Results 131 to 140 of about 14,178 (228)

Load Sharing Design of 8 MW Wind Power Gearbox based on ADAMS Simulation Driving

open access: yesJixie chuandong, 2015
Improving the load sharing property of multiple planets is not only one of the effective methods to improve the large megawatt wind turbine gearbox power density,but also is the key to the design of wind turbine gearbox.
Dong Huimin   +5 more
doaj  

Reliability analysis and prediction of wind turbine gearboxes

open access: yes, 2010
This paper presents a reliability analysis model of wind turbine gearboxes by developing a generic gearbox configuration and modular structure. It encapsulates all the reliability critical components within the gearbox subsystem in a wind turbine.
Smolders, K.   +3 more
openaire   +1 more source

Study of Enhancement Test on Bearings of High Power Wind Turbine Gearboxes

open access: yesJixie chuandong
Bearings are critical components of the gearbox in wind turbine units, and their fatigue life and reliability directly influence the service life of wind turbines.
Dai Haonan   +4 more
doaj  

Development tests for the 2.5 megawatt Mod-2 wind turbine generator [PDF]

open access: yes
The 2.5 megawatt MOD-2 wind turbine generator test program is discussed. The development of the 2.5 megawatt MOD-2 wind turbine generator included an extensive program of testing which encompassed verification of analytical procedures, component ...
Andrews, J. S., Baskin, J. M.
core   +1 more source

Drive train dynamic analysis [PDF]

open access: yes
A method for parametric variations in drive train dynamic analysis is described. The method models the individual components of a drive system, forms the appropriate system interface coordinates and, calculates the system dynamic response at particular ...
Giansante, N.
core   +1 more source

The NASA high-speed turboprop program [PDF]

open access: yes
Technology readiness for Mach 0.7 to 0.8 turboprop powered aircraft with the potential for fuel savings and DOC reductions of up to 30 and 15 percent respectively relative to current in-service aircraft is addressed. The areas of propeller aeroacoustics,
Dugan, J. F.   +3 more
core   +1 more source

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