The invention relates to a system and a method for assembling an aft fuselage section of an aircraft. Systems and methods for forming an aft fuselage section of an aircraft include a front section having a stabilizer channel. The front section comprises an upper sill beam and a lower sill beam. One or more pivot fittings are securely secured between the upper sill and the lower sill. One or more pivot fittings are configured to pivotally couple to a horizontal stabilizer within the stabilizer channel.
本发明涉及用于组装飞行器的后机身段的系统和方法。用于形成飞行器的后机身段的系统和方法包括具有稳定器通道的前段。前段包括上槛梁和下槛梁。一个或多个枢轴配件被牢固地紧固在上槛梁和下槛梁之间。一个或多个枢轴配件被配置为枢转地联接到稳定器通道内的水平稳定器。
System and method for assembling rear fuselage section of aircraft
用于组装飞行器的后机身段的系统和方法
2023-05-19
Patent
Electronic Resource
Chinese
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 rear fuselage section and manufacturing method thereof
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|AIRCRAFT REAR FUSELAGE SECTION AND MANUFACTURING METHOD THEREOF
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|AIRCRAFT REAR FUSELAGE SECTION AND MANUFACTURING METHOD THEREOF
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