Invention Application
- Patent Title: ELECTRIC PROPULSION UNIT OF AN AIRCRAFT COMPRISING A COOLING SYSTEM INCORPORATING AT LEAST ONE FRONT AIR INLET AND AIRCRAFT COMPRISING AT LEAST ONE SUCH ELECTRIC PROPULSION UNIT
-
Application No.: US17737134Application Date: 2022-05-05
-
Publication No.: US20220355943A1Publication Date: 2022-11-10
- Inventor: Jorge CARRETERO BENIGNOS , Benedikt BAMMER , Olivier VERSEUX , Maria Del Sagrario JUANAS FERNANDEZ , Jorge MOLANO REMBIASZ , Thomas SCHERER , Alexander SOLNTSEV
- Applicant: Airbus SAS , Airbus Operations SAS , Airbus Operations GmbH , Airbus Operations S.L.
- Applicant Address: FR BLAGNAC; FR TOULOUSE; DE HAMBURG; ES GETAFE
- Assignee: Airbus SAS,Airbus Operations SAS,Airbus Operations GmbH,Airbus Operations S.L.
- Current Assignee: Airbus SAS,Airbus Operations SAS,Airbus Operations GmbH,Airbus Operations S.L.
- Current Assignee Address: FR BLAGNAC; FR TOULOUSE; DE HAMBURG; ES GETAFE
- Priority: EP21172646.8 20210507
- Main IPC: B64D27/24
- IPC: B64D27/24 ; B64D33/08
Abstract:
An electric propulsion unit of an aircraft including a nacelle housing an electric power system, an electric motor and a cooling system for the electric power system; the nacelle including a central fairing, a front fairing which extends from the central fairing to a front end and a rear fairing which extends from the central fairing to a rear end. The front fairing includes a protrude positioned in a lower part of the front fairing, the protrude having a front face in a transverse plane, a main air inlet of the cooling system being positioned on the front face.
Public/Granted literature
Information query
