초록 ▼

A multiple barrel launcher for simultaneous launching of a number of projectiles by means of gas generated by a propellant charge placed in a pressure cartridge in communication with said barrels via a pressure chamber, wherein the communication comprises channels between each of the barrels and the

A multiple barrel launcher for simultaneous launching of a number of projectiles by means of gas generated by a propellant charge placed in a pressure cartridge in communication with said barrels via a pressure chamber, wherein the communication comprises channels between each of the barrels and the pressure chamber, each of these channels being so dimensioned in relation to the charge that a critical driving gas flow velocity is obtained during the launching course.

대표청구항 ▼

Apparatus for launChing a plurality of projectiles, comprising a. a cavity having bottom, side and top wall portions; b. a receptacle in communication with the cavity for receiving a cartridge providing on its explosion a gas pressure in the cavity; c. a plurality of barrels for receiving projectile

Apparatus for launChing a plurality of projectiles, comprising a. a cavity having bottom, side and top wall portions; b. a receptacle in communication with the cavity for receiving a cartridge providing on its explosion a gas pressure in the cavity; c. a plurality of barrels for receiving projectiles, the barrels being mounted on the top wall portion of the cavity in proximity to one another, at least one of the barrels having an elevation which differs from the elevation of at least one other barrel; d. a plurality of channels extending through the top wall portion, each channel connecting one of the barrels with the cavity and forming flow paths for said gas pressure from the cavity to the barrels for propelling said projectiles out of the barrels, at least one of the channels having a cross-sectional area which differs from the cross-sectional area of at least one other channel; e. the cross-sectional area of each of the channels being substantially smaller than that of the respective barrel associated therewith, thereby causing the gas flow from the cavity into each barrel to reach critical velocity during at least part of the launching course.