Initial Design Considerations For A Hierarchical Ic Design System

Author(s):  
W.M. vanCleemput ◽  
E.A. Slutz
2019 ◽  
Vol 2019 (1) ◽  
pp. 000284-000288
Author(s):  
Bill Acito ◽  

Abstract Just as we transitioned from simplistic lead frames to large ball grid arrays decades ago, we find ourselves again at another inflection point in design. Originally a derivative of PCB design, IC package design finds itself straddling both PCB-style design and traditional IC design. Dimensions have shrunk to place IC package design squarely in the same design dimensions as integrated circuits. Likewise, with Moore's law rapidly losing steam to support SoC's as a system integration vehicle, advanced package technologies have been asked to fill the system enablement gap. We now see advanced packaging technologies with silicon content as the system enabler in 2.5D, 3D and fanout wafer-level packaging. Because of the silicon and small geometries, IC design flows and signoff mechanisms are being used to design the next-generation of packaged systems. Package design now finds itself in the forefront of system-level design enablement. Where once system aggregation was done in a SoC at the silicon level, packaging is being used to build a system from technology-optimized die from each functional area (memory, processing, and interfaces). Silicon is no longer just a substrate material for IC manufacturing but a “package” substrate and functional integration vehicle. As such, package design teams find themselves adding IC-based design flows and methodologies. Package designers must look to the IC tools for routing, DRC, and signoff capabilities. Designers are looking for next-generation EDA tools to support these new integration and design challenges, including LVS-like validation checks and IC-based design rules. Rather than transitioning the design team from traditional packaging tools to IC tools entirely, we propose that users can leverage complete design flows that merge the best-in-class capabilities from each of their respective design domains. Is this regard, the best-in-class capabilities can remain in their respective domains, and a design flow can be created that relies on tight integration between both domains. These flows can also leverage a single point of entry for design capture and system level management. Flows based on the system management tool and the appropriate features in each of the domains can be created that enable and optimize complex designs that meet physical, signal integrity, cost and performance requirements. We will describe how capabilities can be leveraged from both domains in a tightly coupled flow, overseen by a design system-management tool, to address the challenges of advanced-technology and silicon-based system.


1990 ◽  
Vol 112 (2) ◽  
pp. 212-216 ◽  
Author(s):  
J. E. Jenista ◽  
D. S. Bodden

The program covering the design and early technology development of Configuration E-7, a supersonic STOVL Fighter/Attack aircraft, is described. This aircraft uses the ejector principle to augment engine fan air for vertical lift. The initial design objectives selected in 1980 are listed and discussed. Some design considerations applicable to the propulsion concept and the chosen configuration are mentioned. The test program accomplished thus far, including wind tunnel models plus other test articles and activities, is outlined. The program has proceeded without major technological obstacles and a full-scale engine-powered model will soon be ready for testing.


Author(s):  
Wolfgang A. Sandel ◽  
Max J. Miller

A new, comprehensive, flexible, integrated design system for the aerodynamic design of fans, compressors, and turbines was developed during the past decade. It operates in both batch and interactive modes. The system contains a flow path generator, a through-flow solver, a stacked airfoil geometry generator, and a flank-milled airfoil geometry generator. This paper describes the interactive interface in more detail. In particular, it describes the design considerations, appearance, and functionality of the interactive interface. Top level requirements were established before the interface was designed. These requirements are explained and some of the key reasoning that drove the high level design of the interface is discussed. The four principal windows in the interface are described in detail. The interactive interface that was developed has significantly increased the productivity of fan, compressor and turbine aero designers.


Author(s):  
C. Schmalhorst ◽  
B. Fluri ◽  
R. Schilling

An integrated computer-aided system for the initial design and optimisation of hydraulic machinery components, i.e. bladings of centrifugal pumps and fans as well as of water turbines, is presented. The IDS developed at the Institute of Fluidmechanics consists of an artificial neural network (ANN) for the initial design of components, a finite volume CFD-code based on the Reynolds-averaged Navier-Stokes equations and a finite element based computational structural analysis (CSA) code, as well as of an efficient module for the interactive modification of geometry of components. The design and optimisation process is demonstrated for a Francis turbine runner blading. The process starts with an initial design taken from the ANN which is in the next step analysed by means of our inhouse Navier-Stokes solver NS3D with respect to the performances to be guaranteed. The turbine stage is modelled as a single blade passage of the rotor and a stator blading. The CFD-results may be analysed by tailor-made post-processing. Based on the numerical simulation results the initial design may be interactively improved in an iterative process. The design targets in this stage of the process are efficiency and cavitation behaviour of the runner. Finally, the CFD-results are used as boundary conditions for a steady state CSA simulation yielding the distribution and magnitude of stresses within the runner, especially between the blades and the runner band (shroud). In addition to the time-independant CFD- and CSA-simulations a transient Fluid-Structur-Interaction (FSI) analysis may be simulated taking into account all blade passages in the rotor as well as in the stator. This simulation model yields a much more accurate loading of the structure due to unsteady pressure distributions. In this step the design can be scrutinised with respect to its fatigue resistance. After generating a design satisfying all requirements and boundary conditions the optimised geometry is fed back into the ANN to be used for similar applications. After having carried out design and optimisation processes for a number of characteristic hydraulic machinery a higher level of efficiency and cavitation behaviour may be reached.


1976 ◽  
Author(s):  
William V. Herrick ◽  
James R. Sims
Keyword(s):  

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