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Effects of a Circumferential Bowing of the Outlet Stator Vanes in a Stage of the Axial Compressor

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Języki publikacji
EN
Abstrakty
EN
Results of measurement of flow parameters in a stage of the axial compressor at radial, crescent and sabre vanes of the outlet stator are presented. Essential influence of a circumferential bowing of the stator vanes on time-averaged rotor flow parameters is established at preservation of the effects connected to influence of a mutual tangential position of stators on the rotor blade pressure pulsations and generated noise.
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autor
  • Central Institute of Aviation Motors, Moscow, Russia
autor
  • Central Institute of Aviation Motors, Moscow, Russia
Bibliografia
  • 1. Saren V.E., Savin N.М., Petrovitchev А.М., “ Research of stator clocking effects in a stage of the axial compressor at radial and bowed stator vanes ”, Compressor engineering and pneumatic, No.5, 2002, pp. 24-32. (Rus.).
  • 2. Petrovitchev А.М., Savin N.М., Smirnov S.A., “ Influence of an tangential bowing of stator blades to the characteristics of a stage of the axial compressor ”, Coll. of papers “Blade machines and stream apparatus ”, Vol. 12, 1990, pp. 29-42.. Trans. of CIAM No.1280. (Rus.).
  • 3. Saren V.E., Savin N.М., Petrovitchev А.М., Smirnov S.A., “Research of stator clocking effects in a stage of the axial compressor at radial and bowed stator vanes”, Int. Conf. SYMKOM’02, CMP Turbomachinery 122, 2002, pp. 261-268.
  • 4. “Bowed airfoil”, European Patent No.0829619 B1, F01D5/14, 2003. United Technologies Corp., USA.
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-LOD5-0007-0019
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