Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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GARAY MANRIQUE JOSE JESUS
PUENTE PICO JOSE MARIA
Original Assignee
GARAY MANRIQUE JOSE JESUS
PUENTE PICO JOSE MARIA
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Filing date
Publication date
Application filed by GARAY MANRIQUE JOSE JESUS, PUENTE PICO JOSE MARIAfiledCriticalGARAY MANRIQUE JOSE JESUS
Priority to ES1978235338UpriorityCriticalpatent/ES235338Y/es
Publication of ES235338UpublicationCriticalpatent/ES235338U/es
Application grantedgrantedCritical
Publication of ES235338YpublicationCriticalpatent/ES235338Y/es
Nueva cometa de vuelo dirigido. La cometa que la invención propone se caracteriza esencialmente porque se constituye a partir de una serie de largueros y travesaños combinados funcionalmente con un puntal vertical, todo ello dando forma a un armazón en funciones de estructura portante para una lámina textil de configuración hexagonal. El conjunto integrado por los ya mencionados largueros y travesaños se distribuyen de tal forma que uno de los travesaños ocupa un plano superior para relacionarse por sus extremos sobre dos puntos opuestos de la lámina textil, otro de los elementos que componen el armazón de la cometa se constituye en un larguero que ocupa un plano inferior al previsto para el elemento anteriormente citado, imprimiendo a la lámina textil un amplio rehundido que discurre en coincidencia con el eje de simetría longitudinal de la cometa
ES1978235338U1978-04-121978-04-12Nueva cometa de vuelo dirigido.
ExpiredES235338Y
(es)
Full-scale wind-tunnel investigation of the static longitudinal and lateral characteristics of a light single-engine airplane(Full scale wind tunnel investigation of static longitudinal and lateral stability and control characteristics of light single-engine low-wing monoplane)
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)