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VALS de la CONCHA RAMON
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VALS de la CONCHA RAMON
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Application filed by VALS de la CONCHA RAMONfiledCriticalVALS de la CONCHA RAMON
Priority to ES1974199790UpriorityCriticalpatent/ES199790Y/es
Publication of ES199790UpublicationCriticalpatent/ES199790U/es
Application grantedgrantedCritical
Publication of ES199790YpublicationCriticalpatent/ES199790Y/es
Juego aéreo, de pericia perfeccionado, caracterizado porque consta de una plataforma portadora de un cordel fijado, a su superficie, ubicada en la posible trayectoria do un avión de motor eléctrico, en cuya base de fuselaje, pende preferentemente.cerca.de la zona de la, cola, un gancho en. sentido de. vuelo del avión el cual va vinculado a un medio de amarre, a través de un cable conductor, portador de la fuente de energía que será regulada, por medio de un reostato para que, dicho avión en su posición de vuelo describa órbitas, alrededor. del medio de. amarre, a más o menos altura del suelo según convenga; todo ello de modo que al iniciar el avión:un vuelo rasante sobre la mesa y pasar así por encima del cordel, el gancho atrape a este en orden a retener el vuelo del avión, para quedar éste posado sobre la plataforma simulando el aterrizaje de un avión sobre su porta avión.
ES1974199790U1974-01-241974-01-24Juego aereo de pericia perfeccionado.
ExpiredES199790Y
(es)
Evaluation of in-flight simulation using a helicopter of variable stability and control with regard to its use as an auxiliary in aircraft development(Evaluation of in-flight simulation of flying platform using helicopter with variable stability and maneuverability)
The development of an integrated flight guidance and control system for modern high- performance aircraft(VTOL aircraft fly by wire system eliminating errors automatically, discussing electronic and electrohydraulic control components, flight test model design, prototype, etc)
Effect of artificial stability on aircraft performances(Effect of artificial longitudinal stability on aircraft performance, based on control configured vehicle concept)
An automatic guidance concept for VTOL aircraft(V/STOL aircraft automatic flight control, guidance and navigation by onboard computer, discussing mathematical model and simulation results)
Consideration of the high bypass ratio tip turbine cruise fan for long range and long endurance aircraft(Tip turbine fan system developed as cruise propulsion device for long range and endurance aircraft)
Effect of ground proximity on the longitudinal aerodynamic characteristics of an airplane with a jet-flapped high lift wing(Wind tunnel tests to determine effects of ground proximity on lift, drag, and pitching moment of rectangular wing equipped with jet flaps)