The Steam Injector
A theoretical and practical treatise on the design and operation of injectors and on the flow of fluids through and the design of nozzles.
Forfatter: V. A. B. Hughes
År: 1912
Forlag: The Technical Publishing Company Limited
Sted: London
Sider: 145
UDK: 621.176
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108
THE STKAM INJECTOB.
That is the velocity per unit mass (1 Ib.) of the jet is
197 3 ft. per second. If a water jet were discharging from
a boiler into a region at an absolute pressure of 6 Ibs. per
square inch, then to give said jet a velocity of 197*3 ft.
per second, the boiler would require to be under a gauge
pressure of about 254 Ibs. per square inch. Thus if we
neglect all consideration of losses, an exhaust injector
working under the conditions just described should be able
to feed a boiler under a pressure of nearly 254 Ibs. per
square inch. To illustrate the actual performance of an
injector under conditions very similar to those descriLeu,
the result of a test is here given : —
Exhaust steam pressure. Pounds per square inch absolute. Feed water temperature. Head of Feed water. , 2 feet Delivery temperature. Delivery pressure. Pounds per square inch absolute.
16 Deg. Fah. 60 Deg. Fali. 162 95
The reasons for the low delivery pressure have already
been fully discussed.
One of the drawbacks of exhaust injectors as made until
quite recently lias been the lowness of the maximum de-
livery pressure when exhaust steam alone is employed;
80 Ibs. by gauge lias been tlie liighest obtainable under
ordinary working conditions.
To vary the delivery pressure without altering the con-
struction of the injector or the water head, two courses
are open, namely: —
(1) To increase the water inlet area, so as to ’ncrease
the rate of condensation of the steam and intensify the
vacuum at the steam nozzle mouth.
(2) To recluce the water inlet area, so as to lessen the
load which the steam has to carry.
Both of these courses can be adopted successfully within
narrow limits, but eventually the disadvantages outwedgli
the advantages. Thus, if the water supply is increased,
there comes a point when the rate of retardation of the
velocity of the jet through tlie combining nozzle is greater