Section
1 General requirements
1.1 Application
1.1.3 The requirements of this Chapter are applicable to reciprocating internal
combustion engines operating on liquid, gas or dual fuel for use in Mobility or Ship
Type systems (hereinafter referred to as engines). The requirements of Vol 2, Pt 2, Ch 1, 3 Crankshaft design do not apply to engines intended for Mobility or Ship Type
systems where power does not exceed 110 kW.
1.2 Scope
1.2.1 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.
1.2.2 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.
1.3 Approval process
1.3.1 All engines intended for installation on an LR Class ship are to be type approved by
LR (see LR Type Approval System Procedure TA14 for details of the LR Type
Approval process).
1.3.2 Each complete engine, as defined in Vol 2, Pt 2, Ch 1, 1.2 Scope, intended for installation on an LR Classed
vessel, is to have an LR Engine Certificate.
1.3.3 For the first engine of a type the approval process and the engine
certification process may be performed simultaneously.
1.3.4 To apply for an LR Engine Certificate, the following are to be submitted:
- a list of all documents identified in the
‘for information’ and ‘for appraisal’ columns of Table 1.1.1 Plans and particulars to be
submitted with the relevant drawing numbers and revision status.
This list is to cross-reference the approved plans previously submitted as
part of the engine Type Approval and identify any plans that have been
modified.
- where there is a licensor/licensee
arrangement the list required by Vol 2, Pt 2, Ch 1, 1.3 Approval process 1.3.4.(a) is to cross-reference the drawings
submitted by the designer as part of the engine Type Approval. This list is
to identify all changes where the approved design has been modified by the
licensee. Where the licensee proposes design modifications to components, a
statement is to be made confirming the licensor’s acceptance of the proposed
changes. If designer/licensor’s acceptance is not confirmed, the engine is
to be regarded as a different type and is subject to the complete appraisal
and type testing process.
- all documents with changes from the approved
design are to be submitted for review/appraisal.
- In all cases the complete set of endorsed documents and the list referenced
in Vol 2, Pt 2, Ch 1, 1.3 Approval process 1.3.4.(a), which are to be provided by the
manufacturer, will be required by the Surveyor(s) attending the
manufacturer’s works. Where a licensee/licensor arrangement is in place,
this set of documents may be a combination of licensor and licensee
documents.
1.3.5 An LR Engine Certificate is issued upon satisfactory completion of engine
assembly, with associated component testing (see
Vol 2, Pt 2, Ch 1, 2 Materials and components) and factory acceptance testing (see
Vol 2, Pt 2, Ch 1, 11 Factory Acceptance Test and Shipboard Trials of Internal Combustion Engines) or issued in accordance with the
alternative approach for product assurance approved by LR, see
Vol 2, Pt 1, Ch 1, 6.4 Alternative system of inspection.
1.4 Submission requirements
1.4.1 The plans and information are to be submitted as required in Table 1.1.1 Plans and particulars to be
submitted and Vol 2, Pt 2, Ch 1, 1.4 Submission requirements 1.4.2 to
Vol 2, Pt 2, Ch 1, 1.4 Submission requirements 1.4.8 as
applicable
Table 1.1.1 Plans and particulars to be
submitted
Document
|
For information
|
For appraisal
|
(X indicates reason for
submission)
|
Engine particulars (LR Form
2073 with general engine and ancillaries information, Project Guide,
Marine Installation Manual), see Note 1
|
X
|
|
Material specifications of
principal components with information on non-destructive material
tests and pressure tests
|
|
X
|
Engine cross-section
|
X
|
|
Engine longitudinal section
|
X
|
|
Engine frames, welding
drawings, see Notes 2 and 3
|
|
X
|
Main engine foundation and
holding down and securing arrangements
|
X (metal chocks)
|
X (non-metallic chocks)
|
Bedplate and crankcase of cast
design
|
X
|
|
Bedplate and crankcase of
welded design, with welding details and welding instructions,
see Notes 2 and 3
|
|
X
|
Bedplate/oil sump welding
drawings, see Note 2
|
|
X
|
Thrust bearing assembly,
see Note 4
|
X
|
|
Thrust shaft or intermediate
shaft (if integral with engine)
|
|
X
|
Thrust bearing bedplate of
welded design, with welding details and welding instructions, see
Note 2
|
|
X
|
Frame, see Note 3,
framebox, see Note 3, and gearcase of cast
construction
|
X
|
|
Tie rod
|
X
|
|
Connecting rod, assembly,
see Note 5
|
X
|
|
Crosshead, assembly,
see Note 5
|
X
|
|
Piston rod, assembly, see
Note 5
|
X
|
|
Piston, assembly, see
Note 5
|
X
|
|
Piston head
|
X
|
|
Cylinder jacket/ block of cast
construction, see Note 3
|
X
|
|
Cylinder cover, assembly,
see Note 5
|
X
|
|
Cylinder liner
|
X
|
|
Counterweights (if not
integral with crankshaft), including fastening
|
X
|
|
Crankshaft, details (for each
crankthrow)
|
|
X
|
Crankshaft, assembly (for each
crankthrow)
|
|
X
|
Crankshaft calculations,
(see
Vol 2, Pt 2, Ch 1, 3 Crankshaft design)
|
X
|
|
Camshaft drive, assembly,
see Note 5
|
X
|
|
Flywheel or
turning-wheel
|
X
|
|
Shaft coupling interface
arrangement including dimensions and material details
|
|
X
|
Details of shielding and
insulation of exhaust pipes and other parts operating at an elevated
temperature, which might be impinged by flammable fluid(s) as a
result of a system failure
|
X
|
|
Schematic layout or other
equivalent documents for the engine, see Note 6
|
|
|
- Starting and control air systems
|
|
X
|
|
|
X
|
|
|
X
|
|
|
X
|
|
|
X
|
- Engine control and safety system
|
|
X
|
High pressure fuel injection
pump assembly
|
X
|
|
High pressure parts for fuel
oil injection system, see Note 7
|
|
X
|
Shielding arrangements for
high pressure piping - fuel, hydraulic and flammable oils, (see
Vol 2, Pt 2, Ch 1, 8.1 Fuel oil, hydraulic and high-pressure oil systems 8.1.1)
|
|
X
|
Fastening arrangements for main
bearings
|
X
|
|
Fastening arrangements for
cylinder heads and exhaust valve (two stroke design)
|
X
|
|
Fastening arrangements for
connecting rods
|
X
|
|
Vibration dampers/detuners and
moment compensators
|
X
|
|
Construction and arrangement of
vibration dampers
|
X
|
|
Details of mechanical joints
of piping systems
|
|
X
|
Oil mist detection and/or
alternative arrangements
|
|
X
|
Construction of accumulators
for electronically controlled engine
|
|
X
|
Construction of common
accumulators for electronically controlled engine
|
|
X
|
Construction of accumulators
for hydraulic oil and fuel oil
|
|
X
|
Arrangement and details of the
crankcase explosion relief valve where applicable (see
Vol 2, Pt 2, Ch 1, 10 Safety arrangements)
|
|
X
|
Calculation results for
crankcase explosion relief valves (see
Vol 2, Pt 2, Ch 1, 10 Safety arrangements)
|
|
X
|
Construction and arrangements
of hydraulic systems for actuation of sub-systems:
|
|
|
- Control valves, high-pressure pumps, pipes and
accumulators
|
X
|
|
- Drive for high pressure pumps
|
X
|
|
- Valve bodies, if applicable
|
X
|
|
For engine control, alarm
monitoring and safety systems, the plans and information Vol 2, Pt 2, Ch 1, 1.4 Submission requirements 1.4.3, see Note 8
|
|
X
|
Generator set test results that
state the engine maximum load steps which satisfy the quality of
power supply requirements specified in Vol 2, Pt 9, Ch 1, 2.1 Quality of power supplies (QPS))
|
|
X
|
Planned operating profiles for
the vessel at sea and during manoeuvring as agreed with the
Operators
|
|
X
|
List of sub-contractors for
main parts
|
X
|
|
Operation and service manuals,
see Note 9
|
X
|
|
Risk-based analysis (for
engine control system), see Note 10
|
X
|
|
Test program resulting from
risk-based analysis (for engine control system), see Note
10
|
X
|
|
Production specifications for
castings and welding procedures
|
X
|
|
Evidence of quality control
system for engine design, production and in-service maintenance,
see Notes 5 and 11
|
X
|
|
Type approval certification
for environmental tests of control components, see Note
12
|
X
|
|
Details of the engine type
test program and the type test report, see Note 13
|
|
X
|
Engine test schedule (FAT and
shipboard trials, see
Vol 2, Pt 2, Ch 1, 1.4 Submission requirements 1.4.2)
|
|
X
|
Documentation verifying
compliance with inclination limits (see
Vol 2, Pt 1, Ch 3, 4.6 Inclination of ship )
|
|
X
|
Combustion
pressure—displacement relationship
|
|
X
|
Plans and details for dead ship
condition starting arrangements, see
Vol 2, Pt 7, Ch 3, 12.11 Dead ship condition starting arrangements.
|
|
X
|
|
Note 2. For
approval of materials and weld procedure specifications. The
weld procedure specification is to include details of pre- and
post-weld heat treatment, weld consumables and fit-up
conditions.
|
Note 3. For each
cylinder for which dimensions and details differ.
|
Note 4. If integral
with engine and not integrated in the bedplate.
|
|
Note 6. Details of
the system so far as supplied by the engine manufacturer such
as: main dimensions, operating media and maximum working
pressures.
|
Note 7. The
documentation to contain specifications for pressures, pipe
dimensions and materials.
|
Note 8. The
submission is to include a general overview of the operating
principles, supported by schematics explaining the functionality
of individual systems and sub-systems. The information is to
relate to the engine capability and functionality under defined
operating and emergency conditions such as recovery from a
failure or malfunction, with particular reference to the
functioning of programmable electronic systems and any
sub-systems. The information is also to indicate if the engine
has different modes of operation, such as to limit exhaust gas
emissions and/or to run under an economic fuel consumption mode
or any other mode that is electronically controlled.
|
Note 9. Operational
manuals are to contain maintenance requirements (servicing and
repair) including details of any special tools and gauges that
are to be used with their fitting/settings together with any
test requirements on completion of maintenance. They are to
include a description of each system’s particulars and include
reference to the functioning of sub-systems.
|
Note 10. Where
engines rely on hydraulic, pneumatic or electronic control of
fuel injection and/or valves, the risk-based analysis is to
address the mechanical, pressure containing, electrical,
electronic and programmable electronic systems and arrangements
that support the operation of the engine. It is to demonstrate
that failure of the control system will not result in the
operation of the engine being degraded beyond acceptable
performance criteria for the engine and that suitable risk
mitigation has been achieved in accordance with Vol 2, Pt 2, Ch 1, 3.3 Information to be submitted. The risk-based analysis will not be
explicitly approved by LR.
|
|
Note 12. Tests are
to demonstrate the ability of the control, protection and safety
equipment to function as intended under the specified testing
conditions as per Lloyd’s Register Type Approval Test
Specification Number 1.
|
Note 13. The type
test report may be submitted shortly after the conclusion of the
type test. For electronically controlled engines evidence of
type testing of the engine with the programmable electronic
system, or a proposed factory acceptance test plan at the engine
builders with the programmable electronic system functioning, is
to be submitted to verify the functionality and behaviour under
normal operating and fault conditions of the programmable
electronic control system. Where required this is to include
proposals for short-term, high power operation.
|
1.4.2 A schedule of testing at the engine packager’s or system integrator’s
facility, pre-sea trial commissioning and sea trials is to be submitted. The test
schedules are to identify all modes of engine operation and the sea trials are to
include typical port manoeuvres under all intended engine operating modes. The
schedule is to include:
-
testing and trials to demonstrate that the engine is capable
of operating as described in Table 1.1.1 Plans and particulars to be
submitted, Note 10;
-
tests to verify that the response of the complete
mechanical, hydraulic, electrical and electronic system is as predicted
for the intended operational modes; and
-
testing required to verify the conclusions of the risk-based
analysis.
The scope of these tests is to be agreed with LR based on
the risk-based analysis.
1.4.3 In addition to the applicable plans and particulars required by Vol 2, Pt 9, Ch 1, 1.4 Documentation required for design review the following information for control, alarm, monitoring and
safety systems relating to the operation of an electronically controlled engine is
to be submitted:
-
Engine configuration details, see
Vol 2, Pt 2, Ch 1, 4.3 Control engineering systems 4.3.2.
- Local and remote means to carry out
system configuration.
- Engine builder procedures for
undertaking configuring.
- Roles and responsibilities for
configuration (e.g. Engine builder, engine packager, system
integrator or other nominated party) with accompanying
schedule.
- Configurable settings and
parameters (including those not to be modified from a default
value).
- Configuration for propulsion,
auxiliary or emergency engine application.
-
Software quality plans, including configuration management
documents.
-
Software safety evidence.
-
Software assessment inspection report such as SCA or IEC
61508, as applicable.
Configuration records are to be maintained and are to be made available
to the Surveyor at testing and trials and on request in accordance with Vol 2, Pt 9, Ch 1, 1.7 Alterations and additions and Vol 2, Pt 9, Ch 12, 1.2 Trials 1.2.3.
1.4.5 For turbochargers, the following plans and particulars are to be
submitted. The submission requirements vary depending on the category of the
turbocharger; category A, B and C turbochargers are defined in Vol 2, Pt 2, Ch 1, 12.1 General 12.1.2:
- Category A (on request):
- Turbocharger specification including type, compression ratio and
operating condition.
- Cross-sectional drawing with principal dimensions and names of
components.
- Containment test report.
- Test program.
- Category B:
- Turbocharger specification including type of turbine and compressor,
compression ratio, bearing and cooling method.
- Cross-sectional drawing with principal dimensions and materials of
housing components for containment evaluation.
- Documentation of containment in the event of disc fracture.
- Operational data and limitations, i.e.:
- Arrangement of lubrication system, all variants within a range.
- A list of main current suppliers and subcontractors for rotating parts
and an operation and maintenance manual.
- Type test reports.
-
Category C:
- Plans and particulars as for Category B.
- Drawings of the housing and rotating parts (shaft, wheels, blades and
nozzle) including details of blade fixing for turbine and compressor.
- Material specifications (including density, Poisson’s ratio, range of
chemical composition and mechanical properties (at room temperature),
and high-temperature strength characteristics as well as creep rate and
rupture strength for the design service life (parts subject to 450
degrees Celsius or more)) of all parts mentioned above including details
of the material and quality control system to be used for these parts.
- Welding details and welding procedure of above-mentioned parts, if
applicable.
- Documentation* of safe torque transmission when the disc is connected to
the shaft by an interference fit.
- Information on expected lifespan, considering creep, low cycle fatigue
and high cycle fatigue.
- Operation and maintenance manuals*.
- Arrangements of cooling system.
Note * Documentation is to
be provided applicable to two representative sizes in a generic
range of turbochargers.
1.4.6 Where considered necessary LR may require additional documentation to be
submitted.
1.4.7 The following information is to be submitted to LR for acceptance of oil mist
detection equipment and alarm arrangements:
- Description of oil mist detection equipment and system including alarms.
- Copy of the test house report in accordance with the
requirements of Test Specification No. 4. See also
Vol 2, Pt 2, Ch 1, 13.4 Crankcase oil mist detection system.
- Schematic layout of engine oil mist detection arrangements showing location
of detectors/sensors and piping arrangements and dimensions.
- Maintenance and test manual which is to include the following
information:
- Intended use of equipment and its operation;
- Functionality tests to demonstrate that the equipment is operational
and that any faults can be identified and corrective actions
notified;
- Maintenance routines and spare parts recommendations;
- Limit setting and instructions for safe limit levels; and
- Where necessary, details of configurations in which the equipment is
and is not to be used.
1.4.8 Where engine components are subject to autofrettage, the following
information is to be submitted ( see also
Vol 2, Pt 2, Ch 1, 2.4 Autofrettage):
- Drawings and other related documents/information for products
to be subjected to autofrettage, including material grade and
dimensions.
- Details of product quality assurance processes.
- Place of manufacture and details of external providers of
products subjected to autofrettage.
- A report detailing how repeatability and reliability of the
autofrettage process is achieved. This is to include the following:
- method of autofrettage;
- method to control extent of autofrettage;
- calibration of the autofrettage system; and
- details of how the critical parameters affecting product
characteristics are controlled.
- Method for recording results and list of data that is
recorded.
- Finished component and/or system testing.
1.5 Additional submission requirements for naval
vessels
1.5.2 Risk Assessment (RA) as required by Vol 2, Pt 1, Ch 3 Requirements for Design, Construction, Installation and Sea Trials of Engineering Systems is to be submitted. The RA is to be carried out in
accordance with the requirements of Vol 2, Pt 1, Ch 3, 18 Risk Assessment (RA) and is to include the following associated
sub-systems:
- Starting and stopping.
- Fuel oil.
- Lubricating oil.
- Cooling water (fresh and sea).
- Air induction.
- Exhaust.
- Engine mounting.
- Control and monitoring.
- Electrical power supplies.
- Hydraulic oil (for valve lift).
It is not necessary to consider failure modes relating to the engine
components.
Table 1.1.2 Plans and particulars to be
submitted for naval vessels
Document
|
For information
|
For appraisal
|
(X indicates reason for
submission)
|
Control engineering aspects in accordance with Vol 2, Pt 9 Electrotechnical Systems.
|
|
X
|
Details of the securing and collision arrangements (see also
Vol 2, Pt 1, Ch 3, 3.3 Calculations and specifications 3.3.5 and Vol 2, Pt 1, Ch 3, 5.3 Machinery fastenings to Vol 2, Pt 1, Ch 3, 5.7 Resin chocks).
|
|
X
|
Arrangement of interior lighting, where provided.
|
|
X
|
Calculations and information for short-term high power operation
where applicable.
|
X
|
|
Power/speed operational envelope.
|
X
|
|
Where it is proposed to use alloy castings, micro alloyed or alloy
steel forgings or iron castings: Details of the
chemical composition, heat treatment and mechanical
properties.
|
|
X
|
System Operational Concept covering the Propulsion system,
see
Vol 2, Pt 1, Ch 3, 3.4 System operational concept.
|
|
X
|
System Design Description for engine systems, see
Vol 2, Pt 1, Ch 3, 3 Documentation required for design review.
|
|
X
|
|