An aircraft and aircraft wing stabilizer, the aircraft including a bracket for supporting a wing of the aircraft, the bracket including a first end coupled to the wing and a second end coupled to a fuselage of the aircraft, the bracket including a strut extending between the first end and the second end, and including an airfoil portion, the airfoil portion has a cavity for receiving a strut.
本发明公开了一种飞机和飞机机翼稳定器,该飞机包括支架,该支架用于支撑飞机的机翼,该支架包括联接到机翼的第一端以及联接到飞机的机身的第二端,该支架包括在第一端与第二端之间延伸的支柱,并且包括翼型部,该翼型部具有用于容纳支柱的腔体。
Aircraft and aircraft wing stabilizer
飞机和飞机机翼稳定器
31.12.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
Pitch stabilizer and rotary-wing aircraft equipped with such stabilizer
Europäisches Patentamt | 2015
|Swept-Wing Outboard-Horizontal-Stabilizer Aircraft Configuration
Online Contents | 2004
|