by Gsearch » Mon 19 Oct 2015, 20:15:28
$this->bbcode_second_pass_quote('', 'S')uperconducting shaftless gyroscope aerospace vehicle
CN 102390532 A
ABSTRACT
The invention discloses a superconducting shaftless gyroscope aerospace vehicle, which comprises a framework (1), a shell (2), a control cabin (3), rotors (4), stators (5), landing leg spray pipes (7) and a parabolic reverse thrust plate (6), wherein the stators (5) and the rotors (4) are divided into two parts, i.e. one part of an upper stator (13), an upper rotor (12), an inner stator (10) and another part of a lower rotor (15) and a lower stator (14); the lower part of the control cabin (3) is provided with a reflector lamp (9), the inner stator (10) and the parabolic reverse thrust plate (6); the inner periphery of the lower rotor is provided with a beam head (11); and the inner end of the lower stator (14) is provided with a spray head (8). The superconducting shaftless gyroscope aerospace vehicle can be used for both civil and military purposes, and is low-carbon and environmentally-friendly; the overall structure and the technical application are suitable for controllable nuclear energy fusion, supercomputing energy accumulators, low-frequency power generation and replacement of coal-fired boilers; and a series of bottleneck problems in economic restriction of development at present are solved.
http://www.google.com/patents/CN102390532A?cl=en$this->bbcode_second_pass_quote('', 'E')mbodiments of the subject invention relate to a Wingless Hovering Micro Air Vehicle (WHOMAV) and its Power Source Unit (PSU). Embodiments can operate at reasonable power levels for hovering and withstanding expected wind gusts. Embodiments of the subject invention can have a diameter less than 15 cm. Embodiments can have one or more smooth (continuous curvature) surface and can be operated using electromagnetic and electrohydrodynamic principles. The wingless design of specific embodiments can allow operation with no rotating or moving components. Additional embodiments can allow active response to the surrounding flow conditions. The issue of low lift to drag ratio and degradation of airfoil efficiency due to the inability of laminar boundary layers attachment can also be significantly reduced, or eliminated. The electromagnetic force can be generated by applying a pulsed (alternating/rf) voltage between a set of grounded and powered electrodes separated by a polymer insulator, dielectric, or other material with insulating properties.