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US 5,343,619 AGranted
Hollow blade for a turbomachine and method of manufacturing said blade
AssigneeSociete Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
InventorAlain M. J. Lardellier
Life of this patent
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Abstract
A hollow blade for a turbomachine comprises a unitary body having a multiplicity of transverse cavities in at least the airfoil shaped portion of the blade, and plugs disposed within the cavities and restoring the surface continuity of the intrados and extrados faces of the aerofoil shaped portion, the plugs being rigidly secured to the unitary body, such as by welding.
Claims2
A method of manufacturing a hollow blade for a turbomachine comprising the following steps:
- a) producing a unitary blade blank by forging, said blade blank including an airfoil shaped portion;
- b) machining a multiplicity of holes in said airfoil shaped portion such that a zone of specific width is left clear at the edge of said airfoil shaped portion and said holes are substantially evenly distributed over the remaining area of said airfoil portion and provide a cavity ratio of about 90% in said remaining area;
- c) producing plugs with a shape adapted to the holes formed during step (b) and to the profile of the respective surface of said airfoil shaped portion, be it the intrados face or the extrados face;
- d) placing said plugs in position in said holes formed during step (b);
- e) fixing said plugs to said blade blank by high energy beam welding while said plugs are in position in said holes;
- and
- f) finishing said blank to obtain the required aerodynamic profile.
4 more elements
Dependencies are inferred from the claim text.