Development and Implementation of Rotorcraft Preliminary Design Methodology using Multidisciplinary Design Optimization

All at Once;Aeronautical design standards;Blade element theory;Contributing analyses;Concurrent engineering;Collaborative optimization;Design structure matrix;Fixed point iteration;Genetic algorithms;Global sensitivity equation;Multidisciplinary design analysis;Multidisciplinary design optimization;Optimizer based decomposition;Overall evaluation criteria;Request for proposal;Response surface equation;Simultaneous analysis and design;Sequential quadratic programming;System sensitivity analysis;Total quality management

Khalid, Adeel S. ; Aerospace Engineering

University:Georgia Institute of Technology

Department:Aerospace Engineering

关键词: All at Once;    Aeronautical design standards;    Blade element theory;    Contributing analyses;    Concurrent engineering;    Collaborative optimization;    Design structure matrix;    Fixed point iteration;    Genetic algorithms;    Global sensitivity equation;    Multidisciplinary design analysis;    Multidisciplinary design optimization;    Optimizer based decomposition;    Overall evaluation criteria;    Request for proposal;    Response surface equation;    Simultaneous analysis and design;    Sequential quadratic programming;    System sensitivity analysis;    Total quality management;   

Others  :  https://smartech.gatech.edu/bitstream/1853/14013/1/khalid_adeel_s_200612_phd.pdf

美国|英语

来源: SMARTech Repository

【 摘 要 】

A formal framework is developed and implemented in this research for preliminary rotorcraft design using IPPD methodology. All the technical aspects of design are considered including the vehicle engineering, dynamic analysis, stability and control, aerodynamic performance, propulsion, transmission design, weight and balance, noise analysis and economic analysis. The design loop starts with a detailed analysis of requirements. A baseline is selected and upgrade targets are identified depending on the mission requirements. An Overall Evaluation Criterion (OEC) is developed that is used to measure the goodness of the design or to compare the design with competitors. The requirements analysis and baseline upgrade targets lead to the initial sizing and performance estimation of the new design. The digital information is then passed to disciplinary experts. This is where the detailed disciplinary analyses are performed. Information is transferred from one discipline to another as the design loop is iterated. To coordinate all the disciplines in the product development cycle, Multidisciplinary Design Optimization (MDO) techniques e.g. All At Once (AAO) and Collaborative Optimization (CO) are suggested. The methodology is implemented on a Light Turbine Training Helicopter (LTTH) design. Detailed disciplinary analyses are integrated through a common platform for efficient and centralized transfer of design information from one discipline to another in a collaborative manner. Several disciplinary and system level optimization problems are solved. After all the constraints of a multidisciplinary problem have been satisfied and an optimal design has been obtained, it is compared with the initial baseline, using the earlier developed OEC, to measure the level of improvement achieved. Finally a digital preliminary design is proposed. The proposed design methodology provides an automated design framework, facilitates parallel design by removing disciplinary interdependency, current and updated information is made available to all disciplines at all times of the design through a central collaborative repository, overall design time is reduced and an optimized design is achieved.