Gas Turbine Innovation : Flying Machine to Ground Utilities

Gas turbine technology flying machine to ground utilities l.jpg
1 / 28
0
0
1033 days ago, 345 views
PowerPoint PPT Presentation
1914: Application for a gas turbine motor recorded by Charles Curtis. ... To begin with Gas turbine electro train 2500 HP requested from BBC by Swiss Federal Railways ...

Presentation Transcript

Slide 1

Gas Turbine Technology : Flying Machine to Ground Utilities P M V Subbarao Professor Mechanical Engineering Department A White Collar Power Generation Method…

Slide 2

Progress in Rankine Cycle

Slide 3

The most Unwanted Characteristic of Rankine Group of Power Generation Systems The measure of cooling required by any steam-cycle control plant is dictated by its warm efficiency.  It has nothing basically to do with whether it is fuelled by coal, gas or uranium.  Where accessibility of cooling water is restricted, cooling does not should be a limitation on new producing capacity.  Alternative cooling choices are accessible at marginally higher cost. Atomic power plants have more prominent adaptability in area than coal-let go plants because of fuel coordinations, giving them more potential for their siting to be dictated by cooling contemplations.

Slide 4

Cooling Problems !!!! The greater the temperature distinction between the inner warmth source and the outside environment where the surplus warmth is dumped, the more effective is the procedure in accomplishing mechanical work.  The attractive quality of having a high temperature inside and a low temperature environmentally.  In a coal-let go or ordinarily gas-let go plant it is conceivable to run the interior boilers at higher temperatures than those with finely-built atomic fuel congregations which must maintain a strategic distance from damage.  The outer thought offers ascend to alluringly siting power plants close by exceptionally cool water.

Slide 5

Steam Cycle Heat Transfer For the warmth exchange work the water is circled ceaselessly in a shut circle steam cycle and scarcely any is lost.  The water should be spotless and genuinely unadulterated. This capacity is much the same whether the power plant is atomic, coal-let go, or customarily gas-fired.  Cooling to gather the steam and surplus warmth release. The second capacity for water in such a power plant is to cool the framework in order to gather the low-weight steam and reuse it.  This is a noteworthy thought in siting power plants, and in the UK siting study in 2009 all proposals were for destinations inside 2 km of inexhaustible water - ocean or estuary.

Slide 6

Water, Water & Water … .!!!!! An atomic or coal plant running at 33% warm effectiveness should dump around 14% more warmth than one at 36% efficiency.  Nuclear plants as of now being manufactured have around 34-36% warm productivity, contingent upon site (particularly water temperature).  Older ones are frequently just 32-33% efficient.   The moderately new Stanwell coal-let go plant in Queensland keeps running at 36%, however some new coal-let go plants approach 40% and one of the new atomic reactors claims 39%.

Slide 7

History & Repetition 1791: A patent was given to John Barber, an Englishman, for the primary genuine gas turbine. His development had a large portion of the components introduce in the advanced gas turbines. The turbine was intended to control a horseless carriage. 1872: The primary genuine gas turbine motor was composed by Dr Franz Stikze, yet the motor never kept running under its own energy. 1903: A Norwegian, Ægidius Elling, could manufacture the principal gas turbine that could deliver more power than expected to run its own parts, which was viewed as an accomplishment in a period when information about streamlined features was restricted. Utilizing rotational compressors and turbines it delivered 11 hp (gigantic for those days). He assist built up the idea, and by 1912 he had built up a gas turbine framework with isolated turbine unit and compressor in arrangement, a mix that is currently normal.

Slide 8

1914: Application for a gas turbine motor recorded by Charles Curtis. 1918: One of the main gas turbine makers of today, General Electric, began their gas turbine division. 1920: The reasonable hypothesis of gas move through sections was created into the more formal (and pertinent to turbines) hypothesis of gas stream past airfoils by Dr A. A. Griffith. 1930: Sir Frank Whittle protected the plan for a gas turbine for fly drive.

Slide 9

THE WORLD'S FIRST INDUSTRIAL GAS TURBINE SET – GT NEUCHÂTEL

Slide 10

4 MW GT for Power Generation

Slide 11

First turbojet-fueled air ship – Ohain's motor on He 178 The world's first flying machine to fly absolutely on turbojet control, the Heinkel He 178. Its first genuine flight was on 27 August, 1939.

Slide 12

Steam Turbine Vs Gas Turbine : Power Generation Experience picked up from countless gas turbines for diesel motors, a temp. of 538°C was considered completely alright for uncooled warm opposing steel turbine cutting edges. This would bring about realistic yields of 2000-8000 KW with compressor turbine efficiencies of 73-75%, and a general cycle productivity of 17-18%. Initially Gas turbine electro train 2500 HP requested from BBC by Swiss Federal Railways The appearance of high weight and temperature steam turbine with regenerative warming of the condensate and air pre-warming, brought about coupling efficiencies of approx. 25%. The gas turbine having been viewed as aggressive with steam turbine plant of 18% which was considered not exactly agreeable. The Gas turbine was not able contend with "cutting edge" base load steam turbines of 25% effectiveness. There was a consistent advancement in steam control plant which prompted to increment of Power Generation Efficiencies of 35% + This hard reality required thought of an alternate application for the gas turbine.

Slide 13

6 4 2 5 1 3 Anatomy of A Jet Engine

Slide 14

Variation of Jet Technologies

Slide 15

Thermal Energy Distribution

Slide 16

6f 7f 6p 7p Ideal Jet Cycles ~1970s Aero Rejected Engines & Aero Derivative Engines 4 TurboJet 3 5 6j T 0 Turbofan 1 2 Turboprop Direction

Slide 17

Brayton Cycle 1-2 Isentropic pressure (in a compressor) 2-3 Constant weight warm expansion 3-4 Isentropic development (in a turbine) 4-1 Constant weight warm dismissal

Slide 18

pv & Ts graphs SSSF Analysis of Control Volumes Making a Brayton Cycle:

Slide 19

Specific Energy condition of SSSF : No Change in potential vitality over any CV Calorically flawless and Ideal Gas as working liquid.

Slide 20

1 –2 : Specific work input : 2 – 3 : Specific warmth input : 3 – 4 : Specific work yield : 4 – 1 : Specific warmth dismissal : Isentropic Processes:

Slide 21

Constant Stagnation Pressure Processes:

Slide 25

Pressure Ratio Vs Efficiency

Slide 26

Pressure Ratio Vs Specific Workoutput

Slide 27

h th w net h,%

Slide 28

1872, Dr Franz Stikze's Paradox

SPONSORS