anastasios papadopoulos · 2016-11-09 · anastasios papadopoulos thermodynamics & i.c....

2
Event: ENERGY in TRANSPORTATION 2016 Date: Saturday November 12, 2016 Place: Athens, Hellas # Anastasios Papadopoulos Thermodynamics & I.C. Engines, Hellenic Air Force Academy, Dpt of Aeronautical Sciences, Section of Thermodynamics, Propulsion & Power Systems, Dekelia Air Force Base ) Title: HAF Officer (Second Lieutenant) Presentation title: Thermodynamic Exhaust Heat Recovery Analysis of an Aero- derivative Gas Turbine using a Subcritical Steam Rankine Cycle Gas turbines are well-known for their high power to weight ratio, significantly low starting – acceleration times, high flexibility and high reliability. However, conventional gas turbines suffer from low thermal efficiencies especially at partial load. As known, aero-derivative gas turbines are used from many navies around the world, mainly as combined propulsion systems, in various types of naval vessels. Hence, one of the most promising technologies nowadays for efficiency improvement of commercial gas turbines is the combination of a conventional gas turbine cycle with a bottoming Rankine cycle constituting thus a so-called “combined cycle”. According to the combined cycle concept, exhaust gas heat is used for steam production in a specially-designed heat exchanger, which is often called heat recovery steam generator (HRSG). High-enthalpy generated steam is then expanded in a turbine producing thus, additional mechanical power. Hence, for the same fuel heating rate in the gas turbine, an increased power output is attained through bottoming Rankine cycle improving thus, the overall efficiency of the combined cycle facility.A diploma thesis in Hellenic Air Force Academy (HAFA) was recently performed investigating more thoroughly the thermodynamic performance of a combined cycle comprised of an aero-derivative gas turbine and a steam Rankine bottoming cycle. Under the aforementioned thesis, a thermodynamic analysis computational model was developed for examining the thermal performance of a subcritical steam Rankine bottoming cycle, which recovers exhaust gas heat from an aero-derivative gas turbine. The operational behavior of the combined cycle was examined at various gas turbine operating loads and also under various ambient conditions i.e. dry bulb air temperatures and humidity ratios using HAFA’s gas turbine training and simulation software. The technical findings of the present study can be proven quite useful to the military-related scientific community working on materializing solutions for seriously improving the efficiency and downplaying the infrared “signature” of gas turbine- propelled transportation units.

Upload: donga

Post on 13-Jun-2018

220 views

Category:

Documents


0 download

TRANSCRIPT

Event: ENERGYinTRANSPORTATION2016Date: SaturdayNovember12,2016 Place: Athens,Hellas

#

Anastasios Papadopoulos Thermodynamics & I.C. Engines, Hellenic Air Force Academy, Dpt of Aeronautical Sciences, Section of

Thermodynamics, Propulsion & Power Systems, Dekelia Air Force Base

)

Title: HAF Officer (Second Lieutenant)

Presentationtitle: Thermodynamic Exhaust Heat Recovery Analysis of an Aero-derivative Gas Turbine using a Subcritical Steam Rankine Cycle

Gas turbines are well-known for their high power to weight ratio, significantly low starting – acceleration times, high flexibility and high reliability. However, conventional gas turbines suffer from low thermal efficiencies especially at partial load. As known, aero-derivative gas turbines are used from many navies around the world, mainly as combined propulsion systems, in various types of naval vessels. Hence, one of the most promising technologies nowadays for efficiency improvement of commercial gas turbines is the combination of a conventional gas turbine cycle with a bottoming Rankine cycle constituting thus a so-called “combined cycle”. According to the combined cycle concept, exhaust gas heat is used for steam production in a specially-designed heat exchanger, which is often called heat recovery steam generator (HRSG). High-enthalpy generated steam is then expanded in a turbine producing thus, additional mechanical power. Hence, for the same fuel heating rate in the gas turbine, an increased power output is attained through bottoming Rankine cycle improving thus, the overall efficiency of the combined cycle facility.A diploma thesis in Hellenic Air Force Academy (HAFA) was recently performed investigating more thoroughly the thermodynamic performance of a combined cycle comprised of an aero-derivative gas turbine and a steam Rankine bottoming cycle. Under the aforementioned thesis, a thermodynamic analysis computational model was developed for examining the thermal performance of a subcritical steam Rankine bottoming cycle, which recovers exhaust gas heat from an aero-derivative gas turbine. The operational behavior of the combined cycle was examined at various gas turbine operating loads and also under various ambient conditions i.e. dry bulb air temperatures and humidity ratios using HAFA’s gas turbine training and simulation software. The technical findings of the present study can be proven quite useful to the military-related scientific community working on materializing solutions for seriously improving the efficiency and downplaying the infrared “signature” of gas turbine-propelled transportation units.

Event: ENERGYinTRANSPORTATION2016Date: SaturdayNovember12,2016 Place: Athens,Hellas

CV: Anastasios Papadopoulos 30 Aghias Paraskevis Street, Chalkis Email: [email protected] Tel: 6984279692

I am an ambitious and personable individual starting my military career in Hellenic Airforce.

Education and quali f ications

• 2012 – 2016 Hellenic Airforce Academy BSc Aeronautical Sciencies Modules included: Thermodynamics & I.C Engines, Theoretical Mechanics, Machine Elements, Materials Science and Engineering, Aerodynamics, Mechanics of Flight, Materials, Avionics, Aircraft Design, Aeroelasticity, Operation Management, Aeronautics, Ballistics, Control Systems, Technology of Fuels, Physics, Theoretical Physics, Mathematics, Electrotechnics, AC/DC Machines, Principles of Electronics, Propulsive Systems, Flight Test, Quality Control and Assurance. Dissertation: Thermodynamic Exhaust Heat Recovery Analysis of an Aero-derivative Gas Turbine using a Subcritical Steam Rankine Cycle. 2006 – 2012: High School Education General Degree: 19.5 Work experience:

Nov 2016 - Present Attending seminars on QC & QA at KEA, Eleusina Attiki.

Sept 2016 – Nov 2016 Atteding seminars on CAD, CAE Computing Analysis, Aircraft and Engine Structural Integrity Program and Radars at ETHM, Elliniko Attiki.

Aug 2016 – Sept 2016 Atteding seminars on HAF Officer’s Duties at 128ΣΕΤΗ, Kavouri Attiki.

Addit ional ski l ls and achievement IT Skills:

• Confident in Microshoft Office packages.

• Personal occupation on Autocad and CATIA software.

• Familiar to Matlab, Octave and Scilab packages.

• Speaking Engish (proficient adequacy). Interest and hobbies:

• Reader of flight magazine.

• Enjoy occupying with martial arts, Tae Kwon Do athlete.