Results 91 to 100 of about 10,932 (224)

A study of low-cost reliable actuators for light aircraft. Part B: Appendices [PDF]

open access: yes
Computer programs written in FORTRAN are given for time response calculations on pneumatic and linear hydraulic actuators. The programs are self-explanatory with comment statements.
Eijsink, H., Rice, M.
core   +1 more source

Viscous rotary vane actuator/damper [PDF]

open access: yes, 1976
A compact viscous rotary actuator/damper for use on the Mariner '71 and Viking Programs was developed. Several functions were combined into this single mechanism to control the deployment, latching, and damping of the solar panel arrays used on these ...
Harper, J. D.
core   +1 more source

Energy transfer process and evolution characteristics in impeller of contra-rotating axial fan

open access: yesMeitan kexue jishu
Energy is transferred to the airflow during the rotation of impeller. In engineering, the efficient energy conversion is a key issue. Mastering the energy transfer process in impeller is the premise and basis for realizing efficient energy conversion. In
Yongping CHEN   +5 more
doaj   +1 more source

Long-term CF6 engine performance deterioration: Evaluation of engine S/N 451-479 [PDF]

open access: yes
The performance testing and analytical teardown of CF6-6D engine is summarized. This engine had completed its initial installation on DC-10 aircraft. The investigative test program was conducted inbound prior to normal overhaul/refurbishment.
Kramer, W. H., Smith, J. J.
core   +1 more source

Influence of impeller and diffuser geometries on the lateral fluid forces of whirling centrifugal impeller [PDF]

open access: yes
Lateral fluid forces on two-dimensional centrifugal impellers, which whirl on a circular orbit in a vaneless diffuser, were reported. Experiments were further conducted for the cases in which a three-dimensional centrifugal impeller, a model of the ...
Nishihama, Jiro   +2 more
core   +1 more source

Investigation on predicting the stall limit of compressor at low rotating speed

open access: yesAdvances in Mechanical Engineering
In order to realize fast and accurate prediction of the stall limit of compressor, a study on predicting the stall limit of compressor at low rotating speed is conducted with throughflow calculation and maximum static pressure rise coefficient.
Hong Wu   +4 more
doaj   +1 more source

Erosion in radial inflow turbines. Volume 3: Trajectories of erosive particles in radial inflow turbines [PDF]

open access: yes
The theoretical trajectories that erosive particles follow in the gas flow fields of a typical radial inflow turbine were investigated. A discussion of the theoretical trajectories that the particles follow in the scroll, in the nozzles, in the vortex ...
Clevenger, W. B., Jr., Tabakoff, W.
core   +1 more source

Dynamic characteristics of rotating shrouded-bladed-disc.

open access: yes, 1986
This investigation deals with the vibration problem of a rotating shrouded bladed disc and with the dynamic stresses of blades and packets of turbine blades. The wave propagation technique in periodic structures is introduced into the finite element method to reduce the overall number of degrees of freedom. The application of wave propagation technique
openaire   +1 more source

Influence of delayed excitation on vibrations of turbine blades couple

open access: yesApplied and Computational Mechanics, 2013
In the presented paper, the computational model of the turbine blade couple is investigated with the main attention to the influence two harmonic excitation forces, having the same frequency and amplitude but with moderate delay in time.
Půst L., Pešek L.
doaj  

A high pressure, high temperature combustor and turbine-cooling test facility [PDF]

open access: yes
A new test facility is being constructed for developing turbine-cooling and combustor technology for future generation aircraft gas turbine engines. Prototype engine hardware will be investigated in this new facility at gas stream conditions up to 2480 K
Cochran, R. P., Norris, J. W.
core   +1 more source

Home - About - Disclaimer - Privacy