Explore: Circulation Control Rotors

end, this program did not proceed.[citation needed] The X-Wing Circulation Control Rotor Concept was developed in the mid-1970s by the David W. Taylor

rotorcraft: Tandem rotors are two counter-rotating rotors with one mounted behind the other. Transverse rotors are pair of counter-rotating rotors transversely

helicopter Coaxial rotors Fenestron Intermeshing rotors (synchropter) Tandem rotors Transverse rotors Multirotors Quadrotors Tiltrotors Tip jet rotor Youngcopter

concept in the 1970s and took out a number of patents. The X-Wing circulation control rotor was developed in the mid-1970s under DARPA funding. The concept

adjustable thermostatically controlled circulation pump mounted at the last fixture on the loop. Thermostatically controlled circulation pumps allow owners to

valves use spherical rotors with a cylindrical hole drilled as a fluid passage. Plug valves use cylindrical or conically tapered rotors called plugs.[ambiguous]

form of either a re-entrant leading circle or electrical spiral waves (rotors); these localized sources may be in the left atrium near the pulmonary veins

incorporate three-lobe or four-lobe rotors; this allows the lobes to have a slight twist[clarification needed] along the rotor axes, which reduces pulsing in

Westinghouse motors were two-phase motors with wound rotors until B. G. Lamme developed a rotating bar winding rotor. The General Electric Company (GE) began developing

TVV-500. The turbine and the generator rotors are mounted on the same shaft. The combined weight of the rotors is almost 200 t (220 short tons) and their