Alfred Gessow Rotorcraft Center, Department of Aerospace
Engineering, University of Maryland. College Park College Park,
USA, 101 стр. (PDF) + 20 стр. (презентация), 2005
In response to the 2005 Annual The American Helicopter Society
(AHS) Inteational Student Design Competition – Graduate
Category
Ответ на Международный студенческий проектный конкурс, проходящий в рамках Американского вертолетного общества (AHS) в 2005 году - Выпускная работа Содержание: Acknowledgements
List of figures
List of tables
List of symbols / abbreviations
RFP compliance
Performance summary and design features
Introduction
Historical considerations
Identification of design drivers
FCS Transport Performance Capabilities
FCS Logistics Mission Requirements:
Mission Profile
Configuration Selection Drivers
Configuration selection
Preliminary sizing
Design Requirements
Method of Analysis
Initial Sizing
Trade Studies
Mission Timeline Prediction
Preliminary Design Cost Analysis
Main rotor and hub design
Blade Aerodynamic Characteristics
Blade Structural Design:
Hub Design
Rotor Control
Active Trim Tab
Vibration Control
Rotor Dynamics
Anti-torque system
Anti-torque comparison
Tail Rotor Detailed Design
Tail Rotor Structure
Tail Rotor Performance
Airframe and landing gear design
Cargo Bay Cross-Section
Airframe Design
Airframe Layout
Cargo Loading
Manufacturing
Landing Gear Design
Folding systems
Overview
Automatic Main Rotor Blade Folding
Automatic Tail Boom Folding
Handling qualities and stability
Stability
Effect of Design Elements
Flight control system
Primary Flight Control System (PFCS)
Automatic Flight Control System (AFCS)
Cockpit and cabin systems
Flight Crew Station and Controls
Cabin and Cargo area systems
Fault detection and health and usage monitoring system (HUMS)
Main Rotor and Rotating Components
Engines and Main Gearbox
Flight Control System and Avionics
Tail Rotor and Tail Gearbox Structure
Self-defense equipment/countermeasures
Mechanical subsystems (engine / transmission)
Engine Design
Transmission Design
Performance Analysis
Drag Estimation
Hover Performance
Forward Flight Performance
Retu trip (Without FCS)
Additional applications and capabilities
Conclusions
Appendix A: mil-std-1374 weight summary
References
Ответ на Международный студенческий проектный конкурс, проходящий в рамках Американского вертолетного общества (AHS) в 2005 году - Выпускная работа Содержание: Acknowledgements
List of figures
List of tables
List of symbols / abbreviations
RFP compliance
Performance summary and design features
Introduction
Historical considerations
Identification of design drivers
FCS Transport Performance Capabilities
FCS Logistics Mission Requirements:
Mission Profile
Configuration Selection Drivers
Configuration selection
Preliminary sizing
Design Requirements
Method of Analysis
Initial Sizing
Trade Studies
Mission Timeline Prediction
Preliminary Design Cost Analysis
Main rotor and hub design
Blade Aerodynamic Characteristics
Blade Structural Design:
Hub Design
Rotor Control
Active Trim Tab
Vibration Control
Rotor Dynamics
Anti-torque system
Anti-torque comparison
Tail Rotor Detailed Design
Tail Rotor Structure
Tail Rotor Performance
Airframe and landing gear design
Cargo Bay Cross-Section
Airframe Design
Airframe Layout
Cargo Loading
Manufacturing
Landing Gear Design
Folding systems
Overview
Automatic Main Rotor Blade Folding
Automatic Tail Boom Folding
Handling qualities and stability
Stability
Effect of Design Elements
Flight control system
Primary Flight Control System (PFCS)
Automatic Flight Control System (AFCS)
Cockpit and cabin systems
Flight Crew Station and Controls
Cabin and Cargo area systems
Fault detection and health and usage monitoring system (HUMS)
Main Rotor and Rotating Components
Engines and Main Gearbox
Flight Control System and Avionics
Tail Rotor and Tail Gearbox Structure
Self-defense equipment/countermeasures
Mechanical subsystems (engine / transmission)
Engine Design
Transmission Design
Performance Analysis
Drag Estimation
Hover Performance
Forward Flight Performance
Retu trip (Without FCS)
Additional applications and capabilities
Conclusions
Appendix A: mil-std-1374 weight summary
References