An assembly is includes a regulator manifold and a regulator element (162). The regulator manifold includes an inlet passage (154), a first outlet passage (156) and a second outlet passage (158). The inlet passage (154) is configured to receive bleed gas from a core flowpath. The regulator element (162) is within the regulator manifold and configured to pivot to a first position, a second position and an intermediate position between the first position and the second position. The regulator element (162) is configured to fluidly couple the inlet passage (154) with the first outlet passage (156) in the first position. The regulator element (162) is configured to fluidly couple the inlet passage (154) with the second outlet passage (158) in the second position. The regulator element (162) is configured to fluidly decouple the inlet passage (154) from the first outlet passage (156) and the second outlet passage (158) in the intermediate position.
AERIAL VEHICLE FLUID CONTROL SYSTEM WITH MULTI-WAY FLOW REGULATOR
LUFTFAHRZEUG-FLUIDREGELSYSTEM MIT MEHRWEG-DURCHFLUSSREGLER
SYSTÈME DE COMMANDE DE FLUIDE DE VÉHICULE AÉRIEN AVEC RÉGULATEUR DE DÉBIT MULTIVOIE
2024-07-03
Patent
Electronic Resource
English
AERIAL VEHICLE FLUID CONTROL SYSTEM WITH MULTI-WAY FLOW REGULATOR
European Patent Office | 2024
|