Chapter 4 – Approval for serially manufactured engines: engine family and engine
group concept
1 Paragraph 4.4.6.1 of the NOx Technical Code reads as follows:
"4.4.6.1 The engine group may be defined by basic characteristics and specifications in
addition to the parameters defined in 4.3.8 for an engine family."
Interpretation:
Paragraph 4.4.6.1 cross references paragraph 4.3.8 which provides guidance
for selection of an engine family. For engines fitted with an SCR system to reduce
NOx emissions, it is recognized that some of the parameters provided may
not be common to all engines within a group, in particular paragraphs 4.3.8.2.3 and
4.3.8.2.4 state that:
For engines fitted with an SCR system to reduce NOx emissions,
the number and arrangement of cylinders may not be common to all members of the engine
group. These parameters may be replaced with new parameters derived from the SCR chamber
and catalyst blocks, such as the SCR space velocity (SV), catalyst block geometry and
catalyst material.
2 Paragraph 4.4.6.2 of the NOx Technical Code reads as follows:
"4.4.6.2 The following parameters and specifications shall be common to engines within
an engine group:
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.1 bore and stroke dimensions;
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.2 method and design features of pressure charging and exhaust gas system:
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- constant pressure;
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- pulsating system;
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.3 method of charge air cooling system:
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.4 design features of the combustion chamber that affect
NOx emission;
-
.5 design features of the fuel injection system, plunger and injection
cam that may profile basic characteristics that affect NOx emission;
and
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.6 rated power at rated speed. The permitted ranges of engine power (kW/cylinder)
and/or rated speed are to be declared by the manufacturer and approved by the
Administration."
Interpretation:
For engines fitted with an SCR system to reduce NOX emissions it is
recognized that some of the parameters provided may not be common to all engines within
a group and that new parameters derived from the SCR chamber and catalyst blocks may be
used instead, such as the SCR space velocity (SV), catalyst block geometry and catalyst
material.
Whilst the provisions of paragraph 4.4.6.2.1 should remain common to all engines within
the group, the remaining parameters listed in paragraph 4.4.6.2 may be replaced by
alternative SCR parameters, provided that the applicant is able to demonstrate that
these alternative parameters are suitable for defining the engine group.
The applicant remains responsible for selecting the parent engine and demonstrating the
basis of this selection to the satisfaction of the Administration.