A configuration of the pneumatic installation in the tail...

B - Operations – Transporting – 64 – D

Patent

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B64D 41/00 (2006.01)

Patent

CA 2720891

Which comprises an auxiliary power unit (1) for supply of pneumatic and electrical power, whose pneumatic power outlet is linked to a duct (2) which conventionally, incorporates bends (7) and compensation elements (6) for thermal expansion and for compensation of the vibrations produced by the APU (1) in its functioning. It is characterized in that the power outlet of the APU (1) is arranged in its front part in which is connected the duct consisting of a straight pipe (2a) inclined downwards toward the lower part of the aircraft in which compensation elements (6) for thermal expansion and for compensation of vibrations are inserted in order to reduce the length of the duct (2) and eliminate the bends, so that the pressure losses are considerably reduced.

Que comprende una unidad auxiliar de potencia (1) de suministro de potencia neumática y eléctrica, cuya salida de potencia neumática está unida a una conducción (2) que convencionalmente incorpora codos (2) y elementos de compensación (6) de dilatación térmica y de compensación de las vibraciones que produce la APU (1) en su funcionamiento. Se caracteriza porque la salida de potencia de la APU (1) está dispuesta en su parte frontal en la que conecta la conducción que está constituida por un tubo (2a) recto inclinado descendente hacia la parte inferior del avión en el que se intercalan los elementos de compensación de dilatación térmica y de compensación (6) de las vibraciones, para reducir la longitud de la conducción (2) y eliminar los codos, de forma que se reducen las pérdidas de presión considerablemente.

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