FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Atlas
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
1948
1948 - 0304.PDF
AIR OOMPRESSOR- EVACJATORS AIR AMMONIA LIQUID AMMONIA CAS BRINE RESEARCH FOR SPEED. . . Layout of the tunnel buildings looking North and showing the motor room at the East end, the control room over the offices, and the refrigera- tion end compressorjcvacuator plant at the West end. The arrange- ment of the fatter and the flow circuits is shown at lower left, and in the centre and at right are respectively sections through the working section and the control room and through the fan and motor drive. tunnel of + 4 deg C is adequate for all normal work; thiscan, however, be reduced if necessary to —10 deg C. From the main tanks the brine is sucked to a batteryof three pumps, and a thermostatic device in the delivery line from these brings a mixing valve into operation as-required, whereby cold brine from the main body of the tank is introduced to mix with, the warm brine beingcirculated. These pumps deliver into the tunnel jackets from which
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events
