Showing posts with label Heat Exchangers. Show all posts
Showing posts with label Heat Exchangers. Show all posts

Basic process and component description

 

Industrial Steam turbine Based power plants

 

1)  These are thermal power plants.

2)  Fuel used in these power stations is Coal, Oil or Natural gas. (Fossil fuels)

3)   In many countries steam turbine power plants produce bulk of the energy.

4)  In these plants Boilers convert chemical energy of the fuel into heat energy and iturbines use this energy in steam coming from Boiler to rotate the generator and produce electricity.

5)  In refineries oil is abundantly available as bi product hence oil will be uded as fuel, otherwise coal or natural gas are used based on cost and availability.

First step :Conversion of chemical energy to heat

 

In the Boiler furnace, Fuel and air mixture is burnt and enormous heat energy is released.

\textrm{Fuel} + \textrm{Air} \rightarrow \; \textrm{Heat}  + \textrm{Carbon dioxide} + \textrm{Water}

Second Step :Conversion of heat into mechanical energy

In steam turbine the energy in the steam is employed to rotate the turbine. Which in turn operates the generator to produce power.

 Associated processes in Steam Turbine based Power plants

Feedwater heating and deaeration

The feedwater used in the boiler is a means of transferring heat energy from the burning fuel to the mechanical energy of the spinning steam turbine. The total feedwater consists of recirculated condensate water and purified makeup water. Because the metallic materials it contacts are subject to corrosion at high temperatures and pressures, the makeup water is highly purified before use. A system of ion exchange.


Deaeator primarily helps to remove dissolved oxygen from feedwater in addition it also helps to condition the water by dosing various chemicals.

In deaerator water is sprayed and maintained at high temperature to help  the oxygen to escape from the system. Remaining oxygen is eliminated by dosing oxygen removing chemical hydrazine, Ph controlling chemicals are also dosed in Deaerator..

Boiler operation

The boiler is a rectangular furnace of around 40 feet height and 20 feet length and width.

Oil is fired from four burners located in front side. Air required for effective combustion is fired through a fan.

Steam turbine generator

The turbine generator consists of 13 stages of blades. Steam starts to flow from first stage at 103 Kg/Cm2. At fourth stage it reaches 42 Kg/Cm2. At the final stage pressure is maintained at vacuum.

 

 

 Steam condenser



The condenser condenses the steam from the exhaust of the turbine into liquid to allow it to be pumped. If the condenser can be made cooler, the pressure of the exhaust steam is reduced and efficiency of the cycle increases.

The condenser is usually a shell and tube type heat exchanger.

Cooling water circulates through the tubes in the condenser's shell and the low pressure exhaust steam is condensed by flowing over the tubes as shown in the adjacent diagram.

The condenser, in effect, creates the low pressure required to drag steam through and increase the efficiency of the turbines. The limiting factor is the temperature of the cooling water and that, in turn, is limited by the prevailing average climatic conditions at the power plant's location

From the bottom of the condenser, powerful condenstae pumps recycle the condensed steam (water) back to the water/steam cycle through deaerator.

The most powerful lightweight heat exchangers in the world

Reaction Engines Ltd (REL) 's ultra-lightweight heat exchangers are the key enabling components in SABRE engines for Mach 5 cruise and aircraft-like access to space.
Heat exchangers that cool the incoming air are the biggest technical challenge to the realisation of the SABRE engine. At Mach 5 (5 times the speed of sound) the heat exchanger needs to cool air from 1,000°C to minus 150°C, in 1/100th of a second, displacing 400 Mega-Watts of heat energy (equivalent to the power output of a typical gas-powered power station) yet weighs less than 1¼ tonnes.

Using Heat Exchangers in Aerospace Engines

In the 1970s REL's founder Alan Bond started exploring the potential impact of heat exchangers light enough to be usefully integrated into rocket engine cycles. The main idea was that heat exchangers could remove heat where it caused a problem, and the energy extracted could then be used to drive the pumps and compressors that supply propellants to the rocket engine. While the potential to create a significant increase in engine efficiency was clear, the problem was that the weight of heat exchangers using conventional technology was so large that all the potential benefit was lost.
The SABRE Cycle
Inspired by the miniaturisation of the silicon chip, and understanding that heat exchangers were far from reaching their physical limit in terms of miniaturisation, developing high power lightweight heat exchangers became the focus of REL when it was founded by Alan Bond in 1989.
The impact of successfully developing lightweight heat exchangers on aerospace propulsion systems is seen as comparable to the impact of the silicon chip on computing: new products, new markets, new capabilities.
Heat Exchangers for the SABRE Engine
In the case of the SABRE engine there are two uses for heat exchangers. The first use is to cool the incoming air (which becomes very hot at high speed) so that it can be compressed to the pressure required for it to enter the rocket combustion chamber whilst concurrently heating helium, which is used to drive the engine machinery. We call the heat exchanger on the Sabre engine a Pre-cooler.
Location of the Precooler in the SABRE engine (shown in blue).
The second use is to cool the hot helium using the cold liquid hydrogen fuel, but this uses more conventional heat exchanger technology.
The team at REL has found ways to produce heat exchangers light enough to be viable for the first time in a flying engine. REL has also pioneered solutions to the other practical problems in this application, such as the control of frost formation (where the water in the atmosphere freezes in the heat exchanger, icing it up).
Although REL has developments in other technology areas of the SABRE engine, its heat exchangers are the key to its success and also represent the biggest advance over existing technology.

Sectional view of a Convection Recuperator

Convection recuperators also referred to as "flue" or "canal" recuperators are tubular heat exchangers that utilize convection heat transfer to preheat combustion air or gas for the purpose of saving fuel. The heat is recovered from the hot waste gas exiting a furnace and transfer it to the combustion air feeding the burners, fuel usage can be reduced by an average of twenty-five percent (25%), and in many cases, greater savings are realized. Waste gas temperatures entering convection recuperators are usually in the 1500°F to 2000°F range, and combustion air preheat temperatures are usually in the 800°F to 1200°F range. 

Heat Wheel Animation

Heat or enthalpy wheels are rotary air-to-air heat exchangers. Adjacent supply and exhaust air counterflow streams each flow through half of the wheel. Heat wheels have a fill that transfers only sensible heat while an enthalpy wheel's fill transfers total heat.

TESTING OF TUBESKIN THERMOCOUPLES



During outages, tube skin thermocouples should be tested for accuracy and potential failure. Tube skin thermocouples have a reputation for being inaccurate and failing prematurely. Inspection and testing during outages is an important step to improve reliability. Thermocouple leads are often the root failure by being exposed to flame and radiation, or lifting off the tube surface. Attachment welds should be inspected with dye penetrant for cracks that can cause the thermocouple to read firebox temperature. The sheathing protecting the thermocouple leads should be inspected for any breaches and kinks.

Some thermocouples will have a temperature drift due to long term exposure or temperature cycling. Procedures can be developed to determine if the tube temperature is accurately measured by heating an area adjacent to the tube and monitoring the temperature rise. A calibrated contact pyrometer can measure temperature at that point and be used for comparison to the thermocouple.