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Investigation into the Aircraft Hydraulic Platform with Multi-pumps and Systems
Author: ZhengHeFeng
Tutor: YangHuaYongï¼›OuYangXiaoPing
School: Zhejiang University
Course: Mechanical and Electronic Engineering
Keywords: Large passenger aircraft Aircraft hydraulic system Principle test Platform Self - pressurized fuel tank Load simulation
CLC: V227.82
Type: Master's thesis
Year: 2012
Downloads: 43
Quote: 0
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Abstract
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Development and testing of aircraft hydraulic system is divided into the component level, the principle and system-level three test aircraft hydraulic system test after the component level tests, system-level test (iron bird test) before principle explore and verify. The topic for the performance requirements of the aircraft hydraulic system test, developed by a multi-institutional multi-pump hydraulic system of a certain type of passenger principle test platform principle test level for three different pressure hydraulic system exploration. The main contents are: Chapter 1: Introduction large airliner aircraft hydraulic system structure and future development trends of current domestic and foreign aircraft hydraulic principle test bench, pointed out that the objectives and significance of research on the subject of research content and key technologies. Chapter II: the overall objectives and performance parameters of the test platform for multi-institutional multi-pump hydraulic system, analysis of the composition of the system (divided into three parts hydraulic, electrical and data acquisition) module for various functional modules of the hydraulic system: pump source self-pressurized fuel tank module, analog load module, piping vibration module and cooling module technology requirements, proposed solutions and test principle and test schematic of the hydraulic test platform. The design of the major components of the hydraulic system and achieve institutional and completed the three-dimensional modeling. Chapter 3: carry out a multi-pump multi-institutional hydraulic principles performance simulation study of the test platform. The hydraulic principle simulation model, and according to the system hydraulic component design and selection set simulation parameters to 3000PSI pressure level simulation analysis system to verify hydraulic system performance. Chapter 4: test the platform electrical and data acquisition system developed. Analysis of electrical power module, control modules and data acquisition module performance requirements, develop a total power of 240kW power module and IPC in conjunction with the PLC electrical control module, developed a 50-way, such as pressure and temperature data acquisition system based on PXI bus The signals are collected and recorded, the test platform supply, control and data acquisition functions. Chapter 5: for each module of the test platform engineering, and carry out the corresponding test research. A 5000psi pressure test, the flow pressure of the pump source and the simulated load test, self-pressurized fuel tank test, test, test results show that the test platform able to meet the design requirements of the target, and can be used for further research. Chapter 6: summary of the content of the research, and put forward the future work.
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CLC: > Aviation, aerospace > Aviation > Aircraft Construction and Design > Control system > Manipulation of power type > Hydraulic
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