MADEsmart:: An environment for improved development of aircraft components in preliminary design

被引:2
|
作者
Hirsh, J
Hajela, P
Spering, JC
Coen, GA
Mytych, E
机构
[1] Boeing Phantom Works, Math & Comp Technol, Philadelphia, PA 19142 USA
[2] Rensselaer Polytech Inst, Dept Mech Engn Aeronaut Engn & Mech, Troy, NY 12180 USA
[3] Boeing Aircraft & Missiles Syst, Lean Proc & Tools, Philadelphia, PA USA
关键词
genetic algorithms; intelligent agents; multidisciplinary design optimization; natural language processing; neural networks;
D O I
10.1007/s003660170017
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
The MADEsmart Project represents a unique contribution to the Defense Advanced Research Project Agency's (DARPA) Rapid Design Exploration and Optimization (RaDEO) Program and to U.S. industrial aircraft design practice. The project team's work focused heavily on the introduction of design and manufacturing constraint information early in the product development lifecycle. Since conventional aircraft development efforts are highly inefficient for identifying and managing product requirements and design constraints, a development team's ability to effectively evaluate proposed design solutions can be negatively impacted. This project's work employed three main technologies to accomplish its vision of greatly improving the design of aircraft components: (1) intelligent agent technology to streamline coordination between development team resources: (2) Multidisciplinary Design Optimization (MDO) technology to allow for rapid design exploration and optimization; and (3) the introduction of design evaluation for manufacturing process constraints at the preliminary stage of design using a natural language processing representation known as Lexical Conceptual Structures (LCS). This paper provides motivation for the MADEsmart project's research, an overview of each of its three main focus areas. a more detailed description of each of the technology applications, and some concluding remarks.
引用
收藏
页码:162 / 185
页数:24
相关论文
共 50 条
  • [41] Sustainability-Driven Design of Aircraft Composite Components
    Filippatos, Angelos
    Markatos, Dionysios
    Tzortzinis, Georgios
    Abhyankar, Kaushik
    Malefaki, Sonia
    Gude, Maik
    Pantelakis, Spiros
    AEROSPACE, 2024, 11 (01)
  • [42] Additive manufacturing process design for complex aircraft components
    Dogea, Ramona
    Yan, Xiu T.
    Millar, Richard
    INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2022, 123 (11-12): : 4195 - 4211
  • [43] INVERSE AERODYNAMIC DESIGN METHOD FOR AIRCRAFT-COMPONENTS
    MALONE, JB
    VADYAK, J
    SANKAR, LN
    JOURNAL OF AIRCRAFT, 1987, 24 (01): : 8 - 9
  • [44] Aircraft Composites Components Concurrent Design Process Management
    Cong, Peiyong
    Younus, Muhammad
    Fan Yuqing
    2010 INTERNATIONAL CONFERENCE ON NETWORKING AND INFORMATION TECHNOLOGY (ICNIT 2010), 2010, : 274 - 278
  • [45] INVERSE AERODYNAMIC DESIGN METHOD FOR AIRCRAFT COMPONENTS.
    Malone, J.B.
    Vadyak, J.
    Sankar, L.N.
    1600, (24):
  • [46] Development of an aircraft lap joint simulant environment
    Ferrer, KS
    Kelly, RG
    CORROSION, 2002, 58 (05) : 452 - 459
  • [47] PRELIMINARY DEVELOPMENT OF LOCOMOTIVE CRASHWORTHY COMPONENTS
    Liana, Patricia
    Stringfellow, Richard
    PROCEEDINGS OF THE ASME/ASCE/IEEE JOINT RAIL CONFERENCE, 2012, : 309 - 318
  • [48] Preliminary Design of Aerial Spraying System for Microlight Aircraft
    Omar, Zamri
    Idris, Nurfazliawati
    Rahim, M. Zulafif
    INTERNATIONAL CONFERENCE ON MATERIALS PHYSICS AND MECHANICS 2017, 2017, 914
  • [49] PRELIMINARY DESIGN OF AIRCRAFT WINGS FOR DYNAMIC LOADS IN LANDING
    RACZ, E
    PERIODICA POLYTECHNICA-MECHANICAL ENGINEERING, 1969, 13 (03): : 229 - &
  • [50] Methodologies for Preliminary Design of Variable Wing Geometry Aircraft
    Ishtiaq, Shehryar
    Israr, Asif
    2013 INTERNATIONAL CONFERENCE ON AEROSPACE SCIENCE & ENGINEERING (ICASE), 2013, : 19 - 22