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ویرایش: 1
نویسندگان: Yaobao Yin. Jiangwei Wu
سری:
ISBN (شابک) : 9811522014, 9789811522017
ناشر: Springer Nature
سال نشر: 2020
تعداد صفحات: 396
زبان: English
فرمت فایل : PDF (درصورت درخواست کاربر به PDF، EPUB یا AZW3 تبدیل می شود)
حجم فایل: 16 مگابایت
در صورت تبدیل فایل کتاب Gaosu Startup Control Theory and Application Technology/ Gaosu Qidong Kongzhi Lilun He Yingyong Jishu: Control System and Energy System به فرمت های PDF، EPUB، AZW3، MOBI و یا DJVU می توانید به پشتیبان اطلاع دهید تا فایل مورد نظر را تبدیل نمایند.
توجه داشته باشید کتاب نظریه کنترل راه اندازی Gaosu و فناوری کاربرد / Gaosu Qidong Kongzhi Lilun He Yingyong Jishu: سیستم کنترل و سیستم انرژی نسخه زبان اصلی می باشد و کتاب ترجمه شده به فارسی نمی باشد. وبسایت اینترنشنال لایبرری ارائه دهنده کتاب های زبان اصلی می باشد و هیچ گونه کتاب ترجمه شده یا نوشته شده به فارسی را ارائه نمی دهد.
این کتاب آخرین پیشرفتها و دستاوردهای تحقیقاتی خود نویسنده در تئوری کنترل پنوماتیک با سرعت بالا و فناوری کاربردی را برجسته میکند. عمدتاً با تمرکز بر سیستم کنترل و سیستم انرژی، تئوری اساسی و فنآوریهای پیشگام برای هوافضا و هوانوردی را ارائه میکند، در حالی که به عنوان مثال به آن میپردازد. تئوری کنترل سروو پنوماتیک، مکانیسمهای غیرخطی پنوماتیک، آیروترمودینامیک، مکانیسمهای سروو پنوماتیک، و کاربردهای نمونه سیستمهای توربین گازی با دمای بالا و سرعت بالا در هوا فضا، هوانوردی و تجهیزات اصلی.
This book highlights the latest developments and the authors own research achievements in high speed pneumatic control theory and applied technology. Chiefly focusing on the control system and energy system, it presents the basic theory and pioneering technologies for aerospace and aviation, while also addressing e.g. pneumatic servo control theory, pneumatic nonlinear mechanisms, aerothermodynamics, pneumatic servo mechanisms, and sample applications of high temperature and high speed gas turbine systems in aerospace, aviation, and major equipment.
Preface Summary Contents 8 Pneumatic Actuators, Driving Elements, and Accessories 8.1 Pneumatic Cylinder and Hydraulic Cylinder 8.1.1 Classification of Pneumatic Cylinder and Hydraulic Cylinder 8.1.2 Natural Frequency of Pneumatic Cylinder 8.1.2.1 Natural Frequency of Single Acting Cylinder 8.1.2.2 Natural Frequency of Double Acting Cylinder 8.1.3 Natural Frequency of Hydraulic Cylinder 8.1.4 Comparison of Pneumatic Cylinder System and Hydraulic Cylinder System 8.1.5 Conclusions 8.2 Structure and Characteristics of Actuators 8.2.1 Pneumatic Cylinder 8.2.1.1 Static Characteristics of Cylinders 8.2.1.2 Dynamic Characteristics of Cylinder 8.2.1.3 Motion Characteristics of Piston 8.2.1.4 Cylinder Natural Frequency 8.2.1.5 Positioning Stop Accuracy of Piston 8.2.2 Pneumatic Motor 8.2.2.1 The Form and Characteristics of Pneumatic Motor 8.2.2.2 Natural Frequency of Pneumatic Motor 8.3 Aircraft Hydraulic Accumulator and Cylinder in Extreme Temperature Environment 8.3.1 Extreme Temperature Environment 8.3.2 Van der Waals Equation for Real Gases 8.3.3 Inflation Mass of High-Pressure Gas Cylinders 8.3.4 Gas Pressure Service Characteristics of High-Pressure Cylinders and Cavities 8.3.5 Service Characteristics of Accumulator 8.3.6 Conclusions Bibliography 9 High-Temperature and High-Speed Gas Turbine Pump Electro-Hydraulic Energy System for Aircraft 9.1 Electro-Hydraulic Servo Control Technology of Aircraft Gas Turbine Pump 9.1.1 Overview of Electro-Hydraulic Control Technology 9.1.1.1 Development Status of Airborne Electro-Hydraulic Control Technology 9.1.1.2 Development Trend 9.1.1.3 Material—An Important Contributing Factor to the Evolution of Electro-Hydraulic Technology 9.1.1.4 Electrorheological Technology 9.1.2 Elastic O-Ring Sealing Technology 9.1.2.1 Configuration and Sealing Principle of O-Ring 9.1.2.2 Characteristics of O-Ring Seal 9.1.2.3 O-Ring Material 9.1.2.4 Selection and Design of O-Ring 9.1.2.5 Protection and Fault Prevention of O-Ring 9.1.3 Technical Characteristics of Electric-Hydraulic Servo System for Aircraft 9.1.3.1 High Power 9.1.3.2 High Pressure and High Temperature 9.1.3.3 High Speed 9.1.3.4 High Reliability 9.1.3.5 Digitization and Informatization 9.1.4 Design Method of Air Defense Missile Control Execution System 9.1.4.1 Comprehensive Requirements 9.1.4.2 Demonstration Process 9.1.4.3 Main Criterion 9.1.4.4 Performance Test 9.1.4.5 Summary 9.1.5 Auxiliary Energy for Air Defense Missiles 9.1.5.1 Classification of Energy Program 9.1.5.2 Application Examples 9.1.5.3 Summary 9.1.6 Hydraulic Energy Application Technology of Gas Turbine Pump for Aircraft 9.1.6.1 Application of Gas Primary Energy 9.1.6.2 Application of Gas Turbine Pump 9.1.6.3 Working Area of Gas Turbine Pump Hydraulic System 9.2 Power Matching Design of Steering System 9.2.1 Load Model of Steering System 9.2.1.1 Load Trajectory 9.2.1.2 Load Maximum Power Point 9.2.1.3 Load Trajectory Characteristics 9.2.2 Optimal Matching of Output Characteristics and Load Trajectories of Servo Mechanism 9.2.3 Energy Demand of Actual Steering System 9.2.4 Variation Factors of Working Pressure and Frequency Characteristics of System 9.3 Design Principle of Gas Generator 9.3.1 Theoretic Derivation 9.3.1.1 Hypothesis 9.3.1.2 Correlation Analysis 9.3.1.3 Derivation of Equations 9.3.2 Application Discussion 9.3.2.1 Applied Range 9.3.2.2 Case Analysis 9.3.2.3 Related Discussion 9.4 Design Principle of Small Gas Turbine for Missile 9.4.1 Thermodynamic Process in Small Gas Turbine Nozzle for Missile 9.4.2 Efficiency of Small Gas Turbine in Missile Hydraulic System 9.4.3 Graphical Analysis Method for Stress of Small Gas Turbine Disk for Missile 9.5 Starting Characteristics of Electronic and Hydraulic Power Unit 9.5.1 Description of EHPU Starting Characteristic 9.5.2 EHPU Theoretical Modeling 9.5.3 Starting Characteristics of Hydraulic System 9.5.4 Starting Characteristics of Power Supply System 9.5.4.1 Effect of Gas Peak Pressure on Starting Characteristics 9.5.4.2 Effect of Pressure Impulse on Starting Characteristics 9.5.4.3 Effect of High and Low-Temperature Performance on Starting Characteristics 9.5.4.4 Main Ways to Improve Starting Characteristic of Power Supply System Bibliography 10 Application of Aerodynamic Technology in Attitude Control of Aerocraft 10.1 Aerodynamic Attitude Control Principle and Attitude Control Method of Aircraft 10.1.1 New Method and Principle of Attitude Control of Aircraft 10.1.2 Lateral Force Analysis of Attitude Control 10.1.3 Experiments and Analysis 10.1.3.1 Design Scheme 10.1.3.2 Experimental Results and Analysis of Thrust 10.1.4 Conclusions 10.2 Laval Nozzle for Attitude Control of Aircraft 10.2.1 Flow Field Analysis of Laval Nozzle 10.2.1.1 Physical Model 10.2.1.2 Boundary Conditions for Throttle Ports 10.2.1.3 Basic Equation of Fluid 10.2.1.4 Distribution Law of Flow Field 10.2.2 Manufacturing Process Technology 10.3 Device for Changing Missile Motion Direction by Using Gas Generator and Transverse Force of Nozzle 10.4 Process Technology of Gas Steering Engine 10.4.1 Structure and Working Principle 10.4.2 Redundancy Control 10.4.3 Fit Clearance Control 10.4.4 Shell Assembly Quality 10.4.5 Technological Key Problem Test on Symmetry of Reaction Time Bibliography 11 Pneumatic Down-the-Hole Hammer 11.1 Overview 11.2 Principle and Classification of Pneumatic DTH Hammer 11.2.1 Classification of Pneumatic DTH Hammer 11.2.2 Principle of Valve-Type Pneumatic DTH Hammer 11.2.3 Valveless Pneumatic DTH Hammer 11.2.4 Large Diameter Pneumatic DTH Hammer 11.3 Principle and Parameter Design of Large Diameter Pneumatic DTH Hammer Impactor 11.3.1 Design Requirements 11.3.2 Overall Structure 11.3.3 Selection of Working Parameters 11.3.4 Calculation Method of Performance Parameters 11.3.4.1 Calculation Method for General Design of Performance Parameters 11.3.4.2 Piecewise Calculation Method for Calculating Performance Parameters 11.3.4.3 Performance Parameter Linear Equation Method 11.3.5 Design of Key Parts 11.3.5.1 Design of Cylinder 11.3.5.2 Piston Design 11.3.5.3 Design of Valve Distribution Path 11.4 Dynamic Process and Theoretical Model of Large Diameter Pneumatic DTH Hammer 11.4.1 Dynamic Process of Large Diameter Pneumatic DTH Hammer 11.4.2 Theoretical Model of Large Diameter Pneumatic DTH Hammer 11.4.2.1 Hypothesis of Internal Dynamic Process of Pneumatic DTH Hammer 11.4.2.2 Theoretical Model Equations of Pneumatic DTH Hammer 11.4.3 Numerical Calculation of Large Diameter Pneumatic DTH Hammer 11.4.3.1 Analysis of the Results of the Whole Working Process 11.4.3.2 Comparison of Performance Parameters of DTH Hammer Under Different Intake Pressure 11.4.3.3 Pressure Fluctuation Phenomenon Analysis and Parameter Optimization 11.4.4 Summary 11.5 Design of Large Diameter DTH Hammer Bit and Spherical Tooth Layout 11.5.1 Rock-Breaking Process by Impact 11.5.2 Mechanical Model of Side Tooth of Large Diameter Pneumatic DTH Hammer Bit 11.5.2.1 Hypothesis 11.5.2.2 Force Model Under Axial Load 11.5.2.3 Force Model Under Tangential Load 11.5.2.4 Force Model Under Combined Action of Axial and Tangential Loads 11.5.3 Layout Principle of Large Diameter Pneumatic DTH Hammer Bit 11.5.3.1 Spherical Teeth Hydrostatic Rock Breaking 11.5.3.2 Spherical Teeth Breaking Rock by One Impact 11.5.3.3 Basic Principles for Bit Layout of Large Diameter DTH Hammer 11.5.3.4 Example of Rock-Breaking Dynamic Process Analysis of Bit 11.6 Typical Engineering Cases 11.6.1 Project Site 11.6.2 Model and Parameters of Pneumatic DTH Hammer 11.6.3 Construction Process 11.6.4 Analysis of Bit Usage and Phenomenon Bibliography 12 Pneumatic–Hydraulic Pile Driving Hammer 12.1 Pneumatic–Hydraulic Composite Pile Driving Hammer 12.1.1 Hydraulic System of Typical Hydraulic Pile Driving Hammer 12.1.1.1 British BSP Single Acting Hydraulic Hammer 12.1.1.2 Finnish JUNTTAN Single Acting Hydraulic Hammer 12.1.1.3 Dutch IHC Double Acting Hydraulic Hammer 12.1.2 Strike Frequency and Strike Energy 12.1.2.1 Strike Frequency 12.1.2.2 Strike Energy 12.1.3 Main Characteristics and Parameters 12.1.4 Conclusions 12.2 High-Speed Pneumatic–Hydraulic Composite Hammer 12.2.1 Hydraulic System of Pneumatic–Hydraulic Pile Driving Hammer 12.2.1.1 Principle of Pneumatic–Hydraulic Pile Driving Hammer 12.2.1.2 Dynamics Model of Rising Process 12.2.1.3 Dynamics Model of Descending Process 12.2.2 Strike Energy 12.2.3 Characteristics of Pneumatic–Hydraulic Pile Driving Hammer 12.2.4 Conclusions 12.3 Mathematical Model of High-Speed Pneumatic–Hydraulic Composite Hammer 12.3.1 Overview 12.3.2 Mathematical Model 12.3.2.1 Hammer Body Rising Stage 12.3.2.2 Hammer Body Descending Stage 12.3.2.3 Strike Energy 12.3.3 Characteristic and Example of Pneumatic–Hydraulic Composite Pile Driving Hammer 12.3.4 Conclusions 12.4 Rapid Piling Process of High-Speed Pneumatic–Hydraulic Composite Hammer 12.4.1 Principle of Rapid Piling 12.4.1.1 Rising Stage 12.4.1.2 Inertial Rising Stage 12.4.1.3 Descending Stage 12.4.1.4 Pressure-Retaining Stage 12.4.2 Mathematical Model for Descending Stage of Rapid Piling 12.4.3 Influencing Factors of Rapid Piling 12.4.3.1 Influence of Diameter and Length of Oil Return Pipeline 12.4.3.2 Influence of Low-Pressure Accumulator 12.4.4 Conclusions 12.5 Contact Model Pile and Soil 12.5.1 Finite Element Analysis Model of Pile and Soil 12.5.2 Finite Element Solution of Pile and Soil 12.5.2.1 Dynamic Model Parameter Setting 12.5.2.2 Results 12.5.3 Conclusions Bibliography 13 Application of Pneumatic Technology in Fuel Cell Vehicles 13.1 Pneumatic System and Fuel Cell Hydrogen Transmission System 13.1.1 Overview 13.1.2 Space Hydrogen Energy Technology and Its Application 13.1.2.1 Application of Hydrogen Energy Technology in Spacecraft 13.1.2.2 High-Pressure Cylinders for Self-contained Energy Plants 13.1.2.3 Pneumatic Servo Control Technology 13.1.3 Carbon Fiber Winding Cylinder for Fuel Cell Vehicle 13.1.3.1 Fuel Cell Vehicle Hydrogen Storage Device 13.1.3.2 Carbon Fiber Winding Composite Gas Cylinder for Domestic Fuel Cell Vehicle 13.1.4 Fuel Cell Vehicle Hydrogen Transmission System 13.2 Hydrogen Transmission and Hydrogenation Characteristics of Vehicle-Borne High-Pressure Hydrogen Transmission System Cylinders 13.2.1 Characteristics of Vehicle-Borne Hydrogen Transmission and Storage System 13.2.1.1 Hydrogen Storage Mode 13.2.1.2 Hydrogen Supply Capacity 13.2.1.3 Mass of Hydrogen Storage 13.2.2 Hydrogen Transmission Pressure Characteristics of Vehicle-Borne Gas Cylinders 13.2.2.1 Mathematical Model 13.2.2.2 Analysis of Simulation Results 13.2.3 Hydrogenation Pressure Characteristics of Vehicle-Borne Gas Cylinders 13.2.3.1 Mathematical Model 13.2.3.2 Analysis of Simulation Results 13.2.4 Test Results 13.2.4.1 Mass of Hydrogen Storage 13.2.4.2 Hydrogen Supply Capacity 13.2.4.3 Driving Distance 13.2.5 Conclusions Bibliography 14 Pneumatic Principle and Device of Oscillating Water Column Wave Power Generation 14.1 Overview 14.2 Basic Structure and Pneumatic Principle 14.3 Mathematical Model of Oscillating Water Column 14.3.1 Aerodynamic Model of Air Chamber 14.3.2 Frequency Response of Mighty Whale Energy Converter 14.3.3 Examples of Numerical Calculation of Mighty Whale Energy Converter 14.3.4 Characteristics of Floating Oscillating Water Column Wave Energy Converter 14.4 Experimental Technique of Oscillatory Water Column Wave Energy Converter 14.4.1 Test Model 14.4.2 Numerical Analysis 14.5 Application Examples of Oscillating Water Column Power Station 14.5.1 Examples of Oscillating Water Column Wave Power Generation in China 14.5.2 Examples of Oscillating Water Column Wave Power Generation in Foreign Countries 14.6 Key Technologies of Oscillating Water Column Wave Power Generator Bibliography