Transportability Testing of the Marine Corps Light Weight Prime Mover (LWPM) TP-94-01 Transportability Testing Procedures

The possibility of sustained flight by heavier-than-air-machiaes was fully recognised during the last century by those who had studied the aerodynamic problems involved and it was realised that its accomplishment awaited only the development of a prime mover of sufficiently light weight.Of all the known forms of prime mover, the internal combustion engine alone held out any promise of fulfilling the conditions necessary .for sustained flight, namely, light weight not only of the engine itself but also of the fuel it consumes. Early attempts had, however, been made to fly with steam, propulsion and it is of interest to note that the very remarkable and cleverly-designed steam plant employed by Sir Hiram Maxim in 1894 was actually very considerably lighter per h.p., even including the boiler and condenser, than the petrol engine used successfully some nine years later by the Wright Brothers.

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CODAG Propulsion Machinery by Stal-Laval for Royal Danish Navy Frigates

Journal of Engineering for Power ◽

10.1115/1.3616631 ◽

1967 ◽

Vol 89 (1) ◽

pp. 86-93 ◽

Cited By ~ 3

Author(s):

Bo R. V. Kumlin

Keyword(s):

Gas Turbine ◽

Fuel Consumption ◽

Gas Turbines ◽

Light Weight ◽

Prime Mover ◽

Jet Engine

Two gas turbine-powered frigates for the Royal Danish Navy will go on sea trials during 1966. The CODAG propulsion units have good fuel consumption characteristics and light weight. Freewheeling clutches on each prime mover and a controllable pitch propeller have simplified the gear arrangement and the maneuvering procedure. The jet engine-powered gas turbines and the gears are described in some detail in the paper, which ends with a summary of the results from shop tests with the complete propulsion units.

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Microstructure of an extruded rapidly solidified Al-8Fe-2Mo alloy

Proceedings, annual meeting, Electron Microscopy Society of America ◽

10.1017/s0424820100144218 ◽

1986 ◽

Vol 44 ◽

pp. 548-549

Author(s):

W. T. Donlon ◽

J. E. Allison ◽

S. Shinozaki

Keyword(s):

Electron Microscopy ◽

Automotive Industry ◽

Fuel Economy ◽

High Strength ◽

Al Alloys ◽

Light Weight ◽

Thin Sections ◽

Strength And Durability ◽

Rapidly Solidified ◽

Whitney Aircraft

Light weight materials which possess high strength and durability are being utilized by the automotive industry to increase fuel economy. Rapidly solidified (RS) Al alloys are currently being extensively studied for this purpose. In this investigation the microstructure of an extruded Al-8Fe-2Mo alloy, produced by Pratt & Whitney Aircraft, Goverment Products Div. was examined in a JE0L 2000FX AEM. Both electropolished thin sections, and extraction replicas were examined to characterize this material. The consolidation procedure for producing this material included a 9:1 extrusion at 340°C followed by a 16:1 extrusion at 400°C, utilizing RS powders which have also been characterized utilizing electron microscopy.

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