Browse Topic: Computer integrated manufacturing
Rapid advances in high fidelity modeling and high performance computing capabilities have enabled their routine utilization in support of aircraft design. Analysts are able to generate orders of magnitude more data that must then be turned into actionable intelligence to guide design. Enabling effective application of advanced analysis to design requires a robust end-to-end digital transformation to make the simulation processes reusable, repeatable, traceable, scalable and minimize setup errors. This is achieved through the development of a Computational Fluid Dynamic (CFD) modeling framework where streamlining and automation are inserted within the current CFD workflow that involves model setup, simulation and post processing. Workflow automation techniques have been implemented in simulation pre and post processing that reduce the overall process time or enhance the fidelity of the simulation. To conduct CFD evaluations through flight envelope efficiently, space filling methods that take into account uncertainties of complex systems are needed and have driven updates to the boundary condition and design of experiments (DOE) generation within the workflow. Vehicle sub-system design can be highly iterative, performed by a large number of participants in multidisciplinary groups. To ensure traceability across the digital thread, a provenance and metadata storage methodology has been implemented to capture information about CFD simulations and construct a query able database while a model-based systems engineering (MBSE) framework provides a structured and integrated approach to managing information throughout the product lifecycle. The SIM-FIX-SIM approach enabled with a robust analysis framework for digital flight assessment prior to first flight will contribute to the overall goal of reducing development timelines and achieving cost reduction goals for cutting-edge rotorcraft development programs.
A primary factor for the development of military avionics systems is the requirement for a Modular Open System Architecture (MOSA). The US Department of Defense (DoD) is driving MOSA-compliant systems to achieve benefits in cost and flexibility within their procurements. MOSA definitions are examined in light of advances in computing disciplines that open the interfaces necessary for the aircraft operator to update and manage their fleet's Health Awareness Systems (HAS). Opening the relevant HAS interfaces via software configuration toolsets and MOSA building blocks avoids contracting for costly software changes and gives control of the update to the operator. Two business related factors are presented for consideration in developing the best way forward while using MOSA principles to guide development. These factors are (1) Intellectual Property (IP) and (2) the underlying investments companies make to develop IP. The need to routinely update the HAS to incorporate fleet lessons learned is inherent in the system's support. Updates may also reflect new methodologies that deliver the desired system control to the operator. The paper demonstrates a MOSA-compliant architecture via an example. Within the example, efficiencies are driven by an end-to-end Digital Thread that minimizes errors and rework while reducing the overall cost of change for the full platform lifecycle. The approach enables organic operator support, lowering the overall cost of aircraft operations. The design and support of the platform’s Health Awareness System benefits from the application of linked-automation.
The U.S. Army monitors the structural integrity of its rotary-wing aircraft fleet through annual evaluations and reporting via the Airframe Condition Evaluation (ACE) program. ACE evaluations capture the location and character of structural defects for each aircraft, which are then available for trending and detailed analysis by engineers with the U.S. Army Combat Capabilities Development Command Aviation & Missile Center (CCDC AvMC). As analytic methods are increasingly advanced through the digital thread, CCDC AvMC has sought to improve available trending, modeling, and analysis tools beyond status quo to provide higher fidelity visuals to both aid communication with decision makers, and also to reveal structural defect trends which may not otherwise be evident. This paper will detail the development and utility of the ACE Color Mapping Application within the ACE Mapping Module and its impact on product support of U.S. Army aircraft with regard to airframe structural integrity.
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