2results about "Ventillation systems" patented technology

The utility model relates to the field of ammunition launching, in particular to a heat dissipation protective shell for an ammunition locking device seat, which comprises a protective shell, the radiator is installed on the left side of the protective shell, the cooling fan is arranged in the radiator, the cooling fins are arranged at the positions, corresponding to the cooling fan, of the left side of the interior of the protective shell, and the cooling fins are arranged on the left side of the interior of the protective shell. The right end of the cooling fan penetrates through the radiator and the protective shell to be connected with the left sides of the cooling fins, and a limiting sleeve is arranged on the right side in the protective shell. According to the utility model, the heat dissipation protection assembly is arranged, so that the bullet locking device seat in the protection shell can be quickly cooled and dissipated, and the problems that the follow-up use of the bullet locking device seat is influenced by high temperature generated by high-speed friction after ammunition is launched due to the lack of the heat dissipation protection assembly of a common bullet locking device seat, and the service life of the bullet locking device seat is influenced are solved. And the service life of the bullet locking device seat is shortened.

Modular Munition Launching Device Including a Pyrotechnic Jet Mitigation Device for Munitions. The modular munitions (20) launching system (1) comprises at least one munitions receiving chamber (4) forming at least one firing channel (18) for a munition (20) emitting a pyrotechnic jet (24) in a longitudinal direction (L). The modular system further comprises at least one mitigation device (32). This mitigation device (32) comprises at least one jet-breaking element (35) arranged to separate the pyrotechnic jet (24) from the munition (20) into at least two sub-jets (35), each extending in a direction different from the other sub-jet (35) and from the longitudinal direction (L). Figure for abbreviation: 4