CENTRIFUGAL TURBINE ROTOR BLADE,
Abstract
The object of the invention is a centrifugal turbine rotor blade which has a thickness that becomes less in the axial direction. For the purpose of increasing the vibration strength of the rotor, the thickness of the blade in any cylindrical section is made to decrease in accordance with a parabolic dependence with the decreasing of the degree of the parabola with a decreasing radius of the cylindrical cross section. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 20, 1965
- Accession Number
- AD0621781
Entities
People
- Yu. B. Kozlov
Organizations
- National Air and Space Intelligence Center