Device and process for regulating the power of the engines of a rotary wing multi-engine aircraft

   
   

Device and process for regulating the power of the engines of a rotary wing multi-engine aircraft. The regulating device (1) comprises, in addition to main regulating systems (2, 6) associated with the engines (M1, M2) of the aircraft, auxiliary regulating systems (12, 13) associated with said engines (M1, M2) and means (10, 11) for determining the speeds of rotation of the engines (M1, M2). Each auxiliary regulating system (12, 13) is capable of automatically adjusting the flow rate of fuel in such a way as to slave the speed of rotation of the associated engine, when its main regulating system has failed, to the speed of rotation of the other engine of the aircraft.

Dispositivo y proceso para regular la energía de los motores de un avión rotatorio del multi-motor del ala. El dispositivo de regulación (1) abarca, además de los sistemas de regulación principales (2, 6) asociado a los motores (M1, M2) del avión, de los sistemas de regulación auxiliares (12, 13) asociados a los motores dichos (M1, M2) y de los medios (10, 11) para determinar las velocidades de la rotación de los motores (M1, M2). Cada sistema de regulación auxiliar (12, 13) es capaz automáticamente de ajustar el caudal del combustible de tal manera en cuanto a esclavo la velocidad de la rotación del motor asociado, cuando su sistema de regulación principal ha fallado, a la velocidad de la rotación del otro motor del avión.

 
Web www.patentalert.com

< Virtually geostationary satellite array

< Unmanned air vehicle and method of flying an unmanned air vehicle

> Aircraft seat

> Actuation mechanism for swinging an aircraft door

~ 00114