Question

In: Mechanical Engineering

Steam enters the nozzle of an impulse turbine stage at 60 bar and 500 °C and...

Steam enters the nozzle of an impulse turbine stage at 60 bar and 500 °C and leaves at 20 bar. Flow is adiabatic and reversible. The nozzle angle is 20°. The moving blade is symmetric, travels at optimum velocity, and assumed to be frictionless. It is also assumed that there is neither expansion nor contraction of the steam flow through the blade passage. Draw the velocity diagram and calculate (a) the blade efficiency and (b) the stage efficiency.

Solutions

Expert Solution


Related Solutions

The velocity of steam leaving the nozzle of a single-stage impulse turbine is 813 m/sec. The...
The velocity of steam leaving the nozzle of a single-stage impulse turbine is 813 m/sec. The nozzle angle is 20° and the blade speed corresponds to maximum blade efficiency. The moving blade is symmetric, assumed to be frictionless, and there is neither expansion nor contraction of the steam flow through the blade passage. Draw the velocity diagram and determine the relative velocity of steam leaving the blade.
Steam at 50 Bar and 500oC is expanded isentropically through a single stage turbine to a...
Steam at 50 Bar and 500oC is expanded isentropically through a single stage turbine to a condenser operating at 1 bar. Assuming the steam at turbine exit is Dry Saturated Steam and the turbine is required to produce a power output of 5.33MW. Calculate the required steam mass flow rate in kg/s to 2 decimal places.
A single stage steam turbine is supplied with steam at 5 bars, 200 C at the...
A single stage steam turbine is supplied with steam at 5 bars, 200 C at the rate of 50kgmin. It exhausts into a condenser at a pressure of 0.2 bars. The blade speed is 400msec. Nozzles are inclined at an angle of 20 to the plane of the wheel and outlet blade angle 30. Neglecting friction losses, the power developed by the turbine will be?
Refrigerant 134a enters a well-insulated nozzle at 14 bar, 60°C, with a velocity of 37 m/s...
Refrigerant 134a enters a well-insulated nozzle at 14 bar, 60°C, with a velocity of 37 m/s and exits at 1.2 bar with a velocity of 460 m/s. For steady-state operation, and neglecting potential energy effects, determine the exit temperature, in °C.
Steam at 5MPa and 300°C enters a turbine in a steady flow manner, from the turbine...
Steam at 5MPa and 300°C enters a turbine in a steady flow manner, from the turbine the steam expands to 200kPa with a quality of 90%. Find the following: The work done by the steam to the turbine in kj/kg The amount of steam flow rate needed in kg/hr if the turbine produces 200kW of power The efficiency of the expansion process
Consider a vapor power cycle as shown below. Steam enters the first turbine stage at 12...
Consider a vapor power cycle as shown below. Steam enters the first turbine stage at 12 MP a, 480 oC, and expands to 2 MP a. Some steam is extracted at 2 MP a and fed to the closed heater. The remainder expands through the second-stage turbine to 0.3 MP a, where an additional amount is extracted and fed into the open heater operating at 0.3 MP a. The steam expanding through the third-stage turbine enters the condenser at a...
Steam enters an adiabatic turbine at 500C and 4.0MPa and 80m/s. The steam leaves the turbine...
Steam enters an adiabatic turbine at 500C and 4.0MPa and 80m/s. The steam leaves the turbine as saturated liquid-vapor mixture at 30kPa, quality of 92% and 50m/s. The mass flow rate of steam through the turbine is 12kg/s. (10 pts) Determine change in kinetic energy (10 pts) Determine the rate of work (power) done by the steam in the turbine, in kW (neglect potential energy change). (10 pts) Determine the flow area at the entrance to the turbine, in m2....
A multi-stage gas turbine is to be designed with impulse stages, and is to operate with...
A multi-stage gas turbine is to be designed with impulse stages, and is to operate with an inlet pressure and temperature of 6 bar and 900 K, and an outlet pressure of 1 bar. The isentropic efficiency of the turbine is likely to be 85 per cent. All the stages are to have a nozzle outlet angle of 15 degrees, equal inlet and outlet blade angles, a mean blade speed of 250 m/s and equal 5 kJ/kg K o inlet...
In a single stage impulse turbine, the nozzles discharge the fluid on to the blades at...
In a single stage impulse turbine, the nozzles discharge the fluid on to the blades at an angle of 25 o to the plane of rotation, and the fluid leaves the blades with an absolute velocity of 300 m/s at an angle of 120 o to the direction of motion of the blades. If the blades have equal inlet and outlet angles and there is no axial thrust, estimate the blade angle, power produced per kg/s of fluid, and diagram...
A steam turbine receives superheated steam at 18.0 kg/s, 500.°C, and 3.00 MPa and exhausts it...
A steam turbine receives superheated steam at 18.0 kg/s, 500.°C, and 3.00 MPa and exhausts it to 10 kPa with a quality of 96%. If the turbine is assumed to be internally reversible, determine the rate of heat loss from the turbine surface if the power output is 20.MW The surface temperature of the turbine is uniform at 350.°C, and the local environment (ground state) is taken to be saturated liquid water at T0 = 20.0°C. Neglect all flow stream...
ADVERTISEMENT
ADVERTISEMENT
ADVERTISEMENT