An aircraft component assembly jig includes: header plates; positioners provided on each of the header plates, each positioner including a receiver that comes into contact with a lower/upper surface of an aircraft component, each positioner causing the receiver to advance and retract; receiver state detectors, that each detects, as control data, a supporting state of a corresponding one of the receivers; and a circuitry. The circuitry compares each of detection values of the control data with a preset reference value to determine whether an equal support state is achieved, the equal support state being a state where all the receivers are equally supporting the aircraft component. If it is determined that the equal support state is not achieved, the circuitry controls an adjustment-requiring positioner among all the positioners to adjust an advancing/retracting position of the receiver of the adjustment-requiring positioner within a design tolerance.
AIRCRAFT COMPONENT ASSEMBLY JIG AND AIRCRAFT COMPONENT INSPECTION TOOL
2021-08-19
Patent
Elektronische Ressource
Englisch
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 COMPONENT ASSEMBLY JIG, AND AIRCRAFT COMPONENT INSPECTION JIG
Europäisches Patentamt | 2020
|Hinge assembly for aircraft component, aircraft component, wing and aircraft
Europäisches Patentamt | 2022
|Hinge assembly for aircraft component, aircraft component, wing and aircraft
Europäisches Patentamt | 2022
|AIRCRAFT COMPONENT POSITIONING DEVICE, AIRCRAFT ASSEMBLY SYSTEM, AND AIRCRAFT ASSEMBLY METHOD
Europäisches Patentamt | 2020
|AIRCRAFT COMPONENT POSITIONING DEVICE, AIRCRAFT ASSEMBLY SYSTEM AND AIRCRAFT ASSEMBLY METHOD
Europäisches Patentamt | 2016
|