DEVICE FOR REDUCING PRESSURE AND COMBUSTION PRODUCT COOLING IN GAS DUCT ON DESTROYING SOLID-PROPELLANT ROCKET ENGINE CHARGE Russian patent published in 2008 - IPC F23G7/00 

Abstract RU 2341730 C1

FIELD: engines and pumps.

SUBSTANCE: proposed device incorporates localisation and combustion product cooling chamber. Note that the said chamber end section communicates via an intermediate jointing section with a gas duct to make an open surface intended for reduction of excess pressure in the aforesaid jointing section and gas duct by allowing combustion products to escape and cool them by ejecting air from atmosphere in compliance with the following ratio d3/d2=d2/d1 to 1.1 to 2 where dl is diameter of localization and cooling chamber, d2 is diameter of intermediate jointing section, d3 is gas duct diameter. The depth of the intermediate jointing section penetration into gas duct is determined from the ratio L=0.05 to 0.01d where L is the said depth, d is diameter of the section that extends inside.

EFFECT: higher process and ecological safety.

2 dwg

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RU 2 341 730 C1

Authors

Shajkhutdinov Rashid Vagizovich

Kutsenko Gennadij Vasil'Evich

Ponik Anatolij Nikitovich

Kozlov Nikolaj Leonidovich

Aleksandrov Aleksandr Sergeevich

Vikhljaev Jurij Arkad'Evich

Dates

2008-12-20Published

2007-02-19Filed