کد مقاله کد نشریه سال انتشار مقاله انگلیسی نسخه تمام متن
807691 1468224 2016 8 صفحه PDF دانلود رایگان
عنوان انگلیسی مقاله ISI
Derating design for optimizing reliability and cost with an application to liquid rocket engines
ترجمه فارسی عنوان
طراحی بار لازم برای بهینه سازی قابلیت اطمینان و هزینه با یک برنامه کاربردی برای موتور موشک مایع
کلمات کلیدی
نرخ شکست اسمی؛ بار لازم موتور؛ شیب پایداری رشد؛ توزیع نمایشی
موضوعات مرتبط
مهندسی و علوم پایه سایر رشته های مهندسی مهندسی مکانیک
چکیده انگلیسی


• Modeled the effect of derating design on the reliability and the development cost.
• Discovered that derating design may reduce the cost of reliability demonstration test.
• Optimized the derating design parameter for reliability maximization or cost minimization.

Derating is the operation of an item at a stress that is lower than its rated design value. Previous research has indicated that reliability can be increased from operational derating. In order to derate an item in field operation, however, an engineer must rate the design of the item at a stress level higher than the operational stress level, which increases the item׳s nominal failure rate and development costs. At present, there is no model available to quantify the cost and reliability that considers the design uprating as well as the operational derating. In this paper, we establish the reliability expression in terms of the derating level assuming that the nominal failure rate is constant with time for a fixed rated design value. The total development cost is expressed in terms of the rated design value and the number of tests necessary to demonstrate the reliability requirement. The properties of the optimal derating level are explained for maximizing the reliability or for minimizing the cost. As an example, the proposed model is applied to the design of liquid rocket engines.

ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Reliability Engineering & System Safety - Volume 146, February 2016, Pages 13–20
نویسندگان
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