以系統工程管理觀念探討航空器機隊管理之研究

A Research of Fleet Management for Aerial Vehicle by the Concepts of System Engineering Management

李建華(Jiam-Hwa Lee)

《建國科大學報》 24卷4期 (2005/07) Pp. 89-99

https://doi.org/10.6995/JCTU.200507.0089

摘要

系統工程管理係在滿足顧客需求條件下，各部門學科間之工程管理過程中，所展開與驗證相關系統之整合，及壽命循環平衡的答案而言。因此，系統工程管理主要在研究三項主題，其一是全程發展階段，旨在控制設計過程及提供協調設計功能之基本條件；第二是系統工程方法，主要是提供一個架構藉以解決設計問題及設計功能之需求流程；第三係強調壽命循環整合工作，在設計過程中已經考量系統開發之壽命能夠滿足顧客之需求條件。在展開階段與系統工程過程之間應該建構一個基準規範，而系統工程過程與壽命循環整合之間，必須籌組一個整合小組去執行工作。再者，在展開階段與壽命循環間必須擬定一個壽命循環計畫，界定產品之壽命週期之管理方法。
機隊管理主要在規劃飛行器之使用壽命期限內之管理作為，在全程發展階段中依據訂定之飛機結構整合計畫的設計規範說明飛機使用任務分配、類型及耐久性與破壞容許的規格，進行飛行資料收集及分析。在系統工程處理過程內研究所有資料所呈現之趨勢，藉以管理飛機之任務規劃。如何令飛機機隊中每一架飛機之飛行經歷均能紀錄起來，又如何整合全部飛機的飛行歷史，這就是機隊管理執行系統開發壽命研究必須規劃之主軸。然而管理之學門包含非常之廣泛，必須考量機隊實際在執行任務時之特性，以及飛機在設計開發階段中其系統整合方法，研究機隊管理之飛機負載譜驗證、單機追蹤以及結構維修計畫三大主軸的工程。

關鍵字

系統工程管理 ； 結構整合 ； 機隊管理

並列摘要

To satisfy the customer need, systems engineering management is an interdisciplinary engineering management process that evolves and verifies an integrated, life cycle balanced set of system solutions. Systems engineering management is accomplished by integrating three major activities. First, development phasing controls the design process and provides baselines that coordinate design efforts. Second, a systems engineering process provides a structure for solving design problems and tracking requirements flow through the design effort. Third, life cycle integration involves customers in the design process and ensures that the system developed is viable throughout its life. A set of baselines has to be defined between development phasing and systems engineering process. An integrated team processes the linkage of the life cycle integration and the systems engineering process. A life cycle planning has to be developed to combine the development phasing and the life cycle integration.
The fleet management program manages the activities under the aerial vehicle service life. Based on the aircraft structural integrity program, the fleet management provides the elements necessary to maintain the structural integrity by developing the analytical capability to evaluate the effects on safety limits, durability limits, fatigue life, and inspection/repair/modification intervals resulting from variations in fleet and individual airplane operational usage; monitoring the actual usage of production aircraft utilizing data recorded during the operational usage; and assessing the impacts of the actual usage and variations in usage on the structural integrity of the airframe and landing gears.

並列關鍵字

System engineering management ； structural integrity ； and fleet management