mcatltu
Mechanical
- Oct 10, 2009
- 5
Hello,
I have a question about calculating oil film stiffness and damping coefficients. From literature, it says that
Kxx = dFx/dx
Kxy = dFx/dy
Kyx = dFy/dx
Kyy = dFy/dy
Cxx = dFx/dxdot
Cxy = dFx/dydot
Cyx = dFy/dxdot
Cyy = dFy/dydot
My question is that if you have a limit cycle (journal closed orbit), how can you find bearing coefficients from the orbit?
My external load applied on journal is the unbalance (omega is equal to the rotational speed of journal)
m*xdotdot + Fx = m*a*omega^2*cos(omega*t)
m*ydotdot + Fy = m*a*omega^2*sin(omega*t)+W
Where "Fx,Fy" are nonlinear forces, "W" is the gravity load, "t" is time, "m" is rotor mass, "a" is the distance from centre of rotor gravity to the centre of rotor geometry.
Thank you for your help.
I have a question about calculating oil film stiffness and damping coefficients. From literature, it says that
Kxx = dFx/dx
Kxy = dFx/dy
Kyx = dFy/dx
Kyy = dFy/dy
Cxx = dFx/dxdot
Cxy = dFx/dydot
Cyx = dFy/dxdot
Cyy = dFy/dydot
My question is that if you have a limit cycle (journal closed orbit), how can you find bearing coefficients from the orbit?
My external load applied on journal is the unbalance (omega is equal to the rotational speed of journal)
m*xdotdot + Fx = m*a*omega^2*cos(omega*t)
m*ydotdot + Fy = m*a*omega^2*sin(omega*t)+W
Where "Fx,Fy" are nonlinear forces, "W" is the gravity load, "t" is time, "m" is rotor mass, "a" is the distance from centre of rotor gravity to the centre of rotor geometry.
Thank you for your help.