Page 13 - The Jet Engine
P. 13

Basic mechanics





                                                                       velocity. In practice the former is preferred, since by
                                                                       lowering the jet velocity relative to the atmosphere a
                                                                       higher propulsive efficiency is obtained.



                                                                       METHODS OF JET PROPULSION
                                                                       10. The types of jet engine, whether ram jet, pulse
                                                                       jet, rocket, gas turbine, turbo/ram jet or turbo-rocket,
                                                                       differ only in the way in which the 'thrust provider', or
                                                                       engine, supplies and converts the energy into power
                                                                       for flight.
                                                                       11. The ram jet engine (fig. 1-6) is an athodyd, or
                                                                       'aero-thermodynamic-duct to give it its full name. It
                                                                       has no major rotating parts and consists of a duct
                                                                       with a divergent entry and a convergent or









                     Fig. 1-4   Hero’s engine - probably the earliest
                                form of jet reaction.

                      of doing this, as described in Part 2, but in all
                      instances the resultant reaction or thrust exerted on
                      the engine is proportional to the mass or weight of air
                      expelled by the engine and to the velocity change  Fig. 1-6  A ram Jet engine.
                      imparted to it. In other words, the same thrust can be
                      provided either by giving a large mass of air a little  convergent-divergent exit. When forward motion is
                      extra velocity or a small mass of air a large extra  imparted to it from an external source, air is forced
                                                                       into the air intake where it loses velocity or kinetic
                                                                       energy and increases its pressure energy as it
                                                                       passes through the diverging duct. The total energy
                                                                       is then increased by the combustion of fuel, and the
                                                                       expanding gases accelerate to atmosphere through
                                                                       the outlet duct. A ram jet is often the power plant for
                                                                       missiles and .target vehicles; but is unsuitable as an
                                                                       aircraft power plant "because it requires forward
                                                                       motion imparting to it before any thrust is produced.
                                                                       12. The pulse jet engine (fig. 1-7) uses the principle
                                                                       of intermittent combustion and unlike the ram jet it
                                                                       can be run at a static condition. The engine is formed
                                                                       by an aerodynamic duct similar to the ram jet but,
                                                                       due to the higher pressures involved, it is of more
                                                                       robust construction.  The duct inlet has a series of
                                                                       inlet 'valves' that are spring-loaded into the open
                                                                       position. Air drawn through the open valves passes
                                                                       into the combustion chamber and is heated by the
                     Fig. 1-5   A garden sprinkler rotated by the      burning of fuel injected into the chamber.  The
                                reaction of the water jets.            resulting expansion causes a rise in pressure, forcing


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