Power Output and Air Requirements of a Two-stroke Cycle Engine for Aeronautical Use (1927)
NASA Technical Reports Server (NTRS) · leaf 6
d by a combina- tion of a throttling valve, rubber diaphragms, large capacity receivers, and baffles so that this method should give fairly reliable results. A small surge chamber was placed as near the engine as possible to insure freedom from irregular operation due to surging in the air line. ri… … -Fuel injection pump and timing mechanism showed it to give the maximum power output. A sketch of the injection pump is shown in Figure 4. The cam operates the pump plunger by means of a rocker arm having a roller follower. A threaded adjusting sleeve operated by a gear and hand crank (fig. 5)…
NASA Technical Reports Server (NTRS)
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