Jet Propulsion
Introduction:
The following report, submitted to Roy Aircraft Engines Incorporated for an efficiency study, is an analysis of a turbojet engine completed by thermodynamically studying each main component that constitutes a turbojet engine. RAE Incorporated requested software that would calculate the theoretical maximum output velocity, using input data imputed by the user of the program. The calculations are made assuming idealized conditions. In the analysis, the turbojet was broken down into its fundamental parts, which consist of an inlet, compressor, burner, turbine, and nozzle.
Description of Turbojet Components
First, the inlet / diffuser, of a turbojet brings free stream air to the engine and does no thermodynamic work on the flow. It is assumed that the flow through the diffuser is isentropic.
Second, the compressor does work onto the gas passing through to raise the pressure. Again, this process is assumed to be isentropic.
Third, the compressed air is combined with fuel and is ignited within the combustor. The process within the combustor is assumed to be isentropic. The resulting high temperature fluid is used to turn the fourth component of the turbojet, the turbine.
Next, the turbine is used to extract energy from the heated flow coming from the burner. This is done by this flow of gas passing through blades on a free spinning shaft. The turbine generates just enough energy to drive the compressor. When the flow passes through the turbine, the pressure and temperature are decreased.
The next step is optional within the program. Here an afterburner is used to reheat the exiting gas from the turbine. This is done by injecting additional fuel into the gas exiting from the turbine. Igniting this mixture produces a higher temperature at the nozzle, as a result the final velocity of the jet engine is increased.
Finally, the flow comes through the nozzle where no thermodynamic work is performed on the flow by the nozzle. The temperature remains constant through the nozzle while the pressure and velocity of the flow will change as dictated by the design of the nozzle. The nozzle is used to produce thrust and used to conduct the exhaust gases back to the free air.
For the analysis of the turbojet, several assumptions were made and are as follows:
1. Air behaves as a compressible, ideal gas.
2. Flow through the diffuser, nozzle, compressor and combustor is
1.Intake: The intake valve opens allowing fresh oxygen rich air mixed with fuel to enter the cylinder.
...the shock waves created by a shift, which acts as a brake, slowing the turbo and requiring it to be spooled up again. We lose boost pressure but keep our turbo speed this way.
How many times a day do you hear a jet airplane roar over the top of your house, leaving a trail of dark, black smoke behind? People all around the world are complaining about the noise and contamination that jet aircraft produce as they fly over densely populated cities. Airplanes are flying around the clock consuming thousands and thousands of gallons of fuel a minute. So many jet engine manufactures have tried time and time again to reduce the noise and contamination that their engines produce yet so many times to no avail. General Electric is now incorporating new technology into their engines that will reduce not only the fuel consumption and contamination produced by the jet engines, but increase their thrust output.
explosion used to move the pistons up and down is greater however this pressure has to resist combustion in order to achieve
This hot gas is pushed out through the back and it makes the rocket move forward. This is using Newton's third law of
Thrust is able to happen because of Newton’s third law of motion: for every action, there is an equal and opposite reaction. In a rocket that is going into space, there is gas that is pushed out of the engine in one direction, and the thrust is applied in the other direction, to lift the rocket off the ground and up into the sky. Similarly, in an Alka-Seltzer® rocket the thrust is provided by the gas (carbon dioxide), but because the gas is enclosed, it is not able to escape. When the gas finally does escape, it functions as the counter-force, and enables the canister to separate from the cap and fly into the
The trials and tribulations of flight have had their ups and downs over the course of history. From the many who failed to the few that conquered; the thought of flight has always astonished us all. The Wright brothers were the first to sustain flight and therefore are credited with the invention of the airplane. John Allen who wrote Aerodynamics: The Science of Air in Motion says, “The Wright Brothers were the supreme example of their time of men gifted with practical skill, theoretical knowledge and insight” (6). As we all know, the airplane has had thousands of designs since then, but for the most part the physics of flight has remained the same. As you can see, the failures that occurred while trying to fly only prove that flight is truly remarkable.
Firstly, the gas turbine engine operation begins with the air intake process. As of all internal combustion engine, oxygen is required to support the combustion of the fuel and the source of oxygen is from the fresh air that is taken in. Initially, the fan is rotated by a driving shaft that is powered by the turbine of the engine. A negative or vacuum pressure at the intake side is then created by the rotating fan. Next, the surrounding air is drawn towards the inlet and causes it to flow into the gas turbine engine inlet (Cengel & Boles, 2011). At the same time, the pressure on the other side of the fan is increased as it is compressed at a lower pressure ratio and causes the air in the outlet side of the fan to move fu...
The steam engine is a peripheral ignition mechanism, wherein the operating fluids are disconnected from the ignition results. Non-combustion heat resources like nuclear and solar powers or geothermal power could be utilized. Water resorts to vapour in a reservoir and arrive at high pressures. When developed through turbines or pistons, automatic exertion is completed. The condensed-pressure condensation is then compressed, and reverse-pumped to a boiler. Several convenient steam engines remove low-pressure steams rather than compressing it for recycles.
Next Dalton’s law of partial pressure is used. The mixture of gas in the graduated cylinder was filled with two things: water vapor and air. Using the Dalton’s law, it can be concluded that the total pressure is equal to the pressure of air and the pressure of water vapor added together. This is an endothermic reaction which means that it absorbs heat, and when a reaction gains heat, it is repres...
The process need toluene and hydrogen as a main reactor. Then, toluene and hydrogen are converted in a reactor packed with catalyst to produce benzene and methane. This reaction is exothermic and the operating conditions are 500 0C to 660 0C, and 20 to 60 bar of pressure. This process begins with mixing fresh toluene with a stream of recycle unreacted toluene, and the mixing is achieved in a storage tank. Then, the toluene is pumped to combine it with a stream of mixed hydrogen and fresh hydrogen gas. The mixture of toluene and hydrogen is preheated before it is introduce to the heater or furnace. In the furnace, the stream is heated to 600 0C, then introduced into the reactor. Basically, the main reactions occurs in the reactor.
... turned by pistons, it is fueled by a combustion process using turbine exhaust to spin the prop rather, hence the term turboprop. A turbofan is what you will find on all private business jets and airliners. Instead of turning a prop, turbofan engines use the exhaust to turn a fan which helps produce more thrust by helping creating bypass air. Military planes such as the F-22 Raptor use the plain jet engine which produces thrust by in simple terms lighting jet fuel on fire and pushing it out the back. Whatever type of engine it may be, they are all important pieces of a plane.
A steam engine is an external combustion that converts heat energy, in the form of steam, into mechanical energy. Steam is generated through combustion of a fuel, i.e. Coal, heating a boiler filled with water, which evaporates to produce steam that expands do drive a piston connected to a flywheel in a rotary motion. The flywheel then transmits energy created to a crankshaft which is used to provide power to machines, such as locomotives, fluid pumps, and machine tools. Waste steam is then expelled from the engine through an exhaust, or can be condensed and repurposed in some steam engine designs (Croft and Tangerman, 1939).
As the piston rises, the pressure forces the poppet valve closed, and the mixture is compressed. Once the piston reaches its peak, the spark plug fires, igniting the compressed fuel causing the fuel to expand driving the piston downward. The exhaust valve opens after the piston reaches its lowest point. As the piston begins to rise, the exhaust fuel is driven out of the chamber. Large four-stroke engines tend to have more than one cylinder and often feature valves, fuel injectors, and turbochargers (Four Stroke
turbine via interceptor valves and control valves and after expanding enters the L.P. turbine stage via 2 numbers of cross over pipes. In the L.P. stage the steam expands in axially opposite direction to counteract the trust and enters the condenser placed directly below the L.P. turbine. The cooling water flowing throughout the condenser tubes condenses the steam and the condensate collected in the hot well of the condenser. The condensate collected is pumped by means of 3*50% duty condensate pumps through L.P. heaters to deaerator from where the boiler feed pump delivers the water to boiler through H.P. heaters thus forming a closed