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THEORETICAL PRINCIPLES FOR PROVISION OF OPTIMUM ELECTRIC POWER LOSS RATES IN POWER SYSTEM NETWORKS
, 2016 М. И. Фурсанов
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Development of on-board power systems and the concept of a more electric aircraft
Andrzej Szelmanowski +3 more
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Electrically Powered Orthotic Systems
The Journal of Bone & Joint Surgery, 1969Electrically powered orthotic systems have been devised at Rancho Los Amigos to provide quadriplegic and other severely paralyzed patients with mobility and voluntary hand movements. The equipment necessary to fit a totally paralyzed patient for maximum restoration of upper extremity function includes an electric wheelchair, a Rancho electric arm with ...
V L, Nickel, A, Karchak, J R, Allen
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Transactions of the American Institute of Electrical Engineers, 1934
A SYMPOSIUM on switching power at modern large generating plants is included on the program of the Institute's forthcoming winter convention. Five papers, each describing the facilities at one such plant, are to be discussed. Three of these papers are included in this issue, the other 2 having been included in the December 1933 issue.
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A SYMPOSIUM on switching power at modern large generating plants is included on the program of the Institute's forthcoming winter convention. Five papers, each describing the facilities at one such plant, are to be discussed. Three of these papers are included in this issue, the other 2 having been included in the December 1933 issue.
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SYNCOM electrical power system.
Journal of Spacecraft and Rockets, 1964T Syncom satellites were developed for the NASA Goddard Space Flight Center by the Hughes Aircraft Company. Syncom was designed to operate at synchronous altitude as a spin-stabilized satellite with redundant communications, telemetry and command, and attitude control subsystems. The spacecraft nominal launch weight is 147 Ib.
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Transactions of the American Institute of Electrical Engineers, 1940
Electric-power loads are increasing rapidly on airplanes and auxiliary-engine-driven generators offer dependable power sources independent of main engines, Minimum weight for the required capacity is essential in the design of generators, motors, and control.
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Electric-power loads are increasing rapidly on airplanes and auxiliary-engine-driven generators offer dependable power sources independent of main engines, Minimum weight for the required capacity is essential in the design of generators, motors, and control.
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