AERIAL VEHICLE FLUID CONTROL SYSTEM INTEGRATED WITH GAS TURBINE ENGINE

An assembly (20) for an aerial vehicle includes an airframe (24) and a fluid circuit (128). The airframe (24) includes a body (110) and an airfoil (112) projecting out from the body (110). The airfoil (112) includes a first surface (122) and a first aperture (168) in the first surface (122). The flu...

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Bibliographic Details
Main Authors PAULINO, Jose R, JACKSON, Sean R, BINEK, Lawrence A
Format Patent
LanguageEnglish
French
German
Published 06.03.2024
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:An assembly (20) for an aerial vehicle includes an airframe (24) and a fluid circuit (128). The airframe (24) includes a body (110) and an airfoil (112) projecting out from the body (110). The airfoil (112) includes a first surface (122) and a first aperture (168) in the first surface (122). The fluid circuit (128) is configured to bleed gas from a gas turbine engine (22) mounted to the airframe (24) to provide control gas. The fluid circuit (128) is configured to selectively direct the control gas to the first aperture (168).
Bibliography:Application Number: EP20230195217