Browse Topic: Life cycle analysis
ABSTRACT Rubber tracks are now extremely competitive for vehicles up to 50 tons and fully fielded on 39 ton vehicles. They represent the best of what technology can offer for tracked vehicles, in terms of high durability, performance and low life cycle cost. This is mainly attributed to the optimization through the five (5) technological tools described in this paper. Better from its numerous distinctive advantages, rubber tracks can be adapted to suit virtually any specific need. This ductile rubber track technology can be shaped to match today’s requirements, with the help of advanced rubber compounding and computer simulations.
This recommended best practice outlines a method for estimating CO2-equivalent emissions using life cycle analysis.
The Structures Division at the Naval Air Systems Command (NAVAIR) continues to support capital investment in enabling technologies for sustainment of our aircraft which will lower total life cycle costs, ensure safety, and increase operational readiness. This paper presents a general overview of the major improvements which have been made in the area of Structural Health and Usage Management (SHUM), including: usage severity monitoring via regime recognition (RR), gross weight and center of gravity (GW/CG) estimation, local/global damage detection, environmental effects monitoring, damage alleviation, prognostication, and individual asset/component tracking (IAT). Advances in structural analyses have been made in the accuracy of predicted rotorcraft loads using coupled rotor and fuselage interactions. Innovative approaches to fatigue testing at both the component and full scale airframe levels will allow for more accurate introduction of vibratory loading content from operation, reveal failure modes, and improve fatigue life predictions. Additive manufacturing (AM) of fly-away aircraft parts and the standardization of cold spray repair applications present unique qualification challenges and benefits to the warfighter.
ABSTRACT Aftermarket support has become a key component of cost and competitiveness in the rotorcraft industry. Both the operator and the rotorcraft manufacturer play a role in aftermarket support. Many rotorcraft original equipment manufacturers (OEMs) are offering fixed price maintenance service programs in their after-market support programs. Since product support may last well over two decades, the desire for low direct operating cost (DOC) and lower life cycle cost (LCC) has become a more visible consideration in the rotorcraft design phase. Direct maintenance cost (DMC), forms a significant part of the DOC and LCC. A subset of DMC, On-condition maintenance cost is a category with unspecified maintenance intervals and presents one of the more challenging estimating efforts, particularly on a new rotorcraft program with no history. The approach used for estimating maintenance costs can strongly influence decision making within the OEM while also educating the customer on better maintenance philosophy and planning. Incorrectly minimizing or excluding the effect of on-condition cost (within the DMC estimate) could have a profound impact on operator and service organizations of the OEM. This paper presents a high-level discussion on the potential refinements that can be made to the Helicopter Association International’s Economic Committee’s Guide for the Presentation of Helicopter Operating Cost Estimates 2010. Estimating the on-condition direct maintenance cost for airframe manufacturers is the focus of the discussion.
ABSTRACT Current VTOL aircraft design processes require significant changes in computational methodologies resulting from innovations in distributed hybrid and electric propulsion technology. Electric VTOL (eVTOL) aircraft design offers radically different configurations by eliminating limitations in weight, size and location of Internal Combustion Engines (ICE) and associated fuel systems. Hybrid Distributed Electric Propulsion (HDEP) solutions, to include eVTOL, allow designers to incorporate a greater number of smaller, lightweight propulsors throughout the airframe structure as necessary to meet complex mission requirements. Additional benefits of HDEP versus fossil fuel counterparts, include reduced acoustic and thermal signatures and lighter and smaller structures. Because of the many advantages of DEP, it is quickly becoming the preferred choice for autonomous aircraft design. This paper addresses the necessary changes to VTOL Synthesis to include DEP and Autonomy for HDEP aircraft. Two of the authors, Dr. Daniel P. Schrage and Mr. Kaydon Stanzione have substantial expertise and experience in VTOL aircraft design and the methodologies for vehicle synthesis. They will use this expertise and experience to identify and present the necessary changes in the VTOLTradeoff Environment (VTE) for HDEP VTOL aircraft design and assessment. The VTE will also be focused on using an Overall Evaluation Criterions (OEC) for the VTE that address value as a ratio of System Effectiveness to Life Cycle Cost (LCC). The third author, Dr. Apinut "Nate" Sirirovisuth, a research fellow in the Georgia Tech's Integrated Product Lifecycle Engineering (IPLE) Laboratory, and a Cost Research Analyst at PRICE Systems has significant experience in VTE modeling efforts and is an expert in affordability analysis for advanced aerospace systems.
Thales Paris La Défense Cedex, France +33 (0)1 57 77 86 26
ABSTRACT The Department of Defense (DOD) will design, develop, and field a fleet of air vehicles that will ensure the United States' dominance in the vertical lift domain through the 21st century and beyond. DOD will aggressively pursue the most capable aircraft at the best value by minimizing development, acquisition, and life cycle costs through Joint solutions of multi-role, common core technologies, architectures, and training, emphasizing the ability to conduct safe, reliable and continuous operations world-wide in all environmental conditions. Future Vertical Lift (FVL) is a revolutionary approach to vertical lift capabilities development across Joint operations and is aligned with the DOD Strategic Guidance. Strategic advances in capabilities include: worldwide self deployment; twice the average speed of the current fleet; twice the average range of the current fleet; increased payloads; worldwide operations; increased survivability; common systems approach; buildable and affordable; and is informed by government and industry technology development.
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