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The present invention includes a pivotable vane having an airfoil with a vane spindle or stem extending toward a distal end thereof. The vane stem has a head with a pair of tapered flats having an outwardly extending angle as defined from the distal end of the head towards the airfoil. A vane arm ha

The present invention includes a pivotable vane having an airfoil with a vane spindle or stem extending toward a distal end thereof. The vane stem has a head with a pair of tapered flats having an outwardly extending angle as defined from the distal end of the head towards the airfoil. A vane arm having a substantially C-shaped connector with a pair of contact ends is constructed to maintain a gap with the tapered flats at an initial assembly step and positively engage the tapered flats at a final assembly step.

대표청구항 ▼

1. An apparatus comprising: a pivotable gas turbine engine vane having an airfoil with a vane stem extending toward a distal end;a head having a tapered surface formed adjacent the distal end of the vane stem, the tapered surface having an outwardly protruding angle extending from the distal end tow

1. An apparatus comprising: a pivotable gas turbine engine vane having an airfoil with a vane stem extending toward a distal end;a head having a tapered surface formed adjacent the distal end of the vane stem, the tapered surface having an outwardly protruding angle extending from the distal end towards the airfoil; anda vane arm including a substantially C-shaped connector having lateral sides that define the C-shaped connector and a contact end disposed at the end of the lateral sides of the C-shaped connector, wherein the vane arm is constructed to maintain a gap with the tapered surface at an initial assembly step and positively engage the tapered surface at a final assembly step while maintaining a gap between the lateral sides of the C-shaped connector and the tapered surface. 2. The apparatus of claim 1, which further includes a pair of contact ends. 3. The apparatus of claim 2, wherein the pair of contact ends are an identical mirror image pair. 4. The apparatus of claim 1, which further includes pair of tapered surfaces disposed on separate sides of the head. 5. The apparatus of claim 4, wherein the separate sides are opposing sides of the head. 6. The apparatus of claim 1, wherein the tapered surface is a substantially planar surface. 7. The apparatus of claim 1, which further includes a threaded connector operable to engage a threaded aperture in the vane arm, the threaded connector operable to urge the contact end to positively engage the tapered surface when the threaded connector is tightened. 8. The apparatus of claim 7, which further includes a load bearing surface disposed between an end of the connector and the head, the load bearing surface having an outside portion larger than an outside portion of the head. 9. An apparatus comprising: a rotatable gas turbine engine vane;a unison ring operable to impart a rotation to the rotatable gas turbine engine device; andwherein the rotatable gas turbine engine vane is coupled to the unison ring when a contact portion of an extended arm is engaged with a contact surface of a coupling structure, the contact surface oriented at an angle relative to an axis along which the extended arm is urged toward the coupling structure when coupling the extended arm to the coupling structure, the extended arm projecting toward the coupling structure having an angle different than the angle of the contact surface such that a non-contact area is created between the extended arm and the coupling structure when coupled. 10. The apparatus of claim 9, wherein the contact surface is planar and the contact portion includes a face that substantially engages the contact surface. 11. The apparatus of claim 10, wherein the contact portion is an end portion of the extended arm and includes a flat surface. 12. The apparatus of claim 10, wherein the coupling structure is a spindle of the rotatable gas turbine engine vane. 13. The apparatus of claim 9, wherein the extended arm is part of a structure having a C-shape that includes a second contact portion of a second extended arm. 14. The apparatus of claim 9, which further includes a washer and a fastener, the washer disposed between the fastener and the extended arm. 15. The apparatus of claim 14, wherein the fastener includes a threaded surface that engages a complementary threaded surface, wherein the washer urges the extended arm along the axis as the fastener is turned and the threaded surface engages the complementary threaded surface. 16. An apparatus comprising: a gas turbine engine having a row of movable vanes;a unison ring operable to change an orientation of the movable vanes; andmeans for coupling the unison ring to at least one of the movable vanes. 17. A method comprising: positioning a variable vane of a gas turbine engine in preparation for attachment to a unison ring;coupling the variable vane to the unison ring by:urging a contact end of a coupling arm into contact with a tapered surface of a coupling structure; andwherein the urging includes flexing the coupling arm, creating a gripping force between the contact end and the tapered surface, and maintaining a gap between the coupling arm and the tapered surface. 18. The method of claim 17, wherein the urging further includes engaging a portion of a flat surface of the contact end with the tapered surface of the variable vane. 19. The method of claim 18, which further includes pressing an intermediate connection member against the arm with the fastener. 20. The method of claim 17, which further includes engaging a fastener to secure the variable vane to the arm. 21. The method of claim 20, wherein the engaging includes turning the fastener, the fastener having threads.