The requirements of this Chapter are applicable
to reciprocating internal combustion engines operating on liquid,
gas or dual fuel for main propulsion and essential auxiliary services
(hereinafter referred to as engines). Pt 5, Ch 2, 3 Crankshaft Design is not applicable to auxiliary engines having powers of less
than 110 kW.
For the purposes of this Chapter engine type, expressed by the
manufacturer/licensor’s designation, is defined by:
-
the bore and stroke;
-
the method of injection (i.e. direct injection,
indirect injection, pilot injection);
-
the fuel pump and injection system (independent
line to fuel oil valve, common rail);
-
the valve and injection operation (by cams
or electronically controlled);
-
the fuel(s) used (liquid, dual-fuel, gaseous,
etc.);
-
the working cycle (4-stroke, 2-stroke);
-
the gas exchange (naturally aspirated, turbocharged,
etc.);
-
the method of turbocharging (pulsating system,
constant pressure system);
-
the charging air cooling system (with or without
intercooler, number of stages);
-
cylinder arrangement (in-line, vee, etc.);
-
the maximum continuous power per cylinder
(or maximum continuous brake mean effective pressure) at maximum continuous
speed;
-
the manufacturer and type of governor (and
control system if applicable) fitted.
A complete engine includes the control system,
turbocharger(s) and all ancillary systems and equipment referred to
in this Chapter that are used for operation of the engine for which
there are rule requirements; this includes systems allowing the use
of different fuel types.