A method for assembling an aircraft engine nacelle inlet lip includes automatically positioning, with a controller an automated workstation in two degrees of freedom to position an articulated assembly fixture docking station in at least two predetermined joining positions, and effecting, with the controller, an ordered assembly of at least a forward bulkhead joint, a forward bulkhead to lipskin joint, a chord member to lipskin joint, an inner barrel to lipskin joint, an aft bulkhead to lipskin joint and an outer barrel to lipskin joint through an interface between an automated assembly tool and at least one of a plurality of assembly fixtures interchangeably mounted on the docking station, where each assembly fixture corresponds to an assembly step of the aircraft engine nacelle inlet lip and at least one of the assembly fixtures is common to more than one assembly step of the aircraft engine nacelle inlet lip.
Aircraft engine inlet assembly apparatus
2017-08-08
Patent
Electronic Resource
English
IPC: | B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Aircraft-engine inlet and exhaust porting
Engineering Index Backfile | 1944
|The Aircraft Engine Inlet Vortex Problem
AIAA | 2002
|Aircraft-Engine - INLET and EXHAUST PORTING
SAE Technical Papers | 1944
|Aircraft engine air inlet duct and aircraft comprising same
European Patent Office | 2023
|