Results 1 to 10 of about 516 (114)
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
doaj +3 more sources
Study on smoke sealing effectiveness of the air curtain in exit bifurcated tunnel fires
The feasibility of using a smoke prevention air curtain in the exit bifurcated tunnel was investigated through 1:10 scale model experiments. The results indicated that the jet velocity and heat release rate (HRR) significantly influenced the smoke ...
Xinling Lu +3 more
doaj +3 more sources
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
Design, construction, and modeling of aircraft door sealing plate based on SMAs
In this work, a novel aircraft door sealing structure driven by shape memory alloys (SMAs) is proposed that offers much improved sealing capability than traditional sealing plates.
Chen Zhang +5 more
doaj +1 more source
This study focuses on the development and evaluation of a self-sealing component for rotary shafts in Magneto-rheological (MR) fluid-based devices, such as MR brakes and MR clutches.
Vo Van Cuong +6 more
doaj +1 more source
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
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 +1 more source
Effect of Ingress on Flow and Heat Transfer Upstream and Downstream of a Rotating Turbine Disc
Ingress is the penetration of a hot mainstream gas in a turbine annulus through the rim seal into the wheel-space between the rotating turbine disc (the rotor) and the adjacent stationary casing (the stator).
Hui Tang +6 more
doaj +1 more source
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
doaj +1 more source
Spotted seals (Phoca largha) and related crossbreeds maintained at Kamogawa Sea World breed seasonally from the end of January to middle of March. For contraception in these animals, the effect of a single administration of a contraceptive synthetic luteal hormone for dogs, proligestone (PRG), was investigated.
KATSUMATA, Etsuko +2 more
openaire +3 more sources

