Results 11 to 20 of about 215,871 (234)
During the practical operation of gas turbines, relatively cooled air from the compressor and the rim seal is applied in order to prevent mainstream ingestion into the space between the rotor and stator disc cavities, which can prolong the service life ...
Zhenping Feng
exaly +4 more sources
The rim seal of the gas turbine is intended to protect the material of the turbine disk from hot combustion gases. The study of the rim seal structure is important to minimise the coolant flow and maximise the sealing effect. In this paper, a wave-shaped
Seungjin Lee +2 more
exaly +4 more sources
Design of an Improved Turbine Rim-Seal [PDF]
Rim seals are fitted in gas turbines at the periphery of the wheel-space formed between rotor discs and their adjacent casings. These seals, also called platform overlap seals, reduce the ingress of hot gases which can limit the life of highly-stressed components in the engine.
Scobie, James A.; id_orcid 0000-0002-1827-3635 +5 more
core +8 more sources
A rim seal is often used to prevent the ingress of high-temperature gas into the turbine disk cavity and protect the turbine disk from damage. Based on the overlapping rim seal (Seal-A), this paper proposes two more composite sealing structures (Seal-B ...
Qingcai Zhang, Qinqin Wang
exaly +3 more sources
The appropriate coolant mass flow of turbine blade rim seal has become an important issue as turbine blades are exposed to increasingly higher thermal load owing to increased turbine inlet temperature.
Hyung Hee Cho +2 more
exaly +3 more sources
Investigations of the leakage characteristic and the sealing effectiveness on turbine bite rim seals
In order to meet the needs of designing for high performance secondary air system in the turbine, a new turbine bite engineering rim seal of type-A and the related test rig were designed and set up.
Weilin DONG, Suofang WANG, Pengfei LI
doaj +3 more sources
Numerical Investigation of Unsteady Interaction between Rim Seal Flow and Upstream Vane
To investigate unsteady interaction mechanism between the rim seal flow in turbine stator-rotor cavity and main flow, detailed unsteady numerical simulations of the flow field and unsteady characteristic of the vane were conducted under different rim ...
doaj +2 more sources
Aerodynamics and Sealing Performance of the Downstream Hub Rim Seal in a High-Pressure Turbine Stage
The purpose of the paper is to characterize the aerodynamic behavior of a rotor-downstream hub cavity rim seal in a high-pressure turbine (HPT) stage.
Emil Göttlich
exaly +3 more sources
Enhancing Labral Healing in Arthroscopic Hip Surgery: The Marrow Venting Technique [PDF]
The significance of addressing labral tears cannot be overstated given that the labrum plays a crucial role in preventing or mitigating the onset of osteoarthritis.
Ady H. Kahana-Rojkind, M.D. +5 more
doaj +2 more sources
Impact of Purge Injection on Rim Seal Performance
One of the most critical challenges in gas turbine design is preventing the ingestion of hot mainstream gases into the disk space between the stator and rotor disks.
Matteo Caciolli +4 more
doaj +3 more sources

