Practical Conclusions

Airplanes require about one third more power during the take-off than in flight. In diesel-engined airplanes the size of the engine could be reduced by 25 percent by feeding oxygen into the intake air during the takeoff. Applying the results of the experiments to a transport plane, Fig. 31 shows the possible weight saving with various oxygen boosts. The curves are based on 6000 cruising horsepower and an estimated engine weight of 2 lb per hp.

For the take-off 8000 hp are necessary. To supply the additional 2000 hp, 200 lb of oxygen are fed into the intake air during the take-off. The volume of 200 lb of liquid oxygen is approximately 20 gal. Standard liquid air containers of 55 litre capacity weigh 75 lb. Therefore the weight of the oxygen and container is 350 lb while the possible saving in engine weight is 4000 lb. The weight per take-off horsepower is thereby reduced from 2 to 1.54 lb. The calculation is shown in Table 1.

Figure 38.—Effect of Oxygen Boost on Power and Weight. (Cruising horsepower 6000, takeoff horsepower 8000.)

Oxygen addition may be used for starting diesel engines. The raising of the oxygen concentration from the normal 21 per cent to 45 per cent was found to be equivalent to a raise of approximately 10 cetane numbers as far as starting is concerned.

Five per cent increase in oxygen concentration eliminated exhaust smoke completely.

Table 1

Normal horsepower6000
Take-off horsepower8000
Normal fuel consumption0.4 lb per hp-hr, or 53.5 lb per min
Normal air consumption900 lb per min
Normal oxygen consumption, 21 per cent oxygen concentration189 lb per min
Boosted oxygen consumption, 32 per cent oxygen concentration289 lb per min
Oxygen to be supplied100 lb per min
Weight of 8000-hp engine16,000 lb
Weight of boosted 6000-hp engine12,000 lb
Weight of oxygen for 2-min boost200 lb
Weight of container for 29 lb of liquid oxygen150 lb
Net weight saving by oxygen boost3650 lb
Weight per horsepower, nonboosted engine2 lb
Weight per horsepower, boosted engine1.54 lb

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