1. Large Aircraft Design Programme for AVIC 2009/2010 Group Design Project Dr. Shijun Guo Academic Program Director 9 th April 2009 Department of Aerospace Engineering

2. LARGE AIRCRAFT DESIGN PROGRAMME Programme Structure 1. Taught Element (Feb.09 – Dec.09) Intensive Language Training 23 rd Feb – 13 March 2009 Lectures, short courses, seminars Feb. – Dec. 2009 Visit / events / social activities 2. Group Design Project (9 th April – 13 th Aug. 09, 5 weeks loading phase + 13 weeks design) 3. Individual Research Project (March 09- Feb.10)

3. LARGE AIRCRAFT DESIGN PROGRAMME GDP Group Design Project (9 th April – 13 th Aug. 09) Dr S. Guo – GDP Introduction and student role allocation (week-1) Prof. J.P. Fielding - Chief Designer and Chairman (week 2-18) Dr H. Smith – Chair the whole team in loading action (week 2-5) Dr C. Lawson – Chair the Systems Team (week 6-17) Dr H. Jia - Chairman in Avionics Team (week 6-17) All supervisors attend the weekly meeting (Thursday 2 – 5 pm, take weekly meeting minutes)

4. Design ProcessTriangle Phase II: Final Review 130 SEATER AIRCRAFT CONCEPTUAL DESIGN Group Design Project 2008/09

5. Conceptual Design from previous GDP - Market Analysis - Aircraft Configuration - Structure Layout

6. 6  Fuselage Cross-section  Cabin Layout  Flexibility  Cargo Configuration GDP - CABIN LAYOUT

7.  Comfortable Wider cabin width Better cabin pressure  Flexible Longer design range Easy to change Varied cabin layout  Eco-efficient 12% reduction in fuel consumption (estimated) 50% reduction in NOx (estimated) 20 dB reduction in noise (estimated) Flying Crane – Design Target Empty mass breakdown Operating cost breakdown Flying Crane - A 130-seater passenger aircraft conceptual design

8. GDP - Preliminary Design Assessments Group Design Project Reassess the current conceptual design (week 1-4) Loading and preliminary design (week 2 – 17) presentation and final GDP report (week 18 -19) Individual design report marked by supervisors (week 19) Individual Research Project Research progress review (Sept – Oct 2009) Interim Progress Review Final Oral Examination (9-12 Feb. 2010)

9. 3.0 AVIONIC SYSTEMS DESIGN GROUP 1.0 STRUCTURES DESIGN GROUP NAME (surname /1 st name) COMPONENT / TASK ALLOCATION Wang Zhanyi FWD Fuselage Li Xiaolong Centre Fuselage Zhang Haiying Aft Fuselage Li Bo Fin (C) Ning Yu Rudder (C) Li Longbin Tailplane & Connection to Fuselage Wang Ke Elevator (C) Qiu Hongbo Inner & centre wing box (C) Zhou Shijun Outer Wing (C) Ji Shaodong Flaps & Slats (C) Liu Lei Aileron, ribs (C) & engine pylon Tao xiaojiang Landing gear (main & nose) Yang Yongke Airworthiness & internal layout NAME (sur /1 st name) COMPONENT / TASK ALLOCATION Lv Qiming Fuel & Power Plant System Tai Zhongtian Secondary Power System Gao Yunhe Hydraulic and electric system Cheng Junxiang Actuation Systems Fu Yanyan Reliability & Survivability Hong Yuhua Maintainability Jia Xiaopeng Field & Flight Performance. Kou Mingshan Cost and Cabin Liu Yuanping LG System, Tyres, Brakes, pivots NAME (surname /1 st name) COMPONENT / TASK ALLOCATION Hu Rui Avionics architecture and systems integration Lv xingbo Flight Control System Design & Flight Deck Mao Cuifeng Communication & Surveillance System Design - Datalinks and Surveillance Systems design Liu Bingmin Flight Management System & Autopilot Design Jia Xiaopeng Cockpit Guidance, Control Display Design and Field & Flight Performance 2.0 SYSTEMS DESIGN GROUP LARGE AIRCRAFT DESIGN PROGRAM Group Design Project 2009/10

10. Students’ Role in Loading STRUCTURAL LOADING SUB TEAMS 1.1 Symmetrical Loading Team (Pitching Loads) Tailplane & Elevator Loads Wang Ke, Zhang Haiying Fuselage Loads, SF, BM, T Diagrams Wang Zhanyi, Li Xiaolong, Engine Pylon Loads Lv Qiming, Lv Qiming 1.2 Asymmetric Loading Team (Lateral Loads) Fin & Rudder Loads Ning Yu, Li Bo, 1.3 Wing, Aileron & Flap Loading Team Wing – N-V Diagrams including gusts, Wing SF, BM, T diagrams. Qiu Hongbo, Li Longbin, Zhou Shijun Tang kebing, Aileron - Roll Cases Liu Lei, Jia Xiaopeng Flap & Slat Cases, Airbrake & Spoiler Cases Ji Shaodong, Yang Yongke 1.4 Landing Gear Loading Team Tao xiaojiang, Liu Yuanping Work for the students in Systems & Avionics during loading action period needs to be allocated by the GDP chairman or sub-chairman

11. GDP Design Tasks - Draft TASK GENERAL REQUIREMENTS STRUCTURAL COMPONENT REQUIREMENTS FOR STRUCTURAL DESIGN TASKS - Derivation of applied loads (loading actions analysis) - Structural layout using CAD - Initial structural sizing, stress and buckling analysis - Finite element analysis - Aeroelasticity analysis - Fatigue / Damage Tolerance analysis of one component - Mass estimation - Manufacture technology and process consideration - Produce engineering drawings - Airworthiness Compliance Matrix (most important)

12. GDP Design Tasks - Draft TASK GENERAL REQUIREMENTS SYSTEMS COMPONENT REQUIREMENTS FOR SYSTEMS DESIGN TASKS - Estimate power requirements - System architecture - Schematic block diagrams - Mass and size budgets - System layout within flight vehicle airframe (CAD) - Check interfaces with structure and other systems (CAD) - System safety assessment - Reliability analysis - Produce engineering drawings - Airworthiness Compliance Matrix (most important) REQUIREMENTS FOR AVIONICS DESIGN TASKS - Avionic Architecture Design - Flight Control System Design - Communication System Design - Flight Management System & Autopilot Design - Cockpit Guidance & Control Display Design - Airworthiness Compliance Matrix (most important) The above GDP task requirements may be updated and the timetable (April – August) will be determined by the GDP chairman and sub-chairman

13. Flying Crane - GDP 130-Seater Aircraft Preliminary Design HOPE YOU ENJOY THE GDP