Gardner Denver ELECTRA-SAVER EAY, Руководство по эксплуатации и обслуживанию

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13–10–613 Page 1
SECTION 1
GENERAL INFORMATION
FIGURE 1–1 – COMPRESSION CYCLE
COMPRESSOR – The Gardner Denver Electra–Sav-
er
R
compressor is a single stage, positive displace-
ment rotary machine using meshing helical rotors to ef-
fect compression. The input drive shaft and helical
drive gear are supported in the gear case by high ca-
pacity tapered roller bearings. The drive gear meshes
with a driven gear mounted on the main rotor shaft to
drive the rotors. Both rotors are supported between
large capacity anti–friction bearings located outside the
compression chamber. Single width cylindrical roller
bearings are used at the inlet end of the rotors. Early
models used two (2) heavy–duty, single–row, angular
contact ball bearings at the discharge end to locate
each rotor axially and carry all thrust loads; later mod-
els use tapered roller bearings in this location.
COMPRESSION PRINCIPLE (FIGURE 1–1) – Com-
pression is accomplished by the main and secondary
rotors synchronously meshing in a one–piece cylinder.
The main rotor has four (4) helical lobes 90
_
apart. The
secondary rotor has five (5) matching helical grooves
72
_
apart to allow meshing with main rotor lobes.
The air inlet port is located on top of the compressor
near the center. The discharge port is near the bottom
at the opposite end of the compressor cylinder. Figure
1–1 is an inverted view to show inlet and discharge
ports. The compression cycle begins as rotors unmesh
at the inlet port and air is drawn into the cavity between
the main rotor lobes and secondary rotor grooves (A).
When the rotors pass the inlet port cutoff, air is trapped
in the interlobe cavity and flows axially with the meshing
rotors (B). As meshing continues, more of the main ro-
tor lobe enters the secondary rotor groove, normal vol-
ume is reduced and pressure increases.
Oil is injected into the cylinder to remove the heat of
compression and seal internal clearances. Volume re-
duction and pressure increase continues until the air/oil
mixture trapped in the interlobe cavity by the rotors
passes the discharge port and is released to the oil res-
ervoir (C). Each rotor cavity follows the same “fill–com-
press–discharge” cycle in rapid succession to produce
a discharge air flow that is continuous, smooth and
shock free.
AIR FLOW (FIGURE 5–1, page 28) – Air enters the air
filter and passes through the inlet unloader valve to the
compressor. After compression, the air/oil mixture
passes into the oil reservoir where most of the en-
trained oil is removed by velocity change and impinge-
ment and drops back into the reservoir. The air and re-
maining oil then passes through the oil separator; the
separated oil is returned to the system through tubing
connecting the separator and compressor. The air
passes through the reservoir discharge manifold, dis-
charge check valve, minimum pressure valve and the
customer furnished unit shutoff globe valve to the plant
air lines.
LUBRICATION, COOLING AND SEALING – Oil is
forced by air pressure from the oil reservoir through the
oil cooler, thermostatic mixing valve, and oil filter and
discharges into the compressor main oil gallery. A por-
tion of the oil is directed through internal passages to
the bearings, gears and shaft oil seal. The balance of
the oil is injected directly into the compression chamber
to remove heat of compression, seal internal clear-
ances and lubricate the rotors.
TURN VALVE – The turn valve is a rotary helical valve
located on the discharge side of the cylinder toward the
inlet end. The valve opens and closes ports in the cylin-
der which communicates with the inlet passage. This
varies the compressor rotor volume to match the de-
mand for air, thus reducing the part–load power re-
quirement.