46 C.F.R. Subpart 58.10—Internal Combustion Engine Installations
Title 46 - Shipping
(a) Engine design. All installations shall be of marine type engines suitable for the intended service, designed and constructed in conformance with the requirements of this subchapter. (b) Carburetors. (1) Drip collectors shall be fitted under all carburetors, except the down-draft type, to prevent fuel leakage from reaching the bilges and so arranged as to permit ready removal of such fuel leakage. Drip collectors shall be covered with flame screens. Note: It is recommended that drip collectors be drained by a device for automatic return of all drip to engine air intakes. (2) All gasoline engines must be equipped with an acceptable means of backfire flame control. Installations of backfire flame arresters bearing basic Approval Nos. 162.015 or 162.041 or engine air and fuel induction systems bearing basic Approval Nos. 162.015 or 162.042 may be continued in use as long as they are serviceable and in good condition. New installations or replacements must meet the applicable requirements of this section. (3) The following are acceptable means of backfire flame control for gasoline engines: (i) A backfire flame arrester complying with SAE J–1928 or UL 1111 and marked accordingly. The flame arrester must be suitably secured to the air intake with a flametight connection. (ii) An engine air and fuel induction system which provides adequate protection from propagation of backfire flame to the atmosphere equivalent to that provided by an acceptable backfire flame arrester. A gasoline engine utilizing an air and fuel induction system, and operated without an approved backfire flame arrester, must either include a reed valve assembly or be installed in accordance with SAE J–1928. (iii) An arrangement of the carburetor or engine air induction system that will disperse any flames caused by engine backfire. The flames must be dispersed to the atmosphere outside the vessel in such a manner that the flames will not endanger the vessel, persons, on board, or nearby vessels and structures. Flame dispersion may be achieved by attachments to the carburetor or location of the engine air induction system. All attachments must be of metallic construction with flametight connections and firmly secured to withstand vibration, shock, and engine backfire. Such installations do not require formal approval and labeling but must comply with this subpart. (c) Exhaust manifold. The exhaust manifold shall either be water-jacketed and cooled by discharge from a pump which operates whenever the engine is running, or woodwork within nine inches shall be protected by (d) Exhaust pipe. (1) Exhaust pipe installations shall conform to the requirements of the American Boat and Yacht Council Standard P–1 “Safe Installation for Exhaust Systems” and National Fire Protection Association Standard NFPA 302, part 1, section 23 and the following additional requirements: (i) All exhaust installations with pressures in excess of 15 pounds per square inch gage or employing runs passing through living or working spaces shall meet the material requirements of part 56 of this subchapter. (ii) Horizontal dry exhaust pipes are permitted only if they do not pass through living or berthing spaces, they terminate above the deepest load waterline and are so arranged as to prevent entry of cold water from rough or boarding seas, and they are constructed of corrosion resisting material “at the hull penetration.” [CGFR 68–82, 33 FR 18878, Dec. 18, 1968, as amended by CGD 88–032, 56 FR 35824, July 29, 1991] (a) The requirements of §58.10–5 (a), (c), and (d) shall apply to diesel engine installations. (b) A diesel engine air intake on a mobile offshore drilling unit must not be in a classified location.1 (c) A diesel engine exhaust on a mobile offshore drilling unit must not discharge into a classified location.1 1 Sections 108.171 to 108.175 of this chapter define classified locations for mobile offshore drilling units. [CGFR 68–82, 33 FR 18878, Dec. 18, 1968, as amended by CGD 73–251, 43 FR 56801, Dec. 4, 1978; CGD 95–028, 62 FR 51202, Sept. 30, 1997] (a) Standards. The design, construction, workmanship and tests of gas turbines and their associated machinery shall be at least equivalent to the standards of the American Bureau of Shipping or other recognized classification society. (b) Materials. The materials used for gas turbine installations shall have properties suitable for the intended service. When materials not conforming to standard ASTM specifications are employed, data concerning their properties, including high temperature strength data, where applicable, shall be furnished. (c) Exhausts. (1) Where piping is used for gas turbine exhaust lines, Class II is required as a minimum. (See subpart 56.04 of this subchapter.) Where the exhaust pressure exceeds 150 pounds per square inch, such as in closed cycle systems, Class I shall be used. Where ducting other than pipe is employed, the drawings and design data shall be submitted to substantiate suitability and safety for the intended service. (2) Where considered necessary, gas turbines and associated exhaust systems shall be suitably insulated or cooled, by means of lagging, water spray, or a combination thereof. (3) Gas turbine exhausts shall not be interconnected with boiler uptakes except for gas turbines used for emergency power and lighting or for emergency propulsion. Dampers or other suitable means shall be installed to prevent backflow of boiler exhaust gases through the turbine. Interconnected exhausts must be specifically approved by the Commandant. (4) A gas turbine exhaust on a mobile offshore drilling unit must not discharge in a classified location.1 (d) Air inlets. Air inlets must be designed as follows: (1) Each air inlet must have means to protect the safety of life and to prevent the entrance of harmful foreign material, including water, into the system. (2) A gas turbine air inlet must not be in a classified location.1 1 Sections 108.171 to 108.175 of this Chapter define classified locations for mobile offshore drilling units. (e) Cooling and ventilation. Means shall be provided for circulating air, either natural or forced, through the engine compartment for cooling and ventilation. (f) Automatic shutdown. (1) The control system shall be designed for automatic shutdown of the engine with actuation of audible and visible alarms at shutdown. The visible malfunction indicator shall indicate what condition caused the shutdown and remain visible until reset. Automatic shutdown shall occur under the following conditions: (i) Overspeed. (ii) Low lubricating oil pressure. Consideration will be given providing alarm only (without shutdown) in those cases where suitable antifriction bearings are fitted. (2) Audible or visible alarms shall also be provided for: (i) Excessive gas temperature, measured at the turbine inlet, gas generator, interstage turbine or turbine exhaust. (ii) Excessive lubricating oil temperature. (iii) Excessive speed. (iv) Reduced lubricating oil pressure. (3) A remote, manually operated shutdown device shall be provided. Such device may be totally mechanical or may be electrical with a manually actuated switch. (g) Drawings and design data. Drawings and design data of the following components shall be submitted to substantiate their suitability and safety for the service intended: (1) Combustion chamber. (2) Regenerator or recuperator. (3) Casing or piping conveying the gas from the combustion device to the gas turbine. (h) Fuel systems. Gas turbine fuel systems shall meet the requirements of part 56 of this subchapter. (i) Fire extinguishing systems. A special local fire extinguishing system may be required for gas turbine installations if considered necessary by the Commandant. Such a system would be in addition to any other required in the compartment in which the gas turbine is located. [CGFR 68–82, 33 FR 18878, Dec. 18, 1968, as amended by CGFR 72–59R, 37 FR 6190, Mar. 25, 1972; CGD 73–251, 43 FR 56801, Dec. 4, 1978; CGD 83–043, 60 FR 24776, May 10, 1995]
Title 46: Shipping
PART 58—MAIN AND AUXILIARY MACHINERY AND RELATED SYSTEMS
Subpart 58.10—Internal Combustion Engine Installations
§ 58.10-5 Gasoline engine installations.
§ 58.10-10 Diesel engine installations.
§ 58.10-15 Gas turbine installations.
