Evaporators Propeller

Circulation in the standard short tube evaporator depends upon boiling. Should boiling stop any solids present in the liquid will settle out. The earliest type of evaporator that perhaps could be called a forced-circulation system is the propeller calandria illustrated in Figure 11-10. Basically a standard evaporator with a propeller added in the downcomer, the propeller calandria often achieves higher heat transfer rates. The propeller is usually placed as low as possible to avoid cavitation and is placed in an extension of the downcomer. The propeller can be driven from above or below. Improvements in propeller design have permitted longer tubes to be incorporated in the evaporator. Propeller evaporators are sometimes used in Europe when forced circulation or long tube evaporators would be used in the United States. 

Grade C, Type II is typical of Hquid oxygen used as a rocket propellant oxidizer. Particulate content is limited because of the critical clearances found in mechanical parts of the rocket engine. In addition to water, acetylene and methane are limited because, on long standing, oxygen evaporation could cause concentration of these combustible contaminants to reach hazardous levels. 

FIG. 11-122 Evaporator types, a) Forced circulation, (h) Siibmerged-tiihe forced circulation, (c) Oslo-type crystallizer, (d) Short-tube vertical, (e) Propeller calandria. (f) Long-tube vertical, (g) Recirculating long-tube vertical, (h) Falling film, (ij) Horizontal-tube evaporators. G = condensate F = feed G = vent P = product S = steam V = vapor ENT T = separated entrainment outlet. 

Circffiation in the standard short-tube vertical evaporator is dependent entirely on boiling, and when boihng stops, any sohds present settle out of suspension. Consequently, this type is seldom used as a ciystaUizing evaporator. By instalhng a propeller in the downtake, this objection can be overcome. Such an evaporator, usually called a pro-... 

The most common evaporator design is based on the use of the same heating surface in each effec t. This is by no means essential since few evaporators are standard or involve the use of the same patterns. In fac t, there is no reason why all effects in an evaporator must be of the same type. For instance, the cheapest salt evaporator might use propeller calandrias for the early effects and lorced-circiilation effects at the low-temperature end, where their higher cost per unit area is more than offset by higher heat-transfer coefficients. 

Whenever corrosion resistance results from the accumulation of layers of insoluble corrosion products on the metallic surface, the effect of high velocity may be either to prevent their normal formation or to remove them after they have been formed. Either effect allows corrosion to proceed unhindered. This occurs frequently in smaU-diameter tubes or pipes through which corrosive liquids may be circulated at high velocities (e.g., condenser and evaporator tubes), in the vicinity of oends in pipe hnes, and on propellers, agitators, and cen-trifiig pumps. Similar effects are associated with cavitation and impingement corrosion. 

Ille, G. and C. Springer, 1981, The Evaporation and Dispersion of Hydrazine Propellants from Ground Spdls, CEEDO-TR-83-30, ADA059407. 

Tank (containing LOX/LH, propellant) by 13 percent, and NASA is willing to make it 26 percent lighter. Another solution is the hydrogen slush, which is liquid hydrogen hyper cooled almost to the point of solidification (—259° Celsius compared to —252° Celsius for normal LH,). Due to 15 percent greater density, hydrogen slush occupies lesser volume and has lower evaporation losses. 

Ni-Si recovery of HP Processes involving cone. H2SO4 processes. Sulphur stripping columns. Distillation columns containing acidic chlorides. Handling acid sludges processes impellers, propeller shafts, fasteners. Demisters in desalination plants refrigerating brines. Salt production. Evaporators steel... 

In an effort to rationalize the basic mechanism, Brown and Jensen (B12) have solved the dynamic energy- and mass-flow equations, allowing for a finite rate of vaporization of the injected fluid. The results of these calculations have shown that both mechanisms can be important. For propellants which require relatively low depressurization rates (such as polyurethane types), the evaporative-cooling mechanism can develop sufficient depressurization rates. For PBAN propellants, direct surface-cooling is the only mechanism whereby estinguishment can be accomplished. 

Increasing the velocity of flow of the liquor through tubes results in a significant increase in the liquid-film transfer coefficient. This is achieved in the forced circulation units where a propeller or other impeller is mounted in the central downcomer, or a circulating pump is mounted outside the evaporator body. In the concentration of strong brines, for example, an internal impeller, often a turbine impeller, is fitted in the downtake, and this form... 

The evaporation half-life of allyl chloride (1 mg/L) from water at 25 °C using a shallow-pitch propeller stirrer at 200 rpm at an average depth of 6.5 cm was 26.6 min (Dilling, 1977). 

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