Abstract A gas turbine has a casing forming a fluid passage through which a primaryluid flows, and a rotor blade disposed in the fluid passage with a clearance between distal ends of the rotor blades and the casing. The casing has a plurality of spaced blow holes extending circumferentially thereof for communicating an external secondary fluid chamber with the clearance, the blow holes being formed at an incline with respect to the wall of the casing in such a manner that a secondary fluid discharged from the blow holes is imparted with a flow component that opposes a flow of the primary fluid leaking from the clearance. The amount of the secondary fluid discharged from the blow holes and the discharge pressure are controlled to hydromechanically vary the resistance which the secondary fluid offers to the primary fluid leakage flow, thereby making it possible to mimimize the leakage flow.
A turbomachine comprising: a casing forming a fluid passage through which a primary fluid flows; rotor blades disposed for rotation in the fluid passage with a clearance between distal ends of said rotor blades and said casing; a secondary fluid chamber being provided radially outwardly of said casing; and said casing having a plurality of spaced blow holes extending circumferentially thereof for communicating the secondary fluid chamber with the clearance, said blow holes being formed at an incline with respect to the wall of said casing in such a manner that a secondary fluid discharged from said blow holes is imparted with a flow component that opposes a direction of rotation of the blades and a flow of the primary fluid leaking from the clearance.
Claim 2
Dependent Claim
125 words
A turbomachine comprising: a casing forming a fluid passage through which a primary fluid flows; rotor blades disposed for rotation in the fluid passage with a clearance between distal ends of said rotor blades and said casing; a secondary fluid chamber being provided radially outwardly of said casing; and said casing having a plurality of spaced blow holes extending circumferentially thereof for communicating the secondary fluid chamber with the clearance, said blow holes being formed at an incline with respect to the wall of said casing in such a manner that a secondary fluid discharged from said blow holes is imparted with a flow component that opposes a direction of rotation of the blades and a flow of the primary fluid leaking from the clearance.
Claim 3
Dependent Claim
40 words
The turbomachine according to claim 1, wherein said blow holes are inclined at an angle of 30° with respect to the wall of said casing, said blow holes being arranged in a plurality of rows spaced axially of the machine.
Claim 4
Dependent Claim
28 words
The turbomachine according to claim 2, wherein the blow holes in each of said rows have diameters different from the blow holes in the other of said rows.