Steam passing through a multistage impulse...

Study

Question 1 of 205eccefa0bacbc34ba4d470e4

Steam passing through a multistage impulse turbine does not impart any appreciable axial thrust to the rotor. This is primarily due to the __________.

Back

Question 1 of 20

5eccefa0bacbc34ba4d470e4

Steam passing through a multistage impulse turbine does not impart any appreciable axial thrust to the rotor. This is primarily due to the __________.

No comments yet

Be the first to share your thoughts!

If the question has a related picture, it will appear here.

🔍 Key Concepts

• Impulse turbine flow pattern – where does the main pressure drop occur: stationary nozzles or moving blades? • Axial vs. tangential forces – which design feature minimizes net thrust along the shaft? • Purpose of dummy pistons / equalizing holes in turbine rotors

💭 Think About

• First, recall how steam flows through an impulse turbine stage: where is pressure nearly constant, and where does velocity change? • Think about which parts of the rotor or wheel are specifically provided to balance forces on opposite sides of a disc or drum. • Which option describes a feature that directly helps equalize pressure on both sides of the rotor, thereby reducing net axial force?

✅ Before You Answer

• Verify in your notes where the pressure drop occurs in an impulse turbine (nozzles vs. moving blades). • Identify which choices deal with pressure balancing across the rotor rather than just energy conversion. • Ask: which listed feature is explicitly used in turbine design to reduce axial thrust on the rotor?

👋 Hi! I'm Genie, your AI study assistant. How can I help you with this question?

Quick actions

— No credit card needed

Study

Question 1 of 205eccefa0bacbc34ba4d470e4

Steam passing through a multistage impulse turbine does not impart any appreciable axial thrust to the rotor. This is primarily due to the __________.

Back

Question 1 of 20

5eccefa0bacbc34ba4d470e4

Steam passing through a multistage impulse turbine does not impart any appreciable axial thrust to the rotor. This is primarily due to the __________.

No comments yet

Be the first to share your thoughts!

If the question has a related picture, it will appear here.

🔍 Key Concepts

💭 Think About

✅ Before You Answer

👋 Hi! I'm Genie, your AI study assistant. How can I help you with this question?

Quick actions

— No credit card needed