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Research on Parametric Design for Transmission Mechanism of Flight Control System

Author: JiaoZhenShuang
Tutor: XuFeng
School: Nanjing University of Aeronautics and Astronautics
Course: Aircraft design
Keywords: Transmission UG secondary development Parametric Design Virtual Assembly Drive ratio
CLC: V249.1
Type: Master's thesis
Year: 2009
Downloads: 58
Quote: 0
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Abstract


Aircraft flight control system consists of commands ( control ) links, transmission links ( operating system ) and the control object ( aircraft ) three aspects of the composition aircraft control loop to ensure that the aircraft 's stability and precise control. Among them, the aircraft control system is the core part of the flight control , and its static and dynamic handling characteristics directly affect the flying qualities and flight safety. As the complexity of the operating system itself and its importance , the design work is often more complex, long cycle . In this paper, fly- trainer driver-operated device (PCU) and the transmission mechanism is designed for a systematic study . Based on UG / OPEN class development tools VC 6.0 programming tools, developed in UG transmission mechanism typical flight control system design of mechanical parts proprietary modules. By analyzing the characteristics of the transmission mechanism components and characteristics of parameters to UG / Open GRIP and UG / Open API joint programming part of the transmission mechanism of parametric modeling , and as a basis for the research UG principles and virtual assembly methods to achieve operating device driver to manipulate transmission mechanism trainer virtual assembly automation . PCU trainer transmission mechanism established mathematical model to analyze and calculate the typical driver member and a trainer transmission ratio control system . On this basis, the transmission ratio calculation software was developed to achieve a typical transmission components and the overall organization and distribution of transmission ratio calculations . Transmission control system according to the relationship and the size of transmission parts , in accordance with their respective tolerances established gap to query the database to apply to flight control system dynamics simulation modeling transmission components .

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CLC: > Aviation, aerospace > Aviation > Aircraft instrumentation,avionics, flight control and navigation > Flight control system and navigation > Flight control
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