Aircraft auxiliary systems pump

Details Aircraft auxiliary systems pump Aircraft auxiliary systems pump

B - Operations, Transporting

64

D

B64D 33/00 (2006.01) F02C 7/27 (2006.01) F15B 1/033 (2006.01)

Patent

CA 2724685

The invention provides methods and systems for starting auxiliary systems, comprising an auxiliary pump system having: a) a motorpump assembly having a constant displacement pump coupled to an electric motor; b) a hydraulic accumulator in fluid communication with said motorpump assembly; and c) lines to at least on auxiliary system in fluid communication with said motorpump assembly.

L'invention porte sur des procédés et sur des systèmes pour démarrer des systèmes auxiliaires, comprenant un système de pompe auxiliaire comportant : a) un ensemble motopompe doté dune pompe à déplacement constant couplée à un moteur électrique ; b) un accumulateur hydraulique en communication fluidique avec ledit ensemble motopompe ; et c) des conduites vers au moins un système auxiliaire en communication fluidique avec ledit ensemble motopompe.

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