Cessna TURBO CENTURION T210M 1978 Pilot Operating Handbook page 160

SECTION 7
CESSNA
MODEL T210M
AIRPLANE
&
SYSTEMS DESCRIPTIONS
TURBOCHARGING SYSTEM
Because the engine is turbocharged, some of its characteristics are
different from a normally aspirated engine. The following information
describes the system and points out some of the items that are affected by
turbocha rging. Section 4 contains the normal operating procedures for the
turbocha rged engine.
The following steps, when combined with the turbocharger system
schematic (figure 7-5), provide a better understanding of how the turbo-
charger system works. The steps follow the induction air a s it enters and
passes through the engine until it is expelled as exhaust gases.
1.
Engine induction air is taken in through an opening in the nose
cap, ducted through a filter and into the compressor where it is
compressed.
2. The pressurized induction air then passes through the throttle
body and induction manifold into the cylinders.
3. The air and fuel are burned and exhausted to the supercharger
turbine.
4. The exhaust gases drive the turbine which, in turn, drives the
compressor, thus completing the cycle. ,-,
A LTERN AT E
A1R DOOR
COM PRESSOR
U RS INE
CODE
i
ED~~l~i
RAM AI R
INT A KE AIR FROM
COM P RESSOR
_.... EX H A U S T GAS
r:=z:l
ENGI NE
OIL
MEC H AN I CA L
LINKA GE
7-24
Figure 7-5. Turbocharger System
OI L PUM P
\ . EXHAUS T
OVER BOA RD