58.10-15—Gas turbine installations.
(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 the ABS Steel Vessel Rules (incorporated by reference, see 46 CFR 58.03-1 ).
(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
(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.
Code of Federal Regulations
Footnote(s): 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:
(ii)
Low lubricating oil pressure. Consideration will be given providing alarm only (without shutdown) in those cases where suitable antifriction bearings are fitted.
(i)
Excessive gas temperature, measured at the turbine inlet, gas generator, interstage turbine or turbine exhaust.
(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:
(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; USCG-2003-16630, 73 FR 65187, Oct. 31, 2008]