초록 ▼

Apparatus is provided for maintaining minimum clearance between variable position airfoils and the wall forming the gas flow path in a gas turbine engine. A constant clearance is maintained between a radially facing contoured wall surface and a radially facing contoured end face on the airfoil. The

Apparatus is provided for maintaining minimum clearance between variable position airfoils and the wall forming the gas flow path in a gas turbine engine. A constant clearance is maintained between a radially facing contoured wall surface and a radially facing contoured end face on the airfoil. The contour of the wall surface and the end face may each be spherical.

대표청구항 ▼

For use in a gas turbine engine having an axially extending flow path disposed circumferentially about the axial centerline of said engine, the invention comprising: a first axially extending wall disposed circumferentially about said center line, said wall comprising a surface of revolution about s

For use in a gas turbine engine having an axially extending flow path disposed circumferentially about the axial centerline of said engine, the invention comprising: a first axially extending wall disposed circumferentially about said center line, said wall comprising a surface of revolution about said axial center line, said wall disposed with respect to said center line such that the distance between said wall and said center line is non-constant, said wall having a circumferentially and axially extending radially facing spherically contoured face having a first center of curvature disposed at a first location on said centerline; a second axially extending wall disposed circumferentially about said center line, said second wall comprising an entirely non-spherical second surface of revolution about said axial center line, said second wall disposed with respect to said center line such that the distance between said second wall and said center line is substantially constant; a variable position airfoil residing in and extending across said flow path between said first and second wall and having a radially contoured end face having a second center of curvature disposed at a second location, said end face disposed in spaced apart confronting facing relationship with said spherically contoured face of said first wall, said airfoil adapted to rotate about an axis of rotation intersecting said center line at an angle less than 90°at said first location.