2007
DOI: 10.1016/j.cirp.2007.05.027
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Machining of High Strength Light Weight Alloys for Engine Applications

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Cited by 43 publications
(15 citation statements)
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“…As the inner wall diameter is of only φ76mm, it makes the size of the blind hole drilling devices more restricted, not only to achieve a compact overall structure, but also to ensure that the gear has sufficient strength [8]. Bevel gear drive process generally requires consideration of tooth contact fatigue strength and tooth root bending fatigue strength.…”
Section: The Structural Design Of the Blind Hole Drilling Devicementioning
confidence: 99%
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“…As the inner wall diameter is of only φ76mm, it makes the size of the blind hole drilling devices more restricted, not only to achieve a compact overall structure, but also to ensure that the gear has sufficient strength [8]. Bevel gear drive process generally requires consideration of tooth contact fatigue strength and tooth root bending fatigue strength.…”
Section: The Structural Design Of the Blind Hole Drilling Devicementioning
confidence: 99%
“…It is difficult to visually observe the cutting conditions but it is easy to block debris and knife fight [3].…”
Section: Introductionmentioning
confidence: 99%
“…Increasing demands in the turbomachinery sector lead to further use of advanced materials with distinguished physical properties, resulting in high thermal and mechanical loads during machining [1][2][3]. A common task is the manufacture of complex geometrical features, that can be abstracted to notches or slots described by two or three boundaries, as they occur, for example, in the geometries of Blisks (blade integrated discs), single blades, and landing gears; see Figure 1.…”
Section: Applicationsmentioning
confidence: 99%
“…Another way is to reduce the weight of fast rotating turbine blades in aircraft engines. Beside the commonly used Ni-based superalloys γ − titanium aluminides offer the required high specific strength from room-temperature up to 1000°C [1,2]. With a specific weight of 3.8 g/cm³ compared to 8 g/cm³ of Ni-based superalloys the overall weight of the components could be reduced drastically.…”
Section: Introduction *mentioning
confidence: 99%