Results 1 to 10 of about 4,317 (244)

Experimental and Numerical Investigations into the Effects of Rim Seal Structure on Endwall Film Cooling and Flow Field Characteristics

open access: yesEnergies, 2023
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, Feng Zhenping
exaly   +4 more sources

Harmonisation of Coolant Flow Pattern with Wake of Stator Vane to Improve Sealing Effectiveness Using a Wave-Shaped Rim Seal

open access: yesEnergies, 2019
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

Effect of Various Coolant Mass Flow Rates on Sealing Effectiveness of Turbine Blade Rim Seal at First Stage Gas Turbine Experimental Facility

open access: yesEnergies, 2020
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.
Seok Min Choi   +2 more
exaly   +4 more sources

Unsteady Numerical Investigation on the Sealing Effectiveness and Flow Field in Different Rim Seal Geometries

open access: yesAerospace, 2022
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 ...
Zhiguo Zhang   +2 more
exaly   +4 more sources

Design of an Improved Turbine Rim-Seal [PDF]

open access: yesVolume 5C: Heat Transfer, 2015
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.   +5 more
core   +8 more sources

Unsteady Flow Structures within a Turbine Rim Seal Cavity in the Presence of Purge Flow—An Experimental and Computational Unsteady Aerodynamics Investigation

open access: yesAerospace, 2019
Flow within the space between the rotor and stator of a turbine disk, and an area referred to as the rim seal cavity, develops azimuthal velocity component from the rotor disk.
Cengiz Camci   +2 more
exaly   +4 more sources

Investigations of the leakage characteristic and the sealing effectiveness on turbine bite rim seals

open access: yesJournal of Thermal Science and Technology, 2018
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

Enhancing Labral Healing in Arthroscopic Hip Surgery: The Marrow Venting Technique [PDF]

open access: yesArthroscopy Techniques
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

Three dimensional analysis on the deformation of the master cast during maxillary complete denture fabrication [PDF]

open access: yesScientific Reports
This study aimed to assess the changes in maxillary master casts that occur during complete denture fabrication, focusing on a compression molded denture. Digital merging techniques were used to measure the changes in 12 maxillary master casts at various
Junghyun Nam   +4 more
doaj   +2 more sources

Impact of Purge Injection on Rim Seal Performance

open access: yesApplied Sciences
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   +2 more sources

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