کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
5469865 | 1519295 | 2016 | 6 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Assessment of Aero Engine Assemblability During Preliminary Design
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مهندسی صنعتی و تولید
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چکیده انگلیسی
Unabated growth of air traffic interacting with increasing competition between the airlines continuously raises the economic pressure in the aerospace supply chain. New products, such as aircrafts and aero engines, have to be designed to match the resulting requirements. Hence it is important to assess production cost as well as producibility of aero engines already at an early stage during preliminary design. Assessing the assemblability is a vital task in this context. The level of design detail which is required to realize such an assessment has been investigated using a low pressure turbine module as an example. It turns out that the level of detail currently offered by many preliminary design tools will have to be increased moderately.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Procedia CIRP - Volume 57, 2016, Pages 473-478
Journal: Procedia CIRP - Volume 57, 2016, Pages 473-478
نویسندگان
Jochen Rendle, Stephan Staudacher,