Guide vane stage of a compressor
AssigneeTechspace Aero S.A.
InventorMathieu Bos
Life of this patent
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Abstract
The present invention relates to a guide vane stage of a compressor comprising an outer ring and an inner ring, which are both concentric and preferably circular. The rings are connected to each other via a series of fixed vanes, and are characterized in that at least the inner ring is provided with holes or apertures which allows one of the ends of the vanes to pass through these holes or apertures. The vanes also have at their end a second aperture intended to allow the passage of a retaining and rigidifying component having an elastic function, in order to hold them in pairs.
Claims8
A guide vane stage of a compressor comprising:
- an outer ring;
- an inner ring concentric with said outer ring;
- a plurality of fixed vanes connecting said outer ring and said inner ring;
- and
- a retaining and rigidifying component for holding said vanes in pairs;
- wherein said inner ring comprises apertures through which one end of said vanes passes, and
- wherein said vanes comprise an aperture through which said retaining and rigidifying component passes.
A process for mounting a retaining and rigidifying component having an elastic function on a guide vane stage comprising providing a guide vane stage comprising an outer ring and an inner ring, wherein said inner and outer rings are concentric and connected together by a series of fixed vanes and positioning said retaining and rigidifying component having an elastic function between successive vanes,
- wherein said vanes comprise an aperture, said retaining and rigidifying component comprises a cut, shaped and folded metal sheet comprising two flat stubs which are sized so as to allow them to be housed in the apertures of two successive vanes and wherein said positioning step comprises precompressing said retaining and rigidifying component, placing said retaining and rigidifying component such that said stubs of said retaining and rigidifying component are housed in said apertures of said vanes and releasing the pressure exerted on said retaining and rigidifying component.
Dependencies are inferred from the claim text.