A SEMINAR REPORT ON “PULSE DETONATION ENGINE”

Slides:

Advertisements

Similar presentations

Engines and Motors Part - 2. Engines and Motors Turbines Rocket Steam.

Advertisements

1 Lecture 5: Propulsion Jason Mickey For AE 440 A/C Lecture September 2009.

MAE 4261: AIR-BREATHING ENGINES

Lecture #12 Ehsan Roohi Sharif University of Technology Aerospace Engineering Department 1.

Challenges of hypersonic air-breathing flight Dr. David M. Birch Head, Flow Control Research Group Technical Director, Surrey Sensors LLC*

U3AEA04 ELEMENTS OF AERONAUTICS

Review AE430 Aircraft Propulsion Systems Gustaaf Jacobs.

Department of Mechanical Engineering ME 322 – Mechanical Engineering Thermodynamics Lect 27b Jet Aircraft Propulsion.

Propulsion Systems. Propulsion System A machine that produces thrust to push an object forward The amount of thrust depends on the mass flow through the.

Introduction to Propulsion

Aircraft Engines Types and Placement.

What is a Pulse Detonation Engine?

Jet Propulsion and Compressor Design

FLIGHT POWER Know basic engine principles. 1. Define a list of terms related to basic engine principles. 2. Describe the various types and components of.

Thanks to USAFA and USAF Test Pilot School Propulsion 1 Dr. Ken Van Treuren Department of Engineering Baylor University EGR Analysis and Design.

Introduction to Hypersonic Propulsion Systems

Gas turbine cycles for aircraft propulsion In shaft power cycles, power is in form of generated power. In air craft cycles, whole power is in the form.

Thermodynamics Professor Lee Carkner Lecture 18

AME 436 Energy and Propulsion Lecture 15 Propulsion 5: Hypersonic propulsion.

How do aircraft jet engines work?

Gas Turbines By: Katie Steddenbenz.

MAE 4262: ROCKETS AND MISSION ANALYSIS

Jet propulsion and Jet Engines

Thrust Lecture 8 Chapter 4. Thrust Thrust is the force that must be generated in order to overcome the natural resistance of drag. Because drag is the.

Analysis of Turbofan Engine

AE 1350 Lecture Notes #13.

MECHANICAL ENGINEERING

Conestoga Valley High School Aviation Technology Powerplant Engines.

MAE 4261: AIR-BREATHING ENGINES Exam 2 Review Exam 2: November 18 th, 2008 Mechanical and Aerospace Engineering Department Florida Institute of Technology.

Means to Create A Jet P M V Subbarao Professor Mechanical Engineering Department Viable ways of Creating Strong and Reliable Muscles for the Aircraft……

Parametric Cycle Analysis of Ideal Turbo Jet Engine

AEROSPACE 410 AEROSPACE PROPULSION Lecture (10/25/2002) RAMJET ANALYSIS IDEAL RAMJET AND ACTUAL RAMJET DESIGN Dr. Cengiz Camci.

DRAFT. Introduction  Mechanical Power Reciprocating Engines Turbines Turbines are compact machines (high power to weight ratio, having less balancing.

VEL TECH Dr. RR & Dr. SR TECHNICAL UNIVERSITY

Rocket Engines India Morris November 3, What are Rocket Engines??? Jet engines that use only propellant mass for forming the high speed jet/ thrust.

MAE 5360: Hypersonic Airbreathing Engines Ramjet Overview Mechanical and Aerospace Engineering Department Florida Institute of Technology D. R. Kirk.

AE 433 – Introduction to Aircraft Gas Turbine Engines

Lecture #10 Ehsan Roohi Sharif University of Technology Aerospace Engineering Department 1.

Lecture 3b: Aircraft Engines s: Propeller + Piston Engines Era  From 1903 (Wright bros.) until the Early 1940s, all aircraft used the piston.

AME 514 Applications of Combustion

Hello! I am Ahamath Jalaludeen I am here because I love to give presentations. You can find me at

Weapon Propulsion and Architecture Naval Weapons Systems.

Relationship between Super-Knock and Pre-Ignition

POWERPLANT INTRO TO TURBINES PP2 Spokane Community Community College College.

AEROSPACE 410 AEROSPACE PROPULSION Fall 2002 Dr. Cengiz Camci Professor of Aerospace Engineering Turbomachinery Aero/Heat Transfer Laboratory P S U Rotorcraft.

WORK Work = Force x Distance POWER power = work done ÷ time taken ENERGY 1-POTENTIAL ENERGY (Potential Energy = Force x Distance ) 2-KINETIC ENERGY Energy.

Lesson 2: Aircraft Engine Types And Construction.

11.3 Notes. Explosions Product of combustion accompanied by creation of gases and heat and occurring at a rapid rate Most bombings are perpetrated by.

Flame Propagation and Stability Unit

Thermodynamics I Introduction CHAPTER

Ramjets By Robert Espey.

Performance Characteristics of Turbo Jet Engines

AME 436 Energy and Propulsion

MEL 341 : GAS DYNAMICS & PROPULSION

SPARK IGNITION ENGINES

COMBUSTION TA : Donggi Lee PROF. SEUNG WOOK BAEK

MAE 5360: Hypersonic Airbreathing Engines

Analysis of Jet & Rocket Propulsion Systems

PULSE DETONATION ENGINE

Jet Engines Aerospace.

Performance Analysis of Ramjet Engines

AEROSPACE PROPULSION Dr. Cengiz Camci AEROSPACE 410 Fall 2002

Notes 21.1 – Properties of Sound

Axisymetric Inlet Design for Combined-Cycle Engines Jesse R

Irreversibilities in Propulsion Systems

MAE 5380: ROCKETS AND MISSION ANALYSIS

Jet Aircraft Propulsion

Propulsion Systems Aircraft, Rocket, Space © 2011 Project Lead The Way, Inc.Aerospace Engineering.

Presentation transcript:

A SEMINAR REPORT ON “PULSE DETONATION ENGINE” Department of Mechanical Engineering Govt. college of engineering pune Guided by Submited by Prof M T Shete Samir singh

Pulse Detonation Engine(PDE) Introduction Deflagration v/s Detonation Principle of engine Configuration Classification Analysis Advantages Challenges conclusion

Introduction PDE is a propulsion technology that can be used in aviation industries Main objective of PDE is to develop efficient engine that can be used at high speed & at high altitudes.

Various propulsion engine are ramjet engine, scramjet engine, pulse jet engine. PDE is similar to pulse jet engine. the diffrence is that PDE detonate their fuel rather than deflagrate.

Deflagration v/s Detonation Deflagration is process of burning the fuel rapidly with the flame that travel with subsonic speed.it is also called subsonic combustion . Detonation is a violent reaction, violent release of confined energy, usually accompanied by a loud sound and shock waves. It is also called supersonic combustion . .

Principle of engine

Configuration of typical pde

Classification of PDE Pure pulse detonation engine Combined cycle PDE Hybrid pulse detonation engine

Turbofan engine Hybrid PDE

THURST COMPARISON OF PDE WITH CONVENTIONAL TURBOFAN

ADVANTAGES OF PDE: 1) The thermodynamic efficiency of pulse detonation engine is higher. 2) More efficient in specific thurst and specific fuel consumption than current ramjet engine. 3)No fuel turbopump required. 4)reduced cost and complexity than liquid propellant rocket. 5) Mechanical simplicity and high compression ratio.

Challenges for PDE Initiation of detonation Frequency with which detonation has to be repeated Materials for detonation tube needs to be developed

Conclusion PDE makes excellant choice for static thurst & also thermodynamic efficiency PDE is higher than conventional propulsion engine Can be used in aircraft at high altitudes with high speed and efficiency.

Refrences http://www.aardvark.co.nz/pjet/pde.shtml> Kailasanath, K. “Recent Developments in the Research on Pulse Detonation Engines,” 40th AIAA Aerospace Sciences Meeting, AIAA 2002-0470. G.D. Roy, S.M. Frolov, A.A. Borisov, D.W. Netzer “Pulse detonation propulsion: challenges, current status, and future perspective” Pulse detonation engine technology :an overview By Matthew Lam, Daniel Tillie, Timothy Leaver, Brian McFadden, APSC 201 http://www.aardvark.co.nz/pjet/pde.shtml> http://en.wikipedia.org/wiki/Pulse_detonation_engine http://www.af.mil/news/story.asp?id=123099095

THANK YOU

Question?