단일부품 정지능력하의 부하분담시스템의 최적 신뢰성
Optimal Reliability of a Load-Sharing System under One-Component-Out Capability
최지혜(삼성전자 메모리사업부); 간가푸라므 스리단야(건국대학교 산업공학과); 김경미(건국대학교)
48권 1호, 1~10쪽
초록
Most of previous researches in a load sharing system have focused on expressing reliability of a given system under the assumption that the number of components used in the system is pre-fixed. Only one recent research has studied the optimal number of components for maximizing system reliability under one-component-out capability, assuming that the component follows an exponential lifetime distribution and a power function explains the load-life relationship. This paper intends to generalize such a result to consider the general distribution for the component lifetime and the general functional for the load-life relationship. We derive the system reliability in terms of the number of components used in the system. A numerical example is given to illustrate the optimal number of engines to maximize reliability of the liquid rocket propulsion system. The result indicates that a large number of components each withstanding a small load is preferred to a small number of components each withstanding a large load if the component failure rate increases with time and the failure rate decreases fast with the reduction in the design load.
Abstract
Most of previous researches in a load sharing system have focused on expressing reliability of a given system under the assumption that the number of components used in the system is pre-fixed. Only one recent research has studied the optimal number of components for maximizing system reliability under one-component-out capability, assuming that the component follows an exponential lifetime distribution and a power function explains the load-life relationship. This paper intends to generalize such a result to consider the general distribution for the component lifetime and the general functional for the load-life relationship. We derive the system reliability in terms of the number of components used in the system. A numerical example is given to illustrate the optimal number of engines to maximize reliability of the liquid rocket propulsion system. The result indicates that a large number of components each withstanding a small load is preferred to a small number of components each withstanding a large load if the component failure rate increases with time and the failure rate decreases fast with the reduction in the design load.
- 발행기관:
- 한국경영과학회
- 분류:
- 경영학