Zobrazeno 1 - 10
of 32
pro vyhledávání: '"S. Busam"'
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 125:1003-1010
A fundamental study has been performed to examine the disintegration of oil films emerging from axial passages at the face of a rotating cylinder. The investigation has been conducted in parallel to a similar study on atomization processes at rotatin
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 125:1011-1020
A fundamental study has been performed to examine the disintegration of oil films emerging from radial holes in a rotating hollow cylinder. The configuration investigated is an abstraction of one of the droplet generation sources in an aeroengine bea
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 122:314-320
Increasing efficiencies of modern aero-engines are accompanied by rising turbine inlet temperatures, pressure levels and rotational speeds. These operating conditions require a detailed knowledge of two-phase flow phenomena in secondary air and lubri
Publikováno v:
Volume 4: Turbo Expo 2004.
Increasing the efficiency of modern jet engines do not only imply to the mainstream but also to the secondary air and oil system. Within the oil system the bearing chamber is one of the most challenging component. Oil films on the chamber walls are g
Publikováno v:
Volume 5: Turbo Expo 2003, Parts A and B.
For future efficient and light aero-engines it is essential to develop optimized lubrication systems. These systems require increased temperature and pressure levels in combination with high rotational speeds without compromising the high level of sa
Publikováno v:
Volume 3: Turbo Expo 2002, Parts A and B.
The continuous increase of the temperature and pressure levels in modern aeroengines has significantly increased the demands on the design of the lubrication system. Among other things the oil/air system of a gas turbine engine has to ensure that eng
Publikováno v:
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration.
The development of modern aero-engines is leading to increased pressure and temperature levels which makes increasing demands on the engines’ safety and reliability. In particular the vent-system of the bearing chambers located in the hot section o
Publikováno v:
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration.
A fundamental study has been performed to examine oil film disintegration mechanisms at the rim of a rotating disk. The configuration investigated is an abstraction of one of the droplet generation sources in an aero-engine bearing compartment. The p
Publikováno v:
Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration.
A proper matching of the heat transfer to the lubrication oil in bearing chambers and subsequent vent and scavenge pipes is one of the major tasks in the design process of secondary air/lubrication oil systems of modern jet engines. For a calculation
Autor:
S. Busam
Publikováno v:
Journal of Engineering for Gas Turbines and Power. 122:364-364
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