This paper presents a brief description and several illustrations of a new concept of marine reversing gears that utilize high-performance differentially driven epicyclic gear arrangements. This new marine power transmission has the potential to offer high reliability, simplicity, light weight, high mechanical efficiency, compactness, and technological compatibility with aircraft derivative marine gas turbine engines. Further, this new reversing gear minimizes the danger of driving the free turbine in reverse as might be the case with conventional parallel shaft reversing gear arrangements. To illustrate the weight reduction potential, a modern naval ship propulsion system utilizing an aircraft derivative gas turbine engine as the prime mover in conjunction with a conventional parallel shaft reversing gear can be compared to the subject reversing gear differential. A typical 18,642 kW (25,000 hp) marine gas turbine engine might weigh approximately 5000 kg (11,000 lb) and a conventional marine technology parallel shaft reversing gear might weigh on the order of 90,000 to 136,000 kg (200,000 to 300,000 lb). Using gear technology derived from the aircraft industry, a functionally similar differentially driven marine reversing gear might weigh approximately 13,600 kg (30,000 lb).
Skip Nav Destination
Article navigation
October 1988
Research Papers
A New Concept of High-Performance Marine Reversing Reduction Gears
D. J. Folenta
D. J. Folenta
Transmission Technology Co., Inc., Fairfield, NJ 07006
Search for other works by this author on:
D. J. Folenta
Transmission Technology Co., Inc., Fairfield, NJ 07006
J. Eng. Gas Turbines Power. Oct 1988, 110(4): 572-577 (6 pages)
Published Online: October 1, 1988
Article history
Received:
November 30, 1987
Online:
October 15, 2009
Article
Article discussed|
View article
Connected Content
A commentary has been published:
Discussion: “Transient Response of Floating Ring Liquid Seals” (Kirk, R. G., 1988, ASME J. Tribol., 110, pp. 572–577)
Citation
Folenta, D. J. (October 1, 1988). "A New Concept of High-Performance Marine Reversing Reduction Gears." ASME. J. Eng. Gas Turbines Power. October 1988; 110(4): 572–577. https://doi.org/10.1115/1.3240173
Download citation file:
15
Views
Get Email Alerts
Cited By
Temperature Dependence of Aerated Turbine Lubricating Oil Degradation from a Lab-Scale Test Rig
J. Eng. Gas Turbines Power
Multi-Disciplinary Surrogate-Based Optimization of a Compressor Rotor Blade Considering Ice Impact
J. Eng. Gas Turbines Power
Experimental Investigations on Carbon Segmented Seals With Smooth and Pocketed Pads
J. Eng. Gas Turbines Power
Related Articles
A New Approach to Evaluating the In-Service Performance of Marine Gas Turbine Air Filters
J. Eng. Gas Turbines Power (October,1988)
U. S. Navy’s Marine Gas Turbines
J. Eng. Power (January,1967)
Propulsion System Requirements for Long Range, Supersonic Aircraft
J. Fluids Eng (March,2006)
Gear Design and Laboratory Experience—Marine Gas Turbine Propulsion
J. Eng. Power (October,1969)
Related Proceedings Papers
Related Chapters
Novel and Efficient Mathematical and Computational Methods for the Analysis and Architecting of Ultralight Cellular Materials and their Macrostructural Responses
Advances in Computers and Information in Engineering Research, Volume 2
Later Single-Cylinder Engines
Air Engines: The History, Science, and Reality of the Perfect Engine
Direct Monte Carlo Simulation for the Reliability Assessment of a Space Propulsion System Phased Mission (PSAM-0067)
Proceedings of the Eighth International Conference on Probabilistic Safety Assessment & Management (PSAM)