METHOD OF TREATMENT Russian patent published in 2012 - IPC B08B9/93 B08B3/08 B08B3/10 

Abstract RU 2447958 C1

FIELD: process engineering.

SUBSTANCE: invention relates to degreasing surfaces and cavities by solvents, preparing to high-sensitivity tightness tests, and may be used in space engineering, aircraft engineering, instrument making, etc. Proposed method comprises placing rocket to be cleaned on rotary device to revolve rocket body about horizontal lengthwise axis, filling rocket tanks partially with solvent to revolve the rocket about said horizontal axis. Rocket body bottom zone in contact with solvent is heated while surface of tanks is cooled. Proposed method differs from prior art in that MINIMUM amount of solvent Ms makes where CF is initial (before cleaning) mean-statistical specific amount of soluble impurities on inner surface of tanks, kg/m2; CFtol is tolerable residual amount (after cleaning) of soluble impurities, kg/m2; F is total area of inner surface of tanks, m2; δ is mean thickness of solvent film on aforesaid said inner surfaces in cleaning tanks, m; pv,pf are densities of vapor and fluid phases of solvent in cleaning, respectively, kg/m3; V is free inner volume of tanks, m3, while linear rotational speed of rocket cylindrical shell about axis is set to allow evaporation per unit time of maximum amount of solvent Gmax(kg/s): where v is linear rotational speed of rocket cylindrical shell about axis, (m/s); λ is factor of heat transfer from shell outer wall to solvent, kJ/m2 s K; tSMmax is maximum tolerable temperature of tank structural material heating, °C; Fc is total area of contact of solvent with tank inner surface, m2; r is solvent specific evaporation heat, kJ/kg; cSM is heat capacity of rocket tank material, kJ/kg K; ts is solvent temperature in tank necessary for efficient washing effect, °C; tH is tank shell temperature in area not in contact with solvent ( equal to ambient temperature), °C; A is mean thickness of tank shell, m; V is linear speed of tank wall rotation, m/s; L is tank cylindrical section length, m; ρsm is density of tank structural material, kg/m3.

EFFECT: higher quality of cleaning and preparation for high-sensitivity tightness tests, minimised consumption of power and materials, lower costs.

3 cl, 1 dwg

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RU 2 447 958 C1

Authors

Morozov Vladimir Sergeevich

Kozhevnikov Evgenij Mikhajlovich

Osintsev Petr Petrovich

Samar'Jan Valerij Vasil'Evich

Dates

2012-04-20Published

2010-09-15Filed