Open AccessCALCULATION BY PROBABILISTIC METHODS OF LOCATING PIN ASSEMBLY OF ROTOR BLADES IN THE CONSTRUCTION OF AIRCRAFT COMPRESSORS AND TURBINES
Author(s) -
Doru Luculescu,
Ştefan MUSTAŢĂ
Publication year - 2022
Publication title -
scientific research and education in the air force
Language(s) - English
Resource type - Conference proceedings
ISSN - 2247-3173
DOI - 10.19062/2247-3173.2021.22.15
Subject(s) - turboprop , gas compressor , rotor (electric) , reciprocating compressor , probabilistic logic , engineering , turbine , mechanical engineering , gas turbines , automotive engineering , constructive , turbine blade , propeller , turbojet , computer science , aerospace engineering , marine engineering , artificial intelligence , operating system , process (computing)
Compressor and turbine blades, used in the construction of aircraft turboprop engines, are very important constructive elements, by their functional role, and complex by geometric parameters, mechanical and gas-dynamic factors. This paper aims to present a method of probabilistic design of the assembly between the rotor disk and the compressor and turbine blades.
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