FIELD: aviation industry; other industries; production of the aircraft engine compressor straightening blade device with the glued blades.
SUBSTANCE: the invention is pertaining to the aircraft engine compressor straightening blade device with the glued blades and ensures the reliable binding of the blades in the body of the internal shell by means of the adhesive material manufactured on the basis of polyimide. The blades (3) of the presented straightening blade device transiting in the radial direction from the internal shell (1) up to the external shell (2) are tightened on the indicated internal shell by means of the hermetic cement containing the polymeric organic adhesive material manufactured on the basis of polyimide.
EFFECT: the invention ensures the reliable binding of the blades in the body of the internal shell by means of the adhesive material manufactured on the basis of polyimide.
19 cl, 7 dwg
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Authors
Dates
2008-02-20—Published
2004-06-29—Filed