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Journal ArticleDOI

Materials for Gas Turbines

R. J. E. Glenny, +2 more
- 01 Jan 1975 - 
- Vol. 20, Iss: 1, pp 1-28
TLDR
The major components of gas turbines and their materials requirements are outlined in this paper, and the properties, advantages, and limitations of materials which have been and are being used in gas turbines are described in the following groups: aluminium alloys, magnesium alloy, titanium and its alloy, steels, and finally nickel and cobalt base alloys.
Abstract
The major components of gas turbines and their materials requirements are outlined. The properties, advantages, and limitations of materials which have been and are being used in gas turbines are then described in the following groups: aluminium alloys, magnesium alloys, titanium and its alloys, steels, and finally nickel- and cobalt-base alloys. The applications of the last group of alloys and the importance of their metallurgical stability in turbine blades, discs, nozzle guide vanes, and sheet metal components are discussed. Corrosion and its prevention are then considered, followed by sections on experimental materials including alloys of chromium and the refractory metals, ceramics, and fibre composites. Future trends and prospects are discussed briefly in a concluding section.

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Citations
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Metal-ceramic composites via in-situ methods

TL;DR: In this paper, a review of in situ metal/ceramic composite materials with a greater emphasis on directed melt oxidation and nitridation is presented, and the mechanical properties, toughening mechanisms and potential applications are briefly reviewed.
Journal ArticleDOI

Laser cladding of high-temperature coatings

TL;DR: In this article, the processing and microstructural characteristics of nickel-based superalloys obtained by high-power laser surface cladding were studied, where the processing variables were laser power, scan velocity and the composition of the feeder powder.
Journal ArticleDOI

Failure of a low pressure turbine rotor blade of an aeroengine

TL;DR: In this paper, a low-pressure turbine rotor blade had failed during a test run of an aeroengine, during which a Ni-base superalloy of CM 247 LC grade was fabricated by DS investment casting.
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Microstructure and intermediate-temperature mechanical properties of powder metallurgy Ti–6Al–4V alloy prepared by the prealloyed approach

TL;DR: In this paper, the mechanical properties of powder metallurgy (P/M) Ti-6Al-4V alloys, produced from prealloyed powders by hot isostatic pressing, were evaluated over the intermediate temperature range of 300-500°C.
References
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Journal ArticleDOI

Deposition and Corrosion in Gas Turbines

TL;DR: In this paper, the authors discuss deposition and corrosion in Gas Turbines, and propose a method to detect the presence of such defects in a Gas Turbinet.
Journal ArticleDOI

A new protective coating for nickel alloys

TL;DR: In this article, the LDC-2 coating was used to prolong the life of high-temperature components of aircraft turbines by an aluminium diffusion treatment following galvanic platinum deposition.
Journal ArticleDOI

Production and properties of high modulus carbon fibres

TL;DR: Carbon fibres of Young modulus 410 GN m -2 (60 x 10 6 lbf in -2 ) consist of graphite crystal-lites with their basal planes having a preferred orientation of within 10° to the fibre axis.