INDEX:
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Sl. No| Topic| Page no.|
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1| Index| 1|
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2| Introduction| 2|
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3| Scenario 1| 3 to 7|
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4| Scenario 2| 7 to 9|
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5| Scenario 3| 9 to 13|
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6| Scenario 4| 13 to 17|
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7| Scenario 5| 17 to 18|
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8| Conclusion| 19|
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9| reference point| 20|
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INTRODUCTION:
Modern channelizecraft may usance soaked air, or pneumatic systems for a variety of purposes. Some use pneumatics for de-icing purposes, for operation of various flight instruments while others use the pneumatic system, to provide a positive air pressure in the cabin for flight at high altitudes, where pressurization is used to translate the passengers and crew with the environment needed to fly without supplemental oxygen. secernate of the cabin pressurization system is the air cycle unit, humidifier, pressure control & mass airflow control; each integrity performing a distinct and an important function to key the aircraft cabin environment as comfortable as possible, for both(prenominal) the crew and the passengers.
At present; on most multi locomotive aircraft, the fuel manifolds atomic number 18 connected in such a manner that any fuel army tank may translate fuel to any engine. This is known as a send away cross-feed system. Cross feed valves are present, which when opened, transfers fuel from any tank to any engine.
Cabin harnesses, slides and oxygen provisions are provided in aircrafts these days for the safety of its passengers. Theraputic oxygen is also available for the passengers who are susceptible to medical conditions at high altitudes.
SCENARIO 1: R1
In the pneumatic system the compressed air has different advantages on board. Turbine powered aircrafts has a greater advantage as air can simply be extracted from the compressor...If you want to get a full essay, order it on our website: Ordercustompaper.com
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