AMESim Applications in Aeronautics. EADS Military Aircraft / IMAGINE October, 2004 Cédric Roman Project Engineer, IMAGINE S.A.
|
|
|
- Jemima Logan
- 5 years ago
- Views:
Transcription
1 AMESim Applications in Aeronautics EADS Military Aircraft / IMAGINE October, 2004 Cédric Roman Project Engineer, IMAGINE S.A.
2 AMESim Applications in Aeronautics 2 Flight control Braking Structure/actuator coupling Electrical power system Propulsion Ground simulation rig (iron bird) Aeronautics s Refueling System Thermal Management (A/C, Cooling, ) Aircraft control systems Aeronautics Hydraulic Systems Oxygen and
3 3 All types of controlled systems coupling mechanical, electro-mechanical, hydraulic, thermal Mechanism Animation
4 Landing Gear: 2D mechanism 4 mechanism Mechanism Animation
5 5 Nose gear steering systems
6 6 Rear Suspension Relative displacement (piston envelope)
7 7 Integration and coupling Aerodynamic forces V aircraft Vwheel Flight parameters Suspension Angle of attack mechanism Brake > Architectur & System level
8 Life support : Oxygen Systems 8 Intertechnique is using the AMESim software and IMAGINE services in the development of their different products like O2 masks. Example of use of AMESim: System Stability Robust design O 2 consumption
9 Life support : Oxygen Systems 9 Distribution network and consumption over flight profile Points of interest of different consulting projects: - Consumption - Ejector performance - Optimization of dilution Air-O2 - Electro-pneumatic regulator design
10 Life support : Oxygen Systems 10 Gas exchanges in lung O2 and CO2 exchanges between air and blood in lung
11 Life support : Human performances 11 Qinetiq is using the software AMESim for their different study of human performance in extreme environments. Breathing Equipment Library Simple Demand Regulator Simulation
12 Life support : Respiratory mechanics 12 An example of openness in AMESIM Simulation System of Respiratory Mechanics
13 13 Pyrotechnic applications Key points: Powder combustion Real gas modeling Gas mixtures
14 14 From reservoir to injectors Circuit Pumps Valves Ejectors Thermal aspects Control
15 CASE STUDY N.1 (Mr. Georgi): Fuel Pump Test 15 Different Flight Scenarii can control from Excel the pump model in AMESim for different altitude.
16 16 Combustion, thrust, control, Secondary Power Syst. Combustion calculation and control validation Preliminary performance studies
17 17 Heat exchangers and temperature control
18 CASE STUDY N.2 (Mr. Thiele): Heat exchangers and temperature control 18
19 CASE STUDY N.2 (Mr. Thiele): Heat exchangers and temperature control 25 C 35 C C -4 C -16 C 58 C Heat=30kW
20 20 Air moisture modelling Controlling relative humidity Avoiding water condensation in pneumatic circuit
21 Air conditioning 21
22 CASE STUDY N.3 (Mr. Thiele): Air Conditioning Vapour cycle Single Stage Process R134A 22 Libraries TPF/AC: results are coming from geometrical parameters For this case study n.3, AMESim allows a backward calculation method
23 CASE STUDY N.3 (Mr. Thiele): Air Conditioning Backward Calculation Method - 1st Step: searching? 23????
24 CASE STUDY N.3 (Mr. Thiele): Air Conditioning Backward Calculation Method - 1st Step: searching? 24??? Using Optimization facility Design Exploration?
25 CASE STUDY N.3 (Mr. Thiele): Air Conditioning Backward Calculation Method - 1st Step: searching? 25???? Using Optimization facility Design Exploration
26 CASE STUDY N.3 (Mr. Thiele): Air Conditioning Backward Calculation Method 2nd Step: 26
LMS Imagine.Lab AMESim Ground Loads and Flight Controls
LMS Imagine.Lab AMESim Ground Loads and Flight Controls LMS Imagine.Lab Ground Loads and Flight Controls LMS Imagine.Lab Ground Loads and Flight Controls helps designers from the aerospace industry to
Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business. Real-time Mechanism and System Simulation To Support Flight Simulators
Y. Lemmens, T. Benoit, J. de Boer, T. Olbrechts LMS, A Siemens Business Real-time Mechanism and System Simulation To Support Flight Simulators Smarter decisions, better products. Contents Introduction
Aircraft Hydraulic Systems Design and Performance
Unit T25: Aircraft Hydraulic Systems Design and Performance Unit code: T/504/0126 QCF level: 6 Credit value: 15 Aim The aim of this unit is to give learners an understanding of the principles that underpin
LMS Imagine.Lab AMESim Electromechanical
LMS Imagine.Lab AMESim Electromechanical LMS Imagine.Lab Electromechanical LMS Imagine.Lab Electromechanical helps engineers define straightforward strategies throughout the design process of electrical
AN ELECTRICAL FUEL PUMPING AND METERING SYSTEM FOR MORE ELECTRICAL AERO-ENGINES
25 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES AN ELECTRICAL FUEL PUMPING AND METERING SYSTEM FOR MORE ELECTRICAL AERO-ENGINES Jean-Yves ROUTEX HISPANO-SUIZA, SAFRAN GROUP Keywords: Fuel, pumping,
Design Rules and Issues with Respect to Rocket Based Combined Cycles
Respect to Rocket Based Combined Cycles Tetsuo HIRAIWA hiraiwa.tetsuo@jaxa.jp ABSTRACT JAXA Kakuda space center has been studying rocket based combined cycle engine for the future space transportation
ALCOHOL LOX STEAM GENERATOR TEST EXPERIENCE
ALCOHOL LOX STEAM GENERATOR TEST EXPERIENCE Klaus Schäfer, Michael Dommers DLR, German Aerospace Center, Institute of Space Propulsion D 74239 Hardthausen / Lampoldshausen, Germany Klaus.Schaefer@dlr.de
Virtual Testing of the Full Vehicle System
Virtual Testing of the Full Vehicle System Mike Dempsey Claytex Services Limited Software, Consultancy, Training Based in Leamington Spa, UK Office in Cape Town, South Africa Experts in Systems Engineering,
Part II. HISTORICAL AND ENGINEERING ANALYSIS OF AIRSHIP PLAN-AND- DESIGN AND SERVICE DECISIONS
CONTENTS MONOGRAPHER S FOREWORD DEFENITIONS, SYMBOLS, ABBREVIATIONS, AND INDICES Part I. LAWS AND RULES OF AEROSTATIC FLIGHT PRINCIPLE Chapter 1. AIRCRAFT FLIGHT PRINCIPLE 1.1 Flight Principle Classification
SIMULATION OF A SPARK IGNITION ENGINE WITH CYLINDERS DEACTIVATION
F2010-C-198 SIMULATION OF A SPARK IGNITION ENGINE WITH CYLINDERS DEACTIVATION 1 Croitorescu, Valerian *, 1 Maciac Andrei, 1 Oprean Mircea, 1 Andreescu Cristian 1 Univeristy POLITEHNICA of Bucharest, Romania
Design Rules and Issues with Respect to Rocket Based Combined Cycles
Respect to Rocket Based Combined Cycles Tetsuo HIRAIWA hiraiwa.tetsuo@jaxa.jp ABSTRACT JAXA Kakuda space center has been studying rocket based combined cycle engine for the future space transportation
Unmanned Air Vehicles (UAVs): Classification, Legislation and Future applications Presenter: Dr-Ing Dimitrios E. Mazarakos
Unmanned Air Vehicles (UAVs): Classification, Legislation and Future applications Presenter: Dr-Ing Dimitrios E. Mazarakos The presenter Dr-Ing Dimitrios E. Mazarakos Dipl. in Mechanical Engineering and
Diesel Jet at a glance
Company Overview Diesel Jet at a glance DieselJet was established in 2003. Since 2011 it is owned by METATRON, an industrial group operating in the automotive field as CNG and LPG systems manufacturer.
Opportunities For Innovative Collaboration. Propulsion Directorate Propulsion & Power for the 21st Century Warfighter
Opportunities For Innovative Collaboration Propulsion Directorate Propulsion & Power for the 21st Century Warfighter Propulsion Directorate Our Mission Create and transition advanced air breathing and
AIRCRAFT GENERAL KNOWLEDGE (1) AIRFRAME/SYSTEMS/POWERPLANT
1 In flight, a cantilever wing of an airplane containing fuel undergoes vertical loads which produce a bending moment: A highest at the wing root B equal to the zero -fuel weight multiplied by the span
European Workshop on Aircraft Design Education 2002
From Specification & Design Layout to Control Law Development for Unmanned Aerial Vehicles Lessons Learned from Past Experience Zdobyslaw Goraj WUT, Poland Philip Ransom, Paul Wagstaff Kingston University,
Development of a Subscale Flight Testing Platform for a Generic Future Fighter
Development of a Subscale Flight Testing Platform for a Generic Future Fighter Christopher Jouannet Linköping University - Sweden Subscale Demonstrators at Linköping University RAVEN Rafale Flight Test
University of Jordan School of Engineering Mechatronics Engineering Department. Fluid Power Engineering Lab
University of Jordan School of Engineering Mechatronics Engineering Department 0908464 09 The University of Jordan School of Engineering MECHATRONICS ENGINEERING DEPARTMENT EXPERIMENT N0. 1 Introduction
HYDRAULIC AND LANDING GEAR SYSTEMS Author: Antonio Corrales Domínguez DPTO. DE INGENIERÍA AEROESPACIAL Y MECÁNICA DE FLUIDOS
HYDRAULIC AND LANDING GEAR SYSTEMS Author: Antonio Corrales Domínguez DPTO. DE INGENIERÍA AEROESPACIAL Y MECÁNICA DE FLUIDOS TABLE OF CONTENTS Hydraulic System Introduction to hydraulic systems Components
UNCLASSIFIED FY 2017 OCO. FY 2017 Base
Exhibit R-2, RDT&E Budget Item Justification: PB 2017 Air Force Date: February 2016 3600: Research, Development, Test & Evaluation, Air Force / BA 3: Advanced Technology Development (ATD) COST ($ in Millions)
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
CPC - B64D - 2018.08 B64D EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT Dropping, ejecting, releasing
Research on Optimization of Bleed Air Environment Control System of Aircraft Xin-ge WANG, Han BAO* and Kun-wu YE
2017 International Conference on Electronic, Control, Automation and Mechanical Engineering (ECAME 2017) ISBN: 978-1-60595-523-0 Research on Optimization of Bleed Air Environment Control System of Aircraft
Hydraulic Flywheel Accumulator for Mobile Energy Storage
Hydraulic Flywheel Accumulator for Mobile Energy Storage Paul Cronk University of Minnesota October 14 th, 2015 I. Overview Outline I. Background on Mobile Energy Storage II. Hydraulic Flywheel Accumulator
Propulsion Controls and Diagnostics Research at NASA GRC Status Report
Propulsion Controls and Diagnostics Research at NASA GRC Status Report Dr. Sanjay Garg Branch Chief Ph: (216) 433-2685 FAX: (216) 433-8990 email: sanjay.garg@nasa.gov http://www.lerc.nasa.gov/www/cdtb
Design and evaluate vehicle architectures to reach the best trade-off between performance, range and comfort. Unrestricted.
Design and evaluate vehicle architectures to reach the best trade-off between performance, range and comfort. Unrestricted. Introduction Presenter Thomas Desbarats Business Development Simcenter System
CONCEPT STUDY OF AN ARES HYBRID-OS LAUNCH SYSTEM
CONCEPT STUDY OF AN ARES HYBRID-OS LAUNCH SYSTEM AIAA-2006-8057 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference 06-09 November 2006, Canberra, Australia Revision A 07 November
How Does a Rocket Engine Work?
Propulsion How Does a Rocket Engine Work? Solid Rocket Engines Propellant is a mixture of fuel and oxidizer in a solid grain form. Pros: Stable Simple, fewer failure points. Reliable output. Cons: Burns
Propeller Blade Bearings for Aircraft Open Rotor Engine
NTN TECHNICAL REVIEW No.84(2016) [ New Product ] Guillaume LEFORT* The Propeller Blade Bearings for Open Rotor Engine SAGE2 were developed by NTN-SNR in the frame of the Clean Sky aerospace programme.
CONTENTS Duct Jet Propulsion / Rocket Propulsion / Applications of Rocket Propulsion / 15 References / 25
CONTENTS PREFACE xi 1 Classification 1.1. Duct Jet Propulsion / 2 1.2. Rocket Propulsion / 4 1.3. Applications of Rocket Propulsion / 15 References / 25 2 Definitions and Fundamentals 2.1. Definition /
Übersicht der VVT-Systementwicklung bei Hilite. Overview of VVT System development at Hilite
Übersicht der VVT-Systementwicklung bei Hilite Overview of VVT System development at Hilite M.Sc. Mustafa Mohammed Simulation Engineer Business Unit Engine / Simulation Frei verwendbar Contents Company
Balancing operability and fuel efficiency in the truck and bus industry
Balancing operability and fuel efficiency in the truck and bus industry Realize innovation. Agenda The truck and bus industry is evolving Model-based systems engineering for truck and bus The voice of
Corso di Motori Aeronautici
Corso di Motori Aeronautici Mauro Valorani Laurea Magistrale in Ingegneria Aeronautica (MAER) Sapienza, Università di Roma Anno Accademico 2011-12 Sett. 13: Conclusioni 1 FP7 Aero Engine Scenario ERS Strategy
EXPERIMENTAL METHOD OF DETERMINING CHARACTERISTICS OF POWER AND TORQUE ENGINE FOR LOW-POWER UNMANNED AERIAL VEHICLES
Journal of KONES Powertrain and Transport, Vol. 18, No. 3 2011 EXPERIMENTAL METHOD OF DETERMINING CHARACTERISTICS OF POWER AND TORQUE ENGINE FOR LOW-POWER UNMANNED AERIAL VEHICLES Grzegorz Jastrz bski,
Aeroplane Aerodynamics and Flight Controls 1 2
11.1 Theory of Flight 11.1.1. Aeroplane Aerodynamics and Flight Controls 1 2 Operation and effect of: roll control: ailerons and spoilers, pitch control: elevators, stabilators, variable incidence stabilisers
Modeling and Control for Turboelectric Aircraft
Modeling and Control for Turboelectric Aircraft Aidan Dowdle adowdle@mit.edu NASA GRC AS&ASTAR Fellow 11/1/17 This material is based upon work supported by the National Aeronautics and Space Administration
Clean Sky - Systems for Green Operation & links with SESAR
Clean Sky - Systems for Green Operation & links with SESAR Vienna, 3 rd of February, 2011 Helmut Schwarze (CleanSky JU) Ruud den Boer (CleanSky JU) Contents 1. Context & planning 2. Examples of progress
TEMPERATURE MEASURING GALVANIC SEPARATORS CONVERTORS, PRESSURE MEASURING
DELIVERY PROGRAMME TEMPERATURE MEASURING CONVERTORS, GALVANIC SEPARATORS PRESSURE MEASURING - Resistance temperature sensors into a reservoir, - with a reservoir, with protection tube, with cable - Resistance
A combustor design applied to the micro turbine. Taichung, Taiwan;
A combustor design applied to the micro turbine Chuan-Sheng Chen 1, Tzu-Erh Chen 1*, Hong-Chia Hong 1 1 Chung-Shan Institute of Science and Technology, Aeronautical Systems Research Division, Taichung,
TechSim Engineering Company Profile
TechSim Engineering Company Profile TechSim Engineering 14.06.2018 27.2.2018 TechSim Engineering Engineering company delivering cutting edge technologies in the area of virtual prototyping and system simulation
LANLEO11 - SQA Unit Code F9GV 04 Service and repair engines on land-based equipment
Service and repair engines on land-based equipment Overview This standard covers the construction and operating principles of two-stroke and four-stroke spark ignition and compression ignition engines
November 8, 2018 GAS TURBINE ENGINE SECONDARY FLOW SYSTEMS
November 8, 2018 GAS TURBINE ENGINE SECONDARY FLOW SYSTEMS Agenda 1 What is Secondary Flow? Purpose for the Secondary Flow Systems Chargeable Vs Nonchargeable Flows Seals Selection and Leakage Effects
Effect of ZFW / ZFWCG on Aircraft Operations
Operational Liaison Meeting Fly-By-Wire Aircraft 2004 Effect of / on Aircraft Operations Customer Services Contents Single-Aisle (SA) FM Architecture FAC Computation If Incorrect entered on the If Incorrect
NASA Glenn Research Center Intelligent Power System Control Development for Deep Space Exploration
National Aeronautics and Space Administration NASA Glenn Research Center Intelligent Power System Control Development for Deep Space Exploration Anne M. McNelis NASA Glenn Research Center Presentation
LMS Imagine.Lab. Driving Dynamics: Steering Systems Solutions. Marc Alirand BizDev Driving Dynamics 1D division
LMS Imagine.Lab Driving Dynamics: Steering Systems Solutions Marc Alirand BizDev Driving Dynamics 1D division Building a real time model of a hydraulic steering system Using AMESim Know-How The rendering
Power Estimation for a Two Seater Helicopter
Power Estimation for a Two Seater Helicopter JTSE Mohammad Nazri Mohd Jaafar, a,* Mohd Idham Mohd Nayan, a M.S.A. Ishak, b a Department of Aeronautical Engineering, Faculty of Mechanical Engineering, Universiti
Multirotor UAV propeller development using Mecaflux Heliciel
Multirotor UAV propeller development using Mecaflux Heliciel Sale rates of multirotor unmanned aerial vehicles, for both private and commercial uses, are growing very rapidly these days. Even though there
SECTION 6-3 POWER PLANT
SECTION 6-3 SYSTEMS DESCRIPTION Index Page General Description... 6-3-3 Engine Features... 6-3-4 Engine Indication System... 6-3-6 Power Plant Control... 6-3-10 Power Plant System Control... 6-3-12 Power
JAXA's electric propulsion systems
JAXA's electric propulsion systems Akira Nishizawa Emission free aircraft section Innovative Aircraft Systems Research Aircraft Systems Research Team Next Generation Aeronautical Innovation Hub Center
Aircraft Overview. Snowbird Human-Powered Ornithopter. Todd Reichert Cameron Robertson University of Toronto Institute for Aerospace Studies Canada
Aircraft Overview Snowbird Human-Powered Ornithopter Todd Reichert Cameron Robertson University of Toronto Institute for Aerospace Studies Canada August 2010 1 General Overview The project started in the
Innovation Takes Off. Not legally binding
Innovation Takes Off Not legally binding Clean Sky 2 Information Day January 28, Roma Systems ITD Marc FABREGUETTES, Thales Avionics Innovation Takes Off From Clean Sky towards Clean Sky 2 Systems ITD
Flammability Investigation of Different Refrigerants using an operating MAC system in a simulated front end collision situation
Flammability Investigation of Different Refrigerants using an operating MAC system in a simulated front end collision situation Martin Graz, Uwe Wuitz OBRIST Engineering Introduction A flammability investigation
Actuator Force Using Physical Modeling Tools to Design Power Optimized Aircraft
Actuator Force Using Physical Modeling Tools to Design Power Optimized Aircraft 2009 The MathWorks, Inc. Key Points 1. Testing different actuator designs in one environment saves time and encourages innovation
AF Hypersonic Vision
AF Hypersonic Vision Airbreathing hypersonic platform technologies to produce revolutionary warfighting capabilities Goal: S&T efforts to develop and mature robust, comprehensive technology options for:
UNIT 8 OTHER SENSORS
UNIT 8 OTHER SENSORS Aim and Agenda of unit 8 The aim of the presentation Sensors measuring humidity and temperature The agenda of the presentation Accelerometer Types of accelerometers NTC temperature
UNCLASSIFIED FY 2017 OCO. FY 2017 Base
Exhibit R-2, RDT&E Budget Item Justification: PB 2017 Air Force Date: February 2016 3600: Research, Development, Test & Evaluation, Air Force / BA 2: Applied Research COST ($ in Millions) Prior Years FY
World Leaders in Engineered Performance. Regional and Business Aircraft
World Leaders in Engineered Performance Regional and Business Aircraft From Commercial to Combat, This is Where Innovation Is Born Operational Excellence On Two Continents Feet-On-The-Ground Around The
j2 Universal Tool Kit Software in a Performance Prediction Role
j2 Universal Tool Kit Software in a Performance Prediction Role The j2 Universal Tool-Kit Performance Plug-in Derives Even More Value From The Leading Aircraft Design, Analysis and Aircraft Modelling Software
Test Bed 1 Energy Efficient Displacement-Controlled Hydraulic Hybrid Excavator
Test Bed 1 Energy Efficient Displacement-Controlled Hydraulic Hybrid Excavator Enrique Busquets Monika Ivantysynova October 7, 2015 Maha Fluid Power Research Center Purdue University, West Lafayette, IN,
STUDENT APPLICATION CHECKLIST
DIPLOMA OF ENGINEERING TECHNOLOGY IN AEROPLANE MAINTENANCE Module 1 AQD10102 Technical Mathematics 1 Module 2 AJD 10103 Physics & Aerodynamics AKD 10203 Electrical Fundamentals 2 Module 4 AKD 20102 Electronic
Udvavisk. Engineering Analysis with CFD. 1st Floor (B), Tower II, Ramana Complex #322, Velachery Main Road Velachery, Chennai
Udvavisk Engineering Analysis with CFD 1st Floor (B), Tower II, Ramana Complex # Velachery, Chennai 600042 1 Course outline 1.1 Engineering Analysis with CFD Flow and Aero-dynamic analyis around car body
Approche novatrice pour la conception et l exploitation d avions écologiques, sous incertitudes.
Sylvain Prigent Approche novatrice pour la conception et l exploitation d avions écologiques, sous incertitudes. Challenges Air traffic will double in the next 20 years! *Revenue passenger kilometers (number
NASA centers team up to tackle sonic boom 18 March 2014, by Frank Jennings, Jr.
NASA centers team up to tackle sonic boom 18 March 2014, by Frank Jennings, Jr. This rendering shows the Lockheed Martin future supersonic advanced concept featuring two engines under the wings and one
B-COOL. Low Cost and High Efficiency CO 2 Mobile Air Conditioning system for lower segment cars
Low Cost and High Efficiency CO 2 Mobile Air Conditioning system for lower segment cars Carloandrea Malvicino Centro Ricerche Fiat Strada Torino 50-10043 Orbassano Italy carloandrea.malvicino@crf.it -
Vehicle functional design from PSA in-house software to AMESim standard library with increased modularity
Vehicle functional design from PSA in-house software to AMESim standard library with increased modularity Benoit PARMENTIER, Frederic MONNERIE (PSA) Marc ALIRAND, Julien LAGNIER (LMS) Vehicle Dynamics
Development of Energy Balance Simulation Method for Vehicles
New technologies Development of Energy Balance Simulation Method for Vehicles Shigeyoshi Kadokura* Daisuke Konno* Hiroshi Ezaki* Kazunori Sekine** Chiharu Katsuyama** Tomohiro Nishizawa** Abstract In recent
Stress Analysis of Engine Camshaft and Choosing Best Manufacturing Material
Stress Analysis of Engine Camshaft and Choosing Best Manufacturing Material Samta Jain, Mr. Vikas Bansal Rajasthan Technical University, Kota (Rajasathan), India Abstract This paper presents the modeling
Evacuating by sorption or thermal means F04B 37/00. Attention is drawn to the following places, which may be of interest for search:
F04F PUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED {(evacuating by sorption F04B)}; SIPHONS {(conveying materials in bulk by flows of gas, liquid of foam
Crankcase scavenging.
Software for engine simulation and optimization www.diesel-rk.bmstu.ru The full cycle thermodynamic engine simulation software DIESEL-RK is designed for simulating and optimizing working processes of two-
Electric Penguin s philosophy:
UNMANNED PLATFORMS AND SUBSYSTEMS Datasheet v 1.1 Penguin BE Electric Unmanned Platform Up to 110 minutes of endurance 2 with 2.8 kg payload 23 liters of payload volume Quick replaceable battery cartridge
Modelling of Diesel Vehicle Emissions under transient conditions
Modelling of Diesel Vehicle Emissions under transient conditions Dr. Gavin Dober Combustion and Hydraulics Manager, Davide Del Pozzo Delphi Trainee 216-217 Advanced Injection & Combustion Center Delphi
AEROSPACE TEST OPERATIONS
CONTRACT AT NASA PLUM BROOK STATION SANDUSKY, OHIO CRYOGENIC PROPELLANT TANK FACILITY HYPERSONIC TUNNEL FACILITY SPACECRAFT PROPULSION TEST FACILITY SPACE POWER FACILITY A NARRATIVE/PICTORIAL DESCRIPTION
TBM UPGRADE CATALOG Edition 4 - October 2017
TM UPGRDE TLOG Edition 4 - October 2017 Please select the model of your interest. p.3 p.53 p.11 p.51 910 p.21 p.44 p.28 p.33 Price validity has to be checked in the online Spare parts price catalog on
TAKEOFF PERFORMANCE ground roll
TAKEOFF PERFORMANCE An airplane is motionless at the end of a runway. This is denoted by location O. The pilot releases the brakes and pushes the throttle to maximum takeoff power, and the airplane accelerates
SABRE FOR HYPERSONIC & SPACE ACCESS PLATFORMS
SABRE FOR HYPERSONIC & SPACE ACCESS PLATFORMS Mark Thomas Chief Executive Officer 12 th Appleton Space Conference RAL Space, 1 st December 2016 1 Reaction Engines Limited REL s primary focus is developing
PRODUCTS FOR MARTIN BAKER EJECTION SEATS
AIRCRAFT PRODUCTS PRODUCTS FOR MARTIN BAKER EJECTION SEATS ROCKET ENGINES ROCKET ENGINES FOR MARTIN BAKER MK-10 EJECTION SEATS These rocket engines for Martin Baker ejection seats are intended to provide
Component and System Level Modeling of a Two-Phase Cryogenic Propulsion System for Aerospace Applications
Component and System Level Modeling of a Two-Phase Cryogenic Propulsion System for Aerospace Applications J. LoRusso, B. Kalina, M. Van Benschoten, Roush Industries GT Users Conference November 9, 2015
In this lecture... Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay
1 In this lecture... Intakes for powerplant Transport aircraft Military aircraft 2 Intakes Air intakes form the first component of all air breathing propulsion systems. The word Intake is normally used
DESIGN OF AN AIR COOLED CYLINDER HEAD FOR TWO FAMILYS OF DIESEL ENGINES WITH DIRECT INJECTION
DESIGN OF AN AIR COOLED CYLINDER HEAD FOR TWO FAMILYS OF DIESEL ENGINES WITH DIRECT INJECTION 1 Vladimir-Gh. Mărdărescu, 2 Constantin Haşeganu, 1 Sebstian Radu, 1 Ervin Adorean, 1 Călin Itu, 1 Marton Iakab-Peter
CS2 Fast Rotorcraft NGCTR Objectives
CS2 Fast Rotorcraft NGCTR Objectives The main objectives for the Clean Sky 2 NextGenCTR Programme (Next Generation Civil Tiltrotor - NGCTR) are the following: Validation of key tiltrotor technologies for
Prevent corrosion that can decrease the aircraft structure life. Do a thorough inspection for corrosion and other types of damage.
TASK -100-801-A EFFECTIVITY: ALL 1. External Aircraft - Cleaning A. General (1) This task gives the procedures to remove light and heavy dirt from the ACFT external surfaces to: Prevent corrosion that
F135 Propulsion Integration Topics for Symposium on Jet Engines Haifa, Israel
F135 Propulsion Integration Topics for Symposium on Jet Engines Haifa, Israel Tom Johnson Program Chief Engineer Operational Military Engines 25 October 2012 J6924_F135_Propulsion_2012-1 Agenda F135 Development
Irkut Corporation plant is manufacturing fuselage sections and carries out its assembly
MC-21 MC-21 is a perspective commercial aircraft with a capacity of 150 to 211 passengers. Irkut Corporation (a UAC company) is creating the plane within a wide international cooperation First aircraft
Development of an Advanced Rotorcraft Preliminary Design Framework
134 Int l J. of Aeronautical & Space Sciences, Vol. 10, No. 2, November 2009 Development of an Advanced Rotorcraft Preliminary Design Framework Jaehoon Lim* and SangJoon Shin** School of Mechanical and
Overview of Intelligent Power Controller Development for the Deep Space Gateway
Overview of Intelligent Power Controller Development for the Deep Space Gateway Jeffrey Csank NASA Glenn Research Center Presented to Energy Tech 2017 Cleveland, Ohio Agenda Overview of NASA Vision Deep
Evolution of MDO at Bombardier Aerospace
Evolution of MDO at Bombardier Aerospace 6 th Research Consortium for Multidisciplinary System Design Workshop Ann Arbor, Michigan July 26 th - 27 th, 2011 Pat Piperni MDO Project Manager Bombardier Aerospace
Using Physical Modeling Tools to Design Power Optimized Aircraft
Using Physical Modeling Tools to Design Power Optimized Aircraft Rick Hyde Product Developer, Physical Modelling Tools The MathWorks Ltd, Cambridge, UK Rick.Hyde@mathworks.co.uk 2008 The MathWorks Limited
UNCLASSIFIED FY 2016 OCO. FY 2016 Base
Exhibit R-2, RDT&E Budget Item Justification: PB 2016 Air Force Date: February 2015 3600: Research, Development, Test & Evaluation, Air Force / BA 3: Advanced Technology Development (ATD) COST ($ in Millions)
USA FALCON 1. Fax: (310) Telephone: (310) Fax: (310) Telephone: (310) Fax: (310)
1. IDENTIFICATION 1.1 Name FALCON 1 1.2 Classification Family : FALCON Series : FALCON 1 Version : FALCON 1 Category : SPACE LAUNCH VEHICLE Class : Small Launch Vehicle (SLV) Type : Expendable Launch Vehicle
Clean Sky 2 General Information Day 21 November 2013, Brussels
Clean Sky 2 General Information Day 21 November 2013, Brussels Systems ITD Marc FABREGUETTES, THALES Innovation Takes Off From Clean Sky towards Clean Sky 2 Systems ITD follows and expands Clean Sky SGO
MSC/Flight Loads and Dynamics Version 1. Greg Sikes Manager, Aerospace Products The MacNeal-Schwendler Corporation
MSC/Flight Loads and Dynamics Version 1 Greg Sikes Manager, Aerospace Products The MacNeal-Schwendler Corporation Douglas J. Neill Sr. Staff Engineer Aeroelasticity and Design Optimization The MacNeal-Schwendler
FLYING CAR NANODEGREE SYLLABUS
FLYING CAR NANODEGREE SYLLABUS Term 1: Aerial Robotics 2 Course 1: Introduction 2 Course 2: Planning 2 Course 3: Control 3 Course 4: Estimation 3 Term 2: Intelligent Air Systems 4 Course 5: Flying Cars
Ejection Seat Mechanism in Civil Aircraft
International Journal of Scientific & Engineering Research, Volume 3, Issue 10, October-2012 1 Ejection Seat Mechanism in Civil Aircraft Richard Johnson Abstract this paper deals with the ejection system
Investigation of Radiators Size, Orientation of Sub Cooled Section and Fan Position on Twin Fan Cooling Packby 1D Simulation
Investigation of Radiators Size, Orientation of Sub Cooled Section and Fan Position on Twin Fan Cooling Packby 1D Simulation Neelakandan K¹, Goutham Sagar M², Ajay Virmalwar³ Abstract: A study plan to
Pressure Sensor/PS-A (ADP5)
Sensor PS-A sensor Built-in amplifi er and compensating circuit Features Built-in amplifier and temperature compensation circuit, no need for circuit design and characteristic adjustment High accuracy
IAC-04-IAF-S.2.06 NEW PROPELLANT IGNITION SYSTEM IN LV SOYUZ ROCKET ENGINE CHAMBERS
IAC-04-IAF-S.2.06 NEW PROPELLANT IGNITION SYSTEM IN LV SOYUZ ROCKET ENGINE CHAMBERS Igor Yu. Fatuev, Anatoly A.Ganin NPO Energomash named after academician V.P.Glushko, Russia, 141400, Khimky, Moscow area,
Official Journal of the European Union L 298/53
16.11.2011 Official Journal of the European Union L 298/53 A B1 B2 B3 10.6 Continuing airworthiness 2 2 2 2 Detailed understanding of Part-21 provisions related to continuing airworthiness. Detailed understanding
Experience the Hybrid Drive
Experience the Hybrid Drive MAGNA STEYR equips SUV with hybrid drive Hybrid demo vehicle with dspace prototyping system To integrate components into a hybrid vehicle drivetrain, extensive modification
Reducing Landing Distance
Reducing Landing Distance I've been wondering about thrust reversers, how many kinds are there and which are the most effective? I am having a debate as to whether airplane engines reverse, or does something
Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols
Contents Preface Acknowledgments List of Tables Nomenclature: organizations Nomenclature: acronyms Nomenclature: main symbols Nomenclature: Greek symbols Nomenclature: subscripts/superscripts Supplements
Preliminary Detailed Design Review
Preliminary Detailed Design Review Project Review Project Status Timekeeping and Setback Management Manufacturing techniques Drawing formats Design Features Phase Objectives Task Assignment Justification