少有两个支撑表面和可接合的弹簧;效果:完全消除了弹丸飞行的不稳定性和扩大的射程和近距离的火力; 3 dwg

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