AXIAL COMPRESSOR BLADE MAKING METHOD

aircraft industry; turbofan engines. SUBSTANCE: according to proposed method, two flat blanks of variable-thickness aerofoil portions are connected by diffusion soldering over links and soldered pair is twisted to form required profile after which it is subjected to finishing machining. Two longitud...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: KLIMNJUK JU.I, FEDORCHENKO D.G, LAZORENKO T.M, GRITSENKO E.A, IGNACHKOV S.M
Format: Patent
Sprache:eng
Schlagworte:
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