Patent · US Active

Thermally deployable shroud for affordable precision guided projectile

US10030952B1 · kind B1 · utility

1Cited by
3References
11Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 30, 2017
Grant dateJul 24, 2018
Priority date
Expiry dateMar 30, 2037

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF42B10/46
  • WIPO fieldOther special machines
  • WIPO sectorMechanical engineering

Abstract

A deployable shroud provides an aerodynamically smooth surface to minimize the drag otherwise experienced by blunt nose projectiles. The shroud comprises multiple petals mounted at the nose of the projectile that are released at a set time during flight. The deployment mechanism assembly of the shroud provides deployment of the petals without the generation of shock waves into the projectile and comprises a fusible link powered by a thermal source. The shroud assembly is self-powered and does not require energy input from the projectile.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.