Results 91 to 100 of about 86,321 (307)
Investigation of Combustion of the Gas Turbine Engine from Kerosene and Biokerosene and Their Soot Characteristics in Diffusion Flames. [PDF]
ACS Omega, 2022 Hong TD +3 more
europepmc +1 more source
Thermal barrier coating evaluation needs [PDF]
A 0.025 cm (0.010 in) thick thermal barrier coating (TBC) applied to turbine airfoils in a research gas turbine engine provided component temperature reductions of up to 190 C.
Brindley, William J., Miller, Robert A.
core +1 more source
Evaluation of shear mounted elastomeric damper [PDF]
, 1982 Viton-70 elastomeric shear mounted damper was built and tested on a T-55 power turbine spool in the rotor's high speed balancing rig. This application of a shear mounted elastomeric damper demonstrated for the first time, the feasibility of using ...
Walton, J., Zorzi, E.
core +1 more source
Asia-Pacific Journal of Chemical Engineering, EarlyView.ABSTRACT This study proposes a novel integrated system (SDKC‐DORC) that combines a split‐flow dual‐pressure Kalina cycle with a secondary organic Rankine cycle for the synergistic utilization of solar energy and liquefied natural gas (LNG) cold energy.
Ke Xiao +6 more
wiley +1 more source
Известия высших учебных заведений и энергетических объединенний СНГ: Энергетика, 2004 The paper proposes utilization of discharged heat of gas-piston engine (GPE) or contact steam-gas plants (SGP) with the purpose to heat up gas at gas-distribution stations (GDS) of combined power plants with turbine and gas-expansion units.
A. D. Kachan +4 more
doaj +1 more source
The CW251B12 Gas Turbine Engine [PDF]
Volume 4: Heat Transfer; Electric Power; Industrial and Cogeneration, 1989 The latest variant of the W251 family of engines, the CW251B12, rated at 48 MW, is described in this paper. The improved performance, compared to the CW251B10 model, is achieved by the redesign of the compressor for increased mass flow and efficiency and by hot end modifications, which allow a modest increase in firing temperature.
openaire +1 more source
Progress in aircraft gas turbine engine development [PDF]
Aircraft gas turbine engine ...
Silverstein, A.
core +1 more source
From Bench to Bulk: Investigating Kinetics, Recyclability, and Scale‐Up of ZIF‐67
Asia-Pacific Journal of Chemical Engineering, EarlyView.ABSTRACT Zeolitic imidazolate framework‐67 (ZIF‐67), a subclass of metal–organic frameworks (MOFs), has garnered considerable attention due to its high surface area, open crystal structure, tunable porosity, and potential applications in gas separation, catalysis, and carbon capture.
Aaush Bhardwaj Singh +1 more
wiley +1 more source
Effect of Wave Process of Plastic Deformation at Forging on the Fatigue Fracture Mechanism of Titanium Compressor Disks of Gas Turbine Engine. [PDF]
Materials (Basel), 2021 Shanyavskiy AA +2 more
europepmc +1 more source
Evaluation of advanced regenerator systems [PDF]
The major considerations are discussed which will affect the selection of a ceramic regenerative heat exchanger for an improved 100 HP automotive gas turbine engine. The regenerator considered for this application is about 36cm in diameter.
Cook, J. A. +3 more
core +1 more source