Results 31 to 40 of about 4,314 (241)
Fluid-dynamics of Turbine Rim Seal Structures:A physical Interpretation Using URANS [PDF]
Unsteady Reynolds-averaged Navier-Stokes modeling (URANS) is a valuable and costeffective tool for computational fluid dynamics (CFD), including the investigation of mainstream-cavity interaction in turbines. Despite the gap in accuracy with higher order
De Cosmo, Giove +4 more
core +3 more sources
Flow characteristics in turbine wheel space cavity
Unsteady flow structures unrelated to rotating frequency in the turbine wheel space cavity has been observed and reported in a number of recent rim sealing investigations.
Lei Xie +4 more
doaj +1 more source
Aerodynamic performance of turbine rim sealing flows [PDF]
An investigation of the hot gas ingestion phenomenon in the Oxford Rotor Facility ex- amined rotor disc rotation, mainstream pressure asymmetries and unsteady structures in the cavity as main drivers.
Bru Revert, Anna
core +2 more sources
Computational Studies on High Pressure Turbine Rim Seal Cavities [PDF]
The efficiency of a turbine stage is impacted by a number of factors such as the component design philosophy, operating environment, leakage flow and its interaction with the main gas flow path.
Simon Bather +4 more
core +1 more source
Large Eddy Simulation of Externally Induced Ingress about an Axial Seal by Stator Vanes
Turbine inlet temperatures in advanced gas turbines could be as high as 2000 °C. To prevent ingress of this hot gas into the wheelspace between the stator and rotor disks, whose metals can only handle temperatures up to 850 °C, rim seals and sealing ...
Sabina Nketia +3 more
doaj +1 more source
The Aero-Thermal Impact of Rim Seal Purge Flow in Axial Turbines [PDF]
The area between the stationary and rotating hub side endwall segments in axial turbines is featured with a specifically shaped annular clearance, termed as the rim seal.
Ostrowski, Tom
core +1 more source
In turbine disk cavity, rim seals are fitted between the stator and its adjacent rotor disk. A coolant air injected through the turbine disk cavity to prevent the ingress of mainstream hot gases.
Zakaria Mansouri
doaj +1 more source
Effect of Outer Fin Axial Gap on the Sealing Effectiveness and Fluid Dynamics of Radial Rim Seal [PDF]
The modern gas turbine is widely applied in the aviation propulsion and power generation. The rim seal is usually designed at the periphery of the wheel-space and prevented the hot gas ingestion in modern gas turbines.
Zhigang Li +5 more
core +1 more source
Arthroscopic Labralization of the Hip: An Alternative to Labral Reconstruction
Labralization, which may be performed by open or arthroscopic means, may be an attractive alternative to hip labral reconstruction. By preserving the articular cartilage in the region of labral deficit with meticulous rim trimming, the resultant ...
Dean K. Matsuda, M.D.
doaj +1 more source
Measurement of inertial and acoustic waves in a turbine chute rim seal cavity [PDF]
A chute rim seal cavity has been instrumented with time-resolved and time-averaged pressure transducers as well as a gas concentration measurement system at the Oxford Rotor Facility.
Beard, Paul F +2 more
core +2 more sources

