Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Jsc 'UEC-Aviadvigatel'"'
Autor:
Marat Gallyamov, Igor Gribkov, Aleksandr Inozemtsev, Sergey Toropchin, Jsc 'UEC-Aviadvigatel'
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :28-37
The method of advanced bypass turbojet engine core research tests with simulation of target inlet thermogasdynamic parameters at the engine OEM site is considered. It is stated that research testing is traditionally associated with the use of multifu
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :45-56
World manufactures are focused on consumer features of products in the design of TPD.Special attention is paid to im-proving the efficiency of engines. Tip clearance significantly influences on the efficiency of turbine and the specific fuel con-sump
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :69-79
A large number of leading aircraft and engine companies are showing increasing interest in developing projects that re-duce the negative impact of aviation on the environment. One of the promising areas is the electrification of aircraft at different
Autor:
Vakhtang Tsatiashvili, Mikhail V. Panchenko, Aleksey Sazhenkov, Aleksandr Kozlov, Taras Abramchuk, Aleksey Sipatov, Aleksandr Petrov, Jsc 'UEC-Aviadvigatel'
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :20-30
Intensive growth of air transport provides increasing in hazardous substances emission in the atmosphere. Among such emissions also are nano-particulates specific with high- surface area and sometimes high non-uniformity resulting in high concentrati
Autor:
Alexey Sazhenkov, Jsc 'UEC-Aviadvigatel', Aleksandr Inozemtsev, Nadezhda Lamanova, Igor Gribkov, Artur Pleshivykh
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :71-80
The possibility of obtaining measuring in-formation about the parameters of the automatic control and monitoring system of a turbofan engine during its operation in flight conditions and almost no restrictions on computational costs enable using algo
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :30-39
Much attention is paid to increasing the efficiency of turbofan engines by increasing the efficiency of the main modules. The aerodynamic efficiency of a turbine depends on the level of total pressure and kinetic energy losses, which are determined b
Autor:
Igor Gribkov, Igor Lisovin, Artur Pleshivykh, Nadezhda Lamanova, Aleksandr Inozemtsev, Alexey Sazhenkov, Jsc 'UEC-Aviadvigatel'
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :162-171
Autor:
Jsc «UEC-Aviadvigatel», Perm, Russian Federation, Ruslan Kolegov, Nikolay Shuvaev, Aleksandr Siner, Nikita Bolshagin, Jsc «UEC-Saturn», Perm, Russian Federation
Publikováno v:
Perm National Research Polytechnic University Aerospace Engineering Bulletin. :5-15