Assembly fixture for a stator vane assembly
A disclosed fixture for assembling a stator vane assembly for a gas turbine engine includes an outer locating ring including a plurality of outer locating pins defining a position for each of a plurality of vanes relative to an outer fairing and an inner locating ring including a plurality of inner locating rings defining a position of each of the plurality of vanes relative to an inner fairing. A clamp section includes a clamp portion and a clamp pin that define an angular orientation of each of the plurality of vanes relative to each of the inner and outer fairings, and an inner locating section supporting a plurality of radial locating pins defining a radial position of each of the plurality of vanes relative to the inner and outer fairings.
1. A method of assembling a gas turbine engine front architecture comprising the steps of:
securing inner and outer fairings within a fixture relative to one another;
securing multiple vanes between the inner and outer fairing within the fixture, wherein securing the multiple vanes includes positioning each of the multiple vanes within an opening of the inner fairing and an opening of the outer fairings such that no part of the multiple vanes are in direct engagement with the inner fairing and the outer fairing;
applying a curable material at an interface between each of the multiple vanes and the inner and outer fairings;
curing the curable material while maintaining a relative position between the multiple vanes and the inner and outer fairings, wherein the curable material remains flexible once cured;
and releasing the multiple vanes and the inner and outer fairings from the fixture.
2. The method as recited in claim 1 , including positioning each of the multiple vanes by defining a first plane with at least three (3) contact points on the fixture, a second plane with at least two (2) contact points on the fixture and a third plane with at least one (1) contact point defined on the fixture.
3. The method as recited in claim 2 , including defining the first plane with an outer locator pin on an outer locating ring of the fixture, an inner locator pin on an inner locating ring and a clamp disposed between the inner and outer locating rings.
4. The method as recited in claim 3 , including a single clamp for holding each of the vanes in position.
5. The method as recited in claim 4 , wherein the single clamp is disposed between the inner locating pin and the outer locating pin and includes a clamp portion supported on a clamp pin with the vane being clamped between the clamp portion and the clamp pin.
6. The method as recited in claim 3 , including defining the second plane with a surface of the outer locating ring and the inner locating ring.
7. The method as recited in claim 3 , including defining the third plane with a radial locating pin supported radially inward of the inner fairing.
8. The method as recited in claim 1 , wherein the plurality of vanes are held within the fixture during curing of the curable material.