2018
DOI: 10.1007/s11709-018-0493-3
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Impact analysis of compressor rotor blades of an aircraft engine

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Cited by 11 publications
(2 citation statements)
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“…strength, along with their ease of formability for complex shapes and parts [8]. Specifically, 7075-T6 alloy possesses higher yield and ultimate strength, with slightly higher density than the 6061-T6 alloy [9]. In automotive applications, approximately 25% to 30% of a vehicle's weight consists of aluminum components; most of which are fabricated from 5000 and 6000 series aluminum alloys.…”
Section: Journal Of Engineering and Technological Sciencesmentioning
confidence: 99%
“…strength, along with their ease of formability for complex shapes and parts [8]. Specifically, 7075-T6 alloy possesses higher yield and ultimate strength, with slightly higher density than the 6061-T6 alloy [9]. In automotive applications, approximately 25% to 30% of a vehicle's weight consists of aluminum components; most of which are fabricated from 5000 and 6000 series aluminum alloys.…”
Section: Journal Of Engineering and Technological Sciencesmentioning
confidence: 99%
“…A typical low-cost proximity β-titanium alloy (Ti-10V-2Fe-3Al or TB6) can reduce the mass of air vehicles by approximately 20% [7][8][9] compared to a TC4 titanium alloy in aeronautic manufacturing. However, aircrafts are often impacted by flying stones during takeoff and landing, and their structural components are highly susceptible to loss of efficacy due to friction and wear under the long-term accumulation effect 10 . Furthermore, in the joints of a helicopter rotor system under high-frequency alternating loads, the interaction between the central part of the main rotor hub and the surrounding lug connectors lead to severe fretting wear.…”
Section: Introductionmentioning
confidence: 99%