A gas turbine, also called a combustion turbine, is a type of internal combustion engine. It has an upstream rotating compressor coupled toa downstream turbine, and a combustion chamber in-between. Energy is added to the gas stream in the combustor, where fuel is mixed with air and ignited. In the high-pressure environment of the combustor, combustion of the fuel increases the temperature. The products of the combustion are forced into the turbine section
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A gas turbine, also called a combustion turbine, is a type of internal combustion engine. It has an upstream rotating compressor coupled toa downstream turbine, and a combustion chamber in-between. Energy is added to the gas stream in the combustor, where fuel is mixed with air and ignited. In the high-pressure environment of the combustor, combustion of the fuel increases the temperature. The products of the combustion are forced into the turbine section
Visit https://www.topicsforseminar.com to Download
Actual cycles for internal combustion engines differ from air-standard cycles in many respects.
Time loss factor.
Heat loss factor.
Exhaust blow down factor.
Gas Turbine Theory - Principle of Operation and ConstructionSahyog Shishodia
This presentation tells all about basic principle behind Gas Turbine, their working, operation and construction. How they came into existence and where are they used.
COMBNED CYCLE POWER PLANT PPT
(Advanced method of Gas-Thermal based)
How Combined cycle Gas-Thermal Projects in India works.
Basic operation with details of modern Gas Booster Compressor (GBC) and highly efficient Heat Recovery Steam Generator(HRSG), General Electric Gas Turbines and BHEL steam turbines.
[in case anyone need much detail feel free to ping me]
For all the Gas Turbine lovers, the following presentation is aimed to cover the Major Inspection of the Gas Turbine (GE, Fr-9E). It is weaved with all of the major activities involved in MI, tools and tactics with addition of the reference values. Each activity is described with aid of pictures for detailed understanding.
Analysis of the Influence of Piston Cooling Cavity on Its Temperature FieldIJRES Journal
Engine piston cooling design is an important work of engine design. This article based on the finite
element analysis method, by studying two important structure parameters of the diesel engine piston, namely the
cooling oil cavity area and cooling oil cavity location, the diesel engine piston cooling effect and structure
parameters’ influences on the piston temperature field were studied. The results showed that: appropriately
increasing the cross-section of the cooling gallery is favorable for heat dissipation, but over-dimension will lead to
small cooling liquid filling ratio and thus impede the cooling; The movements of cooling gallery of the piston will
have great effect on the top of the piston, the combustion chamber, the fire shore, the first ring shore and the top of
the inner chamber. The research of this paper provides a basis for engine piston cooling design.
Actual cycles for internal combustion engines differ from air-standard cycles in many respects.
Time loss factor.
Heat loss factor.
Exhaust blow down factor.
Gas Turbine Theory - Principle of Operation and ConstructionSahyog Shishodia
This presentation tells all about basic principle behind Gas Turbine, their working, operation and construction. How they came into existence and where are they used.
COMBNED CYCLE POWER PLANT PPT
(Advanced method of Gas-Thermal based)
How Combined cycle Gas-Thermal Projects in India works.
Basic operation with details of modern Gas Booster Compressor (GBC) and highly efficient Heat Recovery Steam Generator(HRSG), General Electric Gas Turbines and BHEL steam turbines.
[in case anyone need much detail feel free to ping me]
For all the Gas Turbine lovers, the following presentation is aimed to cover the Major Inspection of the Gas Turbine (GE, Fr-9E). It is weaved with all of the major activities involved in MI, tools and tactics with addition of the reference values. Each activity is described with aid of pictures for detailed understanding.
Analysis of the Influence of Piston Cooling Cavity on Its Temperature FieldIJRES Journal
Engine piston cooling design is an important work of engine design. This article based on the finite
element analysis method, by studying two important structure parameters of the diesel engine piston, namely the
cooling oil cavity area and cooling oil cavity location, the diesel engine piston cooling effect and structure
parameters’ influences on the piston temperature field were studied. The results showed that: appropriately
increasing the cross-section of the cooling gallery is favorable for heat dissipation, but over-dimension will lead to
small cooling liquid filling ratio and thus impede the cooling; The movements of cooling gallery of the piston will
have great effect on the top of the piston, the combustion chamber, the fire shore, the first ring shore and the top of
the inner chamber. The research of this paper provides a basis for engine piston cooling design.
(
ME- 495 Laboratory Exercise
–
Number 1
– Brayton Cycle -
ME Department, SDSU
-
Nourollahi
) (
11
)Brayton Cycle (Gas Turbine Power Cycle)
Objective
The objective of this lab exercise is to gain practical knowledge of the Brayton cycle. The Brayton cycle illustrates the cold-air-standard assumption (constant specific heats at room temperature) model of a gas turbine power cycle. A portable propulsion laboratory[footnoteRef:1] containing a Model SR-30 turbojet is used in this exercise. The student shall apply the basic equations for Brayton cycle analysis by using empirical measurements at different points in the Brayton cycle. [1: Manufactured by Turbine Technologies Ltd. Called TTL Mini-Lab]
Figure 1: TTL Mini-Lab manufactured by Turbine Technologies Ltd. (TTL)Background
A simple gas turbine engine has three main components: a compressor section, a combustion chamber and a turbine section. Basic operation entails drawing atmospheric air into the compressor where it is heated through compression. The compressed and heated air is mixed with fuel in the combustion chamber. The air/fuel mixture burns at constant pressure in the combustion chamber. The resulting hot gas is directed to the turbine section where it expands. As the gas expands it produces a thrust reaction and performs work by turning the turbine. The turbine is connected to the compressor by a shaft. The resulting shaft work is used to drive the compressor and auxiliary power supplies.
The gas turbine has wide spread application. Most notably, it is used to power and propel aircraft and large ships. In some cases only the thrust resulting from the expanding gas exiting the turbine is used for propulsion and the shaft work is used to drive the compressor and power electrical systems. In turbo-fan engines some of the shaft work is used to drive a large fan that aids in propulsion. In other applications, such as helicopters and ships, propulsion is achieved through the shaft work, which is used to drive transmission/gear boxes that are connected to the rotor blades or propeller, respectively. Gas turbines are also commonly used to drive large electrical generators in power plant applications.Theory
The Brayton cycle consists of four basic processes (see Figure3 & 4). Low-pressure air is drawn into the compressor section and undergoes isentropic compression. Next, the heated and compressed air is combined with fuel in the combustion chamber. The air/fuel mixture experiences reversible constant pressure heat addition. The resulting hot gas enters the turbine section where it undergoes isentropic expansion. To complete the cycle (the exhaust and intake in the open cycle) the gas experiences reversible constant pressure heat rejection.
Thermodynamics and the First Law of Thermodynamics determine the overall energy transfer. The following assumptions are used when analyzing the gas turbine cycles:
1. The working fluid (air) is an ideal gas throughout the cycle.
2. The combust ...
1. INTRODUCTION TO IC ENGINE
2. FUNDAMENTALS OF IC ENGINE
3. CONSTRUCTIONAL FEATURES & FUNCTIONS OF IC ENGINE
4. MATERIALS USED
5.IC ENGINE – TERMINOLOGY
6.SEQUENCE OF OPERATION(A. Four Stroke Engine/B. Two Stroke Engine)
7. COMPARISON BETWEEN TWO STROKE AND FOUR STROKE ENGINES
8.Otto Cycle,Diesel Cycle,Dual Cycle & their Comparison
9.VALVE TIMING DIAGRAM
10.ENGINE PERFORMANCE PARAMETERS RELATED TO IC ENGINE
11. CHARACTERISTICS CURVES OF VARIOUS PERFORMANCE PARAMETERS
12. FUEL-AIR CYCLE & THEIR ANALYSIS ( 1.Brake Specific Fuel Consumption vs Size 2. Brake Specific Fuel Consumption vs Speed 3. Performance Maps )
13. ACTUAL INDICATOR DIAGRAM
14. V.C.R ENGINE SPECIFICATIONS & ITS DESCRIPTION
15. FUTURE WORKS & DISCUSSION
16. CONCLUSION
An inside view of thermal power stations and DDCMIS in power plantsRg Lokkesh
THE SLIDES EXPLAINS ABOUT THE DDCMIS(DITRIBUTED DIGITAL CONTROL SYSTEM AND MANAGMENT INFROMATION SYSTEM) SYSTEM USED IN POWER PLANT WITH THE PICTURE AND EXPLENATION.
Industrial Training at Shahjalal Fertilizer Company Limited (SFCL)MdTanvirMahtab2
This presentation is about the working procedure of Shahjalal Fertilizer Company Limited (SFCL). A Govt. owned Company of Bangladesh Chemical Industries Corporation under Ministry of Industries.
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Dr.Costas Sachpazis
Terzaghi's soil bearing capacity theory, developed by Karl Terzaghi, is a fundamental principle in geotechnical engineering used to determine the bearing capacity of shallow foundations. This theory provides a method to calculate the ultimate bearing capacity of soil, which is the maximum load per unit area that the soil can support without undergoing shear failure. The Calculation HTML Code included.
About
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Technical Specifications
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
Key Features
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface
• Compatible with MAFI CCR system
• Copatiable with IDM8000 CCR
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
Application
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Student information management system project report ii.pdfKamal Acharya
Our project explains about the student management. This project mainly explains the various actions related to student details. This project shows some ease in adding, editing and deleting the student details. It also provides a less time consuming process for viewing, adding, editing and deleting the marks of the students.
Water scarcity is the lack of fresh water resources to meet the standard water demand. There are two type of water scarcity. One is physical. The other is economic water scarcity.
Immunizing Image Classifiers Against Localized Adversary Attacksgerogepatton
This paper addresses the vulnerability of deep learning models, particularly convolutional neural networks
(CNN)s, to adversarial attacks and presents a proactive training technique designed to counter them. We
introduce a novel volumization algorithm, which transforms 2D images into 3D volumetric representations.
When combined with 3D convolution and deep curriculum learning optimization (CLO), itsignificantly improves
the immunity of models against localized universal attacks by up to 40%. We evaluate our proposed approach
using contemporary CNN architectures and the modified Canadian Institute for Advanced Research (CIFAR-10
and CIFAR-100) and ImageNet Large Scale Visual Recognition Challenge (ILSVRC12) datasets, showcasing
accuracy improvements over previous techniques. The results indicate that the combination of the volumetric
input and curriculum learning holds significant promise for mitigating adversarial attacks without necessitating
adversary training.
Cosmetic shop management system project report.pdfKamal Acharya
Buying new cosmetic products is difficult. It can even be scary for those who have sensitive skin and are prone to skin trouble. The information needed to alleviate this problem is on the back of each product, but it's thought to interpret those ingredient lists unless you have a background in chemistry.
Instead of buying and hoping for the best, we can use data science to help us predict which products may be good fits for us. It includes various function programs to do the above mentioned tasks.
Data file handling has been effectively used in the program.
The automated cosmetic shop management system should deal with the automation of general workflow and administration process of the shop. The main processes of the system focus on customer's request where the system is able to search the most appropriate products and deliver it to the customers. It should help the employees to quickly identify the list of cosmetic product that have reached the minimum quantity and also keep a track of expired date for each cosmetic product. It should help the employees to find the rack number in which the product is placed.It is also Faster and more efficient way.
Hybrid optimization of pumped hydro system and solar- Engr. Abdul-Azeez.pdffxintegritypublishin
Advancements in technology unveil a myriad of electrical and electronic breakthroughs geared towards efficiently harnessing limited resources to meet human energy demands. The optimization of hybrid solar PV panels and pumped hydro energy supply systems plays a pivotal role in utilizing natural resources effectively. This initiative not only benefits humanity but also fosters environmental sustainability. The study investigated the design optimization of these hybrid systems, focusing on understanding solar radiation patterns, identifying geographical influences on solar radiation, formulating a mathematical model for system optimization, and determining the optimal configuration of PV panels and pumped hydro storage. Through a comparative analysis approach and eight weeks of data collection, the study addressed key research questions related to solar radiation patterns and optimal system design. The findings highlighted regions with heightened solar radiation levels, showcasing substantial potential for power generation and emphasizing the system's efficiency. Optimizing system design significantly boosted power generation, promoted renewable energy utilization, and enhanced energy storage capacity. The study underscored the benefits of optimizing hybrid solar PV panels and pumped hydro energy supply systems for sustainable energy usage. Optimizing the design of solar PV panels and pumped hydro energy supply systems as examined across diverse climatic conditions in a developing country, not only enhances power generation but also improves the integration of renewable energy sources and boosts energy storage capacities, particularly beneficial for less economically prosperous regions. Additionally, the study provides valuable insights for advancing energy research in economically viable areas. Recommendations included conducting site-specific assessments, utilizing advanced modeling tools, implementing regular maintenance protocols, and enhancing communication among system components.
2. Wheel space
Wheel space is the area between the turbine "wheels" and the stationary
turbine casing. The spaceis below the turbine buckets and nozzles, around the
shaft. The turbine buckets mount on the turbine wheels, and the diaphragms are
the stationary "separators" that the wheels fit in between.
Number of Wheel space:-
There are two wheel spaces per turbine stage--a forward wheel spaceand an
aft wheel space.
A two-stage gas turbine would have four wheel spaces.
A three-stage gas turbine would have six wheels paces.
Fig shows: - 3 Stage Gas Turbine with 6 Wheel Spaces.
Wheel space of a turbine
3. Wheel space thermocouple
Wheel space T/Cs are used to measure temperature around wheel space
region of gas turbine which are inserted from the outside of the turbine
shell/combustion wrapper and one cannot see them as they are pushed through
guide tubes into the thermocouple well area . There are inner set of T/Cs and an
outer set of T/Cs (one set is closer to the shaft than the other set).
Fig shows: - Wheel Space Thermocouple.
Wheel Space Temperature
Wheel spaces temperature are measured because there are seals which
try to keep the hot combustion gases traveling axially through the nozzles and
buckets in an axial path in order to get the most energy from them. And, the
seals also keep the hot combustion gases from getting down into the turbine
wheel/diaphragm area where they could excessively heat them and cause
damage to the turbine shaft and casing/shell.
Mounted wheelspace
thermocouple
4. Wheel Space Over Temperature Alarms:-
If the wheel space temperature of a running turbine starts to increase or
decrease during normal steady-state operation (relatively constant load), then it's
an indication of either a problem with cooling and sealing air flow into the
wheel space or the wheel space seals are not working properly.(usually
combined with a change in turbine rotor axial position).
There are two dual element thermocouples (TC) in wheel space to
monitor the wheel space temperature. The average temperature measured by the
2 thermocouple is computed and compared to an alarm for each location, if the
average temperature exceeds then alarm is generated.
Fig shows: - Alarm wheel spaces Temperature values.
Fig shows: - High wheel space temperature reading by thermocouple.
5. WHEELSPACE THERMOCOUPLE PROBLEMS:-
Higher temperature difference than the normal temperature difference
between some of the thermocouple pair indicate thermocouple problems, or
possible seal leaks. However, these thermocouples rarely detect turbine
problems, but can often have sensor problems, such as: Bad insertion is a
common problem, particularly on the later turbine stages as the thermocouple
has to be pushed down a long and narrow tube with various turns in it. Often it
is not inserted far enough, so the thermocouple will partially detect hot air
inside other turbine spaces, such as the inside of the nozzles. This will give
incorrect and high readings. To get correct insertion, a note should be made of
the thermocouple length and how far it needs to be inserted. These numbers
should then match up after insertion. Other thermocouple problems can occur,
such as cold junction, shorts. If a seal leak is present, this should normally be
detected by both thermocouple pairs.
Recommendation:-
Carry out an inspection on the thermocouples and the wiring, and repair
and recalibrate as required. If the problems persist, check for seal leaks.