Lecture 9 rpm. (c) To seal the faces of two mating flanges. Wor diameter, rotating shaft for a gas turbine engine to limit the escape of air between the shaft and appropriate seal type for the following applications: (a) A high speed, 100 mm 12.1/ Determine an rationary housing. (b)To completely seal the back face of a rotodynamic pump rotating at 2970 12.2/ Determine suitable groove dimensions for on 011

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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diameter, rotating shaft for a gas turbine engine to limit the escape of air between the shaft and
rpm. (c) To seal the faces of two mating flanges.
Wor
12.1/ Determine an
detionary housing. (b)To completely seal the back face of a rotodynamic pump rotating at 2970
Lecture 9
appropriate seal type for the following applications: (a) A high speed, 100 mm
12 2/ Determine suitable groove dimensions for an 0101-16 O' ring to seal against a solid cylinder.
12.3/ Determine the flow rate of air through a labyrinth seal on a 150 mm diameter shaft. The
labyrinth consists of 8 fins, height 4.5mm, pitch 7mm, radial clearance 0.5 mm and tip width
0.35mm. The absolute pressures upstream and downstream of the seal are 2 and 1.01 bar,
respectively. The temperature of the air upstream of the seal is approximately 323 K. Take the
gas constant R as 287 J/(kg K).
Up
PgDr
um
Lock
7
12.4/ The shaft for a small high speed rotating machine has a diameter of 60mm. The absolute
pressure within the machine is 1.2x10SPa and the operating temperature is approximately 318
K. Design a suitable labyrinth seal to limit the flow of air escaping from the machine to
atmospheric conditions to 0.01 kg/s.
12.5/ The shaft for a high speed rotating machine has a diameter of 150 mm. The absolute pressure
within the machine is 2.5x10$Pa and the operating temperature is approximately 443 K. Design
a suitable labyrinth seal to limit the flow of air escaping from the machine to a chamber at an
absolute pressure of 2.2 bar to 0.03 kg/s.
12.6/ An axial bush seal consists of an annular gap with inner and outer radii of 0.025 and 0.0253mm,
pressures upstream and downstream of the seal are 6 and 5.5 bar, respectively. The viscosity
of the oil can be taken as 0.02 Pa s.
respectively. The length of the seal is 30mm. Determine the flow rate of oil through the seal if
the
12.7/ Determine the flow rate of air through an axial bush seal. The outer diameter of the inner
cylinder is 100 mm and the radial clearance is 0.1mm. The length of the seal is 50mm. The
pressures upstream and downstream of the seal are 1.4 and 1.01 bar, respectively. The viscosity
of air can be taken as 1.85×10-5Pa s.
12.8/ A radial bush seal consists of a cylinder with an inner radius of 20 mm and an outer radius of
40mm. The axial gap is 0.2mm. Determine the flow rate of oil through the clearance if the
pressure inside the cylinder is 6 bar and the pressure outside the cylinder is 5.2 bar. Take the
viscosity of oil as 0.022 Pa s.
Transcribed Image Text:diameter, rotating shaft for a gas turbine engine to limit the escape of air between the shaft and rpm. (c) To seal the faces of two mating flanges. Wor 12.1/ Determine an detionary housing. (b)To completely seal the back face of a rotodynamic pump rotating at 2970 Lecture 9 appropriate seal type for the following applications: (a) A high speed, 100 mm 12 2/ Determine suitable groove dimensions for an 0101-16 O' ring to seal against a solid cylinder. 12.3/ Determine the flow rate of air through a labyrinth seal on a 150 mm diameter shaft. The labyrinth consists of 8 fins, height 4.5mm, pitch 7mm, radial clearance 0.5 mm and tip width 0.35mm. The absolute pressures upstream and downstream of the seal are 2 and 1.01 bar, respectively. The temperature of the air upstream of the seal is approximately 323 K. Take the gas constant R as 287 J/(kg K). Up PgDr um Lock 7 12.4/ The shaft for a small high speed rotating machine has a diameter of 60mm. The absolute pressure within the machine is 1.2x10SPa and the operating temperature is approximately 318 K. Design a suitable labyrinth seal to limit the flow of air escaping from the machine to atmospheric conditions to 0.01 kg/s. 12.5/ The shaft for a high speed rotating machine has a diameter of 150 mm. The absolute pressure within the machine is 2.5x10$Pa and the operating temperature is approximately 443 K. Design a suitable labyrinth seal to limit the flow of air escaping from the machine to a chamber at an absolute pressure of 2.2 bar to 0.03 kg/s. 12.6/ An axial bush seal consists of an annular gap with inner and outer radii of 0.025 and 0.0253mm, pressures upstream and downstream of the seal are 6 and 5.5 bar, respectively. The viscosity of the oil can be taken as 0.02 Pa s. respectively. The length of the seal is 30mm. Determine the flow rate of oil through the seal if the 12.7/ Determine the flow rate of air through an axial bush seal. The outer diameter of the inner cylinder is 100 mm and the radial clearance is 0.1mm. The length of the seal is 50mm. The pressures upstream and downstream of the seal are 1.4 and 1.01 bar, respectively. The viscosity of air can be taken as 1.85×10-5Pa s. 12.8/ A radial bush seal consists of a cylinder with an inner radius of 20 mm and an outer radius of 40mm. The axial gap is 0.2mm. Determine the flow rate of oil through the clearance if the pressure inside the cylinder is 6 bar and the pressure outside the cylinder is 5.2 bar. Take the viscosity of oil as 0.022 Pa s.
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