Mechanical Engineering - Compressors, Gas Dynamics and Gas Turbines - Discussion
Discussion Forum : Compressors, Gas Dynamics and Gas Turbines - Section 3 (Q.No. 1)
1.
A compressor at high altitudes will require __________ power.
Discussion:
15 comments Page 1 of 2.
Gaurav said:
1 decade ago
Why is it so?
Harshit Nayal said:
1 decade ago
At higher altitudes molecules of air are few, hence a compressor supplies smaller volume of air at a higher altitude so it requires less power.
Navdeep said:
1 decade ago
As per my opinion, at high altitude power required to compressed air is more because temperature of air at height is more & Pressure is less Called less dense air. So specific volume of air is high due to high temperature & compressor consumes more power for same pressure ration on sea level to compress high temperature air.
Jnk said:
9 years ago
From my point of view answer is more power is required.
Satyabrata Dash said:
9 years ago
In my opinion, in high altitude the pressure is very low so higher power is required to reach the desired than sea level for same compressor ratio. So higher power is required.
Leetu said:
9 years ago
Yes, higher power required.
Omkar said:
9 years ago
More power is required for same compression ratio.
Vara said:
9 years ago
For same compression ratio, discharge pressure is low because of low suction pressure at higher latitudes so power required is less. At higher pressure, further compression required more power.
Himanshu Saini said:
8 years ago
The Answer is B.
Another factor to consider is the effect of altitude and air density on the operation of the engine that is powering the compressor. As altitude increases the air density decreases resulting in a roughly proportional decrease in the horsepower your engine is able to produce. A normally aspirated diesel engine might have 10% less power available at 800m/2600ft and 20% at 1600m/5200ft compared to operation at sea level. Different engines will have different de-rate curves depending on the engine design, for example, some turbocharged engines can compensate for the effects of altitude. Reduced engine power can result in a situation where the engine bogs down and the RPM drops which results in fewer compression cycles per minute and therefore less compressed air output. In extreme cases, the engine may not be able to run the compressor at all without stalling.
Another factor to consider is the effect of altitude and air density on the operation of the engine that is powering the compressor. As altitude increases the air density decreases resulting in a roughly proportional decrease in the horsepower your engine is able to produce. A normally aspirated diesel engine might have 10% less power available at 800m/2600ft and 20% at 1600m/5200ft compared to operation at sea level. Different engines will have different de-rate curves depending on the engine design, for example, some turbocharged engines can compensate for the effects of altitude. Reduced engine power can result in a situation where the engine bogs down and the RPM drops which results in fewer compression cycles per minute and therefore less compressed air output. In extreme cases, the engine may not be able to run the compressor at all without stalling.
Sachin said:
8 years ago
More power required for same compression ratio. And the performance of engine decreases at high altitude.
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