vfp sponsored research projects · outline . introduction 3 bachelor of science in aerospace...

21
Mechanical Engineering Department Alabama A&M University July 15 , 2015 VFP Sponsored Research Projects By Dr. Mebougna L. Drabo DOE-Visiting Faculty Program & BNL - Presentation

Upload: others

Post on 27-Jul-2020

1 views

Category:

Documents


0 download

TRANSCRIPT

Page 1: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Mechanical Engineering Department Alabama A&M University

July 15 , 2015

VFP Sponsored Research Projects By

Dr. Mebougna L. Drabo

DOE-Visiting Faculty Program & BNL - Presentation

Page 2: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

2

v Introduction

v Year 1 : I-DLTS

v Year 2 : Flash Atomization

v Year 3: Development of Fuel Atomizers for Low Firing Rate Modulating Burners

v Acknowledgements

Outline

Page 3: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Introduction

3

Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering University at Buffalo Master of Science in Mechanical Engineering University of Alabama in Tuscaloosa Doctoral of Philosophy in Mechanical Engineering University of Alabama in Tuscaloosa

Page 4: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

4

Research Interest

v  Propulsion v  Flash Atomization v  Improving the efficiency of the jet fuel used by the Air Force v  Improvement of Cadmium Manganese Telluride and Cadmium Zinc

Telluride Nuclear Detectors for Homeland Security Applications v  Current Deep Level Transient Spectroscopy (I-DLTS) v  Cold-Start v  Fuel Vaporization v  Combustion v  Diesel engine v  Alternative fuel v  Internal Combustion engine emissions reduction and efficiency improvement v  Advanced Combustion IC engine concepts v  Laser diagnostics in an internal combustion engine v  Heat Transfer & Thermodynamics v  Images processing v  Humanoid robot

Page 5: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Year 1: I-DLTS

Page 6: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

6

Current Deep Level Transient Spectroscopy(I-DLTS) v  I-DLTS

Ø  current-based microscopic defect analysis technique for high resistivity detector materials((>  106  Ω-­‐cm) such as CdZnTe and heavily irradiated Si.

Ø  Defects are filled by free carriers generated by incident laser pulse.

v  This technique makes it possible to identify & analyze defect levels and their correlation with the detector electrical degradation    

Page 7: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

I-DLTS Study

Defect-level filling

detrapping

•  I-DLTS … Current Deep-Level Transient Spectroscopy

•  Study of energy levels is important to get information about the defect structure in semiconductor materials

•  Deep levels can negatively influence detector performance (low efficiency, poor energy resolution, and polarization)

•  We can obtain activation energy and capture cross-section of defect levels

Temperature range 12 - 360 K

Page 8: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Summary

v Finished with

Ø  I-DLTS manual for Drs. Ralph James & Zheng Li

Ø  I-DLTS Data Analysis manual

v Collaborating with Dr. Budak’s group at AAMU

Ø  I-DLTS on new sample’s materials

ü  Resistivity? •  It changes depending on the sample type

•  It depends on the applied high energy ion beam for bombardment

ü  Band-gap

ü  Bulk / Film

ü  Dimensions •  2mm X 7mm or 1cm X 1cm

Page 9: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Acknowledgements

9

This project was supported in part by the U.S. Department of Energy, Office of Science, Office of Workforce Development for Teachers and Scientists (WDTS) under the Visiting Faculty Program (VFP) National Science Foundation/Domestic Nuclear Detection Office ARI(Academic Research Initiative) Program Entitled: ARI-MA Development of Improved CMT & CZT Nuclear Detectors for Homeland Security Applications Radiation Research Groups at Brookhaven National Laboratory

Page 10: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Year 2: Flash Atomization

Page 11: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Objective for this research

11

v Help aid in the future transition to biofuel technology

ü The outcomes include using a nozzle spray characterization to adjust the spray atomization process

Page 12: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Flash Atomization

12

v  A pure liquid, a liquid mixture, or a liquid with dissolved gas is exposed to sufficient superheating or pressure reduction that causes bubble formation

ü Rapid growth of bubbles is the cause of the explosion of the bubble and generation of finer droplets and spray

Page 13: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Why are Spray Important?

13

v Combustion of liquid fuels ü  Liquid rockets, liquid fueled ramjets ü  Diesel engines, stratified-charge engines ü  Oil-fired furnaces & boilers ü  Gas turbine

v Liquid metal processes ü  Powder production and net- form manufacturing (spray forming)

o Requires precise control of droplet size and trajectory to obtain the desired performances

v Agriculture ü  Insecticides, fertilizer & pesticides

o  Need Correct droplet of size to achieve the desired goal v Application of health care products v Environmental protection

ü  Water injection for NOx reduction ü  Gas scrubbing for dust particles

v Coating & Painting  

v  Important Liquid properties for atomization ü  Surface tension ü  Density ü  Dynamic viscosity

Page 14: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Nozzle

14

Simplex Pressure Nozzle Photo Credit: Hago Manufacturing

Nozzle Components, & Operation Photo Credit: Hago Manufacturing

For more info, please see BNL – 79185-2007 - IR

Primary function of the nozzle is to atomize the fuel into drops so that they can be evaporated and burnt.

Page 15: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

15

Analysis of Malvern Measurement Data For Danfoss 45-degree 0.4 HFD Nozzle with number 2 heating oil

@ 100 PSI

Page 16: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

16

ü  Tests with number 2 oil were performed under transient heating and cool down conditions.

ü  Smaller D[3][2] as the temperature goes up

Page 17: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Summary

v Wrote a proposal “Development of Fuel Atomizers for Low Firing Rate Load Modulating Burners” to National Oilheat Research Alliance(NORA) Ø It addresses the Category F: Atomization Technology of NORA

Project Opportunity Notices (PON) NO. 2014-001 Ø Funded

Page 18: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Acknowledgements

18

This project was supported in part by the U.S. Department of Energy, Office of Science, Office of Workforce Development for Teachers and Scientists (WDTS) under the Visiting Faculty Program (VFP) Sustainable Technology Research Groups at Brookhaven National Laboratory

v Drs. Thomas Butcher, Narinder Tutu, & C.R. Krishna v George Wei & Yusuf Celebi

Page 19: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Year 3: Start working on the Funded Proposal

Page 20: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Comments & Suggestions

20

Page 21: VFP Sponsored Research Projects · Outline . Introduction 3 Bachelor of Science in Aerospace Engineering University at Buffalo Master of Science in Aerospace Engineering ... (VFP)

Nozzle

21

v Primary function of the nozzle is to atomize the fuel into drops so that they can be evaporated and burnt.

v The nozzle basically convert the potential energy that has been packed into the fuel in the form of pressure energy to kinetic energy, in the form of a swirling and extremely turbulent flow. v It causes the liquid sheet formed at the exit of the nozzle to break up into

drops